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Matches 1 - 50 out of 69,424

Document Document Title
WO/2020/183739A1
A tailsitter aircraft 100 provided with a body 120, two pairs of horizontal main wings 30a, 30b, 30c, and 30d when viewed from the front, each connected to the body 120, and eight propellers 50a, 50b, 50c, 50d, 60a, 60b, 60c, and 60d tha...  
WO/2020/184164A1
Provided is a discharge system for a flight vehicle, the system making it possible to display the remaining amount of the content of an aerosol container and systematically manage replacement timing. The discharge system for the flight v...  
WO/2020/184602A1
A rotary-wing aircraft is provided that can transport a person with a simple structure. A rotary-wing aircraft that is operated from outside the aircraft and can fly freely in the air, the rotary-wing aircraft comprising: a machine bod...  
WO/2020/182766A1
Aircraft door (1) comprising an inside door opening lever (6) coupled to a vent flap (5) by a conditional opening mechanism having two modes and comprising a flap stop (20) that is able to cooperate with a stop surface (21). The stop (20...  
WO/2020/185190A1
The present device for scattering ashes from a drone comprises a housing (1) made of a rectangular textile shell formed from a first layer (2) and a second layer (3) of a material, and a mechanism for opening the housing (1) which is con...  
WO/2020/182446A1
A method of controlling an Autonomous Vehicle (AV) 110, comprising the steps of: detecting a fault in a first AV 110-1; in response to detecting said fault, transmitting a communication for alerting an AV of the fault, wherein said commu...  
WO/2020/184477A1
An information processing device as an example of the present disclosure is provided with: an image capturing control unit which controls a first image capturing device so as to acquire a real image while moving at least one among the vi...  
WO/2020/184934A1
A vertical take-off and landing aircraft using a hybrid electric propulsion system, according to an embodiment of the present invention, includes: a first control step (S1) of changing a destination when an engine (10), a power generator...  
WO/2020/181329A1
An active docking station enables improved operation of Unmanned Aerial Vehicles (UAVs). The docking station comprises: a base structure which secures the station to a mounting location; a robotic motion system connected to the base stru...  
WO/2020/182623A1
A spacecraft attitude control module (1) according to the invention is compact and easy to assemble with additional modules to form an operative attitude control system. The module comprises a robust rectangular, preferably cubic support...  
WO/2020/182682A1
The invention relates to an androgynous coupling means (10, 16, 17) exhibiting both male and female coupling sections (11, 12), wherein the androgynous coupling means is configured for form fit coupling with at least one further androgyn...  
WO/2020/182946A1
Disclosed is a landing gear system uplock arrangement (300, 500) comprising: a hook (310) defining a gap (314), wherein the hook is movable between a first position, at which the hook is for retaining a movable element (299, 499) of a la...  
WO/2020/185670A1
A horizontal axis wind turbine airfoil segment with vortex generator tape ("VGT") tape applied downstream of the leading edge and within the boundary layer is disclosed. Placing the VGT tape at distance of 60% chord results in the bounda...  
WO/2020/185274A2
A hybrid electric engine control module (ECU) configured to be operatively connected to a hybrid electric aircraft powerplant having a heat engine system and an electric motor system to control a torque output from each of the heat engin...  
WO/2020/185542A1
The invention relates to a strut (101, 201), such as fiber composite struts used in aircraft or spacecraft, which has a largest possible outer diameter within a cylindrical installation space of the strut (101, 201). The invention concer...  
WO/2020/117384A3
An aircraft capable of Vertical Take-Off and Landing (VTOL) and traverse flight. The aircraft generally includes a fixed outer structure including at least a generally cylindrical wing having an internal body situated within the fixed ou...  
WO/2020/184318A1
An information processing device (10) is provided with: a detection unit (140) for detecting pressure fluctuation of a fluid filled in a deformable filling part (130) provided to a portion at which leg parts of a mobile body (100) each h...  
WO/2020/112199A3
A munitions rack includes a munitions rack structure that houses multiple compact ejectors. The structure includes a pair of internal longitudinal ribs, inboard of a pair of external longitudinal ribs. A spine of the munitions rack struc...  
WO/2020/186107A1
A method in a spacecraft for transporting propellant to be consumed by a thruster includes storing the propellant in the spacecraft in a solid state during at least a portion of a take-off procedure and supplying the propellant to the th...  
WO/2020/184166A1
Provided is a discharge device of a flight vehicle, the device making it possible to easily mount an aerosol container to a vehicle body, and the device being easily replaceable and having high safety. The discharge device of a flight ve...  
WO/2020/184656A1
[Problem] To propose a specialized midair balloon-popping game tool that provides fun and excitement. [Solution] A midair balloon-popping game tool 1 that is used by being attached to a drone 2 that can be remote-controlled, the midair b...  
WO/2020/181855A1
A dihedral trapezoidal lifting and floating integrated aircraft, comprising an aircraft body (1) and a power system. The aircraft body (1) comprises a head part provided with an equipment front compartment (2) and a tail part provided wi...  
WO/2020/096477A8
The invention relates to aerospace engineering, and more particularly to test benches. A thermodynamic test bench for simulating aerodynamic heating consists of a sectional lamp heater fastened inside a vacuum chamber, and a system of se...  
WO/2020/182493A1
The present invention relates to an aircraft seat comprising: - a guide rail (26); - a rack (34); - an actuator (30) provided with a gear (31); - at least one connection portion (35) providing a mechanical connection between the guide ra...  
WO/2020/183594A1
The purpose of the present invention is to provide a tailsitter aircraft capable of roll control, pitch control, and yaw control with higher accuracy and responsiveness than conventionally. A tailsitter aircraft 1 is provided with: a b...  
WO/2020/182692A2
The invention relates to an androgynous coupling means (10) exhibiting both male and female coupling sections, wherein the androgynous coupling means is configured for form fit coupling with at least one further androgynous coupling mean...  
WO/2020/121067A3
A metal air battery electrolyte replenishment system comprised of a base station with docking receptor apparatus and matching docking probe on a flying drone. The probe onboard the drone has a sensor that guides the drone to connect with...  
WO/2020/185947A1
A winged vertical take-off and landing aircraft with compound control surfaces comprising flaps and ailerons which can be operated simultaneously with each other offers improved aerodynamic performance and maneuverability. Configuration ...  
WO/2020/159603A3
A system and method for generating a force from a voltage difference applied across at least one electrically conductive surface. The applied voltage difference creates an electric field resulting in an electrostatic pressure force actin...  
WO/2020/182786A1
The invention relates to a method and a system for an automated re-examination of unaccompanied hold baggage. The system is designed to carry out the following steps: First an according system is activated, wherein at least one digital i...  
WO/2020/180432A1
Provided is an indoor positioning system for light fixtures that includes a drone device which determines a respective location of each light fixture, and assigns identifying information to each light fixture. The system also includes a ...  
WO/2020/179195A1
This control device (100) comprises a communication unit (101) that obtains information about the departure location and destination location of a shipment, and a management unit (102) that manages the route and schedule of an unmanned f...  
WO/2020/178504A2
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/2020/178424A1
A vehicle cleaning tool comprising: a cleaning head (1) comprises a housing, the housing comprising an application face and a recess at the application face; a waiting cavity (7) for cleaning liquid; a supply tube (8) configured for supp...  
WO/2020/179725A1
A landing gear lifting/lowering EHA system (10) is provided with: a hydraulic actuator (2) that elevates/lowers landing gear of an aircraft; at least one electric hydraulic pump (31, 32); a hydraulic path (101); pressure sensors (38, 39)...  
WO/2020/179460A1
This control device comprises: a receiving unit that receives a discretionary wind velocity vector, the vector being measured by at least one external anemometer; a wind force prediction unit that, on the basis of the received wind veloc...  
WO/2020/180173A1
A flying vehicle (1) comprises: - a body (10) having a tail section (20); - a main rotor (100) having a rotation axis on top of the body; - a central thrust unit (200) arranged along the longitudinal axis of the vehicle, at a distance fr...  
WO/2020/180520A2
Apparatus to monitor the position of an aircraft landing gear.  
WO/2020/180376A2
An aircraft includes a fuselage defining a longitudinal axis between a forward end and a aft end. At least one airfoil is laterally extending from the fuselage defining an airfoil axis. An electrical system has an electric storage. The e...  
WO/2020/179461A1
An unmanned aerial vehicle 1 is provided with a main body 10 having a thrust generating unit 12 for flying in midair, a vacuum suction attachment device 20 which includes suction attachment portions 21 and which is attached to the main b...  
WO/2020/178614A1
There is described a capture system (100) adapted to capture orbital objects (2000), in particular for deorbiting purposes. The capture system (110) comprises (i) a deployable capture structure (110) designed to be deployable between a s...  
WO/2020/178505A1
Exchanger (16) for cooling warm primary air with cool secondary air, comprising: a plurality of circulation channels for the secondary air (80); a plurality of circulation channels for the primary air, characterised in that it further co...  
WO/2020/178283A1
Disclosed is an aircraft pressurised cabin door (1), comprising a fuselage panel (2) and a door structure (3) that comprises: two circumferential beams (4) arranged on the lateral edges of the door (1); a plurality of longitudinal beams ...  
WO/2020/179983A1
The present invention provides a drone-passing multiple detection sensor gate comprising: a gate having a ring-like structure through which a drone can pass during flight; a first sensor, disposed on the front or the inner front of the g...  
WO/2020/180380A1
A hybrid propulsion system includes a heat engine configured to drive a heat engine shaft. An electric motor is configured to drive a motor shaft. A transmission system includes at least one gear box. The transmission system is configure...  
WO/2020/177739A1
An aircraft realizing vertical take-off and landing and horizontal flight using bottom-drive flaps tilted in sections. A large-area plate-shaped wing is used, and movable strip-shaped flaps (4; 8; 9) and fixed strip-shaped flaps (5) are ...  
WO/2020/180373A2
The unified command system and/or method includes an input mechanism, a flight processor that receives input from the input mechanism and translates the input into control output, and effectors that are actuated according to the control ...  
WO/2020/180190A1
There is disclosed a device for connecting an aircraft warning marker to a power line, said device being connectable to a helicopter, wherein the device comprises a release mechanism adapted to clamp two halves of the aircraft warning ma...  
WO/2020/180372A2
A hybrid electric engine control module (ECU) can be configured to be operatively connected to a hybrid electric aircraft powerplant having a heat engine system and an electric motor system to control a torque output from each of the hea...  
WO/2020/180370A1
An aircraft propulsion system having dual powerplants is disclosed that includes a combustion powerplant on one wing of the aircraft and a hybrid-electric powerplant on the other wing of the aircraft, wherein the combustion powerplant in...  

Matches 1 - 50 out of 69,424