Title:
DEPLOYMENT SYSTEM FOR AIRBORNE OBJECT COMPRISING A TORSION STOP
Document Type and Number:
WIPO Patent Application WO/2011/046640
Kind Code:
A3
Abstract:
Embodiments of a torsion stop deployment system for utilization onboard an airborne object are provided. In one embodiment, the torsion stop deployment system includes a deployable element hingedly coupled to the airborne object and rotatable from a non-deployed position to a deployed position. The torsion stop deployment system further includes a torsion bar member, which is fixedly coupled to the airborne object and which resiliently resists the rotation of the deployable element to reduce shock to the airborne object during deployment of the deployable element.
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Inventors:
MARTIN ROBERT W (US)
Application Number:
PCT/US2010/038508
Publication Date:
June 09, 2011
Filing Date:
June 14, 2010
Export Citation:
Assignee:
RAYTHEON CO (US)
MARTIN ROBERT W (US)
MARTIN ROBERT W (US)
International Classes:
F42B10/14
Foreign References:
| US4460137A | 1984-07-17 | |||
| US20080078859A1 | 2008-04-03 | |||
| EP0242180A2 | 1987-10-21 | |||
| US4659038A | 1987-04-21 | |||
| US20070102567A1 | 2007-05-10 |
Attorney, Agent or Firm:
LEACH, Justin J. et al. (P.C.7010 East Cochise Roa, Scottsdale Arizona, US)
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