Patent ID: 7637111

Claim:
A jet engine combustion chamber comprising a generally annular outer wall, a generally annular inner wall, a chamber end wall extending between said outer and inner walls and having injector means mounted thereon, and a fairing co-operating with said chamber end wall to define an annular cavity that houses said injector means, said fairing comprising an annular part referred to as an “outer cap” and an annular part referred to as a “inner cap”, wherein inner fastener parts projecting into said annular cavity are fixed to said caps, wherein said chamber end wall includes corresponding inner fastener parts projecting into said annular cavity, and wherein the fastener parts of said caps are assembled directly to the fastener parts of said chamber end wall, wherein said fastener parts are tongues that are distributed circumferentially, and wherein said injector means comprises a plurality of injectors, and wherein each cap has as many tongues as there are injectors, said tongues being offset circumferentially relative to the injectors.