Combustion chamber, especially for gas turbines

Details Combustion chamber, especially for gas turbines Combustion chamber, especially for gas turbines

1978-08-10

1980-04-29

Garrett, Robert E.

Power plants

Combustion products used as motive fluid

With variable oxidizer control

60737, 60 3972R, 60749, F02C 722

Patent

active

041999347

ABSTRACT:
A combustion chamber having an end-wall at the inlet side and an axial inlet opening, which is adjoined by an essentially cylindrical wall section provided with secondary air inlet openings; the end-wall thereby adjoins the inlet opening approximately hemispherically shaped with a sphere diameter which is larger than the diameter of the cylindrical wall section while the adjoining combustion chamber portion is again reduced to the adjacent cylindrical wall section by way of a combustion chamber wall substantially continuing the sphere shape; the fuel injection device is provided upstream of the inlet opening which injects fuel into the inlet opening, itself covered off by a deflection means.

REFERENCES:
patent: 2142601 (1939-01-01), Bleecker
patent: 2920449 (1960-01-01), Johnson et al.
patent: 3306333 (1967-02-01), Mock
patent: 3530667 (1970-09-01), Bryan
patent: 3724207 (1973-04-01), Johnson
patent: 4078377 (1978-03-01), Owens et al.

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