Fuel supply systems

Power plants – Combustion products used as motive fluid – With safety device

Patent

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Details

60734, F02C 7236

Patent

active

046915109

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

REFERENCES:
patent: 2757582 (1956-08-01), Freeman et al.
patent: 2849930 (1958-09-01), Freeman et al.
patent: 4066386 (1978-01-01), Johnson et al.

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