Combustion chamber for gas turbines

Details Combustion chamber for gas turbines Combustion chamber for gas turbines

1977-12-29

1980-05-13

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

With variable oxidizer control

60 3929, 60749, F02C 722, F02C 914

Patent

active

042021707

ABSTRACT:
A combustion chamber for gas turbines with a variable inlet cross section for the primary air, whereby the inlet cross section is so varied in dependence on the fuel pressure determining the injection quantity that with an increasing or decreasing fuel pressure, the inlet cross section is increased or decreased.

REFERENCES:
patent: 1616335 (1927-02-01), Rochefort
patent: 3975900 (1976-08-01), Pfefferle
patent: 3986347 (1976-10-01), Schirmer
patent: 4044549 (1977-08-01), Zwick
patent: 4078377 (1978-03-01), Owens et al.

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