CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT

A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fu...

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Hauptverfasser: EPSTEIN, MICHAEL, JAY, BALADI, MEHDI, MILANI, BUCHHOLZ, TODD, JAMES, KAMATH, DEEPAK, MANOHAR
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Sprache:eng ; fre ; ger
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creator EPSTEIN, MICHAEL, JAY
BALADI, MEHDI, MILANI
BUCHHOLZ, TODD, JAMES
KAMATH, DEEPAK, MANOHAR
description A cryogenic fuel system for an aircraft having a turbine engine with a compressor section and a combustion chamber, including a tank for storing cryogenic fuel, a supply line operably coupling the tank to the combustion chamber and a pump coupling the tank to the supply line to pump the cryogenic fuel at high pressure through the supply line where the pump is operably coupled to the compressor such that operation of the turbine engine drives the pump and a method for delivering fuel in a fuel system to a turbine engine.
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language eng ; fre ; ger
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subjects AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title CRYOGENIC FUEL SYSTEM AND METHOD FOR DELIVERING FUEL IN AN AIRCRAFT
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