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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0096631 (1993-07-22) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 14 인용 특허 : 0 |
A thermal management system for a propulsion engine of a supersonic or hypersonic aircraft is provided that uses a single flow of endothermic fluid as engine fuel and as a heat sink for engine cooling. The system includes a plurality of heat exchangers in flow series arrangement. Each heat exchanger
A method in which a single flow of an endothermic fluid is used as to fuel and cool a propulsion engine mounted on an aircraft operable at high Mach numbers, said aircraft having a stored source of said fluid in a liquid state; comprising the steps of: a) pressurizing said fluid; b) heating said flu
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