FUEL SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE

A liquid fuel supply system for an aircraft engine includes a fuel tank, a suction duct connected to the fuel tank and located higher than the fuel tank, an electric pump, a supply pump that is mechanically driven by an accessory gear box and an outlet of the supply pump being connected to a fuel su...

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Hauptverfasser: SICAIRE, Pierre Anthony, LONGIN, Alexis Thomas Valentin, DARRIEUMERLOU, Gabriel, BENEZECH, Philippe Jean René Marie
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Sprache:eng ; fre ; ger
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creator SICAIRE, Pierre Anthony
LONGIN, Alexis Thomas Valentin
DARRIEUMERLOU, Gabriel
BENEZECH, Philippe Jean René Marie
description A liquid fuel supply system for an aircraft engine includes a fuel tank, a suction duct connected to the fuel tank and located higher than the fuel tank, an electric pump, a supply pump that is mechanically driven by an accessory gear box and an outlet of the supply pump being connected to a fuel supply circuit of the engine, and an air expulsion drain. The electric pump is in communication with the suction duct independently of the supply pump, the electric pump is in communication with the air expulsion drain, and the supply pump is in communication with the suction duct independently of the electric pump.
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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 FUEL SUPPLY SYSTEM FOR AN AIRCRAFT ENGINE
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