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High Temperature Metallic Seal Development For Aero Propulsion and Gas Turbine ApplicationsA viewgraph presentation on metallic high temperature static seal development at NASA for gas turbine applications is shown. The topics include: 1) High Temperature Static Seal Development; 2) Program Review; 3) Phase IV Innovative Seal with Blade Alloy Spring; 4) Spring Design; 5) Phase IV: Innovative Seal with Blade Alloy Spring; 6) PHase IV: Testing Results; 7) Seal Seating Load; 8) Spring Seal Manufacturing; and 9) Other Applications for HIgh Temperature Spring Design
Document ID
20070002990
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
More, Greg (Advanced Products Co. East Greenwich, CT, United States)
Datta, Amit (Advanced Components and Materials, Inc. East Greenwich, RI, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2006
Publication Information
Publication: 2005 NASA Seal/Secondary Air System Workshop, Volume 1
Subject Category
Space Transportation And Safety
Distribution Limits
Public
Copyright
Public Use Permitted.

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IDRelationTitle20070002977Collected Works2005 NASA Seal/Secondary Air System Workshop, Volume 1
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