Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle

作者: Jean Yamanis , David C. Jarmon , Mark A. Sillence , Paul Attridge

DOI:

关键词: Mechanical engineeringThermal energyHeat exchangerWaste heatMaterials scienceThermalElectricity generationElectrical conductorThermoelectric effectScramjet

摘要: An electrical power generation system incorporates thermoelectric devices (TE Devices) for adjacent a flow path heat exchanger (HEX) to vehicle flowpath structure such as scramjet take advantage of the waste heat, high thermal gradients, and available, unused volume. A thermally conductive material communicates energy from external skin TE Device while compliant allows “float” with minimal mechanical stress.

参考文章(25)
Bartholomaus Bichler, Michael Jost, Inlet system for supersonic or hypersonic aircraft ,(1991)
Daniel P. Guinan, Dean Andreadis, Stephen A. Beckel, Alan Drake, Variable geometry inlet design for scram jet engine ,(2002)
Roy N. Guile, David C. Jarmon, Rhonda R. Willigan, Engine heat exchanger with thermoelectric generation ,(2005)
Dennis J. Nemecek, Henry K. Webster, Mark A. Sillence, Costante Salvador, Sergio Rinella, Daniel P. Guinan, Thomas B. Fortin, Revi K. Nigam, Scram jet engine design ,(2002)