Control system for a gas turbine engine

Details Control system for a gas turbine engine Control system for a gas turbine engine

1976-08-05

1978-03-07

Gordon, Clarence R.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60 3928T, F02C 908

Patent

active

040772047

ABSTRACT:
In an acceleration control of a gas turbine engine having a feedback system in which the fuel flow is controlled by comparison of a selected engine speed and an actual engine speed, when the difference between the speeds exceeds a predetermined level the control is performed from the selected speed signal to a temperature limit signal and the fuel flow is controlled so that the actual engine temperature does not exceed the limit.

REFERENCES:
patent: 3045426 (1962-07-01), Brahm
patent: 3620010 (1971-11-01), Davis
patent: 3764785 (1973-10-01), Harner
patent: 3772880 (1973-11-01), Kubota
patent: 3834158 (1974-09-01), Oppmann

Affiliated with

Also associated with

Rating

Control system for a gas turbine engine does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2015169