Combustion chamber for gas turbines

Details Combustion chamber for gas turbines Combustion chamber for gas turbines

1987-07-27

1988-08-23

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60758, F02C 100, F02G 300

Patent

active

047651466

ABSTRACT:
The combustion chamber is characterized by an annular-cylindrical space, which consists of two reaction chambers (8), arranged at the end, and a collision chamber (12) placed therebetween. The reaction chambers (8) are fitted at their face-sided ends with a number of burner elements (A, B), arranged axially parallel, their number depending on the output of the combustion chamber, which burner elements are in each case mirror-symmetrical to each other in relation to the central axis of the collision chamber (12). From the collision chamber (12), an annular mixing chamber (15) goes off to the turbine inlet (17). Each burner element (A, B) is provided with a twist member (6, 11), which in each case is orientated in opposed sense of rotation compared with the mirror-symmetrically arranged twist member.

REFERENCES:
patent: 3872664 (1975-03-01), Lohmann et al.
patent: 3968644 (1976-07-01), Fehler
patent: 4047877 (1977-09-01), Flanagan
patent: 4192139 (1980-03-01), Buchhein
patent: 4275564 (1981-06-01), Kappler et al.

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