Combustion chamber of a gas turbine

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

1992-03-16

1992-10-13

Casaregola, Louis J.

Power plants

Combustion products used as motive fluid

Combustion products generator

60747, F23R 346, F23R 330

Patent

active

051540592

ABSTRACT:
In a combustion chamber (A) of the form of an annular combustion chamber, a row of large and small premixed burners (B, C) are arranged along the annular front wall (10). The large premixed burners (B), which are the main burners of the combustion chamber (A), and the small premixed burners (C), which are the pilot burners of the combustion chamber (A), follow each other alternately and regularly along the front wall (10) where they also emerge into the combustion space of the combustion chamber (A). A plurality of air nozzles (D), whose injection is directed into the combustion space of the combustion chamber (A), are placed between the large premixed burners (B) and the small premixed burners (C).

REFERENCES:
patent: 3512359 (1970-05-01), Pierce
patent: 3834159 (1974-09-01), Vdoviak
patent: 4194358 (1980-03-01), Stenger
patent: 4781030 (1988-11-01), Hellat et al.
patent: 4932861 (1990-06-01), Keller et al.

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