Developments in turbo-Brayton power converters

被引:0
|
作者
Zagarola, MV [1 ]
Crowley, CJ [1 ]
Swift, WL [1 ]
机构
[1] Creare Res & Dev Inc, Hanover, NH 03755 USA
关键词
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暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Design studies show that a Brayton cycle power unit is an extremely attractive option for thermal-to-electric power conversion on long-duration, space missions. At low power levels (50 to 100 We), a Brayton system should achieve a conversion efficiency between 20% and 40% depending on the radiative heat sink temperature. The expected mass of the converter for these power levels is about 3 kg. The mass of the complete system consisting of the converter, the electronics, a radiator, and a single general purpose heat source should be about 6 kg. The system is modular and the technology is readily scalable to higher power levels (to greater than 10 kW(e)) where conversion efficiencies of between 28% and 45% are expected, the exact value depending on sink temperature and power level. During a recently completed project, key physical features of the converter were determined, and key operating characteristics were demonstrated for a system of this size. The key technologies in these converters are derived from those which have been developed and successfully implemented in miniature turbo-Brayton cryogenic refrigerators for space applications. These refrigerators and their components have been demonstrated to meet rigorous requirements for vibration emittance and susceptibility, acoustic susceptibility, electromagnetic interference and susceptibility, environmental cycling, and endurance. Our progress in, extending the underlying turbo-Brayton cryocooler technologies to thermal-to-electric power converters is the subject of this paper.
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页码:580 / 588
页数:9
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