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 |
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代理人 |
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主权项 |
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地址 |
München DE |