Power plants – Combustion products used as motive fluid – With variable oxidizer control
Patent
1986-10-15
1987-09-29
Casaregola, Louis J.
Power plants
Combustion products used as motive fluid
With variable oxidizer control
60 3936, 60748, F02C 314
Patent
active
046961577
ABSTRACT:
A fuel and air injection system for a turbojet engine is disclosed wherein a bowl-shaped member surrounding the fuel injection nozzle defines an impact cooling chamber divided into four sectors. A pair of diametrically opposite sectors have openings to permit air to pass through the cooling chamber into the combustion chamber, while opposite diametrically opposed sectors have openings of larger diameter which also allow communication between the cooling chamber and the combustion chamber. A diaphragm control system allows the air passing into the sectors having the larger diameter openings to be modulated depending upon the throttle setting of the turbojet engine.
REFERENCES:
patent: 2655787 (1953-10-01), Brown
patent: 3490230 (1970-01-01), Pillsbury et al.
patent: 3831854 (1974-08-01), Sato et al.
patent: 3834159 (1974-09-01), Vdoviak
patent: 3901446 (1975-08-01), Petreikis et al.
patent: 3982392 (1976-09-01), Crow
patent: 4050240 (1977-09-01), Vaught
patent: 4162611 (1979-07-01), Caruel et al.
Barbier Gerard Y. G.
Desaulty Michel A. A.
Leboure Gerald J. P. B.
Martinez Rodolphe
Perigne Jerome
Casaregola Louis J.
Societe Nationale D'Etude et de Construction de Moteurs D'Aviati
LandOfFree
Fuel and air injection system for a turbojet 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 Fuel and air injection system for a turbojet engine, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Fuel and air injection system for a turbojet engine will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-1583600