Invention Grant
US08167547B2 Gas turbine engine with canted pocket and canted knife edge seal
有权
燃气涡轮发动机带斜口袋和斜口刀边缘密封
- Patent Title: Gas turbine engine with canted pocket and canted knife edge seal
- Patent Title (中): 燃气涡轮发动机带斜口袋和斜口刀边缘密封
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Application No.: US11714019Application Date: 2007-03-05
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Publication No.: US08167547B2Publication Date: 2012-05-01
- Inventor: Charles C. Wu , Kevin N. McCusker , Roger E. Paolillo , Page Russell Palmiter
- Applicant: Charles C. Wu , Kevin N. McCusker , Roger E. Paolillo , Page Russell Palmiter
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds
- Main IPC: F01D11/02
- IPC: F01D11/02

Abstract:
A gas turbine engine is provided with turbine sealing structures including knife edge seals which extend at an angle relative to an axial center line of the engine. Each knife edge seal is associated with a control pocket defined between a radially inner surface and a spaced radially outer surface. The control pockets and their associated knife edge seals create a difficult flow path to prevent leakage into radially inner portions of the turbine section.
Public/Granted literature
- US20090067997A1 Gas turbine engine with canted pocket and canted knife edge seal Public/Granted day:2009-03-12
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