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Thermal and energy management method and apparatus for an aircraft

  • US 6,182,435 B1
  • Filed: 06/05/1997
  • Issued: 02/06/2001
  • Est. Priority Date: 06/05/1997
  • Status: Expired due to Term
First Claim
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1. A method for cooling components of a vehicle carrying a combustion engine and a fuel supply for the engine, the method comprising the steps of:

  • flowing fuel from the fuel supply through a first fuel recirculating system;

    rejecting heat to the fuel from select components of the vehicle as the fuel flows through the first fuel recirculating system; and

    rejecting heat to the engine from the fuel as the fuel flows through the first fuel recirculating system, wherein the step of rejecting heat to the engine from the fuel includes rejecting heat from the fuel to a compression/expansion cooling device as the fuel flows through the first fuel recirculating system.

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