Invention Grant
- Patent Title: Thermally compliant turbine shroud mounting assembly
- Patent Title (中): 符合标准的涡轮机罩安装组件
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Application No.: US11161516Application Date: 2005-08-06
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Publication No.: US07438520B2Publication Date: 2008-10-21
- Inventor: Michael Anthony Ruthemeyer , Glenn Herbert Nichols , Ching-Pang Lee
- Applicant: Michael Anthony Ruthemeyer , Glenn Herbert Nichols , Ching-Pang Lee
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Adams Intellectual Property Law, PA.
- Agent William Scott Andes, Esq.
- Main IPC: F01D11/08
- IPC: F01D11/08

Abstract:
A shroud assembly is provided for a gas turbine engine that has a temperature at a hot operating condition substantially greater than at a cold assembly condition thereof. The shroud assembly includes: at least one arcuate shroud segment adapted to surround a row of rotating turbine blades which has an arcuate, axially extending mounting flange; a shroud hanger having an arcuate, axially-extending hook disposed in mating relationship to the mounting flange; and an arcuate C-clip having inner and outer arms overlapping the hook and the mounting flange. The curvatures of the mounting flange and the inner arm of the C-clip are selected so as to define a matched interface therebetween. Their curvatures are substantially greater that the curvature of the hook.
Public/Granted literature
- US20070031243A1 Thermally compliant turbine shroud mounting assembly Public/Granted day:2007-02-08
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