Invention Grant
- Patent Title: Metallic seal assembly, turbine component, and method of regulating airflow in turbo-machinery
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Application No.: US13690233Application Date: 2012-11-30
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Publication No.: US09671030B2Publication Date: 2017-06-06
- Inventor: Paul Stephen Dimascio , Michael Douglas Arnett , Rebecca Evelyn Hefner , Christopher D. Higgins
- 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: McNees Wallace & Nurick LLC
- Main IPC: F16K31/00
- IPC: F16K31/00 ; F01D17/08 ; F01D11/00 ; F01D11/18 ; F16J15/16 ; F16J15/44

Abstract:
A metallic seal assembly, a turbine component, and a method of regulating flow in turbo-machinery are disclosed. The metallic seal assembly includes a sealing structure having thermally-responsive features. The thermally-responsive features deploy from or retract toward a surface of the sealing structure in response to a predetermined temperature change. The turbine component includes the metallic seal assembly. The method of regulating flow in turbo-machinery includes providing the metallic seal assembly and raising or retracting the thermally-responsive features in response to the predetermined temperature change.
Public/Granted literature
- US20130259640A1 METALLIC SEAL ASSEMBLY, TURBINE COMPONENT, AND METHOD OF REGULATING AIRFLOW IN TURBO-MACHINERY Public/Granted day:2013-10-03
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