Invention Grant
- Patent Title: Inlet guide vane assembly of gas turbine and gas turbine
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Application No.: US16609568Application Date: 2018-04-20
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Publication No.: US11041406B2Publication Date: 2021-06-22
- Inventor: Yang Wang , Hong Yun Lv
- Applicant: Siemens Aktiengesellschaft
- Applicant Address: DE Munich
- Assignee: Siemens Aktiengesellschaft
- Current Assignee: Siemens Aktiengesellschaft
- Current Assignee Address: DE Munich
- Agency: Harness, Dickey & Pierce, P.L.C.
- Priority: CN201720478719.5 20170502
- International Application: PCT/EP2018/060142 WO 20180420
- International Announcement: WO2018/202441 WO 20181108
- Main IPC: F01D25/24
- IPC: F01D25/24 ; F01D17/16

Abstract:
An inlet guide vane assembly of gas turbine is disclosed. The inlet guide vane assembly includes: a plurality of inlet guide vanes, each including a fixing shaft disposed at the end away from a fixing part; and a fixing assembly including a support ring, a fixing ring and an abutting member. The fixing ring includes a fixing wall facing towards a support part, the fixing wall forming, in cooperation with a support wall, a plurality of accommodating cavities corresponding to the plurality of inlet guide vanes. The fixing shafts are rotatably inserted into the accommodating cavities, and the abutting member is in interference fit with the inner inlet casing and the fixing ring. The inlet guide vane assembly implements support for the inlet guide vanes without affecting installation of the inlet guide vanes.
Public/Granted literature
- US20200063605A1 INLET GUIDE VANE ASSEMBLY OF GAS TURBINE AND GAS TURBINE Public/Granted day:2020-02-27
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