Invention Application
- Patent Title: Launch Tube Restraint System For Unmanned Aerial Vehicle (UAV)
- Patent Title (中): 无人机（UAV）发射管约束系统
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Application No.: US15292908Application Date: 2016-10-13
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Publication No.: US20170029135A1Publication Date: 2017-02-02
- Inventor: Guan H. Su , Marcos Henry Rodriguez
- Applicant: AeroVironment, Inc.
- Main IPC: B64F1/04
- IPC: B64F1/04 ; B64C39/02 ; F41B11/80
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).
Public/Granted literature
- US09873526B2 Launch tube restraint system for unmanned aerial vehicle (UAV) Public/Granted day:2018-01-23
Information query
