Combustion chamber construction

Details Combustion chamber construction Combustion chamber construction

F - Mech Eng,Light,Heat,Weapons

02

C

60/174

F02C 3/14 (2006.01)

Patent

CA 1242893

COMBUSTION CHAMBER CONSTRUCTION ABSTRACT OF THE DISCLOSURE A combustion chamber for use in gas turbine engines is provided with a liner formed of a high temperature material. The liner includes a plurality of annular rings of high temperature material mounted by means of flexible mounting arrangement upon a high strength structural frame. As a result of this mounting arrangement, the liner is substantially isolated from structural forces associated with the combustion chamber, while the frame is substnatially isolated from thermal stresses associated with the liner. The individual liner rings may be easily removed for repair or replace- ment without disassembling the frame and associated components. Furthermore, the "decoupling" of thermal and structural stesses provides longer life and more dependable operation.

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