Redundant fuel manifold sealing arrangement

Details Redundant fuel manifold sealing arrangement Redundant fuel manifold sealing arrangement

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/22 (2006.01) B23P 15/00 (2006.01) F02C 7/28 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2558897

A fuel manifold of gas turbine engines comprises a tube for fluid communication with a fuel source and for connection with at least one fuel nozzle tip to thereby define a fuel conveying passage. There is a means for providing a redundant seal around the tube and covering substantially an entire length thereof to reduce a risk of fuel leakage of the fuel conveying passage.

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