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High Temperature Metallic Seal/Energizer Development for Aero Propulsion and Gas Turbine ApplicationsThe Ultra High Temperature seal program has successfully progressed and developed a high temperature static seal solution. The third prototype has successfully combined the first and second prototypes high performance capabilities in a commercially viable solution. Prototype II and Prototype III are viable solutions: Prototype II offers flexible load tune ability and seating load adjustment and Prototype III offers commercial viability for continuous hoop seals.
Document ID
20080003825
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
More, Greg
(Parker-Hannifin Corp. North Haven, CT, United States)
Datta, Amit
(Advanced Components and Materials, Inc. East Greenwich, RI, United States)
Cornett, Ken
(Parker-Hannifin Corp. North Haven, CT, United States)
Date Acquired
August 24, 2013
Publication Date
October 1, 2007
Publication Information
Publication: 2006 NASA Seal/Secondary Air System Workshop; Volume 1
Subject Category
Mechanical Engineering
Distribution Limits
Public
Copyright
Public Use Permitted.
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