发明名称 BLADE DAMPER
摘要 A turbomachine blade damper has a damper member with first and second dampi ng surfaces far respectively engaging first and second surfaces of adjacent fir st and second blades. The damper has a seal having a first portion engaged in the damper member to resist relative movement of the seal in at least one direction and a second portion engaging at least one of the blades and advantageously forming a seal to resist upstream gas infiltration.
申请公布号 CA2483071(A1) 申请公布日期 2005.04.08
申请号 CA20042483071 申请日期 2004.09.29
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 COLON, DENNIS I.;SURACE, RAYMOND
分类号 F01D5/26;F01D5/22;F01D11/00;F04D29/08;F04D29/38;(IPC1-7):F01D5/22;F02C7/28 主分类号 F01D5/26
代理机构 代理人
主权项
地址