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1. (WO2017038809) FLIGHT POSITION CONTROL DEVICE
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Pub. No.: WO/2017/038809 International Application No.: PCT/JP2016/075305
Publication Date: 09.03.2017 International Filing Date: 30.08.2016
Chapter 2 Demand Filed: 18.01.2017
IPC:
B64F 3/00 (2006.01) ,B64C 27/08 (2006.01) ,B64C 39/02 (2006.01) ,B64D 27/24 (2006.01) ,G05D 1/08 (2006.01) ,B64D 47/08 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
F
GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS
3
Ground installations specially adapted for captive aircraft
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
27
Rotorcraft; Rotors peculiar thereto
04
Helicopters
08
with two or more rotors
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
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
G PHYSICS
05
CONTROLLING; REGULATING
D
SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
1
Control of position, course, altitude, or attitude of land, water, air, or space vehicles, e.g. automatic pilot
08
Control of attitude, i.e. control of roll, pitch, or yaw
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
Applicants:
株式会社プロドローン PRODRONE CO., LTD. [JP/JP]; 愛知県名古屋市中区新栄町二丁目4番地 坂種栄ビル16階 16F Bantane Sakae Building, 2-4, Shinsakae-machi, Naka-ku, Nagoya-shi, Aichi 4600004, JP
Inventors:
市原 和雄 ICHIHARA, Kazuo; JP
菅木 紀代一 SUGAKI, Kiyokazu; JP
Agent:
特許業務法人上野特許事務所 WENO & PARTNERS; 愛知県名古屋市中区栄三丁目21番23号ケイエスイセヤビル8階 KS Iseya Building 8th Floor, 21-23, Sakae 3-chome, Naka-ku, Nagoya-shi, Aichi 4600008, JP
Priority Data:
2015-17462004.09.2015JP
Title (EN) FLIGHT POSITION CONTROL DEVICE
(FR) DISPOSITIF DE COMMANDE DE POSITION DE VOL
(JA) 滞空位置制御装置
Abstract:
(EN) Provided is a flight position control device that can cause a drone having a plurality of rotary wings to quickly move to a prescribed position in a space, and cause the airframe to hover stably in that position. The flight position control device is characterized by being provided with a drone having a plurality of rotary wings, a fixed surface from and on which the drone takes off and lands, and a plurality of cord-shaped members connecting the drone and the fixed surface, all of the plurality of cord-shaped members being long enough to become taut when the drone has reached a designated position which is a prescribed position in a space. The plurality of cord-shaped members preferably include at least three of said cord-shaped members.
(FR) L'invention concerne un dispositif de commande de position de vol qui peut amener un drone comportant une pluralité d'ailes rotatives à se déplacer rapidement jusqu'à une position prédéterminée dans un espace, et amener la cellule à effectuer un vol stationnaire stable dans cette position. Le dispositif de commande de position de vol est caractérisé par le fait qu'il comprend un drone comportant une pluralité d'ailes rotatives, une surface fixe à partir de laquelle le drone décolle et sur laquelle il atterrit, une pluralité d'éléments en forme de corde reliant le drone et la surface fixe, tous les éléments de la pluralité d'éléments en forme de corde étant suffisamment longs pour se tendre lorsque le drone a atteint une position désignée qui est une position prédéterminée dans un espace. La pluralité d'éléments en forme de corde comprend de préférence au moins trois desdits éléments en forme de corde.
(JA) 複数の回転翼を備える小型無人飛行機を空間中の所定位置に速やかに移動させ、機体をその位置で安定してホバリング飛行させることを可能とする滞空位置制御装置を提供する。 複数の回転翼を備える小型無人飛行機と、前記小型無人飛行機が離着陸する固定面と、前記小型無人飛行機と前記固定面とを連結する複数の紐状部材と、を備え、前記複数の紐状部材は、前記小型無人飛行機が空間中の所定の位置である指定位置に至ったときに、すべてが緊張状態となる長さであることを特徴とする滞空位置制御装置により解決する。また、前記複数の紐状部材は少なくとも3本の前記紐状部材を有することが好ましい。
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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, KR, 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)