Invention Grant
- Patent Title: Gas turbine engine sealing structure
- Patent Title (中): 燃气轮机发动机密封结构
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Application No.: US13151355Application Date: 2011-06-02
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Publication No.: US08821114B2Publication Date: 2014-09-02
- Inventor: Gennadiy Afanasiev , John N. Strain , Robert W. Sunshine , Robert D. Barker
- Applicant: Gennadiy Afanasiev , John N. Strain , Robert W. Sunshine , Robert D. Barker
- Applicant Address: US FL Orlando
- Assignee: Siemens Energy, Inc.
- Current Assignee: Siemens Energy, Inc.
- Current Assignee Address: US FL Orlando
- Main IPC: F01D11/00
- IPC: F01D11/00

Abstract:
A turbine section having a plurality flow path components forming a plurality of guide vane rings and ring segments arranged in axial succession to define a boundary of a hot gas duct. A vane carrier located around the gas duct, and sealing elements extend radially between circumferentially extending grooves in the vane carrier and respective grooves in the flow path components. The sealing elements include radially inner and outer edges, and at least one axially facing side defining a chamfered portion extending to one of the edges to accommodate axial movement of the sealing element about the one edge within a respective groove.
Public/Granted literature
- US20110299978A1 GAS TURBINE ENGINE SEALING STRUCTURE Public/Granted day:2011-12-08
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