Reverse flow ceramic matrix composite combustor

Details Reverse flow ceramic matrix composite combustor Reverse flow ceramic matrix composite combustor

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/54 (2006.01)

Patent

CA 2698058

A gas turbine engine has an annular reverse-flow combustor with a combustor inner liner enclosing a combustion chamber. The inner liner having a dome portion at an upstream end of the combustor and a downstream combustor exit defined between a small exit duct portion and a large exit duct portion. At least one of the dome portion, the small exit duct portion and the large exit duct portion is made of a separately formed hemi- toroidal shell composed of a ceramic matrix composite.

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