Invention Application
US20160333890A1 GAS TURBINE ENGINE INNER CASE WITH NON-INTEGRAL VANES 审中-公开
气体涡轮发动机内箱与非集成空气

GAS TURBINE ENGINE INNER CASE WITH NON-INTEGRAL VANES
Abstract:
A gas turbine engine includes a circumferential array of vanes slidably supported in an inner case shroud segment. Multiple segments are secured to one another to provide an annular engine static structure section. The inner case shroud segment and the vanes have different material properties than one another.
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