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Fiber-reinforced superalloy composites provide an added performance edgeFiber reinforcements are being explored as a means to increasing the performance of superalloys past 980 C. Fiber-reinforced superalloys (FRS), particularly tungsten FRS (TFRS) are candidate materials for rocket-engine turbopump blades for advanced Shuttle engines and in airbreathing and other rocket engines. Refractory metal wires are the reinforcement of choice due to tolerance to fiber/matrix interactions. W alloy fibers have a maximum tensile strength of 2165 MPa at 1095 C and a 100 hr creep rupture strength at stresses up to 1400 MPa. A TFRS has the potential of a service temperature 110 C over the strongest superalloy. Manufacturing processes being evaluated to realize the FRS components are summarized, together with design features which will be introduced in turbine blades to take advantage of the FRS materials and to extend their surface life.
Document ID
19870025373
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Petrasek, D. W.
(NASA Lewis Research Center Cleveland, OH, United States)
Mcdaniels, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Westfall, L. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Stephens, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 13, 2013
Publication Date
August 1, 1986
Publication Information
Publication: Metal Progress
ISSN: 0026-0665
Subject Category
Composite Materials
Accession Number
87A12647
Distribution Limits
Public
Copyright
Other

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