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1. (WO2019049313) AERIAL VEHICLE
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Pub. No.: WO/2019/049313 International Application No.: PCT/JP2017/032477
Publication Date: 14.03.2019 International Filing Date: 08.09.2017
IPC:
B64C 39/02 (2006.01) ,B64C 13/20 (2006.01) ,B64D 27/24 (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
13
Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
02
Initiating means
16
actuated automatically, e.g. responsive to gust detectors
20
using radiated signals
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
27
Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02
Aircraft characterised by the type or position of power plant
24
using steam, electricity, or spring force
Applicants:
株式会社アガツマ AGATSUMA CO., LTD. [JP/JP]; 東京都台東区浅草橋3丁目19番4号 3-19-4, Asakusabashi, Taito-ku Tokyo 1118524, JP
Inventors:
戸所 信二 TODOKORO Shinji; JP
Agent:
特許業務法人コスモ国際特許事務所 COSMO INTERNATIONAL PATENT FIRM; 東京都中央区日本橋富沢町10-14 日本橋BSビル3階 3F, Nihonbashi BS Bldg., 10-14, Nihonbashi-Tomizawa-cho, Chuo-ku, Tokyo 1030006, JP
Priority Data:
Title (EN) AERIAL VEHICLE
(FR) VÉHICULE AÉRIEN
(JA) 飛行体
Abstract:
(EN) [Problem] To provide an aerial vehicle having improved responsiveness during transportation. [Solution] An aerial vehicle 1 includes: a fixed rotor 20b (20) that supports a first rotary wing 50b so as to allow rotation thereof; a movable rotor 30d (30) that supports a second rotary wing 50d so as to allow rotation thereof; and a driving unit that changes the angle of a second rotation plane Pf of the second rotary wing 50d with respect to a first rotation plane Pf of the first rotary wing 50b by pivoting the movable rotor 30d (30). The driving unit of the aerial vehicle 1 switches among a normal traveling mode in which the first rotation plane Pf and the second rotation plane Pr are parallel, a high-speed flight mode in which the second rotation plane Pr is inclined with respect to the first rotation plane Pf toward the first rotary wing 50b, and a high-speed running mode in which the second rotation plane Pr is inclined further toward the first rotary wing 50b with respect to the first rotation plane Pf than in the high-speed flight mode.
(FR) Le problème décrit par la présente invention est d'obtenir un véhicule aérien ayant une réactivité améliorée pendant le transport. La solution selon l'invention porte sur un véhicule aérien (1) qui comprend : un rotor fixe (20b) (20) qui porte une première aile rotative (50b) de façon à permettre sa rotation ; un rotor mobile (30d) (30) qui porte une seconde aile rotative (50d) de façon à permettre sa rotation ; et une unité d'entraînement qui modifie l'angle d'un second plan de rotation (Pf) de la seconde aile rotative (50d) par rapport à un premier plan de rotation (Pf) de la première aile rotative (50b) en faisant pivoter le rotor mobile (30d) (30). L'unité d'entraînement du véhicule aérien (1) alterne entre un mode de déplacement normal dans lequel le premier plan de rotation (Pf) et le second plan de rotation (Pr) sont parallèles, un mode de vol à grande vitesse dans lequel le second plan de rotation (Pr) est incliné par rapport au premier plan de rotation (Pf) vers la première aile rotative (50b), et un mode de fonctionnement à grande vitesse dans lequel le second plan de rotation (Pr) est incliné davantage vers la première aile rotative (50b) par rapport au premier plan de rotation (Pf) que dans le mode de vol à grande vitesse.
(JA) 【課題】移動時の応答性を向上させた飛行体を提供すること。 【解決手段】飛行体1は、第1回転翼50bを回転可能に支持する固定ロータ20b(20)と、第2回転翼50dを回転可能に支持する可動ロータ30d(30)と、第1回転翼50bの第1回転面Pfに対する第2回転翼50dの第2回転面Pfの角度を、可動ロータ30d(30)を回動させて切り換える駆動部と、を備える。飛行体1の駆動部は、第1回転面Pfと第2回転面Prとを平行にする通常移動モードと、第1回転面Pfに対して第2回転面Prを第1回転翼側50bへ傾斜させる高速飛行モードと、第1回転面Pfに対して第2回転面Prを高速飛行モードよりもさらに第1回転翼50bへ傾斜させる高速走行モードと、を切り換える。
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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, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, 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: Japanese (JA)
Filing Language: Japanese (JA)