Combustion chamber of a gas turbine

Details Combustion chamber of a gas turbine Combustion chamber of a gas turbine

1990-03-02

1992-01-21

Bertsch, Richard A.

Power plants

Combustion products used as motive fluid

Combustion products generator

60 3937, 60 39826, F02C 100, F23R 346, F23R 330

Patent

active

050818449

ABSTRACT:
In an annular combustion chamber (A), a row of premixed burners (B, C) are located in the peripheral direction at the inlet end. The large premixed burners (B), which are the main burners of the annular combustion chamber (A), and the small premixed burners (C), which are the pilot burners of the annular combustion chamber, are located alternately relative to one another and at a uniform distance apart. Both the main burners (B) and the pilot burners (C) enter into a single annular front wall (10).

REFERENCES:
patent: 4058977 (1977-11-01), Markowski et al.
patent: 4194358 (1980-03-01), Stenger
patent: 4271675 (1981-06-01), Jones et al.
patent: 4587809 (1986-05-01), Ohmori et al.
patent: 4932861 (1990-06-01), Keller et al.

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