Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
VERTICAL TAKE-OFF AND LANDING AIRCRAFT AND TRANSITION METHOD THEREFOR
Document Type and Number:
WIPO Patent Application WO/2018/155739
Kind Code:
A1
Abstract:
A vertical take-off and landing aircraft and a transition method therefor are disclosed. The vertical take-off and landing aircraft comprises: a flight fuselage including a front wing part and a rear wing part; a plurality of tilting propellers respectively provided at a left wing part and a right wing part of the front wing part; a plurality of tilting propellers provided at the rear wing part; and a control part for independently controlling operations of the propellers of the front wing part and the rear wing part.

More Like This:
JP7342250Hybrid power system for different flight modes
WO/2021/233573AIRCRAFT HAVING A DUCTED FAN IN THE AIRFOIL
WO/2016/137362TWO AIRCRAFT FORMING AN AEROPLANE FUSELAGE THAT SEPARATES INTO TWO SELF-CONTAINED AIRCRAFT
Inventors:
KIM DOHYUN (KR)
JANG JINHAN (KR)
Application Number:
PCT/KR2017/002064
Publication Date:
August 30, 2018
Filing Date:
February 24, 2017
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
KOREA FUSION TECHNIQUE COOP (KR)
International Classes:
B64C29/00
Foreign References:
US20160031555A12016-02-04
US5419514A1995-05-30
KR20160070033A2016-06-17
KR20070100092A2007-10-10
KR20140058854A2014-05-15
Attorney, Agent or Firm:
HA, Dongyeop (KR)
Download PDF:
View/Download PDF      PDF Help



 
Previous Patent: QUANTUM NOISE-BASED RANDOM NUMBER GENERATION DEVICE USING MULTIPLE LIGHT SOURCES

Next Patent: WEARABLE MIST SPRAYING DEVICE