Fuel control systems for gas turbine engines

Details Fuel control systems for gas turbine engines Fuel control systems for gas turbine engines

1979-06-27

1981-06-02

Garrett, Robert E.

Power plants

Reaction motor

Condition responsive thrust varying means

F02K 300, F02C 904

Patent

active

042703468

ABSTRACT:
A fuel control system for a gas turbine engine for an aircraft comprising two modes of operation, a first mode in which the net thrust of the engine increases with an increase in the forward speed of the aircraft and a second mode in which the net thrust of the engine is caused to decrease with an increase in the forward speed of the aircraft, a selectively operable control device such as a valve or a valve with a least wins device being provided for selecting one of the modes of operation at a time.

REFERENCES:
patent: 2693081 (1954-11-01), Russ
patent: 3496721 (1970-02-01), Lloyd et al.
patent: 3530666 (1970-09-01), Cross et al.
patent: 3713290 (1973-01-01), Gold
patent: 3813063 (1974-05-01), Martin
patent: 3898796 (1975-08-01), Canale et al.

Affiliated with

Also associated with

Rating

Fuel control systems for gas turbine engines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Fuel control systems for gas turbine engines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuel control systems for gas turbine engines will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1859036