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To view the Trough System Costs page, click Receiver on the main window's navigation menu. Note that for the trough input pages to be available, the technology option in the Technology and Market window must be Concentrating Solar Power - Dish Stirling System. |
The receiver absorbs thermal energy from the parabolic concentrator and transfers the energy to the working fluid of the Stirling engine. The receiver consists of an aperture and absorber. The receiver aperture is located at the parabolic concentrator's focal point. The current version of Solar Advisor models one receiver type, direct illumination receivers, in which solar radiation is directly absorbed by absorber tubes containing the working fluid. Direct illumination receivers are the receiver type most commonly used for dish-Stirling systems.
The relevant sections of the thesis Stirling Dish System Performance Prediction Model (Fraser 2008) https://www.nrel.gov/analysis/sam/pdfs/thesis_fraser08.pdf (4.1 MB) are:
| • | 2.2 Receiver, p 14 |
| • | 6.1 Modifying the Receiver Aperture Diameter, p 133 |
| • | 6.2 Receiver Cover versus no Cover, p 134 |
| • | Appendix A: TRNSYS Receiver Model, p 153 |
Solar Advisor uses the receiver parameters to calculate thermal losses from the receiver, which typically account for over 50% of the system's total losses. Other system losses include collector losses due to mirror reflectivity, receiver intercept losses, and Stirling engine losses. Receiver thermal losses are due to conduction, convection, and radiation:
| • | Conductive losses through the receiver housing. |
| • | Natural convection from the cavity in the absence of wind. |
| • | Forced convection in the presence of wind. |
| • | Emission losses due to thermal radiation emitted from the receiver aperture. |
| • | Radiation losses reflected off of the receiver cavity surfaces and out of the receiver through the aperture. |
Input Variable Reference
Aperture
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Insulation
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Absorber The absorber is a component of the receiver that absorbs solar radiation and transfers thermal energy to the Stirling engine.
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Cavity The cavity parameters determine the cavity's geometry. The internal cavity area is the sum of the cavity wall surface area and absorber area and is used to calculate radiation, conduction and convection losses.
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Table 26. Receiver default parameter values.
Variable |
SES |
WGA |
SBP |
SAIC |
Absorber Absorptance |
0.90 |
0.90 |
0.90 |
0.90 |
Absorber Surface Area |
0.6 |
0.15 |
0.15 |
0.8 |
Cavity Wall Absorptance |
0.6 |
0.6 |
0.6 |
0.6 |
Cavity Wall Surface Area |
0.6 |
0.15 |
0.15 |
0.8 |
Internal Diameter of the Cavity Perpendicular to the Receiver Aperture |
0.46 |
0.35 |
0.37 |
0.5 |
Internal Depth of the Cavity Perpendicular to the Aperture |
0.46 |
0.35 |
0.37 |
0.5 |
Receiver Insulation Thickness |
0.075 |
0.075 |
0.075 |
0.075 |
Insulation Thermal Conductivity |
0.06 |
0.06 |
0.06 |
0.06 |
Delta Temp. for DIR Receiver |
90 |
70 |
70 |
90 |