Fuel supply system for a gas turbine engine

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

Patent

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Details

60 3914, 60 3974R, 239 76, 137597, F02C 722

Patent

active

040621839

ABSTRACT:
In order to improve the start-up of a gas turbine engine, a control system is provided which fills part of the fuel manifold with compressed air during start-up so as to prevent fuel flowing to all the burners and thereby to improve the performance of the remaining burners.

REFERENCES:
patent: 2818110 (1957-12-01), Rulseh
patent: 3087305 (1963-04-01), Hertzog
patent: 3149463 (1964-09-01), Withers et al.
patent: 3158998 (1964-12-01), Robinson et al.
patent: 3288447 (1966-11-01), Withers et al.
patent: 3498056 (1970-03-01), Avery
patent: 3834627 (1974-09-01), Watkins

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