F - Mech Eng,Light,Heat,Weapons – 02 – C
Patent
F - Mech Eng,Light,Heat,Weapons
02
C
60/117, 60/174
F02C 3/14 (2006.01) F23R 3/60 (2006.01)
Patent
CA 1105725
D-2310 C-2954 COMBUSTOR SUPPORT STRUCTURE Abstract of the Disclosure A combustor assembly for a gas turbine engine includes a tubular, multi-layered porous metal wall with pores there- through for distribution of compressor discharge air into a combustion chamber and wherein a rigid combustor support ring is connected to one end of the wall to receive an inlet diffuser member including an ovate inlet and a circular outlet connected to the support ring for axially directing primary air flow into the combustion chamber; and the diffuser member including a flow divider on one outer sur- face thereof including means for fixedly securing the inlet diffuser member with respect to a wall of a gas turbine engine and wherein coacting means are provided between the inlet diffuser member and the rigid combustor support ring of the combustor to radially connect it in place at one end thereof and wherein further coacting means are provided between the inner engine wall and a portion of the porous sleeve for axially indexing of the combustor assembly. * * * * *
320103
Herman Avrum S.
Reider Samuel B.
General Motors Corporation
Gowling Lafleur Henderson Llp
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