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Patent Searching and Data


Title:
VERTICAL TAKEOFF AND LANDING AIRCRAFT USING HYBRID ELECTRIC PROPULSION SYSTEM AND CONTROL METHOD THEREFOR
Document Type and Number:
WIPO Patent Application WO/2020/096254
Kind Code:
A1
Abstract:
A vertical takeoff and landing aircraft using a hybrid electric propulsion system and a control method therefor according to an embodiment of the present invention can: perform control such that, during vertical takeoff and landing of an aircraft (1), a generator (20), a power management device (4), and a battery management system (60) simultaneously provide power to a motor (80); and perform control such that, during a cruise flight or transition flight of the aircraft (1), the thrust of a second propeller (82) is increased and a battery (62) of the battery management system (60) is charged with redundant power generated by the generator (20).

Inventors:
MOON CHANG MO (KR)
MOON JI HO (KR)
Application Number:
PCT/KR2019/014336
Publication Date:
May 14, 2020
Filing Date:
October 29, 2019
Export Citation:
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Assignee:
MOON CHANG MO (KR)
MOON JI HO (KR)
International Classes:
B64D27/02; B64C11/46; B64C29/00; B64D31/00; B64D35/00; B64D41/00
Foreign References:
KR101667330B12016-10-19
KR20180116849A2018-10-26
KR20170135577A2017-12-08
KR20150058197A2015-05-28
KR102004227B12019-07-30
KR20110112402A2011-10-12
KR101667330B12016-10-19
KR101615486B12016-04-26
KR101638964B12016-07-13
Other References:
See also references of EP 3878752A4
Attorney, Agent or Firm:
CHOI, Seung Wook (KR)
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