Invention Application
US20160341061A1 SUPPORT ASSEMBLY FOR A GAS TURBINE ENGINE 有权
燃气涡轮发动机支撑组件

SUPPORT ASSEMBLY FOR A GAS TURBINE ENGINE
Abstract:
A support assembly for a gas turbine engine includes a control ring that extends about a circumferential axis. A plurality of first supports has a cavity that receives the control ring. A plurality of cover plates are attached to the first plurality of supports and enclose the cavity.
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