Invention Grant
- Patent Title: Active tip clearance control arrangement for gas turbine engine
- Patent Title (中): 燃气轮机发动机主动顶盖间隙控制装置
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Application No.: US12411495Application Date: 2009-03-26
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Publication No.: US08092146B2Publication Date: 2012-01-10
- Inventor: Pierre-Yves Legare , Stephen Mah
- Applicant: Pierre-Yves Legare , Stephen Mah
- Applicant Address: CA Longueuil, Quebec
- Assignee: Pratt & Whitney Canada Corp.
- Current Assignee: Pratt & Whitney Canada Corp.
- Current Assignee Address: CA Longueuil, Quebec
- Agency: Norton Rose Or LLP
- Main IPC: F01D11/24
- IPC: F01D11/24
Abstract:
An active tip clearance control (ATCC) apparatus of an aircraft gas turbine engine is situated within a pressurized core case of the engine. First and second portions of bypass air flow passing through the respective compressed core compartment and the ATCC apparatus, are isolated from one another in order to improve both the ATCC performance and bypass air duct performance.
Public/Granted literature
- US20100247297A1 ACTIVE TIP CLEARANCE CONTROL ARRANGEMENT FOR GAS TURBINE ENGINE Public/Granted day:2010-09-30
Information query
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