Axial flow gas turbine engine combustor

Details Axial flow gas turbine engine combustor Axial flow gas turbine engine combustor

1989-07-24

1991-02-19

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combined with regulation of power output feature

60737, F02C 700, F23R 316

Patent

active

049932209

ABSTRACT:
Improved combustor volume in turbine engines without an increased engine envelope is accomplished in an engine 10 have a radial compressor 12, an axial turbine 16, and a radial combustor 20 in which a generally radial flow path extends between a compressed air inlet 30 and a turbine nozzle 22 for gases of combustion produced by combusting fuel introduced through a fuel injector 34 with air introduced through the compressed air inlet 30.

REFERENCES:
patent: 3088279 (1963-05-01), Diedrich
patent: 3266250 (1966-08-01), Freeman et al.
patent: 3285006 (1966-11-01), Freeman et al.
patent: 3333414 (1967-08-01), Saintsbury
patent: 3671171 (1972-06-01), Doyle
patent: 4171614 (1923-10-01), Weller
patent: 4314443 (1982-02-01), Barbeau
patent: 4339925 (1982-07-01), Eggmann et al.
patent: 4429527 (1984-02-01), Teets
patent: 4545196 (1985-10-01), Mozgia et al.

Affiliated with

Also associated with

Rating

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

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

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1133755