发明名称 SLIDE RING SEAL
摘要 A turbomachine in the form of a stationary gas turbine or an aircraft engine, respectively a housing structure therefor; the housing structure including an outer housing wall (1) and an inner wall (2) defining the flow channel; and a hollow space (4) being formed between the inner wall and the outer housing wall. The hollow space is separable into at least two regions (5, 6); a movable wire element (slide ring seal) (10, 10′), which is adapted to rest against the contact faces (8, 9), being configured in the hollow space for purposes of the separation.
申请公布号 US2014321969(A1) 申请公布日期 2014.10.30
申请号 US201414249056 申请日期 2014.04.09
申请人 MTU Aero Engines AG 发明人 Feldmann Manfred;Schinko Norbert;Sangl Janine
分类号 F01D11/02 主分类号 F01D11/02
代理机构 代理人
主权项 1. A housing structure for a turbomachine, the housing structure surrounding a flow channel for a fluid and comprising: an outer housing wall and an inner wall defining the flow channel, a hollow space being formed between the inner wall and the outer housing wall, the hollow space separable into at least two regions; and a movable wire element adapted to rest against contact faces and being configured in the hollow space for purposes of separating the at least two regions.
地址 Muenchen DE