Title:
SEA-LAND-AIR-UNDERWATER ADAPTED VEHICLE CAPABLE OF VERTICAL TAKE-OFF AND LANDING
Document Type and Number:
WIPO Patent Application WO/2020/215304
Kind Code:
A1
Abstract:
A sea-land-air-underwater adapted vehicle capable of vertical take-off and landing, comprising a fuselage (1), two main wings (2), auxiliary wings (3), a vertical tail wing (4), a rudder (5), a horizontal tail wing (6), elevators (7), a propeller (8), rotors (9), rotor supports (10), extension and retraction rotary shafts (11), fuselage rear section sinking-floating cabins (12), fuselage middle section sinking-floating cabins (13), fuselage front section sinking-floating cabins (14), front attitude control compartment covers (15), rear attitude control compartment covers (16), a vector thruster (17) and three undercarriages (18). Said vehicle has the advantages of being adaptable to various environments, having good concealment, and high survivability.
More Like This:
JP2011527264 | A rotating lower part shuttlecock flight object |
WO/2011/139316 | AIRCRAFT VERTICAL LIFT DEVICE |
Inventors:
SUN XIMING (CN)
ZHAO HONGYANG (CN)
JIANG ZHUOCHENG (CN)
ZHAO HONGYANG (CN)
JIANG ZHUOCHENG (CN)
Application Number:
CN2019/084492
Publication Date:
October 29, 2020
Filing Date:
April 26, 2019
Export Citation:
Assignee:
UNIV DALIAN TECH (CN)
International Classes:
B64C29/00; B60F5/02; B64C27/28
Foreign References:
CN107639984A | 2018-01-30 | |||
CN109263954A | 2019-01-25 | |||
CN209290683U | 2019-08-23 | |||
CN207772810U | 2018-08-28 | |||
CN105460214A | 2016-04-06 | |||
EP0384965A2 | 1990-09-05 | |||
US20170036753A1 | 2017-02-09 |
Download PDF: