Hydrostatic flow barrier for flexible fuel manifold

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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Details

F02C 7/22 (2006.01) B32B 1/08 (2006.01) B32B 15/08 (2006.01) F23R 3/28 (2006.01)

Patent

CA 2620415

A fuel manifold segment (34) for gas turbine engines comprises a polymer tube(48) surrounded by a metallic braid layer (50). Means (56) are provided for preventing the polymer material of the tube (48) from flowing through the metallic braid layer (50) at with a location of a joint with a tube fitting (42) under an elevated temperature and compressed condition.

La présente invention concerne un segment de rampe de distribution de carburant (34) pour turbines à gaz, comprenant un tube en polymère (48) entouré d~une couche métallique tressée (50). Des moyens (56) empêchant le matériau polymère du tube (48) de s~écouler à travers la couche métallique tressée (50) sont prévus au niveau d~un joint avec un raccord de tube (42) soumis à une température et à une pression élevées.

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