Gas turbine combustion chamber

Details Gas turbine combustion chamber Gas turbine combustion chamber

1994-11-10

1995-11-14

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combustion products generator

60752, 60 3936, F02C 100, F02G 300

Patent

active

054655773

ABSTRACT:
In a gas turbine combustion chamber, which consists of an inlet zone (1) with injection, an ignition delay zone (2), a reaction zone (3), a burn-out zone (4) and a transition zone (5) to the turbine, the reaction zone (3) has a cross-section which increases in such a way that the gas dynamics of the combustion process can take place at constant pressure or constant Mach number. By this means, the total pressure loss and the combustion chamber length necessary for the combustion are reduced and this is reflected in an improvement to the efficiency and the output.

REFERENCES:
patent: 2685421 (1954-08-01), Klose
patent: 2807139 (1957-09-01), Jackson
patent: 3372542 (1968-03-01), Sevetz
patent: 3620012 (1971-11-01), Wilde
patent: 3783616 (1974-01-01), Norman et al.
patent: 4146357 (1979-03-01), Ward et al.
patent: 4192139 (1980-03-01), Buchheim
patent: 4947641 (1990-08-01), Rodgers

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