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Design and Testing of Braided Composite Fan Case Materials and ComponentsTriaxial braid composite materials are beginning to be used in fan cases for commercial gas turbine engines. The primary benefit for the use of composite materials is reduced weight and the associated reduction in fuel consumption. However, there are also cost benefits in some applications. This paper presents a description of the braided composite materials and discusses aspects of the braiding process that can be utilized for efficient fabrication of composite cases. The paper also presents an approach that was developed for evaluating the braided composite materials and composite fan cases in a ballistic impact laboratory. Impact of composite panels with a soft projectile is used for materials evaluation. Impact of composite fan cases with fan blades or blade-like projectiles is used to evaluate containment capability. A post-impact structural load test is used to evaluate the capability of the impacted fan case to survive dynamic loads during engine spool down. Validation of these new test methods is demonstrated by comparison with results of engine blade-out tests.
Document ID
20090022155
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Roberts, Gary D.
(NASA Glenn Research Center Cleveland, OH, United States)
Pereira, J. Michael
(NASA Glenn Research Center Cleveland, OH, United States)
Braley, Michael S.
(A and P Technology, Inc. Cincinnati, OH, United States)
Arnold, William A.
(Akron Univ. Akron, OH, United States)
Dorer, James D.
(Williams International Walled Lake, MI, United States)
Watson, William R.
(Honeywell Aerospace United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2009
Subject Category
Composite Materials
Report/Patent Number
E-17015
ISABE-2009-1201
Funding Number(s)
WBS: WBS 698259.02.07.03.04.01
Distribution Limits
Public
Copyright
Other

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