可搬型ＲＦ透過性発射筒を有する遠隔操作無人航空機レポート抑制発射機のためのシステムおよび装置

Japanese Patent JP5865247

B2

An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).

Mirages, Carlos Thomas
Suu, Guan H.
Andrekov, Oleksandr
John McNeill

JP2012528905A

February 17, 2016

September 09, 2010

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AEROVIRONMENT,INC.

B64F1/04; F41F3/042

JP5149696A
JP2291703A
JP2005500774A
JP2007228065A
JP5106997A
JP2005240841A
JP2004271216A
JP2003177000A

GB2188713A
WO2005023642A2
US4410151
US6056237

Patent business corporation Kita Aoyama International

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