发明名称 |
Output stage for an axial-flow turbine |
摘要 |
An output stage of an axial-turbine having a high channel divergence has a row of curved vanes and a row of narrowed twisted blades. The curved vanes include, in an axial direction, a positive sweep at their rotor-side end, head and a negative sweep at their stator-side end, with respect to a run of the rotor-side channel boundary. In an area of a stator-side channel boundary a negative sweepback predominates, so that between the curved vanes and the twisted blades an axial diffuser that steadily widens toward the stator-side channel boundary is formed. As a result, an increasing delay of an axial component of a flow agent can occur. The negative sweep at the stator-side end is formed such that at least one of a vane trailing edge and a vane leading edge is directed substantially perpendicularly to the stator-side channel boundary.
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申请公布号 |
US6099248(A) |
申请公布日期 |
2000.08.08 |
申请号 |
US19980190366 |
申请日期 |
1998.11.12 |
申请人 |
ABB ALSTOM POWER (SWITZERLAND) LTD |
发明人 |
MUMM, CARSTEN;WEISS, ANDREAS |
分类号 |
F01D5/14;F01D9/04;(IPC1-7):F01D1/02 |
主分类号 |
F01D5/14 |
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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