Title:
A NOVEL AIRCRAFT DESIGN USING TANDEM WINGS AND A DISTRIBUTED PROPULSION SYSTEM
Document Type and Number:
WIPO Patent Application WO/2020/243364
Kind Code:
A3
Abstract:
The subject matter described herein relates to aircraft designs and more particularly to aircraft designs using tandem wings and a distributed propulsion system. The embodiments described enable synergies between aerodynamics, propulsion, structure, and stability/control. In one embodiment, the tandem wings include a first wing set and a second wing set, each having a wing span with a set of thrustors placed along the wing spans.
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Inventors:
HOSSEINI KAVEH (US)
Application Number:
PCT/US2020/034997
Publication Date:
January 07, 2021
Filing Date:
May 28, 2020
Export Citation:
Assignee:
CRAFT AEROSPACE TECH INC (US)
International Classes:
B64C39/06; B64C1/24; B64C3/16; B64C5/06; B64C11/00; B64C29/00; B64C39/04
Domestic Patent References:
| WO2016135697A1 | 2016-09-01 |
Foreign References:
| US20160207625A1 | 2016-07-21 | |||
| CN105035306A | 2015-11-11 | |||
| US20200269980A1 | 2020-08-27 | |||
| US20060151666A1 | 2006-07-13 | |||
| US20150266571A1 | 2015-09-24 |
Attorney, Agent or Firm:
LIU, Joseph K. (US)
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