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Matches 1 - 50 out of 70,356

Document Document Title
WO/2020/234580A1
A device (10) for spraying a fluid onto a target (14) is provided. The device comprises: a container (16) configured to hold the fluid; a spray nozzle (18) in fluid communication with the container and configured to spray the fluid onto ...  
WO/2020/234336A1
The invention relates to a system for automatically adapting operating parameters of an on-board kitchen facility (4) according to provided supply items (5) for on-board catering in a vehicle, in particular an aircraft (100), comprising ...  
WO/2020/234080A1
The invention relates to a vehicle seat (1) comprising at least: - a seat support structure (2) which is adjustable between an initial upright position (P1) and at least a fully inclined position (P2), - a track assembly (3) configured t...  
WO/2020/234427A1
A device includes hauling means for the movement of a payload while suspended from one or more lines. The or each line is suspended or suspendable from one end, the hauling means being provided at or in the region of the other end of the...  
WO/2020/232645A1
An unmanned aerial vehicle, comprising a center body (10), multiple mechanical arms (20), multiple electric motors (30), multiple propellers, and multiple antennas (50). The multiple mechanical arms (20) are rotatably connected to the ce...  
WO/2020/235834A1
An airfield bird strike system using a robot drone according to the present invention comprises: an SSR secondary surveillance radar for monitoring an aircraft; an ASDE ground surveillance radar for monitoring an aircraft; and a drone wh...  
WO/2020/232585A1
A quick-release connection assembly, a power assembly, a power kit and an unmanned aerial vehicle. The quick-release connection assembly comprises a mounting base for mounting propellers (10) and a locking member (21) for locking the pro...  
WO/2020/233608A1
A dragonfly-like miniature four-winged ornithopter, comprising: an airframe (101), two front flapping wings (102), two front wing connection members (103) with connecting rods, two rear flapping wings (104), two rear wing connection memb...  
WO/2020/232626A1
Provided in the present application is an unmanned aerial vehicle, comprising a central body, a plurality of arms, a plurality of motors, a plurality of propellers, and a plurality of antennae, the plurality of arms being connected to th...  
WO/2020/233132A1
The present application provides an unmanned aerial vehicle component. The component has a waterproof function and is configured to prevent unmanned aerial vehicle parts in the component from contacting water; the component comprises a f...  
WO/2020/235595A1
This aircraft member joining structure employs a joining tool to join a first plate and a second plate in an overlapping state. The first plate includes a first insertion hole, and a first serration formed around the first insertion hole...  
WO/2020/235161A1
Provided is an image processing system capable of detecting the location of an unmanned mobile body and measuring the timing when the unmanned mobile body passed a predetermined location. An image processing system S is provided with: ...  
WO/2020/233290A1
A dual-filter-based transfer alignment method under dynamic deformation. A dynamic deformation angle generated under dynamic deformation and a coupling angle between dynamic deformation and body motion will reduce the accuracy of transfe...  
WO/2020/237082A1
A vertical take-off and landing aircraft which uses fixed rotors for both VTOL and forward flight operations. The rotors form a synthetic wing and are positioned to achieve a high span efficiency. The rotors are positioned to even out th...  
WO/2020/233682A1
The present invention relates to the technical field of unmanned aerial vehicles. Particularly disclosed are an autonomous circling photographing method and apparatus and an unmanned aerial vehicle. The unmanned aerial vehicle comprises ...  
WO/2020/234591A1
The present invention relates to a multi-modal vehicle (2) operable in a first mode as a fixed wing aircraft and reconfigurable to be operable in a second mode as a ground vehicle. The vehicle comprises first (12) and second ends (14) co...  
WO/2020/236015A1
In one aspect the invention provides a method of processing electromagnetic scanning machine data. This method starts with receiving a scan data set generated by an electromagnetic scanning machine scanning an object. Also received is ei...  
WO/2020/234014A1
The present invention relates to a spray unit (10), comprising an axle (20), a body (30), and a plurality of blades (40). The axle is configured to rotate about an axis that extends in a longitudinal direction of the axle. The body is co...  
WO/2020/236485A1
An aircraft door latch apparatus includes a stowage bin assembly having a door (12) that is rotatably moveable between open and closed positions, and a frame structure (13). The aircraft apparatus includes a latch apparatus (11) that is ...  
WO/2020/234564A1
An airborne redirection unit (ARU), for deflecting an RF energy beam, the ARU comprising: A canopy comprising a surface for slowing the rate of descent, A beam director supported at the canopy, the ARU being configured to focus the RF en...  
WO/2020/236961A1
An electrospray apparatus including a plurality of emitters, disposed on a substrate, wherein the plurality of emitters can have a narrow parameter distribution, and where the apparatus can optionally include one or more control systems,...  
WO/2020/232575A1
Disclosed in the present application are a flight task generation method, a control terminal, an unmanned aerial vehicle, and a storage medium. The method comprises: obtaining a flight task file (S101); parsing the flight task file to ob...  
WO/2020/236256A1
A space optical system is disclosed. The space optical system (100) includes a primary support structure (110) in support of a primary mirror (111). The space optical system also includes a sensor mounting structure (101) coupled to the ...  
WO/2020/235744A1
The present invention relates to a drone-attachable/detachable mission device and a drone system. The drone-attachable/detachable mission device according to an embodiment of the present invention comprises: a function unit having functi...  
WO/2020/236697A1
The present disclosure describes various systems, devices, and methods configured to retrieve a fixed-wing aircraft from free flight using a flexible capture member and a monopole assembly.  
WO/2020/234529A1
The present description relates to a device (7) for recognising the attitude of an object, characterized in that it comprises: a sphere (11) comprising a wall (13) able to let a light flux at least partially pass; a ball (17), moveably m...  
WO/2020/234115A1
The invention mainly relates to a seat cushion (12) for a vehicle seat, in particular an aircraft seat, comprising: - at least one lower foam layer (15) having a function of stiffening the seat cushion (12), - at least one upper foam lay...  
WO/2020/234565A1
A method of producing at least part of a structural frame of a vehicle, the method comprising: providing a support structure (300), the support structure (300) comprising: a plurality of elongate members (301); and one or more retaining ...  
WO/2020/234544A1
The invention relates to a regulator, configured to receive a hot air flow via an air inlet (12), to treat this hot air and to transmit the treated hot air to an air outlet (14) configured to supply a pneumatic actuator (16), comprising ...  
WO/2020/234400A1
The invention relates to a device and to a method for avalanche blasting. The device comprises a drone, an explosive charge which is fastened by means of a cord in a freely suspended manner to the drone. An ignition mechanism is provided...  
WO/2020/233683A1
A gimbal control method and apparatus, a control terminal and an aircraft system. The gimbal control method is applied to a control terminal. A gimbal carries a photographing device. The method comprises: obtaining photographing paramete...  
WO/2020/234177A1
The platform comprises supporting legs (12) fastened to the platform (10), and a control unit (13) and provides an electrical charging system including a plurality of coplanar adjacent electroconductive plates (14), with adjacent edges e...  
WO/2020/234540A1
Space launcher comprising a launcher body (1), an engine (2), a combustion chamber (4), a nozzle (5) having a main axis (Z-Z), the nozzle (5) being provided with a plate (6) extending radially, the plate (6) having an inner face and an o...  
WO/2020/234314A1
A retractable fuselage mounted landing gear assembly is disclosed. The landing gear assembly comprises a main strut, a drag stay and a landing gear main fitting. A first end of the drag stay is attached to the main strut and a second end...  
WO/2020/204754A3
The invention relates to the field of aeronautics, and more particularly to vertical take-off and landing aircraft. The technical result is an improvement in the responsiveness and manoeuvrability of an aircraft. The essence of the inven...  
WO/2020/234539A1
Space launcher comprising a launcher body (1), an engine (2), a nozzle (5) provided with a plate (6) extending radially around the nozzle (5) or a combustion chamber (4) and insulating an internal volume of the spacecraft from an externa...  
WO/2020/178504A3
Air conditioning system for a cabin (10) of an aircraft, comprising: an air intake device; an air cycle turbomachine (12); at least one main cooling exchanger (16); a water extraction loop (30); a duct (26) for distributing water extract...  
WO/2020/229287A1
Disclosed is an aircraft assembly comprising: a first aircraft structure, a second aircraft structure, first and second tension bolts arranged to suspend the first aircraft structure below the second aircraft structure, the first and sec...  
WO/2020/181117A8
To manage propellant in a spacecraft, the method of this disclosure includes storing propellant in a tank as a mixture of liquid and gas; transferring the propellant out of the tank; converting the mixture of liquid and gas propellant in...  
WO/2020/230377A1
In this information processing method, a computer: determines whether a target sound was recognized (S11); if the determination was that the target sound was recognized (Yes in S11), acquires a position and a sound collection direction o...  
WO/2020/180368A3
An aircraft includes a fuselage defining a longitudinal axis between a forward end and an aft end. The aircraft includes an electrical system having an electric storage. The electric storage is positioned within the fuselage.  
WO/2020/229800A1
A non-rigid airship or hybrid air vehicle has a pressure-stabilised envelope (100) that includes at least one ballonet (102, 103). A system is provided for measuring the geometry of the lifting gas enclosure (101) within the pressure-sta...  
WO/2020/229081A1
The invention relates to a method for joining a power semiconductor component (1.1) to a heat pipe (2), wherein, during joining, the external pressure (p2) acting on the heat pipe (2) is changed proportionally to the internal pressure (p...  
WO/2020/230964A1
A device for displaying a flight area on the ground and an operation method therefor are disclosed. The device for displaying a flight area on the ground according to an embodiment may comprise: a light generator for projecting an image ...  
WO/2020/229745A1
Turbomachine (1) comprising a cone (40) positioned at an upstream end and secured to rotate as one with the low-pressure shaft (20), a system for deicing said cone (40) comprising resistive heating elements (52) positioned in the cone (4...  
WO/2020/229501A1
An aircraft panel assembly with: a panel; and a plurality of stiffeners on the panel. Each stiffener has an attachment part attached to the panel and a structural part spaced apart from the panel. A rib foot beam crosses the stiffeners a...  
WO/2020/229426A1
A thermally insulated container for storing and serving frozen confectionery items, wherein the container is preferably arranged to be removably mounted within a service cart, such as an inflight service cart.  
WO/2020/229630A1
An aircraft wing comprising a fixed wing and a wing tip device rotatable about a hinge at the tip of the fixed wing. The wing further comprises a hinged panel at the boundary between the wing tip device and the fixed wing. In the flight ...  
WO/2020/229836A1
The present invention provides, an aircraft passenger seat unit (100) comprising a convertible passenger seat (110), a shell (130) defining a planform (180) of the seat unit, the planform having a first end region (182) across a first en...  
WO/2020/230370A1
A setting unit 23 sets the operation mode of an aircraft 10 either to a first operation mode, in which data generated in the host aircraft and data received from other aircraft is transmitted to a processing device that processes the dat...  

Matches 1 - 50 out of 70,356