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1. (WO2017131284) JOINED-WING TYPE UNMANNED AERIAL VEHICLE
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/2017/131284 International Application No.: PCT/KR2016/002715
Publication Date: 03.08.2017 International Filing Date: 17.03.2016
IPC:
B64C 39/02 (2006.01) ,B64C 39/08 (2006.01) ,B64C 39/10 (2006.01) ,B64C 39/06 (2006.01) ,B64C 1/00 (2006.01) ,B64C 3/00 (2006.01) ,B64C 5/00 (2006.01) ,B64D 35/02 (2006.01) ,B64D 47/08 (2006.01) ,B64D 45/00 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
08
having multiple wings
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
10
All-wing aircraft
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
06
having disc- or ring-shaped wings
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
1
Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
3
Wings
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
5
Stabilising surfaces
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
35
Transmitting power from power plant to propellers or rotors; Arrangements of transmissions
02
characterised by the type of power plant
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
47
Equipment not otherwise provided for
08
Arrangements of cameras
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
45
Aircraft indicators or protectors not otherwise provided for
Applicants:
주식회사 케바드론 KEVADRONE CO., LTD. [KR/KR]; 대전시 유성구 대학로 99 충남대 산학연 교육연구관 502호 502 Foundation of University-Industry Research Collaboration Chungnam National Univ., 99, Daehak-ro Yuseong-gu Daejeon 34134, KR
Inventors:
이희우 LEE, Heewoo; KR
Agent:
안재열 AHN, Jaeyul; KR
Priority Data:
10-2016-000855625.01.2016KR
Title (EN) JOINED-WING TYPE UNMANNED AERIAL VEHICLE
(FR) VÉHICULE AÉRIEN SANS PILOTE DU TYPE À AILES RELIÉES
(KO) 조인드윙형 무인항공기
Abstract:
(EN) The present invention relates to a joined-wing type unmanned aerial vehicle. More specifically, the present invention relates to a joined-wing type unmanned aerial vehicle comprising: a fuselage; main wings formed on opposite sides of the fuselage, wherein the main wings are formed in a triangular form in which the opposite ends of the main wings are directed toward the tail of the fuselage; an upper wing connected, at opposite ends thereof, with the main wings by connecting members, wherein the upper wing is disposed above the main wings to form a joined-wing form together with the main wings; a propeller provided at the upper wing to generate a propulsive force; a vertical wing coupled with the central portion of the upper surface of the main wings and the central portion of the lower surface of the upper wing; and a rudder provided at the back of the vertical wing so as to be rotatable to control the direction. According to the present invention, the lifting force applied to the unmanned aerial vehicle can be increased by virtue of the shape of the main wings and the upper wing, thereby enabling the unmanned aerial vehicle to easily land even in a narrow space, and enhancing flight efficiency and take-off/landing performance.
(FR) La présente invention concerne un véhicule aérien sans pilote de type à ailes reliées. Plus précisément, la présente invention concerne un véhicule aérien sans pilote de type à ailes reliées comprenant : un fuselage; des ailes principales formées sur des côtés opposés du fuselage, les ailes principales étant formées dans une forme triangulaire selon laquelle les extrémités opposées des ailes principales sont dirigées vers la queue du fuselage; une aile supérieure reliée, au niveau de ses extrémités opposées, aux ailes principales par des éléments de liaison, l'aile supérieure étant disposée au-dessus des ailes principales pour réaslier une forme en ailes reliées conjointement avec les ailes principales; une hélice disposée au niveau de l'aile supérieure pour générer une force de propulsion; une aile verticale accouplée à la partie centrale de la surface supérieure des ailes principales et à la partie centrale de la surface inférieure de l'aile supérieure; et un gouvernail disposé à l'arrière de l'aile verticale de façon à pouvoir tourner pour commander la direction. Selon la présente invention, la force de levage appliquée sur le véhicule aérien sans pilote peut être augmentée en raison de la forme des ailes principales et de l'aile supérieure, permettant au véhicule aérien sans pilote d'atterrir facilement même dans un espace étroit, et améliorant l'efficacité de vol et la performance de décollage/atterrissage.
(KO) 본 발명은 조인드윙형 무인항공기에 관한 것이다. 더욱 상세하게는, 동체; 상기 동체의 양측에 형성되며, 양 끝단이 상기 동체의 선미 방향을 향하는 삼각형 형태로 이루어지는 메인윙; 양 끝단은 상기 메인윙과 연결대로 연결되며 상기 메인윙의 상부에 배치되어 상기 메인윙과 함께 조인드윙 형태를 이루는 상부윙; 상기 상부윙에 구비되며 추진력을 발생시키는 프로펠러; 상기 메인윙의 상면 중앙부 및 상기 상부윙의 하면 중앙부와 결합되는 수직날개; 및 상기 수직날개의 후미에 회동 가능하게 구비되어 방향을 조절하는 방향타를 포함하는 것을 특징으로 한다. 본 발명에 의하면, 메인윙 및 상부윙의 형상에 의해 양력이 향상되어 좁은 공간에서도 용이하게 착륙할 수 있고, 비행 효율 및 이착륙 성능을 향상시킬 수 있는 효과가 있다.
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JP, KE, KG, KN, KP, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: Korean (KO)
Filing Language: Korean (KO)