NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Bending and Torsion Load Alleviator With Automatic ResetA force transmitting load alleviator apparatus and method are provided for rotatably and pivotally driving a member to be protected against overload torsional and bending (moment) forces. The load alleviator includes at least one bias spring to resiliently bias cam followers and cam surfaces together and to maintain them in locked engagement unless a predetermined load is exceeded whereupon a center housing is pivotal or rotational with respect to a crown assembly. This pivotal and rotational movement results in frictional dissipation of the overload force by an energy dissipator. The energy dissipator can be provided to dissipate substantially more energy from the overload force than from the bias force that automatically resets the center housing and crown assembly to the normally fixed centered alignment. The torsional and bending (moment) overload levels can designed independently of each other.
Document ID
19970016988
Acquisition Source
Johnson Space Center
Document Type
Other - Patent
Authors
delaFuente, Horacio M.
(NASA Johnson Space Center Houston, TX United States)
Eubanks, Michael C.
(NASA Johnson Space Center Houston, TX United States)
Dao, Anthony X.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 17, 2013
Publication Date
September 24, 1996
Subject Category
Structural Mechanics
Report/Patent Number
Patent Number: US-Patent-5,558,182
Patent Number: NASA-Case-MSC-22515-1
Patent Application Number: US-Patent-Appl-SN-428743
Accession Number
97N19356
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-5,558,182|NASA-Case-MSC-22515-1
Patent Application
US-Patent-Appl-SN-428743
No Preview Available