Combustion chamber of a gas turbine

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

F - Mech Eng,Light,Heat,Weapons

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60/174

F23R 3/02 (2006.01) G01K 1/12 (2006.01)

Patent

CA 2016579

ABSTRACT OF THE DISCLOSURE 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 noz- zles (D), whose injection is directed in-to the combus- tion space of the combustion chamber (A), are placed between the large premixed burners (B) and the small premixed burners (C). (Fig. 1)

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