Ring combustion chamber with ring burner for gas turbines

Details Ring combustion chamber with ring burner for gas turbines Ring combustion chamber with ring burner for gas turbines

F - Mech Eng,Light,Heat,Weapons

02

C

60/165

F02C 3/00 (2006.01) F23R 3/10 (2006.01) F23R 3/28 (2006.01) F23R 3/36 (2006.01)

Patent

CA 1189330

ABSTRACT OF THE DISCLOSURE A ring burner of a ring combustion chamber is divided into a large number of honeycomb-like parallel axis canals for the combustion air, by radial and circumferential plate canals or by radial plate canals, longitudinal tubing, radial tubing and annular tubing into which combustion gas is introduced from jets in the surrounding walls. At the burner output there are flame retention jets provided above the frontal surface area of the plate canals or tubes. Fuel jets are provided in front of the burner input for operation as a dual burner with gaseous and liquid fuels.

397577

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