发明名称 Turbine or compressor blade mounting
摘要 In a turbine or compressor blade and supporting disk assembly in which the assembly is by tangential positioning of the blades, the cooperating blade root and groove in the disk have base surfaces that are held in spaced relation to each other by a rib on the blade root extending toward the base surface of the groove and into contact with it.
申请公布号 US4645425(A) 申请公布日期 1987.02.24
申请号 US19840683826 申请日期 1984.12.19
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MORRISON, JR., ROBERT L.
分类号 F01D5/30;(IPC1-7):F01D5/30 主分类号 F01D5/30
代理机构 代理人
主权项
地址
您可能感兴趣的专利