A system for cooling an aircraft includes a fuel tank, a fuel delivery system, a cooling system, and a heat exchanger. The fuel tank is configured to hold cooled fuel for the aircraft. The fuel delivery system is configured to provide at least a portion of the fuel from the fuel tank to an engine of the aircraft. The cooling system is configured to absorb heat generated by components on the aircraft. The heat exchanger is thermally connected to the fuel delivery system and the cooling system. The heat exchanger is configured to transfer at least a portio...
1. A system for cooling an aircraft, the system comprising: a fuel tank configured to hold cooled fuel for the aircraft;a fuel delivery system including a first valve, the fuel delivery system configured to provide at least a portion of the fuel from the fuel tank to an engine of the aircraft;a cooling system configured to absorb heat generated by components on the aircraft;a first heat exchanger thermally connected to the fuel delivery system and the cooling system, the first heat exchanger configured to transfer at least a first portion of the heat fro...
이 특허에 인용된 특허 (12)
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