发明名称 GAS TURBINE AND MOUNTING METHOD
摘要 An insert element fastens to an annular segment body of a turbine of a gas turbine. The annular segment body has a recess on a hot-gas side. The insert element is designed to cover the recess and has a concave front side and a rear side having at least one shaped portion for positioning on the annular segment body. An annular segment has the insert element, a gas turbine has the insert element, and a mounting method mounts the insert element.
申请公布号 US2016201497(A1) 申请公布日期 2016.07.14
申请号 US201415023391 申请日期 2014.08.29
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 Ahmad Fathi;Händler Michael;Kampka Kevin;Kowalski Christian;Kowalzik Christian;Kurt Nihal;Schmitt Stefan;Schröder Peter
分类号 F01D11/08;F01D5/12;F01D5/02 主分类号 F01D11/08
代理机构 代理人
主权项
地址 München DE