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Lightweight engine containmentKevlar fabric styles and weaves were studied, as well as methods of application for advanced gas turbine engines. The Kevlar material was subjected to high speed impacts by simple projectiles fired from a rifle, as well as more complex shapes such as fan blades released from gas turbine rotors in a spin pit. Just contained data was developed for a variety of weave and/or application techniques, and a comparative containment weight efficiency was established for Kevlar containment applications. The data generated during these tests is being incorporated into an analytical design system so that blade containment trade-off studies between Kevlar and metal case engine structures can be made. Laboratory tests and engine environment tests were performed to determine the survivability of Kevlar in a gas turbine environment.
Document ID
19780002137
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Weaver, A. T.
(Pratt and Whitney Aircraft Group East Hartford, CT, United States)
Date Acquired
August 9, 2013
Publication Date
March 1, 1977
Publication Information
Publication: MIT An Assessment of Technol. for Turbojet Engine Rotor Failures
Subject Category
Aircraft Propulsion And Power
Accession Number
78N10080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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