Dual conduit fuel manifold for gas turbine engine

Details Dual conduit fuel manifold for gas turbine engine Dual conduit fuel manifold for gas turbine engine

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/22 (2006.01)

Patent

CA 2557440

Fuel conduit systems (20, 200) for internal installation in a gas turbine engine (10) are provided which are low cost and easy to manufacture. First and second members (44, 46) co-operate to provide a channel (40) to define a discrete fuel carrying conduit. The direction of fuel flow can be adapted to provide desired cooling effect.

L'invention concerne des systèmes de conduite de carburant (20, 200) destinés à s'installer à l'intérieur d'une turbine à gaz (10), qui sont bon marché et faciles à fabriquer. Un premier et un second éléments (44, 46) coopèrent pour présenter un circuit (40) délimitant un conduit d'acheminement du carburant discret. Le sens d'écoulement du carburant peut être adapté pour créer un effet de refroidissement désiré.

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