发明名称 TURBINE ENGINE SHAFT COUPLING
摘要 A turbine engine shaft includes a first sub-shaft, a second sub-shaft and a tie shaft. A first bearing surface of the first sub-shaft axially engages a second bearing surface of the second sub-shaft. The tie shaft includes an intermediate tie shaft segment connected axially between a first tie shaft segment and a second tie shaft segment. The first tie shaft segment includes a first threaded tie shaft surface that is mated with a first threaded shaft surface of the first sub-shaft. The second tie shaft segment includes a second threaded tie shaft surface that is mated with a second threaded shaft surface of the second sub-shaft. The tie shaft also includes a sub-shaft bumper stop extending radially from the intermediate tie shaft segment to a bumper stop distal end, which has a radius that is greater than a radius the first and/or second threaded shaft surfaces.
申请公布号 WO2013119645(A1) 申请公布日期 2013.08.15
申请号 WO2013US24909 申请日期 2013.02.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 COFFIN, JAMES, B.
分类号 F01D25/00;F02C3/04;F02C7/36 主分类号 F01D25/00
代理机构 代理人
主权项
地址