Invention Grant
- Patent Title: Turbine seal system and method
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Application No.: US13937121Application Date: 2013-07-08
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Publication No.: US09605553B2Publication Date: 2017-03-28
- Inventor: Matthew Troy Hafner
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: General Electric Company
- Current Assignee: General Electric Company
- Current Assignee Address: US NY Schenectady
- Agency: Fletcher Yoder, P.C.
- Main IPC: F01D11/00
- IPC: F01D11/00 ; F01D5/30

Abstract:
A system includes a multi-stage turbine. The multi-stage turbine includes a first turbine stage with a first wheel having a plurality of first blade segments spaced circumferentially about the first wheel, a second turbine stage with a second wheel having a plurality of second blade segments spaced circumferentially about the second wheel, and an interstage seal assembly extending axially between the first and second turbine stages. The interstage seal assembly includes a first coverplate coupled to the first turbine stage. The first coverplate includes a first seal. The interstage seal assembly also includes a second coverplate coupled to the second turbine stage. The second coverplate includes a second seal. The interstage seal assembly also includes a spacer wheel extending from a rotor shaft and configured to engage with the first coverplate and the second coverplate.
Public/Granted literature
- US20150010384A1 TURBINE SEAL SYSTEM AND METHOD Public/Granted day:2015-01-08
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