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1. (WO2019046911) UNMANNED AERIAL VEHICLE
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Pub. No.: WO/2019/046911 International Application No.: PCT/AU2018/050984
Publication Date: 14.03.2019 International Filing Date: 11.09.2018
IPC:
B64C 39/02 (2006.01) ,B64C 27/08 (2006.01) ,F42B 15/00 (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
27
Rotorcraft; Rotors peculiar thereto
04
Helicopters
08
with two or more rotors
F MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
42
AMMUNITION; BLASTING
B
EXPLOSIVE CHARGES, e.g. FOR BLASTING; FIREWORKS; AMMUNITION
15
Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
Applicants:
DEFENDTEX PTY LTD [AU/AU]; 442-446 Victoria Street North Melbourne, Victoria 3051, AU
Inventors:
REDDY, Travis; AU
CAHILL, Damien; AU
Agent:
PHILLIPS ORMONDE FITZPATRICK; Level 16 333 Collins Street Melbourne, Victoria 3000, AU
Priority Data:
15/700,43611.09.2017US
201722852511.09.2017AU
Title (EN) UNMANNED AERIAL VEHICLE
(FR) VÉHICULE AÉRIEN SANS PILOTE
Abstract:
(EN) An unmanned aerial vehicle (UAV) adapted for transit in and deployment from a projectile casing is provided. The UAV includes a wing assembly coupled to the projectile casing and the wing assembly moveable between a closed position and a deployed position. The UAV further includes a propulsion system including at least one rotor disposed on the wing assembly to generate lift, wherein in the closed position, the wing assembly is substantially integral with the projectile casing and in the deployed position, the wing assembly is extended outwards from the projectile casing.
(FR) L'invention concerne un véhicule aérien sans pilote (UAV) conçu pour être transporté dans un boîtier de projectile et pour être déployé à partir de ce dernier. L'UAV comprend un ensemble aile accouplé au boîtier de projectile et l'ensemble aile peut passer d'une position fermée à une position déployée et inversement. L'UAV comprend en outre un système de propulsion comprenant au moins un rotor disposé sur l'ensemble aile pour produire une portance. Dans la position fermée, l'ensemble aile fait sensiblement corps avec le boîtier de projectile et dans la position déployée, l'ensemble aile est étendu vers l'extérieur à partir du boîtier de projectile.
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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)