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NASA High Temperature Turbine Seal Rig DevelopmentThis viewgraph presentation describes a turbine seal rig concept to meet next generation engine speed and temperatures requirements. The contents include: 1) Turbomachinery Seal Development Objectives; 2) High Temperature Turbomachinery Seal Test Rig; 3) Test Parameters; 4) Highlights of Engineering Calculations; 5) Seal Rig Global Thermal Analysis; 6) Test Rig Status; 7) Seal Rig Schematic; 8) Test Chamber Enlarged View; and 9) Rig Features Unique Measurement Systems.
Document ID
20080003810
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Steinetz, Bruce M.
(NASA Glenn Research Center Cleveland, OH, United States)
Proctor, Margaret P.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
August 1, 2006
Publication Information
Publication: Seals/Secondary Fluid Flows Workshop 1997; Volume I
Subject Category
Aircraft Propulsion And Power
Distribution Limits
Public
Copyright
Public Use Permitted.
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