Invention Grant
- Patent Title: Thermally compliant turbine shroud assembly
- Patent Title (中): 耐热兼容的涡轮机罩组件
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Application No.: US11161517Application Date: 2005-08-06
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Publication No.: US07452183B2Publication Date: 2008-11-18
- 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, P.A.
- Agent William Scott Andes, Esq.
- Main IPC: F01D11/08
- IPC: F01D11/08

Abstract:
A shroud assembly is provided for a gas turbine engine having 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. The shroud segment has an arcuate, axially extending mounting flange. A shroud hanger includes an arcuate, axially-extending hook. A dimension of one of the shroud segments and the shroud hanger are selected to produce a preselected dimensional relationship therebetween at the hot operating condition.
Public/Granted literature
- US20070031244A1 Thermally compliant turbine shroud assembly Public/Granted day:2007-02-08
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