Fuel injectors for gas turbine engines

Details Fuel injectors for gas turbine engines Fuel injectors for gas turbine engines

1977-11-08

1979-10-09

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

Combustion products generator

239400, 239404, 239406, F02C 722

Patent

active

041701089

ABSTRACT:
A fuel injector for a gas turbine engine consists of a hollow body adapted to be supplied with compressed air and having a number of fuel orifices in the internal surface of the body. An annular member is located inside the body adjacent to the orifices so as to define an annular gap between it and the internal surface of the hollow body. The gap receives fuel from the orifices and has a radial width of 0.015 to 0.020 inches.

REFERENCES:
patent: 3067582 (1962-12-01), Schirmer
patent: 3530667 (1970-09-01), Bryan
patent: 3703259 (1972-11-01), Sturgess et al.
patent: 3866413 (1975-02-01), Sturgess
patent: 3915387 (1975-10-01), Carvel et al.
patent: 3937011 (1976-02-01), Carvel et al.

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