Invention Grant
US08684683B2 Gas turbine nozzle attachment scheme and removal/installation method
有权
燃气轮机喷嘴附件方案及拆卸/安装方法
- Patent Title: Gas turbine nozzle attachment scheme and removal/installation method
- Patent Title (中): 燃气轮机喷嘴附件方案及拆卸/安装方法
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Application No.: US12956554Application Date: 2010-11-30
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Publication No.: US08684683B2Publication Date: 2014-04-01
- Inventor: Thomas James Brunt , Robert Walter Coign , Gregory Thomas Foster
- Applicant: Thomas James Brunt , Robert Walter Coign , Gregory Thomas Foster
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Nixon & Vanderhye P.C.
- Main IPC: F01D9/04
- IPC: F01D9/04 ; F01D25/24

Abstract:
A turbine nozzle attachment assembly includes an outer turbine component (a shroud or a turbine shell) formed with a circumferential groove open in a forward-facing axial direction; a nozzle segment including a vane extending between inner and outer bands, the outer band provided with an upstanding annular hook formed with a hook element extending in an aft-facing axial direction and received in the circumferential groove. The upstanding annular hook and hook element are formed with a circumferentially-oriented slot. An anti-rotation block is located in the circumferentially-oriented slot, and an anti-tipping plate having a circumferential width greater than a corresponding circumferential width of the circumferentially-oriented slot substantially covers a forward face of the anti-rotation block. The anti-rotation block and the anti-tipping plate are fastened directly to the outer turbine component.
Public/Granted literature
- US20120134791A1 GAS TURBINE NOZZLE ATTACHMENT SCHEME AND REMOVAL/INSTALLATION METHOD Public/Granted day:2012-05-31
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