Invention Grant
US07654088B2 Dual conduit fuel manifold for gas turbine engine 有权
用于燃气涡轮发动机的双管道燃料歧管

Dual conduit fuel manifold for gas turbine engine
Abstract:
Fuel conduit systems for internal installation in a gas turbine engine are provided which are low cost and easy to manufacture. First and second members co-operate to provide a channel to define a discrete fuel carrying conduit. The direction of fuel flow can be adapted to provide desired cooling effect.
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