Invention Grant
US08661641B2 Rotor blade assembly tool for gas turbine engine 有权
用于燃气轮机的转子叶片组装工具

Rotor blade assembly tool for gas turbine engine
Abstract:
A rotor blade assembly tool for coupling a plurality of circumferentially spaced rotor blades to a rotor disc of a turbine rotor assembly, includes a base ring with an array of circumferentially spaced resilient fingers axially extending from the base ring. The resilient fingers are configured each to radially abut a blade seal, damper or other engine component against radially inner facing surfaces of platforms of the respective blades when the blades are being seated onto the disc during an assembly procedure.
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