Invention Grant
US08662845B2 Multi-function heat shield for a gas turbine engine 有权
燃气轮机的多功能防护罩

Multi-function heat shield for a gas turbine engine
Abstract:
A rotor disk assembly for a gas turbine engine includes a rotor disk with a circumferentially intermittent slot structure that extends radially outward relative to an axis of rotation. A heat shield has a multiple of radial tabs engageable with the circumferentially intermittent slot structure to provide axial retention of the cover plate to the rotor disk.
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