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TMC Behavior Modeling and Life Prediction Under Multiaxial StressesThe goal of this program was to manufacture and burst test small diameter SCS-6/Ti-6Al-4V composite rings for use in the design of an advanced titanium matrix composite (TMC) impeller. The Textron Specialty Metals grooved foil-fiber process was successfully used to make high quality TMC rings. A novel spin test arbor with "soft touch" fingers to retain the TMC ring was designed and manufactured. The design of the arbor took into account its use for cyclic experiments as well as ring burst tests. Spin testing of the instrumented ring was performed at ambient, 149C (300F), and 316C (600F) temperatures. Assembly vibration was encountered during spin testing but this was overcome through simple modification of the arbor. A spin-to-burst test was successfully completed at 316C (600F). The rotational speed of the TMC ring at burst was close to that predicted. In addition to the spin test program, a number of SCS-6/Ti-6Al-4V test panels were made. Neat Ti-6Al-4V panels also were made.
Document ID
19980223374
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Merrick, H. F.
(Allied-Signal Aerospace Co. Phoenix, AZ United States)
Aksoy, S. Z.
(Aerospace Structural Research Corp. Milford, CT United States)
Costen, M.
(Aerospace Structural Research Corp. Milford, CT United States)
Ahmad, J.
(Research Applications, Inc. San Diego, CA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1998
Subject Category
Composite Materials
Report/Patent Number
AlliedSignal Engines-21-9835
NAS 1.26:207928
NASA/CR-1998-207928
E-11188
Report Number: AlliedSignal Engines-21-9835
Report Number: NAS 1.26:207928
Report Number: NASA/CR-1998-207928
Report Number: E-11188
Funding Number(s)
PROJECT: RTOP 523-21-13
CONTRACT_GRANT: NAS3-27027
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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