VERTICAL TAKE OFF AND LANDING UNMANNED AERIAL VEHICLE AIRFRAME STRUCTURE

Japanese Patent JP2010132280

A

To provide an unmanned aerial vehicle selectively formed of high strength composite structural part portions and lightweight aerodynamic foam portions to provide a low-cost and lightweight UAV that comports with export, civil airspace, and safety regulations.

To further to reduce an overall weight of the UAV, mechanical elements are designed to provide multiple functionalities. Structural elements may be manufactured in same or similar non-specialized processes, and non-structural elements manufactured in same or similar non-specialized processes, reducing overall manufacturing costs. Materials and bonding elements are selected to provide frangibility and yet maintain normal flight structural integrity.

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WO/2015/146528	CAP, CAP MOLD, SECURING STRUCTURE PART USING CAP, AND METHOD FOR MOUNTING CAP

GOOSSEN EMRAY

JP2009268650A

June 17, 2010

November 26, 2009

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HONEYWELL INT INC

B64C1/00; B64C29/00; B64C39/02

JP2003512215A	2003-04-02
JP2008531375A	2008-08-14
JP2002542116A	2002-12-10
JP2001018895A	2001-01-23
JPH0624391A	1994-02-01
JPH06293296A	1994-10-21
JP2007263962A	2007-10-11
JPH06123323A	1994-05-06

US7249732B2	2007-07-31
US20030062443A1	2003-04-03
US20020100834A1	2002-08-01
US20060091258A1	2006-05-04

Shinjiro Ono
Kazuo Shamoto
Yasushi Kobayashi
Akio Chiba
Hiroyuki Tomita
Shigeo Takeuchi

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