Processing

Please wait...

PATENTSCOPE will be unavailable a few hours for maintenance reason on Saturday 31.10.2020 at 7:00 AM CET
Settings

Settings

Goto Application

1. WO2019046911 - UNMANNED AERIAL VEHICLE

Publication Number WO/2019/046911
Publication Date 14.03.2019
International Application No. PCT/AU2018/050984
International Filing Date 11.09.2018
IPC
B64C 39/02 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64C 27/08 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
F42B 15/00 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
42AMMUNITION; BLASTING
BEXPLOSIVE CHARGES, e.g. FOR BLASTING; FIREWORKS; AMMUNITION
15Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
CPC
B60W 2050/007
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
WCONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION; CONTROL SYSTEMS SPECIALLY ADAPTED FOR HYBRID VEHICLES; ROAD VEHICLE DRIVE CONTROL SYSTEMS FOR PURPOSES NOT RELATED TO THE CONTROL OF A PARTICULAR SUB-UNIT
50Details of control systems for road vehicle drive control not related to the control of a particular sub-unit ; , e.g. process diagnostic or vehicle driver interfaces
0062Adapting control system settings
007Switching between manual and automatic parameter input, and vice versa
B64C 1/063
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
06Frames; Stringers; Longerons ; ; Fuselage sections
061Frames
063Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms
B64C 1/30
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
30Parts of fuselage relatively movable to reduce overall size for storage
B64C 2201/027
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
02characterized by type of aircraft
027Flying platforms
B64C 2201/08
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
08characterised by the launching method
B64C 2201/084
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
08characterised by the launching method
084using catapults
Applicants
  • DEFENDTEX PTY LTD [AU]/[AU]
Inventors
  • REDDY, Travis
  • CAHILL, Damien
Agents
  • PHILLIPS ORMONDE FITZPATRICK
Priority Data
15/700,43611.09.2017US
201722852511.09.2017AU
Publication Language English (EN)
Filing Language English (EN)
Designated States
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.
Also published as
Latest bibliographic data on file with the International Bureau