Fuel supply systems

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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123/14

F02C 7/236 (2006.01) B01D 19/00 (2006.01) B64D 37/00 (2006.01)

Patent

CA 1285188

ABSTRACT FUEL SUPPLY SYSTEMS A fuel supply system for use in rotary wing aircraft is described. The system comprises a separating means 10 for: receiving an air, vapour and fuel mixture at relatively low pressure from a fuel tank; separating the air and the vapour from the mixture; and providing a fuel supply at a relatively high pressure, and a pump means 12 for returning the separated air and vapour to the tank.

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