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Composite passive damping struts for large precision structuresIn the field of viscoelastic dampers, a new strut design comprises a viscoelastic material sandwiched between multiple layers, some of which layers bear and dampen load force. In one embodiment, the layers are composite plies of opposing orientation. In another embodiment, the strut utilizes a viscoelastic layer sandwiched between V-shaped composite plies. In a third embodiment, a viscoelastic layer is sandwiched between sine-shaped plies. Strut strength is equal to or greater than conventional aluminum struts due to the unique high interlaminar shear ply design.
Document ID
19930015407
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Dolgin, Benjamin P.
(Jet Propulsion Lab. California Inst. of Tech., Pasadena., United States)
Date Acquired
August 15, 2013
Publication Date
April 20, 1993
Subject Category
Structural Mechanics
Report/Patent Number
Patent Number: NASA-CASE-NPO-17914-1-CU
Patent Application Number: US-PATENT-APPL-SN-575697
Patent Number: US-PATENT-5,203,435
Accession Number
93N24596
Funding Number(s)
CONTRACT_GRANT: NAS7-918
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-NPO-17914-1-CU|US-PATENT-5,203,435
Patent Application
US-PATENT-APPL-SN-575697
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