Title:
TAILSITTER AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2020/183739
Kind Code:
A1
Abstract:
A tailsitter aircraft 100 provided with a body 120, two pairs of horizontal main wings 30a, 30b, 30c, and 30d when viewed from the front, each connected to the body 120, and eight propellers 50a, 50b, 50c, 50d, 60a, 60b, 60c, and 60d that are provided on the two pairs of horizontal main wings 30a, 30b, 30c, and 30d and serve to provide lift or propulsion, wherein the body 120 has an interior space 134 therein and the interior space 134 is provided with a seat 132 that tilts according to the attitude of the vehicle. The seat 132 preferably tilts such that the line of sight of a person on board is directed to the horizontal direction. The tailsitter aircraft 100 can reduce the burden on the person on board when he/she pilots the vehicle.
More Like This:
| WO/2003/022630 | VERTCAL TAKE-OFF AND LANDING VEHICLE FOR LAND, WATER AND AIR TRANSPORT |
| JP2008075582 | PROPELLING SYSTEM FOR V/STOL AIRCRAFT |
| WO/2018/048565 | TILTROTOR PROPULSION SYSTEM FOR AN AIRCRAFT |
Inventors:
OHASHI TOSHIO (JP)
Application Number:
PCT/JP2019/011951
Publication Date:
September 17, 2020
Filing Date:
March 21, 2019
Export Citation:
Assignee:
IND NETWORK CO LTD (JP)
International Classes:
B64C29/00
Foreign References:
| US20160144957A1 | 2016-05-26 | |||
| US20180002011A1 | 2018-01-04 | |||
| JP2007527161A | 2007-09-20 | |||
| JPH11237582A | 1999-08-31 | |||
| JP2016517821A | 2016-06-20 |
Attorney, Agent or Firm:
MEBUKI IP LAW FIRM (JP)
Download PDF:
Previous Patent: XNOR GATE AND BINARY CONVOLUTION CIRCUIT
Next Patent: MINIMALLY-INVASIVE SURGERY EQUIPMENT
Next Patent: MINIMALLY-INVASIVE SURGERY EQUIPMENT