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1. (WO2017034359) UNMANNED FLYING OBJECT CAPABLE OF FLYING WITHOUT PROPELLER
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Pub. No.: WO/2017/034359 International Application No.: PCT/KR2016/009474
Publication Date: 02.03.2017 International Filing Date: 26.08.2016
IPC:
B64C 39/02 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
Applicants:
광주과학기술원 GWANGJU INSTITUTE OF SCIENCE AND TECHNOLOGY [KR/KR]; 광주시 북구 첨단과기로 123 (오룡동) 123 Cheomdan-gwagiro (Oryong-dong), Buk-gu Gwangju 61005, KR
Inventors:
강성모 KANG, Sung Mo; KR
안효성 AHN, Hyo Sung; KR
최영철 CHOI, Young Cheol; KR
이병훈 LEE, Byung Hun; KR
손지환 SON, Ji Hwan; KR
고귀한 KO, Gwi Han; KR
Agent:
김기문 KIM, Ki Moon; KR
Priority Data:
10-2015-012066527.08.2015KR
Title (EN) UNMANNED FLYING OBJECT CAPABLE OF FLYING WITHOUT PROPELLER
(FR) OBJET VOLANT SANS PILOTE POUVANT VOLER SANS HÉLICE
(KO) 프로펠러 없이 비행 가능한 무인 비행체
Abstract:
(EN) An embodiment of the present invention relates to an unmanned flying object flying according to the command of a control module, having a main body part provided at the center thereof, and comprising a plurality of driving parts which are formed to extend from the lateral side of the main body part in a horizontal direction so as to generate thrust in a downward direction, and coupled to form predetermined angles with respect to the main body part, wherein the driving part comprises: a suction part suctioning ambient air so as to generate an air flow; a compression part connected to the suction part, and varying the speed of flowing air; and an air discharge part for discharging the air having flowed through the compression part, and the air discharge part is coupled to a portion of the compression part in the horizontal direction, is formed as a cylindrical frame having an opening in a vertical direction, and has a discharge port, through which the air flowing inside the frame is exhaled in the downward direction, formed on the inner peripheral surface of the frame. In an embodiment, the flying object is manufactured in a form excluding a propeller, which is a means for generating thrust, and suctioning and discharging the air, and thus damage caused by physical injury can be reduced even if contact is made therewith because of the unskilled operation of a user during the takeoff or landing of the unmanned flying object.
(FR) Un mode de réalisation de la présente invention concerne un objet volant sans pilote selon l'instruction d'un module de commande, comportant un élément corps principal situé au centre de celui-ci, et comprenant une pluralité de parties d'entraînement qui sont formées pour s'étendre depuis le côté latéral de l'élément corps principal dans une direction horizontale de manière à produire une poussée dans une direction descendante, et accouplées pour former des angles prédéfinis par rapport à l'élément corps principal, la partie d'entraînement comprenant : un élément d'aspiration aspirant l'air ambiant de manière à produire un flux d'air; un élément de compression raccordé à l'élément d'aspiration, et faisant varier la vitesse d'air d'écoulement; et un élément d'évacuation d'air pour évacuer l'air s'étant écoulé dans l'élément de compression, et l'élément d'évacuation d'air est accouplé à une partie de l'élément de compression dans la direction horizontale, à la forme d'un cadre cylindrique ayant une ouverture dans une direction verticale, et a un orifice d'évacuation, par lequel l'air s'écoulant à l'intérieur du cadre est rejeté dans la direction descendante, formé sur la surface périphérique interne du cadre. Selon un mode de réalisation, l'objet volant est fabriqué selon une forme à l'exclusion d'une hélice, qui est un moyen pour produire une poussée, et aspirer et évacuer l'air, et ainsi les dommages causés par une blessure physique peuvent être réduits même si un contact est fait avec celui-ci en raison de la manœuvre non qualifiée d'un utilisateur pendant le décollage ou l'atterrissage de l'objet volant sans pilote.
(KO) 본 발명의 실시예는 중심에 본체부가 마련되고, 본체부의 측면에서 수평방향으로 연장 형성되어 하방향으로 추력을 발생시키며 상기 본체부를 중심으로 일정한 각도를 이루도록 결합된 복수개의 구동부로 이루어지며, 제어 모듈의 명령에 따라 비행하는 무인 비행체로서, 상기 구동부는 주변공기를 흡입하여 공기의 유동을 발생시키는 흡입부, 상기 흡입부와 연결되며 유동되는 공기의 속도를 가변시키는 압축부, 상기 압축부를 통해 유동된 공기를 방출시키는 공기배출부를 포함하고, 상기 공기배출부는 상기 압축부의 일부와 수평방향으로 결합되며 상하방향으로의 개구를 갖는 원통형의 프레임으로 형성되고, 상기 프레임의 내주면에는 상기 프레임 내부에서 유동되는 공기가 하방향으로 빠져나가는 방출구를 구비한다. 실시예는 추력을 발생시키는 수단인 프로펠러를 배제하고 공기를 흡입 및 배출하는 형태로 제작되기 때문에 무인 비행체의 이륙 또는 착륙시 사용자의 조작 미숙으로 인한 접촉이 발생하여도 신체적 상해에 의한 피해를 줄일 수 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 Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (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)