Fuel cooling system for high-performance aircraft

Kraftstoffkuehlsystem fuer hochleistungsluftfahrzeuge

Abstract

A fuel cooling system for high-performance aircraft is proposed, which uses the vaporisation of fuel to cool devices and components, especially electronic, sensitive components. The pressure of the fuel is reduced using suitable devices, and the cooling medium is cooled down by extracting the heat of vaporisation. A restrictor and an injector are used for this purpose.

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Patent Citations (2)

    Publication numberPublication dateAssigneeTitle
    US-4273304-AJune 16, 1981Frosch Robert A, Lawing Pierce L, Pagel Laverne LCooling system for high speed aircraft
    US-4505124-AMarch 19, 1985The United States Of America As Represented By The Secretary Of The Air ForceHeat management system for aircraft

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Cited By (1)

    Publication numberPublication dateAssigneeTitle
    WO-2014060751-A1April 24, 2014Airbus Operations LimitedAircraft fuel system with fuel return from engine