Bypass lip seal

Details Bypass lip seal Bypass lip seal

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/141 (2006.01) F01D 25/12 (2006.01) F02C 7/06 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2598738

A cooling apparatus for cooling a fluid in a bypass gas turbine engine comprises a heat exchanger disposed within a bypass duct and accommodated by a sub-passage defined by a flow divider affixed to an annular wall of the bypass duct. The sub-passage defines an open upstream end and an open downstream end to direct a portion of the bypass air flow to pass therethrough. A sealing assembly for the bypass duct is also provided.

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