Gas turbine engine component having foam core and composite skin with cooling slot
作者： Richard C. Uskert , David J. Thomas , Ted J. Freeman
DOI:
关键词:
摘要: In one embodiment, a gas turbine engine component includes foam based core and composite skin member. Both the member can be used to structurally support component. The CMC material is partially encapsulate core. take form of an airfoil such as blade or vane, combustor liner, etc. A first portion surface extending past edge creating step approximate section. another members continuous shape for section that forms part path surface.
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