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Patent Searching and Data


Title:
LAUNCH TUBE RESTRAINT SYSTEM FOR UNMANNED AERIAL VEHICLE (UAV)
Document Type and Number:
WIPO Patent Application WO/2013/126111
Kind Code:
A3
Abstract:
An unmanned aerial launch vehicle (UAV) launch apparatus is disclosed that includes a UAV (400) having an exterior surface, an aerial vehicle (AV) tab (510) extending from the exterior surface, a tube (440) containing the UAV (400), the tube (440) including a tab stop (515) configured to controllably hinder travel of the AV tab (510) past the tab stop (515), and a pair of opposing tab guides (700, 705) configured to position the AV tab (510) for travel over the tab stop (515).

Inventors:
SU GUAN (US)
RODRIGUEZ MARCOS (US)
Application Number:
PCT/US2012/067086
Publication Date:
October 17, 2013
Filing Date:
November 29, 2012
Export Citation:
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Assignee:
AEROVIRONMENT INC (US)
SU GUAN (US)
RODRIGUEZ MARCOS (US)
International Classes:
B64C1/00; F41F3/04; B64F1/04; F41A15/00
Domestic Patent References:
WO2011066030A22011-06-03
Foreign References:
US20100281745A12010-11-11
US20100282055A12010-11-11
Attorney, Agent or Firm:
YEDIDSON, Pejman (Suite 108Simi Valley, California, US)
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