Invention Grant
US08453326B2 Method for assembling radially loaded vane assembly of gas turbine engine
有权
燃气轮机发动机径向负载叶片组件的组装方法
- Patent Title: Method for assembling radially loaded vane assembly of gas turbine engine
- Patent Title (中): 燃气轮机发动机径向负载叶片组件的组装方法
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Application No.: US13351634Application Date: 2012-01-17
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Publication No.: US08453326B2Publication Date: 2013-06-04
- Inventor: Eric Durocher , Anca Mateescu
- Applicant: Eric Durocher , Anca Mateescu
- Applicant Address: CA Longueuil
- Assignee: Pratt & Whitney Canada Corp.
- Current Assignee: Pratt & Whitney Canada Corp.
- Current Assignee Address: CA Longueuil
- Agency: Norton Rose Canada LLP
- Main IPC: B21K25/00
- IPC: B21K25/00 ; B23P15/04

Abstract:
A method for assembling a vane ring with a vane support of a vane assembly in a gas turbine engine is described, and includes flexing each of the radial loading elements into the resiliently flexed state simultaneously by sliding the radial loading elements against corresponding lead-in tapers. This can be achieved, for example, using a guide tool which includes a plurality of segments bearing the lead-in tapers and which is previously assembled to the vane support.
Public/Granted literature
- US20120110849A1 METHOD FOR ASSEMBLING RADIALLY LOADED VANE ASSEMBLY OF GAS TURBINE ENGINE Public/Granted day:2012-05-10
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