Invention Grant
- Patent Title: Cover plate with interstage seal for a gas turbine engine
- Patent Title (中): 用于燃气轮机的间隔板盖板
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Application No.: US13004273Application Date: 2011-01-11
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Publication No.: US08740554B2Publication Date: 2014-06-03
- Inventor: Scott D. Virkler , Roger Gates
- Applicant: Scott D. Virkler , Roger Gates
- Applicant Address: US CT Hartford
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Hartford
- Agency: Carlson, Gaskey & Olds, P.C.
- Main IPC: F01D11/08
- IPC: F01D11/08 ; F01D1/10 ; F01D5/30 ; F01D11/00

Abstract:
An air seal assembly for a gas turbine engine includes a first cover plate with a radially extending knife edge seal defined about and axis of rotation. The first cover plate is mountable to a first rotor disk for rotation therewith, the first radially extending knife edge seal interfaces with a vane structure. A second cover plate with a second radially extending knife edge seal defined about the axis of rotation, the second cover plate mountable to the second rotor disk for rotation therewith. The second radially extending knife edge seal interfaces with the vane structure.
Public/Granted literature
- US20120177485A1 COVER PLATE WITH INTERSTAGE SEAL FOR A GAS TURBINE ENGINE Public/Granted day:2012-07-12
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