发明名称 |
Gas turbine with an exhaust gas diffuser and support ribs |
摘要 |
<p>The turbine (10) has an exhaust gas diffuser (21) connected to a turbine unit (24). An inflow-side annular diffuser channel (33) is limited by a conical channel wall (40). Inward extending hollow support ribs (35) are provided at the channel for fastening a radial bearing (51). A blow line (47) for blow air, is led into the diffuser. An inflow side end of the blow line is connected with an axial-flow turbo compressor (18). An outflow-side end of the blow line is fluidically connected with a cavity of the ribs. The ribs comprise apertures (49) for blowing the blow air into the channel.</p> |
申请公布号 |
EP2634381(A1) |
申请公布日期 |
2013.09.04 |
申请号 |
EP20120157273 |
申请日期 |
2012.02.28 |
申请人 |
SIEMENS AKTIENGESELLSCHAFT |
发明人 |
BROEKER, MARC;BUCHAL, TOBIAS |
分类号 |
F01D25/30;F02C6/08 |
主分类号 |
F01D25/30 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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