Reduced-weight fuel system for gas turbine engine, gas...

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

Reexamination Certificate

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Details

C060S734000, C060S786000

Reexamination Certificate

active

11139953

ABSTRACT:
A fuel system (10) for a gas turbine engine (18) having a shaft (30) and requiring fuel to be supplied at a first rate for engine start up, the fuel system (10) including: a main fuel pump (14) for providing fuel to the gas turbine engine (18), the main fuel pump (14) having an output varying with shaft speed, the output being at a windmilling rate when the engine (18) is windmilling, the windmilling rate being less than the first rate; and an auxiliary fuel pump (40) for providing fuel to the gas turbine engine (18) and having an auxiliary output rate greater than or equal to the difference between the first rate and the windmilling rate. A method of operating such a fuel system (10) is also disclosed.

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patent: 2003/0056521 (2003-03-01), Dewis
patent: 0 657 651 (1995-06-01), None
patent: 1 541 486 (1968-10-01), None

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