FR3071480B1 - AIR VEHICLE CAPABLE OF VERTICAL TAKEOFF AND LANDING, VERTICAL AND HORIZONTAL FLIGHT AND IN-FLIGHT ENERGY PRODUCTION - Google Patents

AIR VEHICLE CAPABLE OF VERTICAL TAKEOFF AND LANDING, VERTICAL AND HORIZONTAL FLIGHT AND IN-FLIGHT ENERGY PRODUCTION Download PDF

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Publication number
FR3071480B1
FR3071480B1 FR1853109A FR1853109A FR3071480B1 FR 3071480 B1 FR3071480 B1 FR 3071480B1 FR 1853109 A FR1853109 A FR 1853109A FR 1853109 A FR1853109 A FR 1853109A FR 3071480 B1 FR3071480 B1 FR 3071480B1
Authority
FR
France
Prior art keywords
main
tail
tilt
vertical
wings
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
FR1853109A
Other languages
French (fr)
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FR3071480A1 (en
Inventor
Dong Soo Har
Sang Min Lee
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Korea Advanced Institute of Science and Technology KAIST
Original Assignee
Korea Advanced Institute of Science and Technology KAIST
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from KR1020170125497A external-priority patent/KR20180076278A/en
Priority claimed from KR1020170179808A external-priority patent/KR20180076348A/en
Application filed by Korea Advanced Institute of Science and Technology KAIST filed Critical Korea Advanced Institute of Science and Technology KAIST
Publication of FR3071480A1 publication Critical patent/FR3071480A1/en
Application granted granted Critical
Publication of FR3071480B1 publication Critical patent/FR3071480B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/385—Variable incidence wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00—Type of UAV
    • B64U10/25—Fixed-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/10—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U30/00—Means for producing lift; Empennages; Arrangements thereof
    • B64U30/20—Rotors; Rotor supports
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/13—Propulsion using external fans or propellers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/10—Propulsion
    • B64U50/19—Propulsion using electrically powered motors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U50/00—Propulsion; Power supply
    • B64U50/30—Supply or distribution of electrical power
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Abstract

Un véhicule aérien comprend : un corps principal agencé dans une première direction ; deux ailes principales disposées par rapport au corps principal dans une deuxième direction sensiblement perpendiculaire à la première direction, les deux ailes principales étant agencées de manière opposée l'une par rapport à l'autre ; deux unités de commande d'inclinaison d'aile principale couplées respectivement aux ailes principales et adaptées pour commander les ailes principales pour qu'elles s'inclinent indépendamment l'une de l'autre ; deux unités de propulsion principales agencées respectivement sur les ailes principales ; des ailes de queue agencées sur un côté arrière du corps principal dans les deuxième et troisième directions sensiblement perpendiculaires à la première direction ; une gouverne de direction agencée sur l'aile arrière de la troisième direction ; une unité de commande d'inclinaison de gouverne de direction adaptée pour commander l'inclinaison de la gouverne de direction ; une unité de propulsion de queue agencée sur le côté arrière du corps principal ; une unité de commande d'inclinaison de queue adaptée pour commander l'inclinaison de l'unité de propulsion de queue ; une unité de puissance adaptée pour fournir de la puissance aux unités de propulsion principales et de queue; et une unité de commande de position adaptée pour commander les unités de commande d'inclinaison d'aile principale, les unités de propulsion principales, l'unité de commande d'inclinaison de gouverne de direction, l'unité de propulsion de queue et l'unité de commande d'inclinaison de queue, pour ajuster la position du véhicule aérien tandis qu'il est en l'air.An aerial vehicle comprises: a main body arranged in a first direction; two main wings arranged relative to the main body in a second direction substantially perpendicular to the first direction, the two main wings being arranged opposite to each other; two main wing tilt control units respectively coupled to the main wings and adapted to control the main wings to tilt independently of each other; two main propulsion units arranged respectively on the main wings; tail wings arranged on a rear side of the main body in the second and third directions substantially perpendicular to the first direction; a rudder arranged on the rear wing of the third direction; a rudder tilt control unit adapted to control the tilt of the rudder; a tail propulsion unit arranged on the rear side of the main body; a tail tilt control unit adapted to control the tilt of the tail propulsion unit; a power unit adapted to supply power to the main and tail propulsion units; and a position control unit adapted to control the main wing tilt control units, the main propulsion units, the rudder tilt control unit, the tail propulsion unit and the Tail tilt control unit, to adjust the position of the air vehicle while it is in the air.

FR1853109A 2017-09-27 2018-04-10 AIR VEHICLE CAPABLE OF VERTICAL TAKEOFF AND LANDING, VERTICAL AND HORIZONTAL FLIGHT AND IN-FLIGHT ENERGY PRODUCTION Active FR3071480B1 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
KR1020170125497A KR20180076278A (en) 2016-12-27 2017-09-27 An aircraft capable of vertical take-off and landing, vertical and horizontal flight and on-air energy generation
KR1020170125497 2017-09-27
KR1020170179808 2017-12-26
KR1020170179808A KR20180076348A (en) 2016-12-27 2017-12-26 An aircraft capable of vertical take-off and landing, vertical and horizontal flight and on-air energy generation

Publications (2)

Publication Number Publication Date
FR3071480A1 FR3071480A1 (en) 2019-03-29
FR3071480B1 true FR3071480B1 (en) 2021-05-28

Family

ID=65859711

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1853109A Active FR3071480B1 (en) 2017-09-27 2018-04-10 AIR VEHICLE CAPABLE OF VERTICAL TAKEOFF AND LANDING, VERTICAL AND HORIZONTAL FLIGHT AND IN-FLIGHT ENERGY PRODUCTION

Country Status (1)

Country Link
FR (1) FR3071480B1 (en)

Also Published As

Publication number Publication date
FR3071480A1 (en) 2019-03-29

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