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1. (WO2014108459) AERODYNAMIC MULTICOPTER / QUADROCOPTER
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/2014/108459 International Application No.: PCT/EP2014/050280
Publication Date: 17.07.2014 International Filing Date: 09.01.2014
IPC:
B64C 27/20 (2006.01) ,A63H 27/00 (2006.01) ,B64C 39/02 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
27
Rotorcraft; Rotors peculiar thereto
20
Rotorcraft characterised by having shrouded rotors, e.g. flying platforms
A HUMAN NECESSITIES
63
SPORTS; GAMES; AMUSEMENTS
H
TOYS, e.g. TOPS, DOLLS, HOOPS, BUILDING BLOCKS
27
Toy aircraft; Other flying toys
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
Applicants:
MICRODRONES GMBH [DE/DE]; Gutenbergstraße 86 57078 Siegen, DE
Inventors:
SCHÜBELER, Daniel; DE
JÜRß, Sven; DE
Agent:
ISFORT, Olaf; Scheiders & Behrendt Huestraße 23 44787 Bochum, DE
Priority Data:
10 2013 000 168.409.01.2013DE
Title (DE) AERODYNAMISCHER MULTIKOPTER / QUADROKOPTER
(EN) AERODYNAMIC MULTICOPTER / QUADROCOPTER
(FR) MULTICOPTER/QUADCOPTER AÉRODYNAMIQUE
Abstract:
(DE) Die Erfindung betrifft eine Drohne (1) umfassend zumindest vier Rotoren (2, 3, 4, 5) und einen aerodynamisch geformten Rumpf (6), wobei zumindest zwei Rotoren (2, 3) entlang einer Längsachse des Rumpfs (6) und zumindest zwei Rotoren (4, 5) entlang einer Querachse des Rumpfs (6) angeordnet sind, wobei der entlang der Längsachse in Flugrichtung angebrachte Rotor (2) in einem ersten Abstand, die Rotoren (4, 5) entlang der Querachse in einem zweiten Abstand und der entlang der Längsachse entgegen der Flugrichtung angebrachte Rotor (3) in einem dritten Abstand zum Rumpf (6) entlang einer Hochachse vorgesehen ist. Insbesondere sind die Rotoren (2, 3, 4, 5) in einer in Bezug auf die Hochachse geneigten Ebene und in Flugrichtung von vorne nach hinten in absteigender Höhe angeordnet.
(EN) The invention relates to a drone (1) comprising at least four rotors (2, 3, 4, 5) and an aerodynamically shaped fuselage (6), wherein at least two rotors (2, 3) are arranged along a longitudinal axis of the fuselage (6) and at least two rotors (4, 5) are arranged along a transverse axis of the fuselage (6), wherein the rotor (2) that is installed along the longitudinal axis in the direction of flight is provided at a first distance from the fuselage (6) along a vertical axis, the rotors (4, 5) along the transverse axis are provided at a second distance from the fuselage (6) along a vertical axis, and the rotor (3) that is installed along the longitudinal axis counter to the direction of flight is provided at a third distance from the fuselage (6) along a vertical axis. In particular, the rotors (2, 3, 4, 5) are arranged in a plane which is inclined relative to the vertical axis and in decreasing height from front to rear as viewed in the direction of flight.
(FR) L'invention concerne un drone (1) comprenant au moins quatre rotors (2, 3, 4, 5) et un fuselage formé aérodynamique (6), au moins deux rotors (2, 3) étant disposés le long d'un axe longitudinal du fuselage (6), et au moins deux rotors (4, 5) étant disposés le long d'un axe transversal du fuselage (6), le rotor (2), monté le long de l'axe longitudinal, dans la direction du vol, étant prévu dans une première distance, les rotors (4, 5) le long de l'axe transversal, étant prévus dans une deuxième distance, et le rotor (3), monté le long de l'axe longitudinal, à l'encontre de la direction du vol, étant prévu, le long d'un axe vertical, dans une troisième distance par rapport au fuselage (6). En particulier, les rotors (2, 3, 4, 5) sont disposés dans un plan incliné, par rapport à l'axe vertical, et en direction du vol, de l'avant vers l'arrière, à une hauteur décroissante.
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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, LT, 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, 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: German (DE)
Filing Language: German (DE)