Invention Grant
- Patent Title: Gas turbine combustor exit duct and hp vane interface
- Patent Title (中): 燃气轮机燃烧器出口管和hp叶片接口
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Application No.: US12905663Application Date: 2010-10-15
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Publication No.: US08166767B2Publication Date: 2012-05-01
- Inventor: Nicolas Grivas , Bhawan B. Patel , Oleg Morenko , Eric Durocher
- Applicant: Nicolas Grivas , Bhawan B. Patel , Oleg Morenko , Eric Durocher
- 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: F02C7/20
- IPC: F02C7/20 ; F01D25/26

Abstract:
An assembly for a gas turbine engine includes a combustor and a vane assembly disposed downstream thereof. A portion of an outer platform of the vane assembly defines an axial sliding joint connection with the combustor, and includes a plurality of depressions located in an outer circumferential surface thereof opposite the combustor. The depressions are disposed in regions of expected higher thermal growth about the circumference of the outer platform such that thermal growth of the entire outer platform is substantially uniform circumferentially therearound.
Public/Granted literature
- US20110023499A1 GAS TURBINE COMBUSTOR EXIT DUCT AND HP VANE INTERFACE Public/Granted day:2011-02-03
Information query
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