Compressor power unit fuel flow control

Details Compressor power unit fuel flow control Compressor power unit fuel flow control

1986-12-22

1988-05-31

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

With closed pocket turbine

60 3927, F02C 952, F02C 948

Patent

active

047472626

ABSTRACT:
In a gas turbine engine compressor power unit fuel is supplied at an essentially constant pressure to a fuel nozzle for injection into the combustion liner of the power unit's combustor. Nozzle fuel flow is modulated solely by bleeding off combustor supply air to vary the internal liner pressure, thereby altering the fuel pressure drop across the nozzle.

REFERENCES:
patent: 3037348 (1962-06-01), Gassmann
patent: 3224195 (1965-12-01), Walsh
patent: 3707074 (1972-12-01), Meyer et al.
patent: 3910035 (1975-10-01), Juhasz et al.
patent: 4149371 (1979-04-01), Spraker et al.
patent: 4470798 (1984-09-01), Graat et al.

Affiliated with

Also associated with

Rating

Compressor power unit fuel flow control does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Compressor power unit fuel flow control, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Compressor power unit fuel flow control will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1867666