发明名称 TURBINE ENGINE BALANCING STRUCTURE AND METHOD
摘要 An example method of balancing a shaft includes inserting a balancing insert into one of a plurality of cavities. The plurality of cavities are radially inside an outermost surface of the shaft.
申请公布号 US2016326876(A1) 申请公布日期 2016.11.10
申请号 US201515111364 申请日期 2015.01.09
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 Lopez Jesus S.;Borja Mark
分类号 F01D5/02 主分类号 F01D5/02
代理机构 代理人
主权项 1. A method of turbine engine balancing a shaft, comprising: inserting a balancing insert into one of a plurality of cavities, the plurality of cavities radially inside an outermost surface of a shaft.
地址 Hartford CT US