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Latching mechanism for deployable/re-stowable columns useful in satellite constructionA column longeron latch assembly provides the securing mechanism for the deployable, telescoping column of a hoop/column antenna. The column is an open lattice structure with three longerons disposed 120 deg apart as the principle load bearing member. The column is deployed from a pair of eleven nested bays disposed on opposite sides of a center section under the influence of a motor-cable-pulley system. The longeron latch is a four bar linkage mechanism using the over-center principle for automatically locking the longeron sections into position during deployment. The latch is unlocked when the antenna is to be restowed. A spring pack disposed in the end of each longeron serves to absorb stress forces on the deployed column through the cam head piston and abutting latch from an adjacent longeron.
Document ID
19860016319
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Ahl, E. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
May 6, 1986
Subject Category
Mechanical Engineering
Report/Patent Number
Patent Application Number: US-PATENT-APPL-SN-606431
Patent Number: NASA-CASE-LAR-13169-1
Patent Number: US-PATENT-4,587,526
Accession Number
86N25791
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LAR-13169-1|US-PATENT-4,587,526
Patent Application
US-PATENT-APPL-SN-606431
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