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US Patent 11987393 Launch lock system with increased release clearance in all directions

Patent 11987393 was granted and assigned to HONEYWELL INTERNATIONAL INC on May, 2024 by the United States Patent and Trademark Office.

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Is a
Patent
Patent
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Patent attributes

Patent Applicant
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HONEYWELL INTERNATIONAL INC
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Current Assignee
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HONEYWELL INTERNATIONAL INC
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Patent Jurisdiction
United States Patent and Trademark Office
United States Patent and Trademark Office
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Patent Number
119873930
Patent Inventor Names
Ken E. Young0
Timothy Barber0
Timothy Hindle0
Date of Patent
May 21, 2024
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Patent Application Number
169309900
Date Filed
July 16, 2020
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Patent Citations
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US Patent 8568053 Radial release device
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US Patent 8678323 Launch lock assemblies including axial gap amplification devices and spacecraft isolation systems including the same
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US Patent 9604738 Non-explosive tension release actuator
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US Patent 9663249 Dual spacecraft design and deployment system and method of use thereof
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US Patent 10232960 Manipulation of a satellite in space
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US Patent 10293960 Rigidizing latch assembly
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US Patent 6935805 High reliability precision latch
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US Patent 7828249 Docking system
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Patent Primary Examiner
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Josh Skroupa
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CPC Code
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Y10T 403/7066
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B64G 1/64
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B64G 1/641
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B64G 1/645
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B64G 2001/643
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F16B 2/02
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F16B 2/06
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F16B 2/10
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Patent abstract

A launch lock system includes a first portion rigidly coupled to the second portion in a first state and the first portion movable in all directions relative to the second portion in a second state. The launch lock system includes a fastener subassembly coupled to the second portion, and the fastener subassembly is movable relative to the second portion from a first position to a second position. The launch lock system includes at least one pivot arm subassembly having a pivot arm movable between a first position and a second position. The pivot arm is coupled to the first portion in the first position. In the first state, the pivot arm is in the first position and cooperates with the fastener subassembly in the first position, and in the second state, the pivot arm is uncoupled from the first portion and the fastener subassembly.

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