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1. (WO2018218370) UNMANNED AERIAL VEHICLE WITH SYNCHRONIZED SENSOR NETWORK
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Pub. No.: WO/2018/218370 International Application No.: PCT/CA2018/050657
Publication Date: 06.12.2018 International Filing Date: 01.06.2018
IPC:
B64C 17/00 (2006.01) ,B64C 13/30 (2006.01) ,B64C 3/38 (2006.01) ,B64C 31/032 (2006.01) ,B64C 39/02 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
17
Aircraft stabilisation not otherwise provided for
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
24
Transmitting means
26
without power amplification or where power amplification is irrelevant
28
mechanical
30
using cable, chain, or rod mechanisms
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
3
Wings
38
Adjustment of complete wings or parts thereof
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
31
Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
028
Hang-glider-type aircraft; Microlight-type aircraft
032
having delta shaped wing
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
Applicants:
ROMAERIS CORPORATION [CA/CA]; 1183 Newmarket Street, Unit M Ottawa, Ontario K1B 3V1, CA
Inventors:
PIZARRO, Anthony F.; CA
DOERWALD, Bruno C.; CA
Agent:
RIDOUT & MAYBEE LLP; 11 Holland Avenue, Suite 601 Ottawa, Ontario K1Y 4S1, CA
Priority Data:
62/513,67501.06.2017US
Title (EN) UNMANNED AERIAL VEHICLE WITH SYNCHRONIZED SENSOR NETWORK
(FR) VÉHICULE AÉRIEN SANS PILOTE POURVU D'UN RÉSEAU DE CAPTEURS SYNCHRONISÉS
Abstract:
(EN) Disclosed is an aircraft and a method of controlling an aircraft. The aircraft comprises a continuous wing assembly extending from port to starboard sides of the aircraft. The aircraft is controlled partially by flexing portions of the wing, and partially or totally by mechanical systems that alter the position of a fuselage with respect to the wing. The fuselage is attached to the wing by a wing/fuselage joint structure that permits at least two mutually orthogonal axes of rotation of the fuselage relative to the wing. The aircraft includes a sensors, a telemetry system linked to a remote server, and a control system for programming flight information and aircraft control instructions and a plurality of actuators responsive to the control system for rotating the fuselage relative to the wing and flexing the wing for controlling the flight of the aircraft in response to instructions from the control system.
(FR) L'invention concerne un aéronef et un procédé de commande d'un aéronef. L'aéronef comprend un ensemble aile continue s'étendant depuis le côté bâbord vers le côté tribord de l'aéronef. L'aéronef est commandé partiellement par des parties de flexion de l'aile et partiellement ou totalement par des systèmes mécaniques qui modifient la position d'un fuselage par rapport à l'aile. Le fuselage est fixé à l'aile par une structure d'articulation aile/fuselage qui offre au moins deux axes de rotation mutuellement orthogonaux du fuselage par rapport à l'aile. L'aéronef comprend des capteurs, un système de télémesure relié à un serveur distant et un système de commande permettant de programmer des informations de vol et des instructions de commande d'aéronef et comprend une pluralité d'actionneurs répondant au système de commande permettant de faire tourner le fuselage par rapport à l'aile et faire fléchir l'aile pour commander le vol de l'aéronef en réponse à des instructions provenant du système de commande.
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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: English (EN)
Filing Language: English (EN)