{"id":6729,"date":"2024-11-29T12:26:21","date_gmt":"2024-11-29T12:26:21","guid":{"rendered":"https:\/\/workhouse.sweetdishy.com\/?p=6729"},"modified":"2024-11-29T12:26:23","modified_gmt":"2024-11-29T12:26:23","slug":"concentrating-collectors","status":"publish","type":"post","link":"https:\/\/workhouse.sweetdishy.com\/index.php\/2024\/11\/29\/concentrating-collectors\/","title":{"rendered":"\u00a0Concentrating collectors"},"content":{"rendered":"\n<p id=\"P2010\">As we have seen in Section\u00a03.2, concentrating collectors work by interposing an optical device between the source of radiation and the energy-absorbing surface. Therefore, for concentrating collectors, both optical and thermal analyses are required. In this book, only two types of concentrating collectors are analyzed: compound parabolic and parabolic trough collectors. Initially, the concentration ratio and its theoretical maximum value are defined.<\/p>\n\n\n\n<p id=\"P2015\">The concentration ratio (<em>C<\/em>) is defined as the ratio of the aperture area to the receiver\u2013absorber area; that is,<\/p>\n\n\n\n<p id=\"FD182\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si194.png\" alt=\"image\" width=\"54\" height=\"36\"><strong>(3.87)<\/strong><\/p>\n\n\n\n<p>For FPCs with no reflectors,\u00a0<em>C<\/em>\u00a0=\u00a01. For concentrators,\u00a0<em>C<\/em>\u00a0is always greater than 1. Initially the maximum possible concentration ratio is investigated. Consider a circular (three-dimensional) concentrator with aperture\u00a0<em>A<\/em><sub>a<\/sub>\u00a0and receiver area\u00a0<em>A<\/em><sub>r<\/sub>\u00a0located at a distance\u00a0<em>R<\/em>\u00a0from the center of the sun, as shown in\u00a0Figure 3.35. We saw in\u00a0Chapter 2\u00a0that the sun cannot be considered a point source but a sphere of radius\u00a0<em>r<\/em>; therefore, as seen from the earth, the sun has a half angle,\u00a0<em>\u03b8<\/em><sub>m<\/sub>, which is the acceptance half angle for maximum concentration. If both the sun and the receiver are considered to be blackbodies at temperatures\u00a0<em>T<\/em><sub>s<\/sub>\u00a0and\u00a0<em>T<\/em><sub>r<\/sub>, the amount of radiation emitted by the sun is given by:<\/p>\n\n\n\n<p id=\"FD183\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si195.png\" alt=\"image\" width=\"113\" height=\"21\"><strong>(3.88)<\/strong><a><\/a><\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-35-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.35<\/strong>&nbsp;<a><\/a>Schematic of the sun and a concentrator.<\/p>\n\n\n\n<p id=\"P2025\">A fraction of this radiation is intercepted by the collector, given by:<\/p>\n\n\n\n<p id=\"FD184\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si196.png\" alt=\"image\" width=\"88\" height=\"35\"><strong>(3.89)<\/strong><\/p>\n\n\n\n<p>Therefore, the energy radiated from the sun and received by the concentrator is:<\/p>\n\n\n\n<p id=\"FD185\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si197.png\" alt=\"image\" width=\"223\" height=\"37\"><strong>(3.90)<\/strong><\/p>\n\n\n\n<p>A blackbody (perfect) receiver radiates energy equal to&nbsp;<img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si198.png\" alt=\"image\" width=\"59\" height=\"24\">&nbsp;and a fraction of this reaches the sun, given by:<\/p>\n\n\n\n<p id=\"FD186\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si199.png\" alt=\"image\" width=\"122\" height=\"19\"><strong>(3.91)<\/strong><\/p>\n\n\n\n<p>Under this idealized condition, the maximum temperature of the receiver is equal to that of the sun. According to the second law of thermodynamics, this is true only when\u00a0<em>Q<\/em><sub>r\u2013s<\/sub>\u00a0=\u00a0<em>Q<\/em><sub>s\u2013r<\/sub>. Therefore, from Eqs\u00a0(3.90)\u00a0and\u00a0(3.91),<\/p>\n\n\n\n<p id=\"FD187\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si200.png\" alt=\"image\" width=\"90\" height=\"38\"><strong>(3.92)<\/strong><\/p>\n\n\n\n<p>Since the maximum value of&nbsp;<em>F<\/em><sub>r\u2013s<\/sub>&nbsp;is equal to 1, the maximum concentration ratio for three-dimensional concentrators is [sin(<em>\u03b8<\/em><sub>m<\/sub>)&nbsp;=&nbsp;<em>r<\/em>\/<em>R<\/em>]:<\/p>\n\n\n\n<p id=\"FD188\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si201.png\" alt=\"image\" width=\"110\" height=\"38\"><strong>(3.93)<\/strong><\/p>\n\n\n\n<p>A similar analysis for linear concentrators gives:<\/p>\n\n\n\n<p id=\"FD189\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si202.png\" alt=\"image\" width=\"103\" height=\"37\"><strong>(3.94)<\/strong><\/p>\n\n\n\n<p>As was seen in\u00a0Chapter 2, 2<em>\u03b8<\/em><sub>m<\/sub>\u00a0is equal to 0.53\u00b0 (or 32\u2032), so\u00a0<em>\u03b8<\/em><sub>m<\/sub>, the half acceptance angle, is equal to 0.27\u00b0 (or 16\u2032). The half acceptance angle denotes coverage of one half of the angular zone within which radiation is accepted by the concentrator\u2019s receiver. Radiation is accepted over an angle of 2<em>\u03b8<\/em><sub>m<\/sub>, because radiation incident within this angle reaches the receiver after passing through the aperture. This angle describes the angular field within which radiation can be collected by the receiver without having to track the concentrator.<\/p>\n\n\n\n<p id=\"P2060\">Equations\u00a0(3.93)\u00a0and\u00a0(3.94)\u00a0define the upper limit of concentration that may be obtained for a given collector viewing angle. For a stationary CPC, the angle\u00a0<em>\u03b8<\/em><sub>m<\/sub>\u00a0depends on the motion of the sun in the sky. For a CPC having its axis in an N\u2013S direction and tilted from the horizontal such that the plane of the sun\u2019s motion is normal to the aperture, the acceptance angle is related to the range of hours over which sunshine collection is required; for example, for 6\u00a0h of useful sunshine collection, 2<em>\u03b8<\/em><sub>m<\/sub>\u00a0=\u00a090\u00b0 (sun travels 15\u00b0\/h). In this case,\u00a0<em>C<\/em><sub>max<\/sub>\u00a0=\u00a01\/sin(45\u00b0)\u00a0=\u00a01.41.<\/p>\n\n\n\n<p id=\"P2065\">For a tracking collector,&nbsp;<em>\u03b8<\/em><sub>m<\/sub>&nbsp;is limited by the size of the sun\u2019s disk, small-scale errors, irregularities of the reflector surface, and tracking errors. For a perfect collector and tracking system,&nbsp;<em>C<\/em><sub>max<\/sub>&nbsp;depends only on the sun\u2019s disk. Therefore,<\/p>\n\n\n\n<p id=\"P2070\">For single-axis tracking,&nbsp;<em>C<\/em><sub>max<\/sub>&nbsp;=&nbsp;1\/sin(16\u2032)&nbsp;=&nbsp;216.<\/p>\n\n\n\n<p id=\"P2075\">For full tracking,&nbsp;<em>C<\/em><sub>max<\/sub>&nbsp;=&nbsp;1\/sin<sup>2<\/sup>(16\u2032)&nbsp;=&nbsp;46,747.<\/p>\n\n\n\n<p id=\"P2080\">It can therefore be concluded that the maximum concentration ratio for two-axis tracking collectors is much higher. However, high accuracy of the tracking mechanism and careful construction of the collector are required with an increased concentration ratio, because&nbsp;<em>\u03b8<\/em><sub>m<\/sub>&nbsp;is very small. In practice, due to various errors, much lower values than these maximum ones are employed.<\/p>\n\n\n\n<p>EXAMPLE 3.7<\/p>\n\n\n\n<p id=\"P2085\">From the diameter of the sun and the earth and the mean distance of sun from earth, shown in\u00a0Figure 2.1, estimate the amount of energy emitted from the sun, the amount of energy received by the earth, and the solar constant for a sun temperature of 5777\u00a0K. If the distance of Venus from the sun is 0.71 times the mean sun\u2013earth distance, estimate the solar constant for Venus.<\/p>\n\n\n\n<p id=\"BOXSECTITLE0040\">Solution<\/p>\n\n\n\n<p id=\"P2090\">The amount of energy emitted from the sun,&nbsp;<em>Q<\/em><sub>s<\/sub>, is:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si203.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p>or<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si204.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2095\">From Eq.\u00a0(3.90), the solar constant can be obtained as:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si205.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2100\">The area of the earth exposed to sunshine is \u03c0<em>d<\/em><sup>2<\/sup>\/4. Therefore, the amount of energy received from earth\u00a0=\u00a0\u03c0(1.27\u00a0\u00d7\u00a010<sup>7<\/sup>)<sup>2<\/sup>\u00a0\u00d7\u00a01.363\/4\u00a0=\u00a01.73\u00a0\u00d7\u00a010<sup>14<\/sup>\u00a0kW. These results verify the values specified in the introduction to\u00a0Chapter 2.<\/p>\n\n\n\n<p id=\"P2105\">The mean distance of Venus from the sun is 1.496&nbsp;\u00d7&nbsp;10<sup>11<\/sup>&nbsp;\u00d7&nbsp;0.71&nbsp;=&nbsp;1.062&nbsp;\u00d7&nbsp;10<sup>11<\/sup>&nbsp;m. Therefore, the solar constant of Venus is:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si206.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"FD193\"><\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"CESECTITLE0140\">3.6.1 Optical analysis of a compound parabolic collector<\/h3>\n\n\n\n<p id=\"P2110\">The optical analysis of CPC collectors deals mainly with the way to construct the collector shape. A CPC of the Winston design (Winston and Hinterberger, 1975) is shown in\u00a0Figure 3.36. It is a linear two-dimensional concentrator consisting of two distinct parabolas, the axes of which are inclined at angles \u00b1<em>\u03b8<\/em><sub>c<\/sub>\u00a0with respect to the optical axis of the collector. The angle\u00a0<em>\u03b8<\/em><sub>c<\/sub>, called the collector\u00a0<em>half acceptance angle<\/em>, is defined as the angle through which a source of light can be moved and still converge at the absorber.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-36-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.36<\/strong>&nbsp;<a><\/a>Construction of a flat receiver compound parabolic collector.<\/p>\n\n\n\n<p id=\"P2115\">The Winston-type collector is a non-imaging concentrator with a concentration ratio approaching the upper limit permitted by the second law of thermodynamics, as explained in previous section.<\/p>\n\n\n\n<p id=\"P2120\">The receiver of the CPC does not have to be flat and parallel but, as shown in\u00a0Figure 3.5, can be bifacial, a wedge, or cylindrical.\u00a0Figure 3.37\u00a0shows a collector with a cylindrical receiver; the lower portion of the reflector (AB and AC) is circular, while the upper portions (BD and CE) are parabolic. In this design, the requirement for the parabolic portion of the collector is that, at any point P, the normal to the collector must bisect the angle between the tangent line PG to the receiver and the incident ray at point P at angle\u00a0<em>\u03b8<\/em><sub>c<\/sub>\u00a0with respect to the collector axis. Since the upper part of a CPC contributes little to the radiation reaching the absorber, it is usually truncated, forming a shorter version of the CPC, which is also cheaper. CPCs are usually covered with glass to avoid dust and other materials entering the collector and reducing the reflectivity of its walls. Truncation hardly affects the acceptance angle but\u00a0results in considerable material saving and changes the height-to-aperture ratio, the concentration ratio, and the average number of reflections.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-37-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.37<\/strong>&nbsp;<a><\/a>Schematic diagram of a CPC collector.<\/p>\n\n\n\n<p id=\"P2125\">These collectors are more useful as linear or trough-type concentrators. The orientation of a CPC collector is related to its acceptance angle (2<em>\u03b8<\/em><sub>c<\/sub>, in\u00a0Figures 3.36\u00a0and\u00a03.37). The two-dimensional CPC is an ideal concentrator, that is, it works perfectly for all rays within the acceptance angle, 2<em>\u03b8<\/em><sub>c<\/sub>. Also, depending on the collector acceptance angle, the collector can be stationary or tracking. A CPC concentrator can be oriented with its long axis along either the north\u2013south or east\u2013west direction and its aperture tilted directly toward the equator at an angle equal to the local latitude. When oriented along the north\u2013south direction, the collector must track the sun by turning its axis to face the sun continuously. Since the acceptance angle of the concentrator along its long axis is wide, seasonal tilt adjustment is not necessary. It can also be stationary, but radiation will be received only during the hours when the sun is within the collector acceptance angle.<\/p>\n\n\n\n<p id=\"P2130\">When the concentrator is oriented with its long axis along the east\u2013west direction, with a little seasonal adjustment in tilt angle, the collector is able to catch the sun\u2019s rays effectively through its wide acceptance angle along its long axis. The minimum acceptance angle in this case should be equal to the maximum incidence angle projected in a north\u2013south vertical plane during the times when output is needed from the collector. For stationary CPC collectors mounted in this mode, the minimum acceptance angle is equal to 47\u00b0. This angle covers the declination of the sun from summer to winter solstices (2\u00a0\u00d7\u00a023.5\u00b0). In practice, bigger angles are used to enable the collector to collect diffuse radiation at the expense of a lower concentration ratio. Smaller (less than 3) concentration ratio CPCs are of greatest practical interest. These, according to\u00a0Pereira (1985), are able to accept a large proportion of diffuse radiation incident on their apertures and concentrate it without the need to track the sun. Finally, the required frequency of collector adjustment is related to the collector concentration ratio.\u00a0Thus, for\u00a0<em>C<\/em>\u00a0\u2264\u00a03 the collector needs only biannual adjustment, while for\u00a0<em>C<\/em>\u00a0>\u00a010 the collector requires almost daily adjustment; these systems are also called\u00a0<em>quasi-static<\/em>.<\/p>\n\n\n\n<p id=\"P2135\">Concentrators of the type shown in\u00a0Figure 3.5\u00a0have an area concentration ratio that is a function of the acceptance half angle,\u00a0<em>\u03b8<\/em><sub>c<\/sub>. For an ideal linear concentrator system, this is given by Eq.\u00a0(3.94)\u00a0by replacing\u00a0<em>\u03b8<\/em><sub>m<\/sub>\u00a0with\u00a0<em>\u03b8<\/em><sub>c<\/sub>.<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"CESECTITLE0145\">3.6.2 Thermal analysis of compound parabolic collectors<\/h3>\n\n\n\n<p id=\"P2140\">The instantaneous efficiency,&nbsp;<em>\u03b7<\/em>, of a CPC is defined as the useful energy gain divided by the incident radiation on the aperture plane; that is,<\/p>\n\n\n\n<p id=\"FD194\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si207.png\" alt=\"image\" width=\"68\" height=\"36\"><strong>(3.95)<\/strong><\/p>\n\n\n\n<p>In Eq.\u00a0(3.95),\u00a0<em>G<\/em><sub>t<\/sub>\u00a0is the total incident radiation on the aperture plane. The useful energy,\u00a0<em>Q<\/em><sub>u<\/sub>, is given by an equation similar to Eq.\u00a0(3.60), using the concept of absorbed radiation as:<\/p>\n\n\n\n<p id=\"FD195\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si208.png\" alt=\"image\" width=\"211\" height=\"16\"><strong>(3.96)<\/strong><\/p>\n\n\n\n<p>The absorbed radiation,\u00a0<em>S<\/em>, is obtained from (Duffie and Beckman, 2006):<\/p>\n\n\n\n<p id=\"FD196\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si209.png\" alt=\"image\" width=\"449\" height=\"17\"><strong>(3.97)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0370\"><a><\/a><em>\u03c4<\/em><sub>c<\/sub>&nbsp;=&nbsp;transmittance of the CPC cover.<\/p>\n\n\n\n<p id=\"U0375\"><a><\/a><em>\u03c4<\/em><sub>CPC<\/sub>&nbsp;=&nbsp;transmissivity of the CPC to account for reflection loss.<\/p>\n\n\n\n<p>The various radiation components in Eq.\u00a0(3.97)\u00a0come from radiation falling on the aperture within the acceptance angle of the CPC and are given as follows:<\/p>\n\n\n\n<p id=\"FD197\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si210.png\" alt=\"image\" width=\"471\" height=\"20\"><strong>(3.98a)<\/strong><\/p>\n\n\n\n<p id=\"FD198\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si314.png\" alt=\"image\" width=\"346\" height=\"98\"><strong>(3.98b)<\/strong><\/p>\n\n\n\n<p id=\"FD199\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si211.png\" alt=\"image\" width=\"347\" height=\"80\"><strong>(3.98c)<\/strong><\/p>\n\n\n\n<p>In Eqs\u00a0(3.98a)\u2013(3.98c),\u00a0<em>\u03b2<\/em>\u00a0is the collector aperture inclination angle with respect to horizontal. In Eq.\u00a0(3.98c), the ground-reflected radiation is effective only if the collector receiver \u201csees\u201d the ground, that is, (<em>\u03b2<\/em>\u00a0+\u00a0<em>\u03b8<\/em><sub>c<\/sub>)\u00a0>\u00a090\u00b0.<\/p>\n\n\n\n<p id=\"P2175\">It has been shown by\u00a0Rabl et al. (1980)\u00a0that the insolation,\u00a0<em>G<\/em><sub>CPC<\/sub>, of a collector with a concentration\u00a0<em>C<\/em>\u00a0can be approximated very well from:<\/p>\n\n\n\n<p id=\"FD200\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si212.png\" alt=\"image\" width=\"423\" height=\"39\"><strong>(3.99)<\/strong><\/p>\n\n\n\n<p><a><\/a>It is convenient to express the absorbed solar radiation,&nbsp;<em>S<\/em>, in terms of&nbsp;<em>G<\/em><sub>CPC<\/sub>&nbsp;in the following way:<\/p>\n\n\n\n<p id=\"FD201\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si213.png\" alt=\"image\" width=\"376\" height=\"84\"><strong>(3.100)<\/strong><\/p>\n\n\n\n<p>or<\/p>\n\n\n\n<p id=\"FD202\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si214.png\" alt=\"image\" width=\"135\" height=\"15\"><strong>(3.101)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0380\"><a><\/a><em>\u03c4<\/em><sub>cover<\/sub>&nbsp;=&nbsp;transmissivity of the cover glazing.<\/p>\n\n\n\n<p id=\"U0385\"><a><\/a><em>\u03c4<\/em><sub>CPC<\/sub>&nbsp;=&nbsp;effective transmissivity of CPC.<\/p>\n\n\n\n<p id=\"U0390\"><a><\/a><em>\u03b1<\/em><sub>r<\/sub>&nbsp;=&nbsp;absorptivity of receiver.<\/p>\n\n\n\n<p id=\"U0395\"><a><\/a><em>\u03b3<\/em>&nbsp;=&nbsp;correction factor for diffuse radiation, given by:<\/p>\n\n\n\n<p id=\"FD203\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si215.png\" alt=\"image\" width=\"147\" height=\"39\"><strong>(3.102)<\/strong><\/p>\n\n\n\n<p>The factor\u00a0<em>\u03b3<\/em>, given by Eq.\u00a0(3.102), accounts for the loss of diffuse radiation outside the acceptance angle of the CPC with a concentration\u00a0<em>C<\/em>. The ratio\u00a0<em>G<\/em><sub>D<\/sub>\/<em>G<\/em><sub>t<\/sub>\u00a0varies from about 0.11 on very clear sunny days to about 0.23 on hazy days.<\/p>\n\n\n\n<p id=\"P2210\">It should be noted that only part of the diffuse radiation effectively enters the CPC, and this is a function of the acceptance angle. For isotropic diffuse radiation, the relationship between the effective incidence angle and the acceptance half angle is given by (Brandemuehl and Beckman, 1980):<\/p>\n\n\n\n<p id=\"FD204\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si216.png\" alt=\"image\" width=\"343\" height=\"19\"><strong>(3.103)<\/strong><\/p>\n\n\n\n<p>The effective transmissivity,&nbsp;<em>\u03c4<\/em><sub>CPC<\/sub>, of the CPC accounts for reflection loss inside the collector. The fraction of the radiation passing through the collector aperture and eventually reaching the absorber depends on the specular reflectivity,&nbsp;<em>\u03c1<\/em>, of the CPC walls and the average number of reflections,&nbsp;<em>n<\/em>, expressed approximately by:<\/p>\n\n\n\n<p id=\"FD205\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si217.png\" alt=\"image\" width=\"66\" height=\"15\"><strong>(3.104)<\/strong><\/p>\n\n\n\n<p>This equation can also be used to estimate\u00a0<em>\u03c4<\/em><sub>CPC,B<\/sub>,\u00a0<em>\u03c4<\/em><sub>CPC,D<\/sub>, and\u00a0<em>\u03c4<\/em><sub>CPC,G<\/sub>\u00a0in Eq.\u00a0(3.97), which are usually treated as the same. Values of\u00a0<em>n<\/em>\u00a0for full and truncated CPCs can be obtained from\u00a0Figure 3.38. As noted before, the upper ends of CPCs contribute little to the radiation reaching the receiver, and usually CPCs are truncated for economic reasons. As can be seen from\u00a0Figure 3.38, the average number of reflections is a function of concentration ratio,\u00a0<em>C<\/em>, and the acceptance half angle,\u00a0<em>\u03b8<\/em><sub>c<\/sub>. For a truncated concentrator, the line (1\u00a0\u2212\u00a01\/<em>C<\/em>) can be taken as the lower bound for the number of reflections for radiation within the acceptance angle. Other effects of truncation are shown in\u00a0Figures 3.39\u00a0and\u00a03.40.\u00a0Figures 3.38\u20133.40\u00a0can be used to design a CPC, as shown in the following example. For more accuracy, the equations representing the curves of\u00a0Figures 3.38\u20133.40\u00a0can be used as given in\u00a0Appendix 6.<\/p>\n\n\n\n<p>EXAMPLE 3.8<\/p>\n\n\n\n<p id=\"P2225\">Find the CPC characteristics for a collector with acceptance half angle&nbsp;<em>\u03b8<\/em><sub>c<\/sub>&nbsp;=&nbsp;12\u00b0. Find also its characteristics if the collector is truncated so that its height-to-aperture ratio is 1.4.<\/p>\n\n\n\n<p id=\"BOXSECTITLE0045\">Solution<\/p>\n\n\n\n<p id=\"P2230\">For a full CPC, from\u00a0Figure 3.39\u00a0for\u00a0<em>\u03b8<\/em><sub>c<\/sub>\u00a0=\u00a012\u00b0, the height-to-aperture ratio\u00a0=\u00a02.8 and the concentration ratio\u00a0=\u00a04.8. From\u00a0Figure 3.40, the area of the reflector is 5.6 times the aperture area; and from\u00a0Figure 3.38, the average number of reflections of radiation before reaching the absorber is 0.97.<\/p>\n\n\n\n<p id=\"P2235\">For a truncated CPC, the height-to-aperture ratio\u00a0=\u00a01.4. Then, from\u00a0Figure 3.39, the concentration ratio drops to 4.2; and from\u00a0Figure 3.40, the reflector-to-aperture area drops to 3, which indicates how significant is the saving in reflector material. Finally, from\u00a0Figure 3.38, the average number of reflections is at least 1\u00a0\u2212\u00a01\/4.2\u00a0=\u00a00.76.<\/p>\n\n\n\n<p>EXAMPLE 3.9<\/p>\n\n\n\n<p id=\"P2240\">A CPC has an aperture area of 4&nbsp;m<sup>2<\/sup>&nbsp;and a concentration ratio of 1.7. Estimate the collector efficiency given the following:<a><\/a><\/p>\n\n\n\n<p id=\"U0400\"><a><\/a>Total radiation&nbsp;=&nbsp;850&nbsp;W\/m<sup>2<\/sup>.<\/p>\n\n\n\n<p id=\"U0405\"><a><\/a>Diffuse to total radiation ratio&nbsp;=&nbsp;0.12.<\/p>\n\n\n\n<p id=\"U0410\"><a><\/a>Receiver absorptivity&nbsp;=&nbsp;0.87.<\/p>\n\n\n\n<p id=\"U0415\"><a><\/a>Receiver emissivity&nbsp;=&nbsp;0.12.<\/p>\n\n\n\n<p id=\"U0420\"><a><\/a>Mirror reflectivity&nbsp;=&nbsp;0.90.<\/p>\n\n\n\n<p id=\"U0425\"><a><\/a>Glass cover transmissivity&nbsp;=&nbsp;0.90.<\/p>\n\n\n\n<p id=\"U0430\"><a><\/a>Collector heat loss coefficient&nbsp;=&nbsp;2.5&nbsp;W\/m<sup>2<\/sup>&nbsp;K.<\/p>\n\n\n\n<p id=\"U0435\"><a><\/a>Circulating fluid&nbsp;=&nbsp;water.<\/p>\n\n\n\n<p id=\"U0440\"><a><\/a>Entering fluid temperature&nbsp;=&nbsp;80&nbsp;\u00b0C.<\/p>\n\n\n\n<p id=\"U0445\"><a><\/a>Fluid flow rate&nbsp;=&nbsp;0.015&nbsp;kg\/s.<\/p>\n\n\n\n<p id=\"U0450\"><a><\/a>Ambient temperature&nbsp;=&nbsp;15&nbsp;\u00b0C.<\/p>\n\n\n\n<p id=\"U0455\"><a><\/a>Collector efficiency factor&nbsp;=&nbsp;0.92.<\/p>\n\n\n\n<p id=\"BOXSECTITLE0050\">Solution<\/p>\n\n\n\n<p id=\"P2305\">The diffuse radiation correction factor,\u00a0<em>\u03b3<\/em>, is estimated from Eq.\u00a0(3.102):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si218.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2310\">From\u00a0Figure 3.38\u00a0for\u00a0<em>C<\/em>\u00a0=\u00a01.7, the average number of reflections for a full CPC is\u00a0<em>n<\/em>\u00a0=\u00a00.6. Therefore, from Eq.\u00a0(3.104),<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si219.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2315\">The absorber radiation is given by Eq.\u00a0(3.101):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si220.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2320\">The heat removal factor is estimated from Eq.\u00a0(3.58):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si221.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2325\">The receiver area is obtained from Eq.\u00a0(3.87):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si222.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2330\">The useful energy gain can be estimated from Eq.\u00a0(3.96):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si223.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2335\">The collector efficiency is given by Eq.\u00a0(3.95):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si224.png\" alt=\"image\"\/><\/figure>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-38-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.38<\/strong>\u00a0Average number of reflections for full and truncated CPCs.\u00a0Reprinted from\u00a0Rabl (1976)\u00a0with permission from Elsevier.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-39-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.39<\/strong>\u00a0Ratio of height to aperture for full and truncated CPCs.\u00a0Reprinted from\u00a0Rabl (1976)\u00a0with permission from Elsevier.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-40-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.40<\/strong>\u00a0Ratio of reflector to aperture area for full and truncated CPCs.\u00a0Reprinted from\u00a0Rabl (1976)\u00a0with permission from Elsevier.<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"CESECTITLE0150\">3.6.3 Optical analysis of parabolic trough collectors<\/h3>\n\n\n\n<p id=\"P2340\">A cross-section of a parabolic trough collector is shown in\u00a0Figure 3.41, where various important factors are shown. The incident radiation on the reflector at the rim of the collector (where the mirror radius,\u00a0<em>r<\/em><sub>r<\/sub>, is maximum) makes an angle,\u00a0<em>\u03c6<\/em><sub>r<\/sub>, with the center line of the collector, which is called the\u00a0<em>rim angle<\/em>. The equation of the parabola in terms of the coordinate system is:<\/p>\n\n\n\n<p id=\"FD213\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si225.png\" alt=\"image\" width=\"61\" height=\"19\"><strong>(3.105)<\/strong><\/p>\n\n\n\n<p>where&nbsp;<em>f<\/em>&nbsp;=&nbsp;parabola focal distance (m).<a><\/a><\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-41-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.41<\/strong>&nbsp;<a><\/a>Cross-section of a parabolic trough collector with circular receiver.<\/p>\n\n\n\n<p id=\"P2345\">For specular reflectors of perfect alignment, the size of the receiver (diameter\u00a0<em>D<\/em>) required to intercept all the solar image can be obtained from trigonometry and\u00a0Figure 3.41, given by:<\/p>\n\n\n\n<p id=\"FD214\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si226.png\" alt=\"image\" width=\"104\" height=\"16\"><strong>(3.106)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U8020\"><a><\/a><em>\u03b8<\/em><sub>m<\/sub>&nbsp;=&nbsp;half acceptance angle (degrees).<\/p>\n\n\n\n<p>For a parabolic reflector, the radius,\u00a0<em>r<\/em>, shown in\u00a0Figure 3.41\u00a0is given by:<\/p>\n\n\n\n<p id=\"FD215\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si227.png\" alt=\"image\" width=\"101\" height=\"38\"><strong>(3.107)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U8025\"><em>\u03c6<\/em>\u00a0=\u00a0angle between the collector axis and a reflected beam at the focus; see\u00a0Figure 3.41.<\/p>\n\n\n\n<p>As&nbsp;<em>\u03c6<\/em>&nbsp;varies from 0 to&nbsp;<em>\u03c6<\/em><sub>r<\/sub>,&nbsp;<em>r<\/em>&nbsp;increases from&nbsp;<em>f<\/em>&nbsp;to&nbsp;<em>r<\/em><sub>r<\/sub>&nbsp;and the theoretical image size increases from 2<em>f<\/em>&nbsp;sin(<em>\u03b8<\/em><sub>m<\/sub>) to 2<em>r<\/em><sub>r<\/sub>&nbsp;sin(<em>\u03b8<\/em><sub>m<\/sub>)\/cos(<em>\u03c6<\/em><sub>r<\/sub>&nbsp;+&nbsp;<em>\u03b8<\/em><sub>m<\/sub>). Therefore, there is an image spreading on a plane normal to the axis of the parabola.<\/p>\n\n\n\n<p id=\"P2360\">At the rim angle,\u00a0<em>\u03c6<\/em><sub>r<\/sub>, Eq.\u00a0(3.107)\u00a0becomes:<\/p>\n\n\n\n<p id=\"FD216\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si228.png\" alt=\"image\" width=\"111\" height=\"38\"><strong>(3.108)<\/strong><\/p>\n\n\n\n<p>Another important parameter related to the rim angle is the aperture of the parabola,\u00a0<em>W<\/em><sub>a<\/sub>. From\u00a0Figure 3.41\u00a0and simple trigonometry, it can be found that:<\/p>\n\n\n\n<p id=\"FD217\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si229.png\" alt=\"image\" width=\"109\" height=\"16\"><strong>(3.109)<\/strong><\/p>\n\n\n\n<p>Substituting Eq.\u00a0(3.108)\u00a0into Eq.\u00a0(3.109)\u00a0gives:<\/p>\n\n\n\n<p id=\"FD218\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si230.png\" alt=\"image\" width=\"120\" height=\"38\"><strong>(3.110)<\/strong><\/p>\n\n\n\n<p>which reduces to:<\/p>\n\n\n\n<p id=\"FD219\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si231.png\" alt=\"image\" width=\"115\" height=\"30\"><strong>(3.111)<\/strong><\/p>\n\n\n\n<p>The half acceptance angle,\u00a0<em>\u03b8<\/em><sub>m<\/sub>, used in Eq.\u00a0(3.106)\u00a0depends on the accuracy of the tracking mechanism and the irregularities of the reflector surface. The smaller these two effects, the closer\u00a0<em>\u03b8<\/em><sub>m<\/sub>\u00a0is to the sun disk angle, resulting in a smaller image and higher concentration. Therefore, the image width depends on the magnitude of the two quantities. In\u00a0Figure 3.41, a perfect collector is assumed and the solar beam is shown striking the collector at an angle 2<em>\u03b8<\/em><sub>m<\/sub>\u00a0and leaving at the same angle. In a practical collector, however, because of the presence of errors, the angle 2<em>\u03b8<\/em><sub>m<\/sub>\u00a0should be increased to include the errors as well. Enlarged images can also result from the tracking mode used to transverse the collector. Problems can also arise due to errors in the positioning of the receiver relative to the reflector, which results in distortion, enlargement, and displacement of the image. All these are accounted for by the intercept factor, which is explained later in this section.<\/p>\n\n\n\n<p id=\"P2380\">For a tubular receiver, the concentration ratio is given by:<\/p>\n\n\n\n<p id=\"FD220\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si232.png\" alt=\"image\" width=\"60\" height=\"33\"><strong>(3.112)<\/strong><\/p>\n\n\n\n<p>By replacing\u00a0<em>D<\/em>\u00a0and\u00a0<em>W<\/em><sub>a<\/sub>\u00a0with Eqs\u00a0(3.106)\u00a0and\u00a0(3.110), respectively, we get:<\/p>\n\n\n\n<p id=\"FD221\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si233.png\" alt=\"image\" width=\"95\" height=\"38\"><strong>(3.113)<\/strong><\/p>\n\n\n\n<p>The maximum concentration ratio occurs when\u00a0<em>\u03c6<\/em><sub>r<\/sub>\u00a0is 90\u00b0 and sin(<em>\u03c6<\/em><sub>r<\/sub>)\u00a0=\u00a01. Therefore, by replacing sin(<em>\u03c6<\/em><sub>r<\/sub>)\u00a0=\u00a01 in Eq.\u00a0(3.113), the following maximum value can be obtained:<\/p>\n\n\n\n<p id=\"FD222\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si234.png\" alt=\"image\" width=\"114\" height=\"37\"><strong>(3.114)<\/strong><\/p>\n\n\n\n<p>The difference between this equation and Eq.\u00a0(3.94)\u00a0is that this one applies particularly to a PTC with a circular receiver, whereas Eq.\u00a0(3.94)\u00a0is the idealized case. So, by using the same sun half acceptance angle of 16\u2032 for single-axis tracking,\u00a0<em>C<\/em><sub>max<\/sub>\u00a0=\u00a01\/\u03c0sin(16\u2032)\u00a0=\u00a067.5.<\/p>\n\n\n\n<p id=\"P2400\">In fact, the magnitude of the rim angle determines the material required for the construction of the parabolic surface. The curve length of the reflective surface is given by:<\/p>\n\n\n\n<p id=\"FD223\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si235.png\" alt=\"image\" width=\"363\" height=\"32\"><strong>(3.115)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U8030\"><a><\/a><em>H<\/em><sub>p<\/sub>&nbsp;=&nbsp;lactus rectum of the parabola (m). This is the opening of the parabola at the focal point.<\/p>\n\n\n\n<p>As shown in\u00a0Figure 3.42\u00a0for the same aperture, various rim angles are possible. It is also shown that, for different rim angles, the focus-to-aperture ratio, which defines the curvature of the parabola, changes. It can be demonstrated that, with a 90\u00b0 rim angle, the mean focus-to-reflector distance and hence the reflected beam spread is minimized, so that the slope and tracking errors are less pronounced. The collector\u2019s surface area, however, decreases as the rim angle is decreased. There is thus a temptation to use smaller rim angles because the sacrifice in optical efficiency is small, but the saving in reflective material cost is great.<\/p>\n\n\n\n<p>EXAMPLE 3.10<\/p>\n\n\n\n<p id=\"P2410\">For a PTC with a rim angle of 70\u00b0, aperture of 5.6&nbsp;m, and receiver diameter of 50&nbsp;mm, estimate the focal distance, the concentration ratio, the rim radius, and the length of the parabolic surface.<\/p>\n\n\n\n<p id=\"BOXSECTITLE0055\">Solution<\/p>\n\n\n\n<p id=\"P2415\">From Eq.\u00a0(3.111),<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si231.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2420\">Therefore,<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si236.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2425\">From Eq.\u00a0(3.112), the concentration ratio is:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si237.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2430\">The rim radius is given by Eq.\u00a0(3.108):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si238.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2435\">The parabola lactus rectum,\u00a0<em>H<\/em><sub>p<\/sub>, is equal to\u00a0<em>W<\/em><sub>a<\/sub>\u00a0at\u00a0<em>\u03c6<\/em><sub>r<\/sub>\u00a0=\u00a090\u00b0 and\u00a0<em>f<\/em>\u00a0=\u00a02\u00a0m. From Eq.\u00a0(3.111),<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si239.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2440\">Finally, the length of the parabola can be obtained from Eq.&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#FD223\">(3.115)<\/a>&nbsp;by recalling that sec(<em>x<\/em>)&nbsp;=&nbsp;1\/cos(<em>x<\/em>):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si240.png\" alt=\"image\"\/><\/figure>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-42-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.42<\/strong>&nbsp;<a><\/a>Parabola focal length and curvature.<\/p>\n\n\n\n<h4 class=\"wp-block-heading\" id=\"CESECTITLE0155\">Optical efficiency<\/h4>\n\n\n\n<p id=\"P2445\"><em>Optical efficiency<\/em>\u00a0is defined as the ratio of the energy absorbed by the receiver to the energy incident on the collector\u2019s aperture. The optical efficiency depends on the optical properties of the materials involved, the geometry of the collector, and the various imperfections arising from the construction of the collector. In equation form (Sodha et al., 1984):<\/p>\n\n\n\n<p id=\"FD230\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si241.png\" alt=\"image\" width=\"224\" height=\"20\"><strong>(3.116)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0460\"><a><\/a><em>\u03c1<\/em>&nbsp;=&nbsp;reflectance of the mirror.<\/p>\n\n\n\n<p id=\"U0465\"><a><\/a><em>\u03c4<\/em>&nbsp;=&nbsp;transmittance of the glass cover.<\/p>\n\n\n\n<p id=\"U0470\"><a><\/a><em>\u03b1<\/em>&nbsp;=&nbsp;absorptance of the receiver.<a><\/a><\/p>\n\n\n\n<p id=\"U0475\"><a><\/a><em>\u03b3<\/em>&nbsp;=&nbsp;intercept factor.<\/p>\n\n\n\n<p id=\"U0480\"><a><\/a><em>A<\/em><sub>f<\/sub>&nbsp;=&nbsp;geometric factor.<\/p>\n\n\n\n<p id=\"U0485\"><a><\/a><em>\u03b8<\/em>&nbsp;=&nbsp;angle of incidence.<\/p>\n\n\n\n<p>The geometry of the collector dictates the geometric factor,\u00a0<em>A<\/em><sub>f<\/sub>, which is a measure of the effective reduction of the aperture area due to abnormal incidence effects, including blockages, shadows, and loss of radiation reflected from the mirror beyond the end of the receiver. During abnormal operation of a PTC, some of the rays reflected from near the end of the concentrator opposite the sun cannot reach the receiver. This is called the\u00a0<em>end effect<\/em>. The amount of aperture area lost is shown in\u00a0Figure 3.43\u00a0and given by:<\/p>\n\n\n\n<p id=\"FD231\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si242.png\" alt=\"image\" width=\"184\" height=\"40\"><strong>(3.117)<\/strong><\/p>\n\n\n\n<p>Usually, collectors of this type are terminated with opaque plates to preclude unwanted or dangerous concentration away from the receiver. These plates result in blockage or shading of a part of the reflector, which in effect reduces the aperture area. For a plate extending from rim to rim, the lost area is shown in\u00a0Figure 3.43\u00a0and given by:<\/p>\n\n\n\n<p id=\"FD232\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si243.png\" alt=\"image\" width=\"131\" height=\"34\"><strong>(3.118)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U8035\"><a><\/a><em>h<\/em><sub>p<\/sub>&nbsp;=&nbsp;height of parabola (m).<\/p>\n\n\n\n<p>It should be noted that the term tan(<em>\u03b8<\/em>) shown in Eqs\u00a0(3.117)\u00a0and\u00a0(3.118)\u00a0is the same as the one shown in Eq.\u00a0(3.116), and it should not be used twice. Therefore, to find the total loss in aperture area,\u00a0<em>A<\/em><sub>l<\/sub>, the two areas,\u00a0<em>A<\/em><sub>e<\/sub>\u00a0and\u00a0<em>A<\/em><sub>b<\/sub>, are added together without including the term tan(<em>\u03b8<\/em>) (Jeter, 1983):<\/p>\n\n\n\n<p id=\"FD233\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si244.png\" alt=\"image\" width=\"206\" height=\"40\"><strong>(3.119)<\/strong><\/p>\n\n\n\n<p>Finally, the geometric factor is the ratio of the lost area to the aperture area. Therefore,<\/p>\n\n\n\n<p id=\"FD234\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si245.png\" alt=\"image\" width=\"58\" height=\"36\"><strong>(3.120)<\/strong><\/p>\n\n\n\n<p>The most complex parameter involved in determining the optical efficiency of a PTC is the intercept factor. This is defined as the ratio of the energy intercepted by the receiver to the energy reflected by<a><\/a>&nbsp;the focusing device, that is, the parabola. Its value depends on the size of the receiver, the surface angle errors of the parabolic mirror, and the solar beam spread.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-43-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.43<\/strong>&nbsp;<a><\/a>End effect and blocking in a parabolic trough collector.<\/p>\n\n\n\n<p id=\"P2505\">The errors associated with the parabolic surface are of two types: random and non-random (Guven and Bannerot, 1985).\u00a0<em>Random errors<\/em>\u00a0are defined as those errors that are truly random in nature and, therefore, can be represented by normal probability distributions. Random errors are identified as apparent changes in the sun\u2019s width, scattering effects caused by random slope errors (i.e., distortion of the parabola due to wind loading), and scattering effects associated with the reflective surface.\u00a0<em>Non-random errors<\/em>\u00a0arise in manufacture assembly or the operation of the collector. These can be identified as reflector profile imperfections, misalignment errors, and receiver location errors. Random errors are modeled statistically, by determining the standard deviation of the total reflected energy distribution, at normal incidence (Guven and Bannerot, 1986), and are given by:<\/p>\n\n\n\n<p id=\"FD235\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si246.png\" alt=\"image\" width=\"190\" height=\"29\"><strong>(3.121)<\/strong><\/p>\n\n\n\n<p>Non-random errors are determined from a knowledge of the misalignment angle error\u00a0<em>\u03b2<\/em>\u00a0(i.e., the angle between the reflected ray from the center of the sun and the normal to the reflector\u2019s aperture plane) and the displacement of the receiver from the focus of the parabola (<em>d<\/em><sub>r<\/sub>). Since reflector profile errors and receiver mislocation along the\u00a0<em>Y<\/em>\u00a0axis essentially have the same effect, a single parameter is used to account for both. According to\u00a0Guven and Bannerot (1986), random and non-random errors can be combined with the collector geometric parameters, concentration ratio (<em>C<\/em>), and receiver diameter (<em>D<\/em>) to yield error parameters universal to all collector geometries. These are called\u00a0<em>universal error parameters<\/em>, and an asterisk is used to distinguish them from the already defined parameters. Using the universal error parameters, the formulation of the intercept factor,\u00a0<em>\u03b3<\/em>, is possible (Guven and Bannerot, 1985):<\/p>\n\n\n\n<p id=\"FD236\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si247.png\" alt=\"image\" width=\"562\" height=\"112\"><strong>(3.122)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0490\"><a><\/a><em>d<\/em><sup>\u2217<\/sup>&nbsp;=&nbsp;universal non-random error parameter due to receiver mislocation and reflector profile errors,&nbsp;<em>d<\/em><sup>\u2217<\/sup>&nbsp;=&nbsp;<em>d<\/em><sub>r<\/sub>\/<em>D<\/em>.<\/p>\n\n\n\n<p id=\"U0495\"><a><\/a><em>\u03b2<\/em><sup>\u2217<\/sup>&nbsp;=&nbsp;universal non-random error parameter due to angular errors,&nbsp;<em>\u03b2<\/em><sup>\u2217<\/sup>&nbsp;=&nbsp;<em>\u03b2<\/em>C.<\/p>\n\n\n\n<p id=\"U0500\"><a><\/a><em>\u03c3<\/em><sup>\u2217<\/sup>&nbsp;=&nbsp;universal random error parameter,&nbsp;<em>\u03c3<\/em><sup>\u2217<\/sup>&nbsp;=&nbsp;<em>\u03c3C<\/em>.<\/p>\n\n\n\n<p id=\"U0505\"><a><\/a><em>C<\/em>&nbsp;=&nbsp;collector concentration ratio,&nbsp;=&nbsp;<em>A<\/em><sub>a<\/sub>\/<em>A<\/em><sub>r<\/sub>.<\/p>\n\n\n\n<p id=\"U0510\"><a><\/a><em>D<\/em>&nbsp;=&nbsp;riser tube outside diameter (m).<\/p>\n\n\n\n<p id=\"U0515\"><a><\/a><em>d<\/em><sub>r<\/sub>&nbsp;=&nbsp;displacement of receiver from focus (m).<\/p>\n\n\n\n<p id=\"U0520\"><a><\/a><em>\u03b2<\/em>&nbsp;=&nbsp;misalignment angle error (degrees).<\/p>\n\n\n\n<p>Another type of analysis commonly carried out in concentrating collectors is ray tracing. This is the process of following the paths of a large number of rays of incident radiation through the optical system to determine the distribution and intensity of the rays on the surface of the receiver. Ray tracing determines the radiation concentration distribution on the receiver of the collector, called the\u00a0<em>local concentration ratio<\/em>\u00a0(LCR). As was seen in\u00a0Figure 3.41, the radiation incident on a differential element of reflector area is a cone having a half angle of 16\u2032. The reflected radiation is a similar cone, having the same apex angle if the reflector is perfect. The intersection of this cone with the receiver surface determines the image size and shape for that element, and the total image is the sum of the images for all the elements of the reflector. In an actual collector, the various errors outlined previously, which enlarge the image size and lower the LCR, are considered. The distribution of the LCR for a parabolic trough collector is shown in\u00a0Figure 3.44. The shape of the curves depends on the random and non-random errors mentioned above and on the angle of incidence. It should be noted that the distribution for half of the receiver is shown in\u00a0Figure 3.44. Another more representative way to show this distribution for the whole receiver is in\u00a0Figure 3.45. As can be seen , the top part of the receiver essentially receives\u00a0only direct sunshine from the sun and the maximum concentration for this particular collector, about 36 suns, occurs at 0 incidence angle and at an angle\u00a0<em>\u03b2<\/em>\u00a0of 120\u00b0 (Figure 3.44).<\/p>\n\n\n\n<p>EXAMPLE 3.11<\/p>\n\n\n\n<p id=\"P2555\">For a PTC with a total aperture area of 50&nbsp;m<sup>2<\/sup>, aperture of 2.5&nbsp;m, and rim angle of 90\u00b0, estimate the geometric factor and the actual area lost at an angle of incidence equal to 60\u00b0.<\/p>\n\n\n\n<p id=\"BOXSECTITLE0060\">Solution<\/p>\n\n\n\n<p id=\"P2560\">As\u00a0<em>\u03c6<\/em><sub>r<\/sub>\u00a0=\u00a090\u00b0, the parabola height\u00a0<em>h<\/em><sub>p<\/sub>\u00a0=\u00a0<em>f<\/em>. Therefore, from Eq.\u00a0(3.111),<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si248.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2565\">From Eq.\u00a0(3.119):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si249.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2570\">The area lost at an incidence angle of 60\u00b0 is:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si250.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2575\">The geometric factor\u00a0<em>A<\/em><sub>f<\/sub>\u00a0is obtained from Eq.\u00a0(3.120):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si251.png\" alt=\"image\"\/><\/figure>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-44-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.44<\/strong>&nbsp;<a><\/a>Local concentration ratio on the receiver of a parabolic trough collector.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-45-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.45<\/strong>&nbsp;<a><\/a>A more representative view of LCR for a collector with receiver diameter of 20&nbsp;mm and rim angle of 90\u00b0.<\/p>\n\n\n\n<h3 class=\"wp-block-heading\" id=\"CESECTITLE0160\">3.6.4 Thermal analysis of parabolic trough collectors<\/h3>\n\n\n\n<p id=\"P2580\">The generalized thermal analysis of a concentrating solar collector is similar to that of a flat-plate collector. It is necessary to derive appropriate expressions for the collector efficiency factor,&nbsp;<em>F\u2032<\/em>; the loss coefficient,&nbsp;<em>U<\/em><sub>L<\/sub>; and the collector heat removal factor,&nbsp;<em>F<\/em><sub>R<\/sub>. For the loss coefficient, standard heat transfer relations for glazed tubes can be used. Thermal losses from the receiver must be estimated, usually in terms of the loss coefficient,&nbsp;<em>U<\/em><sub>L<\/sub>, which is based on the area of the receiver. The method for calculating thermal losses from concentrating collector receivers cannot be as easily summarized as for the flat-plate ones, because many designs and configurations are available. Two such designs are presented in this book: the PTC with a bare tube and the glazed tube receiver. In both cases, the calculations must include radiation, conduction, and convection losses.<\/p>\n\n\n\n<p id=\"P2585\">For a bare tube receiver and assuming no temperature gradients along the receiver, the loss coefficient considering convection and radiation from the surface and conduction through the support structure is given by:<\/p>\n\n\n\n<p id=\"FD241\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si252.png\" alt=\"image\" width=\"126\" height=\"13\"><strong>(3.123)<\/strong><a><\/a><\/p>\n\n\n\n<p id=\"P2590\">The linearized radiation coefficient can be estimated from:<\/p>\n\n\n\n<p id=\"FD242\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si253.png\" alt=\"image\" width=\"77\" height=\"19\"><strong>(3.124)<\/strong><\/p>\n\n\n\n<p>If a single value of&nbsp;<em>h<\/em><sub>r<\/sub>&nbsp;is not acceptable due to large temperature variations along the flow direction, the collector can be divided into small segments, each with a constant&nbsp;<em>h<\/em><sub>r<\/sub>.<\/p>\n\n\n\n<p id=\"P2600\">For the wind loss coefficient, the Nusselt number can be used.<\/p>\n\n\n\n<p id=\"P2605\">For 0.1&nbsp;&lt;&nbsp;Re&nbsp;&lt;&nbsp;1000,<\/p>\n\n\n\n<p id=\"FD243\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si254.png\" alt=\"image\" width=\"162\" height=\"20\"><strong>(3.125a)<\/strong><\/p>\n\n\n\n<p>For 1000&nbsp;&lt;&nbsp;Re&nbsp;&lt;&nbsp;50,000,<\/p>\n\n\n\n<p id=\"FD244\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si255.png\" alt=\"image\" width=\"108\" height=\"20\"><strong>(3.125b)<\/strong><\/p>\n\n\n\n<p>Estimation of the conduction losses requires knowledge of the construction of the collector, that is, the way the receiver is supported.<\/p>\n\n\n\n<p id=\"P2620\">Usually, to reduce the heat losses, a concentric glass tube is employed around the receiver. The space between the receiver and the glass is usually evacuated, in which case the convection losses are negligible. In this case,&nbsp;<em>U<\/em><sub>L<\/sub>, based on the receiver area&nbsp;<em>A<\/em><sub>r<\/sub>, is given by:<\/p>\n\n\n\n<p id=\"FD245\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si256.png\" alt=\"image\" width=\"229\" height=\"45\"><strong>(3.126)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0525\"><em>h<\/em><sub>r,c\u2013a<\/sub>\u00a0=\u00a0linearized radiation coefficient from cover to ambient estimated by Eq.\u00a0(3.124)\u00a0(W\/m<sup>2<\/sup>\u00a0K).<\/p>\n\n\n\n<p id=\"U0530\"><a><\/a><em>A<\/em><sub>g<\/sub>&nbsp;=&nbsp;external area of glass cover (m<sup>2<\/sup>).<\/p>\n\n\n\n<p id=\"U0535\"><em>h<\/em><sub>r,r\u2013c<\/sub>\u00a0=\u00a0linearized radiation coefficient from receiver to cover, given by Eq.\u00a0(2.74):<\/p>\n\n\n\n<p id=\"FD246\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si257.png\" alt=\"image\" width=\"203\" height=\"62\"><strong>(3.127)<\/strong><\/p>\n\n\n\n<p>In the preceding equations, to estimate the glass cover properties, the temperature of the glass cover,&nbsp;<em>T<\/em><sub>g<\/sub>, is required. This temperature is closer to the ambient temperature than the receiver temperature. Therefore, by ignoring the radiation absorbed by the cover,&nbsp;<em>T<\/em><sub>g<\/sub>&nbsp;may be obtained from an energy balance:<\/p>\n\n\n\n<p id=\"FD247\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si258.png\" alt=\"image\" width=\"304\" height=\"20\"><strong>(3.128)<\/strong><\/p>\n\n\n\n<p>Solving Eq.\u00a0(3.128)\u00a0for\u00a0<em>T<\/em><sub>g<\/sub>\u00a0gives:<\/p>\n\n\n\n<p id=\"FD248\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si259.png\" alt=\"image\" width=\"243\" height=\"44\"><strong>(3.129)<\/strong><\/p>\n\n\n\n<p>The procedure to find\u00a0<em>T<\/em><sub>g<\/sub>\u00a0is by iteration, that is, estimate\u00a0<em>U<\/em><sub>L<\/sub>\u00a0from Eq.\u00a0(3.126)\u00a0by considering a random\u00a0<em>T<\/em><sub>g<\/sub>\u00a0(close to\u00a0<em>T<\/em><sub>a<\/sub>). Then, if\u00a0<em>T<\/em><sub>g<\/sub>\u00a0obtained from Eq.\u00a0(3.129)\u00a0differs from original value, iterate. Usually, no more than two iterations are required.<\/p>\n\n\n\n<p id=\"P2655\">If radiation absorbed by the cover needs to be considered, the appropriate term must be added to the right-hand side of Eq.&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#FD245\">(3.126)<\/a>. The principles are the same as those developed earlier for the flat-plate collectors.<\/p>\n\n\n\n<p id=\"P2660\">Next, the overall heat transfer coefficient,&nbsp;<em>U<\/em><sub>o<\/sub>, needs to be estimated. This should include the tube wall because the heat flux in a concentrating collector is high. Based on the outside tube diameter, this is given by:<\/p>\n\n\n\n<p id=\"FD249\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si260.png\" alt=\"image\" width=\"250\" height=\"42\"><strong>(3.130)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0540\"><a><\/a><em>D<\/em><sub>o<\/sub>&nbsp;=&nbsp;receiver outside tube diameter (m).<\/p>\n\n\n\n<p id=\"U0545\"><a><\/a><em>D<\/em><sub>i<\/sub>&nbsp;=&nbsp;receiver inside tube diameter (m).<\/p>\n\n\n\n<p id=\"U0550\"><a><\/a><em>h<\/em><sub>fi<\/sub>&nbsp;=&nbsp;convective heat transfer coefficient inside the receiver tube (W\/m<sup>2<\/sup>&nbsp;K).<\/p>\n\n\n\n<p>The convective heat transfer coefficient,&nbsp;<em>h<\/em><sub>fi<\/sub>, can be obtained from the standard pipe flow equation:<\/p>\n\n\n\n<p id=\"FD250\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si261.png\" alt=\"image\" width=\"169\" height=\"20\"><strong>(3.131)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0555\"><a><\/a>Re&nbsp;=&nbsp;Reynolds number&nbsp;=&nbsp;<em>\u03c1VD<\/em><sub>i<\/sub>\/<em>\u03bc<\/em>.<\/p>\n\n\n\n<p id=\"U0560\"><a><\/a>Pr&nbsp;=&nbsp;Prandtl number&nbsp;=&nbsp;<em>c<\/em><sub>p<\/sub><em>\u03bc<\/em>\/<em>k<\/em><sub>f<\/sub>.<\/p>\n\n\n\n<p id=\"U0565\"><a><\/a><em>\u03bc<\/em>&nbsp;=&nbsp;fluid viscosity (kg\/m&nbsp;s).<\/p>\n\n\n\n<p id=\"U0570\"><a><\/a><em>k<\/em><sub>f<\/sub>&nbsp;=&nbsp;thermal conductivity of fluid (W\/m&nbsp;K).<\/p>\n\n\n\n<p>It should be noted that Eq.\u00a0(3.131)\u00a0is for turbulent flow (Re\u00a0>\u00a02300). For laminar flow, Nu\u00a0=\u00a04.364\u00a0=\u00a0constant.<\/p>\n\n\n\n<p id=\"P2710\">A detailed thermal model of a PTC is presented by\u00a0Kalogirou (2012). In this all modes of heat transfer were considered in detail and the set of equations obtained were solved simultaneously. For this purpose the program Engineering Equation Solver (EES) is used which includes routines to estimate the properties of various substances and can be called from TRNSYS (see\u00a0Chapter 11, Section 11.5.1) which allows the development of a model that can use the capabilities of both programs.<\/p>\n\n\n\n<p id=\"P2715\">The instantaneous efficiency of a concentrating collector may be calculated from an energy balance of its receiver. Equation&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#FD76\">(3.31)<\/a>&nbsp;also may be adapted for use with concentrating collectors by using appropriate areas for the absorbed solar radiation (<em>A<\/em><sub>a<\/sub>) and heat losses (<em>A<\/em><sub>r<\/sub>). Therefore, the useful energy delivered from a concentrator is:<\/p>\n\n\n\n<p id=\"FD251\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si262.png\" alt=\"image\" width=\"211\" height=\"16\"><strong>(3.132)<\/strong><\/p>\n\n\n\n<p>Note that, because concentrating collectors can utilize only beam radiation,\u00a0<em>G<\/em><sub>B<\/sub>\u00a0is used in Eq.\u00a0(3.132)\u00a0instead of the total radiation,\u00a0<em>G<\/em><sub>t<\/sub>, used in Eq.\u00a0(3.31).<\/p>\n\n\n\n<p id=\"P2725\">The useful energy gain per unit of collector length can be expressed in terms of the local receiver temperature,&nbsp;<em>T<\/em><sub>r<\/sub>, as:<\/p>\n\n\n\n<p id=\"FD252\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si263.png\" alt=\"image\" width=\"249\" height=\"34\"><strong>(3.133)<\/strong><\/p>\n\n\n\n<p>In terms of the energy transfer to the fluid at the local fluid temperature,\u00a0<em>T<\/em><sub>f<\/sub>\u00a0(Kalogirou, 2004),<\/p>\n\n\n\n<p id=\"FD253\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si264.png\" alt=\"image\" width=\"145\" height=\"53\"><strong>(3.134)<\/strong><\/p>\n\n\n\n<p>If&nbsp;<em>T<\/em><sub>r<\/sub>&nbsp;is eliminated from Eqs&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#FD252\">(3.133)<\/a>&nbsp;and&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#FD253\">(3.134)<\/a>, we have:<\/p>\n\n\n\n<p id=\"FD254\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si265.png\" alt=\"image\" width=\"226\" height=\"39\"><strong>(3.135)<\/strong><\/p>\n\n\n\n<p>where&nbsp;<em>F<\/em>\u2032 is the collector efficiency factor, given by:<\/p>\n\n\n\n<p id=\"FD255\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si266.png\" alt=\"image\" width=\"220\" height=\"49\"><strong>(3.136)<\/strong><\/p>\n\n\n\n<p>As for the flat-plate collector,\u00a0<em>T<\/em><sub>r<\/sub>\u00a0in Eq.\u00a0(3.132)\u00a0can be replaced by\u00a0<em>T<\/em><sub>i<\/sub>\u00a0through the use of the heat removal factor, and Eq.\u00a0(3.132)\u00a0can be written as:<\/p>\n\n\n\n<p id=\"FD256\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si267.png\" alt=\"image\" width=\"237\" height=\"16\"><strong>(3.137)<\/strong><\/p>\n\n\n\n<p>The collector efficiency can be obtained by dividing&nbsp;<em>Q<\/em><sub>u<\/sub>&nbsp;by (<em>G<\/em><sub>B<\/sub><em>A<\/em><sub>a<\/sub>). Therefore,<\/p>\n\n\n\n<p id=\"FD257\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si268.png\" alt=\"image\" width=\"188\" height=\"39\"><strong>(3.138)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U8045\"><a><\/a><em>C<\/em>&nbsp;=&nbsp;concentration ratio,&nbsp;<em>C<\/em>&nbsp;=&nbsp;<em>A<\/em><sub>a<\/sub>\/<em>A<\/em><sub>r<\/sub>.<\/p>\n\n\n\n<p>For\u00a0<em>F<\/em><sub>R<\/sub>, a relation similar to Eq.\u00a0(3.58)\u00a0is used by replacing\u00a0<em>A<\/em><sub>c<\/sub>\u00a0with\u00a0<em>A<\/em><sub>r<\/sub>\u00a0and using\u00a0<em>F<\/em>\u2032, given by Eq.\u00a0(3.136), which does not include the fin and bond conductance terms, as in FPCs. This equation explains why high temperatures can be obtained with concentrating collectors. This is because the heat losses term is inversely proportional to\u00a0<em>C<\/em>, so the bigger the concentration ratio the smaller the losses.<\/p>\n\n\n\n<h4 class=\"wp-block-heading\" id=\"CESECTITLE0165\">Consideration of vacuum in annulus space<\/h4>\n\n\n\n<p id=\"P2755\">In the analysis presented so far, the convection losses in the annulus space are ignored. In fact convection heat transfer depends on the annulus pressure. At low pressures (&lt;0.013\u00a0Pa), heat transfer is by molecular conduction, whereas at higher pressures is by free convection. When the annulus is under vacuum (pressure &lt;0.013\u00a0Pa), the convection heat transfer between the receiver pipe and glass envelope occurs by free molecular convection and the heat transfer coefficient is given by (Ratzel et al., 1979):<\/p>\n\n\n\n<p id=\"FD258\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si269.png\" alt=\"image\" width=\"190\" height=\"55\"><strong>(3.139)<\/strong><\/p>\n\n\n\n<p>This equation is applicable for: Ra&nbsp;&lt;&nbsp;(<em>D<\/em><sub>g<\/sub>\/(<em>D<\/em><sub>g<\/sub>&nbsp;\u2212&nbsp;<em>D<\/em><sub>r<\/sub>))<sup>4<\/sup>.<\/p>\n\n\n\n<p id=\"P2765\">And<\/p>\n\n\n\n<p id=\"FD259\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si270.png\" alt=\"image\" width=\"129\" height=\"38\"><strong>(3.140)<\/strong><\/p>\n\n\n\n<p id=\"FD260\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si271.png\" alt=\"image\" width=\"208\" height=\"44\"><strong>(3.141)<\/strong><\/p>\n\n\n\n<p><a><\/a>where<a><\/a><\/p>\n\n\n\n<p id=\"U0575\"><a><\/a><em>k<\/em><sub>std<\/sub>&nbsp;=&nbsp;thermal conductivity of the annulus gas at standard temperature and pressure (W\/m&nbsp;\u00b0C)<\/p>\n\n\n\n<p id=\"U0580\"><a><\/a><em>D<\/em><sub>r<\/sub>&nbsp;=&nbsp;outside receiver pipe diameter (m)<\/p>\n\n\n\n<p id=\"U0585\"><a><\/a><em>D<\/em><sub>g<\/sub>&nbsp;=&nbsp;inside glass envelope diameter (m)<\/p>\n\n\n\n<p id=\"U0590\"><a><\/a><em>b<\/em>&nbsp;=&nbsp;interaction coefficient<\/p>\n\n\n\n<p id=\"U0595\"><a><\/a><em>\u03bb<\/em>&nbsp;=&nbsp;mean free path between collisions of a molecule (cm)<\/p>\n\n\n\n<p id=\"U0600\"><a><\/a><em>a<\/em>&nbsp;=&nbsp;accommodation coefficient<\/p>\n\n\n\n<p id=\"U0605\"><a><\/a><em>\u03b3<\/em>&nbsp;=&nbsp;ratio of specific heats for the annulus gas (air)<\/p>\n\n\n\n<p id=\"U0610\"><a><\/a><em>T<\/em><sub>r\u2013g<\/sub>&nbsp;=&nbsp;average temperature (<em>T<\/em><sub>r<\/sub>&nbsp;+&nbsp;<em>T<\/em><sub>g<\/sub>)\/2 (\u00b0C)<\/p>\n\n\n\n<p id=\"U0615\"><a><\/a><em>P<\/em><sub>a<\/sub>&nbsp;=&nbsp;annulus gas pressure (mmHg) and<\/p>\n\n\n\n<p id=\"U0620\"><a><\/a><em>\u03b4<\/em>&nbsp;=&nbsp;molecular diameter of annulus gas (cm).<\/p>\n\n\n\n<p>Equation\u00a0(3.139)\u00a0slightly overestimates the heat transfer for very small pressures (&lt;0.013\u00a0Pa). The molecular diameters of air,\u00a0<em>\u03b4<\/em>, is equal to 3.55 \u00d7 10<sup>\u22128<\/sup>\u00a0cm (Marshal, 1976), the thermal conductivity of air is 0.02551\u00a0W\/m\u00a0\u00b0C, the interaction coefficient is 1.571, the mean free path between collisions of a molecule is 88.67\u00a0cm, and the ratio of specific heats for the annulus air is 1.39. These are for average fluid temperature of 300\u00a0\u00b0C and pressure equal to 0.013\u00a0Pa. Using these values, the convection heat transfer coefficient (<em>h<\/em><sub>c,r\u2013c<\/sub>) is equal to 0.0001115\u00a0W\/m<sup>2<\/sup>\u00a0\u00b0C, which is the reason why usually it is ignored.<\/p>\n\n\n\n<p id=\"P2825\">If for more accuracy this heat loss is considered Eq.\u00a0(3.126)\u00a0should include\u00a0<em>h<\/em><sub>c,r\u2013c<\/sub>\u00a0in the second term as well as Eq.\u00a0(3.128)\u00a0for the appropriate estimation of\u00a0<em>T<\/em><sub>g<\/sub>.<\/p>\n\n\n\n<p id=\"P9000\">If the receiver is filled or partially filled with ambient air or if the receiver annulus vacuum is lost, the convection heat transfer between the receiver pipe and glass envelope occurs by natural convection and for this purpose, the correlation for natural convection in an annular space (enclosure) between horizontal concentric cylinders can be used, found in many heat transfer books.<a><\/a><a><\/a><\/p>\n\n\n\n<p>EXAMPLE 3.12<\/p>\n\n\n\n<p id=\"P2830\">A 20&nbsp;m long PTC with an aperture width of 3.5&nbsp;m has a pipe receiver of 50&nbsp;mm outside diameter and 40&nbsp;mm inside diameter and a glass cover of 90&nbsp;mm in diameter. If the space between the receiver and the glass cover is evacuated, estimate the overall collector heat loss coefficient, the useful energy gain, and the exit fluid temperature. The following data are given:<a><\/a><\/p>\n\n\n\n<p id=\"U0625\"><a><\/a>Absorbed solar radiation&nbsp;=&nbsp;500&nbsp;W\/m<sup>2<\/sup>.<\/p>\n\n\n\n<p id=\"U0630\"><a><\/a>Receiver temperature&nbsp;=&nbsp;260&nbsp;\u00b0C&nbsp;=&nbsp;533&nbsp;K.<\/p>\n\n\n\n<p id=\"U0635\"><a><\/a>Receiver emissivity,&nbsp;<em>\u03b5<\/em><sub>r<\/sub>&nbsp;=&nbsp;0.92.<\/p>\n\n\n\n<p id=\"U0640\"><a><\/a>Glass cover emissivity,&nbsp;<em>\u03b5<\/em><sub>g<\/sub>&nbsp;=&nbsp;0.87.<\/p>\n\n\n\n<p id=\"U0645\"><a><\/a>Circulating fluid,&nbsp;<em>c<\/em><sub>p<\/sub>&nbsp;=&nbsp;1350&nbsp;J\/kg&nbsp;K.<\/p>\n\n\n\n<p id=\"U0650\"><a><\/a>Entering fluid temperature&nbsp;=&nbsp;220&nbsp;\u00b0C&nbsp;=&nbsp;493&nbsp;K.<\/p>\n\n\n\n<p id=\"U0655\"><a><\/a>Mass flow rate&nbsp;=&nbsp;0.32&nbsp;kg\/s.<\/p>\n\n\n\n<p id=\"U0660\"><a><\/a>Heat transfer coefficient inside the pipe&nbsp;=&nbsp;330&nbsp;W\/m<sup>2<\/sup>&nbsp;K.<\/p>\n\n\n\n<p id=\"U0665\"><a><\/a>Tube thermal conductivity,&nbsp;<em>k<\/em>&nbsp;=&nbsp;15&nbsp;W\/m&nbsp;K.<\/p>\n\n\n\n<p id=\"U0670\"><a><\/a>Ambient temperature&nbsp;=&nbsp;25&nbsp;\u00b0C&nbsp;=&nbsp;298&nbsp;K.<\/p>\n\n\n\n<p id=\"U0675\"><a><\/a>Wind velocity&nbsp;=&nbsp;5&nbsp;m\/s.<\/p>\n\n\n\n<p id=\"BOXSECTITLE0065\">Solution<\/p>\n\n\n\n<p id=\"P2890\">The receiver area&nbsp;<em>A<\/em><sub>r<\/sub>&nbsp;=&nbsp;\u03c0<em>D<\/em><sub>o<\/sub><em>L<\/em>&nbsp;=&nbsp;\u03c0&nbsp;\u00d7&nbsp;0.05&nbsp;\u00d7&nbsp;20&nbsp;=&nbsp;3.14&nbsp;m<sup>2<\/sup>. The glass cover area&nbsp;<em>A<\/em><sub>g<\/sub>&nbsp;=&nbsp;\u03c0<em>D<\/em><sub>g<\/sub><em>L<\/em>&nbsp;=&nbsp;\u03c0&nbsp;\u00d7&nbsp;0.09&nbsp;\u00d7&nbsp;20&nbsp;=&nbsp;5.65&nbsp;m<sup>2<\/sup>. The unshaded collector aperture area&nbsp;<em>A<\/em><sub>a<\/sub>&nbsp;= (3.5&nbsp;\u2212&nbsp;0.09)&nbsp;\u00d7&nbsp;20&nbsp;=&nbsp;68.2&nbsp;m<sup>2<\/sup>.<\/p>\n\n\n\n<p id=\"P2895\">Next, a glass cover temperature,\u00a0<em>T<\/em><sub>g<\/sub>, is assumed to evaluate the convection and radiation heat transfer from the glass cover. This is assumed to be equal to 64\u00a0\u00b0C\u00a0=\u00a0337\u00a0K. The actual glass cover temperature is obtained by iteration by neglecting the interactions with the reflector. The convective (wind) heat transfer coefficient\u00a0<em>h<\/em><sub>c,c\u2013a<\/sub>\u00a0=\u00a0<em>h<\/em><sub>w<\/sub>\u00a0of the glass cover can be calculated from Eq.\u00a0(3.125). First, the Reynolds number needs to be estimated at the mean temperature \u00bd(25\u00a0+\u00a064)\u00a0=\u00a044.5\u00a0\u00b0C. Therefore, from\u00a0Table A5.1\u00a0in\u00a0Appendix 5, we get:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si272.png\" alt=\"image\"\/><\/figure>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si273.png\" alt=\"image\"\/><\/figure>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si274.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2900\">Now<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si275.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2905\">Therefore, Eq.\u00a0(3.125b)\u00a0applies, which gives:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si276.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p>and<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si277.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2910\">The radiation heat transfer coefficient,\u00a0<em>h<\/em><sub>r,c\u2013a<\/sub>, for the glass cover to the ambient is calculated from Eq.\u00a0(2.75):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si278.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2915\">The radiation heat transfer coefficient,\u00a0<em>h<\/em><sub>r,r\u2013c<\/sub>, between the receiver tube and the glass cover is estimated from Eq.\u00a0(3.127):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si279.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2920\">Since the space between the receiver and the glass cover is evacuated, there is no convection heat transfer. Therefore, based on the receiver area, the overall collector heat loss coefficient is given by Eq.\u00a0(3.126):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si280.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2925\">Since&nbsp;<em>U<\/em><sub>L<\/sub>&nbsp;is based on the assumed&nbsp;<em>T<\/em><sub>g<\/sub>&nbsp;value, we need to check if the assumption made was correct. Using Eq.&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#FD248\">(3.129)<\/a>, we get:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si281.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2930\">This is about the same as the value assumed earlier.<\/p>\n\n\n\n<p id=\"P2935\">The collector efficiency factor can be calculated from Eq.\u00a0(3.136):<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si282.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2940\">The heat removal factor can be calculated from Eq.\u00a0(3.58)\u00a0by using\u00a0<em>A<\/em><sub>r<\/sub>\u00a0instead of\u00a0<em>A<\/em><sub>c<\/sub>:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si283.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2945\">The useful energy is estimated from Eq.\u00a0(3.137)\u00a0using the concept of absorbed radiation:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si284.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2950\">Finally, the fluid exit temperature can be estimated from:<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si285.png\" alt=\"image\"\/><\/figure>\n\n\n\n<p id=\"P2955\">Another analysis usually performed for PTCs applies a piecewise two-dimensional model of the receiver by considering the circumferential variation of solar flux shown in\u00a0Figures 3.44\u00a0and\u00a03.45. Such an analysis can be performed by dividing the receiver into longitudinal and isothermal nodal sections, as shown in\u00a0Figure 3.46, and applying the principle of energy balance to the glazing and receiver nodes (Karimi et al., 1986).<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-46-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.46<\/strong>&nbsp;<a><\/a>Piecewise two-dimensional model of the receiver assembly.&nbsp;<a href=\"https:\/\/learning.oreilly.com\/library\/view\/solar-energy-engineering\/9780123972705\/xhtml\/CHP003.html#BIB31\">Karimi et al. (1986)<\/a>.<\/p>\n\n\n\n<p id=\"P2960\">The generalized glazing and absorber nodes, showing the various modes of heat transfer considered, are shown in\u00a0Figure 3.47. It is assumed that the length of each section is very small so that the\u00a0working fluid in that section stays in the inlet temperature. The temperature is adjusted in a stepwise fashion at the end of the longitudinal section. By applying the principle of energy balance to the glazing and absorber nodes, we get the following equations.<\/p>\n\n\n\n<figure class=\"wp-block-image\"><img decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030f03-47-9780123972705.jpg\" alt=\"image\"\/><\/figure>\n\n\n\n<p><strong>FIGURE 3.47<\/strong>\u00a0Generalized glazing and absorber nodes, showing the various modes of heat transfer.\u00a0Karimi et al. (1986).<\/p>\n\n\n\n<p id=\"P2965\">For the glazing node,<\/p>\n\n\n\n<p id=\"FD275\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si286.png\" alt=\"image\" width=\"336\" height=\"14\"><strong>(3.142)<\/strong><\/p>\n\n\n\n<p>For the absorber node,<\/p>\n\n\n\n<p id=\"FD276\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/learning.oreilly.com\/api\/v2\/epubs\/urn:orm:book:9780123972705\/files\/images\/F000030si287.png\" alt=\"image\" width=\"336\" height=\"14\"><strong>(3.143)<\/strong><\/p>\n\n\n\n<p>where<a><\/a><\/p>\n\n\n\n<p id=\"U0680\"><a><\/a><em>q<\/em><sub>G1<\/sub>&nbsp;=&nbsp;solar radiation absorbed by glazing node&nbsp;<em>i.<\/em><\/p>\n\n\n\n<p id=\"U0685\"><a><\/a><em>q<\/em><sub>G2<\/sub>&nbsp;=&nbsp;net radiation exchange between glazing node&nbsp;<em>i<\/em>&nbsp;to the surroundings.<\/p>\n\n\n\n<p id=\"U0690\"><a><\/a><em>q<\/em><sub>G3<\/sub>&nbsp;=&nbsp;natural and forced convection heat transfer from glazing node&nbsp;<em>i<\/em>&nbsp;to the surroundings.<\/p>\n\n\n\n<p id=\"U0695\"><a><\/a><em>q<\/em><sub>G4<\/sub>&nbsp;=&nbsp;convection heat transfer to the glazing node from the absorber (across the gap).<\/p>\n\n\n\n<p id=\"U0700\"><a><\/a><em>q<\/em><sub>G5<\/sub>&nbsp;=&nbsp;radiation emitted by the inside surface of the glazing node&nbsp;<em>i.<\/em><\/p>\n\n\n\n<p id=\"U0705\"><a><\/a><em>q<\/em><sub>G6<\/sub>&nbsp;=&nbsp;conduction along the circumference of glazing from node&nbsp;<em>i<\/em>&nbsp;to&nbsp;<em>i<\/em>&nbsp;+&nbsp;1.<\/p>\n\n\n\n<p id=\"U0710\"><a><\/a><em>q<\/em><sub>G7<\/sub>&nbsp;=&nbsp;conduction along the circumference of the glazing from node&nbsp;<em>i<\/em>&nbsp;to&nbsp;<em>i<\/em>&nbsp;\u2212&nbsp;1.<\/p>\n\n\n\n<p id=\"U0715\"><a><\/a><em>q<\/em><sub>G8<\/sub>&nbsp;=&nbsp;fraction of the total radiation incident upon the inside glazing surface that is absorbed.<\/p>\n\n\n\n<p id=\"U0720\"><a><\/a><em>q<\/em><sub>A1<\/sub>&nbsp;=&nbsp;solar radiation absorbed by absorber node&nbsp;<em>i.<\/em><\/p>\n\n\n\n<p id=\"U0725\"><a><\/a><em>q<\/em><sub>A2<\/sub>&nbsp;=&nbsp;thermal radiation emitted by outside surface of absorber node&nbsp;<em>i.<\/em><\/p>\n\n\n\n<p id=\"U0730\"><a><\/a><em>q<\/em><sub>A3<\/sub>&nbsp;=&nbsp;convection heat transfer from absorber node to glazing (across the gap).<\/p>\n\n\n\n<p id=\"U0735\"><a><\/a><em>q<\/em><sub>A4<\/sub>&nbsp;=&nbsp;convection heat transfer to absorber node&nbsp;<em>i<\/em>&nbsp;from the working fluid.<\/p>\n\n\n\n<p id=\"U0740\"><a><\/a><em>q<\/em><sub>A5<\/sub>&nbsp;=&nbsp;radiation exchange between the inside surface of absorber and absorber node&nbsp;<em>i.<\/em><\/p>\n\n\n\n<p id=\"U0745\"><a><\/a><em>q<\/em><sub>A6<\/sub>&nbsp;=&nbsp;conduction along the circumference of absorber from node&nbsp;<em>i<\/em>&nbsp;to&nbsp;<em>i<\/em>&nbsp;+&nbsp;1.<\/p>\n\n\n\n<p id=\"U0750\"><a><\/a><em>q<\/em><sub>A7<\/sub>&nbsp;=&nbsp;conduction along the circumference of the absorber from node&nbsp;<em>i<\/em>&nbsp;to&nbsp;<em>i<\/em>&nbsp;\u2212&nbsp;1.<\/p>\n\n\n\n<p id=\"U0755\"><a><\/a><em>q<\/em><sub>A8<\/sub>&nbsp;=&nbsp;fraction of the total radiation incident upon the inside absorber node that is absorbed.<\/p>\n\n\n\n<p>For all these parameters, standard heat transfer relations can be used. The set of non-linear equations is solved sequentially to obtain the temperature distribution of the receiver, and the solution is obtained by an iterative procedure. In Eqs\u00a0(3.142)\u00a0and\u00a0(3.143), factors\u00a0<em>q<\/em><sub>G1<\/sub>\u00a0and\u00a0<em>q<\/em><sub>A1<\/sub>\u00a0are calculated by the optical model, whereas factor\u00a0<em>q<\/em><sub>A5<\/sub>\u00a0is assumed to be negligible.<\/p>\n\n\n\n<p id=\"P3060\">This analysis can give the temperature distribution along the circumference and length of the receiver, so any points of high temperature, which might reach a temperature above the degradation temperature of the receiver selective coating, can be determined.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>As we have seen in Section\u00a03.2, concentrating collectors work by interposing an optical device between the source of radiation and the energy-absorbing surface. Therefore, for concentrating collectors, both optical and thermal analyses are required. In this book, only two types of concentrating collectors are analyzed: compound parabolic and parabolic trough collectors. Initially, the concentration ratio [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":6688,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[699],"tags":[],"class_list":["post-6729","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-3-solar-energy-collectors"],"jetpack_featured_media_url":"https:\/\/workhouse.sweetdishy.com\/wp-content\/uploads\/2024\/11\/battery_1976451.png","_links":{"self":[{"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/posts\/6729","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/comments?post=6729"}],"version-history":[{"count":1,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/posts\/6729\/revisions"}],"predecessor-version":[{"id":6730,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/posts\/6729\/revisions\/6730"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/media\/6688"}],"wp:attachment":[{"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/media?parent=6729"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/categories?post=6729"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/workhouse.sweetdishy.com\/index.php\/wp-json\/wp\/v2\/tags?post=6729"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}