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Load Transfer Mechanism for a Turbine DiskA load transferring system wherein a composite turbine disk mounted on a shaft is in contact with a backup disk which is secured to the shaft. The turbine disk is made of layers of woven carbon fibers held in a rigid configuration in a ceramic matrix. The composite disk has a plurality of lugs which have trapezoidal cross sections when cut by planes which are perpendicular to each other, with both planes being normal to the disk. The backup disk is provided with recesses which are the negative of the trapezoidal lugs to lock the two disks together. A second backup disk may be secured to the shaft to secure the composite turbine disk between the backup disks.
Document ID
20020005124
Acquisition Source
Marshall Space Flight Center
Document Type
Other - Patent
External Source(s)
MFS-31270-1
Authors
Michael R Effinger
(Marshall Space Flight Center Redstone Arsenal, United States)
Date Acquired
August 20, 2013
Publication Date
December 19, 2000
Publication Information
Publisher: United States Patent and Trademark Office
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-Patent-Appl-SN-190784
Patent Number: US-Patent-6,162,019
Patent Number: NASA-Case-MFS-31270-1
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-6,162,019
Patent Application
US-Patent-Appl-SN-190784
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