Invention Grant
US08951010B2 Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine
有权
用于燃气涡轮发动机中可变入口导叶结构的内径罩组件
- Patent Title: Inner diameter shroud assembly for variable inlet guide vane structure in a gas turbine engine
- Patent Title (中): 用于燃气涡轮发动机中可变入口导叶结构的内径罩组件
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Application No.: US13531679Application Date: 2012-06-25
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Publication No.: US08951010B2Publication Date: 2015-02-10
- Inventor: Daniel W. Major , John C. Ditomasso , Nathan F. Champion
- Applicant: Daniel W. Major , John C. Ditomasso , Nathan F. Champion
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds P.C.
- Main IPC: F04D29/54
- IPC: F04D29/54 ; F01D17/16 ; F01D25/24
Abstract:
An inner shroud assembly includes an aft core segment mountable to a forward core segment to support a multiple of vanes for rotational movement relative thereto. A shroud backing plate segment engageable with the aft core segment and at least one fastener which passes through the shroud backing plate, the aft core segment and the forward core segment.
Public/Granted literature
- US20120257963A1 INNER DIAMETER SHROUD ASSEMBLY FOR VARIABLE INLET GUIDE VANE STRUCTURE IN A GAS TURBINE ENGINE Public/Granted day:2012-10-11
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