Invention Grant
US08453326B2 Method for assembling radially loaded vane assembly of gas turbine engine 有权
燃气轮机发动机径向负载叶片组件的组装方法

Method for assembling radially loaded vane assembly of gas turbine engine
Abstract:
A method for assembling a vane ring with a vane support of a vane assembly in a gas turbine engine is described, and includes flexing each of the radial loading elements into the resiliently flexed state simultaneously by sliding the radial loading elements against corresponding lead-in tapers. This can be achieved, for example, using a guide tool which includes a plurality of segments bearing the lead-in tapers and which is previously assembled to the vane support.
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