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Development of advanced lightweight containment systemsParametric type data were obtained on advanced lightweight containment systems. These data were used to generate design methods and procedures necessary for the successful development of such systems. The methods were then demonstrated through the design of a lightweight containment system for a CF6 size engine. The containment concept evaluated consisted basically of a lightweight structural sandwich shell wrapped with dry Kevlar cloth. The initial testing was directed towards the determination of the amount of Kevlar required to result in threshold containment for a specific set of test conditions. A relationship was then developed between the thickness required and the energy of the released blade so that the data could be used to design for conditions other than those tested.
Document ID
19810015645
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stotler, C.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Subject Category
Composite Materials
Report/Patent Number
R81AEG208
NASA-CR-165212
Report Number: R81AEG208
Report Number: NASA-CR-165212
Accession Number
81N24180
Funding Number(s)
CONTRACT_GRANT: NAS3-21823
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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