Turbine engine fuel injector

Details Turbine engine fuel injector Turbine engine fuel injector

2005-08-30

2005-08-30

Gartenberg, Ehud (Department: 3746)

Power plants

Combustion products used as motive fluid

Combustion products generator

Reexamination Certificate

active

06935117

ABSTRACT:
A gas turbine engine is piloted with a pilot flow of fuel delivered to a combustor as a liquid. A first additional flow of the fuel is also delivered to the combustor as a liquid. A second additional flow of the fuel is vaporized and delivered to the combustor as a vapor. A fuel injector may have passageways associated with each of the three flows.

REFERENCES:
patent: 3691765 (1972-09-01), Carlisle
patent: 4258544 (1981-03-01), Gebhart et al.
patent: 4566268 (1986-01-01), Hoffeins et al.
patent: 5361578 (1994-11-01), Donlan
patent: 5375995 (1994-12-01), Dobbeling et al.
patent: 6148603 (2000-11-01), Althaus
patent: 6321541 (2001-11-01), Wrubel et al.
patent: 6434945 (2002-08-01), Mandai et al.
patent: 6609905 (2003-08-01), Eroglu et al.
Von M. Valk and H. Weisser, VGB Kraftwerks Technik, 1999, vol. 79, No. 3, pp. 34-39.

Affiliated with

Also associated with

Rating

Turbine engine fuel injector does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Turbine engine fuel injector, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine engine fuel injector will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-3524040