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Structurally-Tailorable, Nonlinear, Snap-Through SpringAbrupt change in load/deflection response controllable and predictable. Structurally-tailorable, nonlinear, snap-through spring (STNSTS) exhibits controllable and predictable abrupt change in load/deflection response and based upon known phenomenon of snap-through structural response. Composed of pin-connected two-bar linkage which depicts combined tension/compression springs. As load applied to STNSTS, stiffness is function of internal spring and bending stiffness of pin-connected bars. As load increases, bars deform laterally until they collapse and snap through. Has application in passively-tailored rotor-blade flap, pitch, and lag response, to improve aerodynamic performance and stability characteristics of rotors; in aerodynamically- and aeroelastically-tailored wing spars and ribs, to produce tailored deformation state for improved effectiveness in maneuvering, aerodynamic performance, and stability characteristics; and in energy absorbers for automobile bumpers and aircraft land
Document ID
19890000311
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Starnes, James H., Jr.
(NASA Langley Research Center, Hampton, VA.)
Farley, Gary L.
(Army Aerostructures Directorate)
Mantay, Wayne R.
(Army Aerostructures Directorate)
Date Acquired
August 14, 2013
Publication Date
June 1, 1989
Publication Information
Publication: NASA Tech Briefs
Volume: 13
Issue: 6
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13729
Accession Number
89B10311
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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