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Advanced High Temperature Polymer Matrix Composites for Gas Turbine Engines Program ExpansionThis document, submitted by AlliedSignal Engines (AE), a division of AlliedSignal Aerospace Company, presents the program final report for the Advanced High Temperature Polymer Matrix Composites for Gas Turbine Engines Program Expansion in compliance with data requirements in the statement of work, Contract No. NAS3-97003. This document includes: 1 -Technical Summary: a) Component Design, b) Manufacturing Process Selection, c) Vendor Selection, and d) Testing Validation: 2-Program Conclusion and Perspective. Also, see the Appendix at the back of this report. This report covers the program accomplishments from December 1, 1996, to August 24, 1998. The Advanced High Temperature PMC's for Gas Turbine Engines Program Expansion was a one year long, five task technical effort aimed at designing, fabricating and testing a turbine engine component using NASA's high temperature resin system AMB-21. The fiber material chosen was graphite T650-35, 3K, 8HS with UC-309 sizing. The first four tasks included component design and manufacturing, process selection, vendor selection, component fabrication and validation testing. The final task involved monthly financial and technical reports.
Document ID
19990116848
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Hanley, David (Allied-Signal Engines Phoenix, AZ United States)
Carella, John (Allied-Signal Engines Phoenix, AZ United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1999
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.26:208889
E-11634
NASA/CR-1999-208889
Funding Number(s)
CONTRACT_GRANT: NAS3-97003
PROJECT: RTOP 523-21-13
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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