Thermal and Structural Analysis of the Heat Receiver for the Solar Dynamic Ground Test Demonstrator-Reference-Cited by-同舟云学术

Thermal and Structural Analysis of the Heat Receiver for the Solar Dynamic Ground Test Demonstrator

Published:1995-05-01 Issue:2 Volume:117 Page:85-90
ISSN:0199-6231
Container-title:Journal of Solar Energy Engineering
language:en
Short-container-title:

Author:

Strumpf H. J.¹,Avanessian V.¹,Ghafourian R.¹,Huang F.¹

Affiliation:

1. Allied Signal Aerospace Systems and Equipment, 2525 W. 190th Street, Torrance, CA 90509-2960

Abstract

A solar dynamic ground test demonstrator space power system is being developed. The system comprises a complete Brayton engine—a heat receiver, concentrator, radiator, recuperator, heat rejection gas cooler, and turboalternator compressor. All of these components will be operated inside a vacuum tank. The engine is powered by simulated sunlight from an external bank of lights. Successful completion of the testing will indicate the readiness of solar dynamic power for space applications. This paper discusses the thermal and structural analysis of the heat receiver component. The analysis performed indicates that all components comfortably meet the life and cold start requirements, while maintaining the necessary overall performance.

Publisher

ASME International

Subject

Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment

Link

http://asmedigitalcollection.asme.org/solarenergyengineering/article-pdf/117/2/85/5578325/85_1.pdf

Reference13 articles.

1. Castelli, M., 1990, NASA-Lewis Research Center, personal communication.

2. Halford, G., 1988, NASA-Lewis Research Center, personal communication.

3. Kerslake, T. W., and Ibrahim, M. B., 1990, “Analysis of Thermal Energy Storage Material with Change-of-Phase Volumetric Effects,” Proceedings of the 12th Annual ASME International Solar Energy Conference, ASME, New York, pp. 315–325 (also NASA TM-102457).

4. NASA-Lewis, 1993, “Solar Dynamic Power System Development for Space Station Freedom,” NASA RP-1310, July.

5. Rubly, R. P., 1991, “Long-term Compatibility of a Cobalt-base Superalloy with Molten LiF-CaF2 Eutectic Composition Salt,” 24th International Metallographic Society, Monterey, CA.

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