Invention Grant
US07694417B2 Installation tool for assembling a rotor blade of a gas turbine engine fan assembly 失效
用于组装燃气涡轮发动机风扇组件的转子叶片的安装工具

Installation tool for assembling a rotor blade of a gas turbine engine fan assembly
Abstract:
A method enables rotor assembly for a gas turbine engine to be assembled. The method includes providing a plurality of rotor blades that each include a dovetail, providing a rotor disc that includes a plurality of dovetail slots spaced circumferentially about the disc, partially inserting each rotor blade dovetail into a respective rotor dovetail slot, and seating the plurality of rotor blades in the respective rotor dovetail slot substantially simultaneously using an annular blade installation tool.
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