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Matches 451 - 500 out of 70,945

Document Document Title
WO/2020/180520A3
Apparatus to monitor the position of an aircraft landing gear.  
WO/2020/190349A3
Systems for insulating a space vehicle or space borne container from an external environment as well as cryogens from heat sources. Such systems also protect the vehicle from the high dynamic pressures, the high heat loads encountered in...  
WO/2020/217417A1
The purpose of the present invention is to provide an unmanned aerial vehicle capable of preventing a transported item from falling unintentionally. An unmanned aerial vehicle 1 according to one aspect of the present invention comprises:...  
WO/2020/216712A1
The invention relates to an air intake (1) of a turbojet engine nacelle comprising an annular structure (110) including an outer fairing (100) defining an aerodynamic outer surface and an inner fairing (102) defining an aerodynamic inner...  
WO/2020/219466A1
A system and method for controlling a seat device. A control unit broadcasts an identifier associated with a seat assigned to a passenger, and establishes a personal wireless area network connection with a personal electronic device (RED...  
WO/2020/219692A1
Systems and methods for localizing and tracking mobile objects are provided. A method includes determining (1210) an initial location of a node in a multi-hop network based on multi-lateration from an unmanned aerial vehicle. The method ...  
WO/2020/212225A1
A process for using an air input (2) of a turboreactor nacelle (1) of an aircraft, comprising an air input lip (23) which comprises at least one fixed portion and at least one portion (3, 3', 4, 4', 5, 5', 6, 6', 7) which can be moved be...  
WO/2020/212087A1
The invention pertains to a filler preform in a wedge form (1) comprising reinforcing fiber bundles (2) consisting of reinforcing fiber filaments, wherein the filaments are directed parallel to each other within the fiber bundle, wherein...  
WO/2020/213290A1
Provided are an information management method, identification-information-imparting device, and information management system whereby objects can be identified using a simple method. The present invention is characterized in that: a li...  
WO/2020/211028A1
Provided are a propeller, a power assembly, and an aerial vehicle. The propeller comprises: a hub (20) and at least two blades (10) arranged at equal intervals along the circumference of the hub (20). The blades (10) are rotatably connec...  
WO/2020/214236A2
A system for landing an unmanned aerial vehicle has an unmanned aerial vehicle and a ground-based platform. A guide structure for receiving the unmanned aerial vehicle is mounted on the ground base platform. The guide structure has an in...  
WO/2020/212504A1
The invention relates to a water scooping apparatus (2) for an aircraft, comprising a water scooping unit (7) that is associated with a water tank (10) via an extendible tubular member (5), the water scooping unit being provided with an ...  
WO/2020/211812A1
An aircraft landing method and apparatus, a storage medium and a computer device for implementing the method, and an aircraft. The method comprises: obtaining the current image of a preset take-off/landing site acquired by an aircraft in...  
WO/2020/212224A1
An aircraft turbojet engine (1) extending along an X axis and comprising a blower configured to provide a reverse thrust and a nacelle comprising an air intake (2) which comprises at least one deflection member (3, 4, 5) movably mounted ...  
WO/2020/214532A1
A grommet (200, 300, 400), a stud (102), an assembly of a grommet and a stud forming a fastener (100), and a method of assembling a grommet and a stud to form a fastener has the grommet with an interengaging element (250) in a channel wa...  
WO/2020/213831A1
The present invention directly drives an electric motor (115) through the power of power generators (100, 102) that produce electric power by means of the driving of a gasoline engine (103), so as to drive propellers (116), provides a po...  
WO/2020/213198A1
The present invention provides an unmanned flight body, a control method, and a program with which it is possible to suppress a reduction in flight performance of the unmanned flight body while maintaining or improving the quality of sou...  
WO/2020/215030A1
An airport runway light for use as a runway approach light for a runway lighting system, the runway light having a light body with a base configured to support the runway light in a light socket of a runway lighting system, the base havi...  
WO/2020/212568A1
The invention concerns a spar structure (11) for connecting a moveable component (4) to an aircraft. The structure is formed from a single continuous body of material defining a plurality of attachment/actuation brackets (10A-10F) and a ...  
WO/2020/212226A1
An aircraft turbojet engine (1) comprising a fan (11) configured to provide a reverse thrust and a nacelle comprising an air intake (2), the air intake (2) comprising at least one circulation duct (3) in the annular cavity (20) opening, ...  
WO/2020/214081A1
The invention relates to a surfing arrangement (3) for mounting to underneath an aircraft (1), comprising at least a tank of a water collecting system (10), which arrangement (3) is configured for providing a gliding surface (7) on which...  
WO/2020/212655A1
The invention relates to a method for controlling an electrical power supply network (10) for an aircraft, comprising: - at least one generator (30) associated with a gas turbine (90) and with a rectifier (20), - at least one distributio...  
WO/2020/214381A1
An apparatus includes a structure (100, 300, 700) configured to receive and transport thermal energy. The structure includes one or more materials configured to undergo a solid-solid phase transformation at a specified temperature or in ...  
WO/2020/214552A1
An airship (100) includes a ballonet (110), a ballonet tracking system (125), and a vehicle management system (140). The ballonet is disposed within the airship and includes a ballonet surface (120). The ballonet tracking system includes...  
WO/2020/180373A3
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/2020/212665A1
The invention relates to a system for monitoring the health of a helicopter, comprising a helicopter and a device for determining a change in state of the engine that is configured to collect data measured by engine sensors and external ...  
WO/2020/212989A1
A system comprising: one or more Unmanned Aerial Vehicles (UAVs); and a UAV carrier configured to carry the UAVs from an origin to a destination; wherein the UAV carrier comprises a first controller configured to release the UAVs from th...  
WO/2020/212836A1
The invention relates to a propulsion device (1) for a rotating blade aerodyne with vertical take-off and landing, comprising a hollow chassis (4) and contra-rotating coaxial rotors (2, 3) with fixed-pitch blades (22, 32). The means for ...  
WO/2020/210904A1
There is provided a cable-mounted apparatus, a proximal end of the cable mounted to a winch to extend and retract the cable, the apparatus including: a housing connected to a distal end of the cable; a manipulator located underneath the ...  
WO/2020/212656A1
The invention relates to a hybrid propulsion system (100) for a multi-rotor rotary-wing aircraft, comprising: an internal combustion engine (12), an electric machine (14) coupled to the internal combustion engine, a rectifier (16) connec...  
WO/2020/212228A1
Disclosed is a method for using an aircraft turbojet engine (1) comprising an air inlet (2) comprising a plurality of rectifier vanes (3), each rectifier vane (3) being mounted such that it can move between a retracted position to assist...  
WO/2020/211919A1
This alerting system (10) for a light aircraft includes a reception unit (12) for receiving a piece of information to be released, a release unit (40) able to generate an alert for addressing a piece of information received by the recept...  
WO/2020/212208A1
According to the present invention, a system and a method for evaluating performance of a porous skin of an aircraft is presented. The aircraft comprises at least the porous skin, and a boundary layer control system. The performance eval...  
WO/2020/211818A1
Disclosed are an airport power-assisted take-off and landing device, a take-off and landing method, and an ornithopter take-off device. The airport power-assisted take-off and landing device comprises a transverse cable (IV), fixed pulle...  
WO/2020/212966A1
A system comprising: an Unmanned Aerial Vehicle (UAV) carrier comprising a power supply, the UAV carrier connected, via respective wires, to one or more UVs, wherein: (a) each of the UVs is capable of performing maneuvers irrespective of...  
WO/2020/215056A1
A propulsion method includes: providing a pair of synchronized rotors rotatably mounted on a frame with a bearing having a bearing outer race, bearing balls, and bearing inner race; providing a plurality of permanent magnets mounted on t...  
WO/2020/213450A1
A battery pack comprising an outer case, a battery, a circuit board, a substrate holder in which the circuit board is accommodated, an output terminal which outputs the electric power accumulated in the battery to external equipment, and...  
WO/2020/212424A1
An aircraft comprising a fuselage, a pair of wings connected to an upper portion of the fuselage, and a pair of wing support struts, each wing support strut being connected between a lower portion of the fuselage and an underside of the ...  
WO/2020/208402A1
An aircraft (A, A.1, A.2) comprising at least one bay (1, 1.1, 1.2) for receiving different types of standardized modules, the bay (1, 1.1, 1.2) being configured to receive at least two different types of energy modules (6, 7, 8, 9, 10, ...  
WO/2020/208420A1
A gasper assembly for use in an aircraft that includes a housing that includes an outer wall having an inner surface that defines a central opening, a nose member positioned in the central opening, a plurality of directional blades exten...  
WO/2020/180372A3
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/2020/209255A1
[Problem] To provide a drone system for safely executing a task by using a plurality of drones. [Solution] A drone system (500) comprising at least a plurality of drones (100) that fly within a task area (403a) and execute a task, and a ...  
WO/2020/207862A1
The invention concerns an aircraft propulsion unit (30) comprising at least one first propeller (32) provided with a plurality of radial blades (34) extending about an axis (A) of rotation of the first propeller (32) which is rotated by ...  
WO/2020/208802A1
This joint structure 10 is provided with a connecting member 5 that is provided between and connects a member 1 to be reinforced and a reinforcing member 3. The connecting member 5 has a first coupling part 5a and a second coupling part ...  
WO/2020/208265A2
Aspects of the present invention relate to an aerial firefighting system for a helicopter, the firefighting system comprising: an external reservoir for storing water, wherein the reservoir comprises a water outlet; a supporting frame co...  
WO/2020/207678A1
The invention relates to an air-conditioning arrangement (1) for a vehicle, comprising at least one fluid channel (20), which has at least two identically designed connection devices (22A, 22B), and comprising at least one movable vehicl...  
WO/2020/210607A1
An autonomous farming system (26) comprising one or more ground-based drones (10) and one or more unmanned aerial vehicles (12), whose routes through a field are optimized by an autonomous farming control system (30) that utilizes linear...  
WO/2020/208527A1
An electric power system (300) with integrated fire relief channels for an electric vehicle (100), the electric power system comprising: a power source (104, 180) configured to power a motor (160) that propels a vehicle housing (101), th...  
WO/2020/209167A1
Provided is an information processing device provided with a parameter generating unit that generates a motion parameter for controlling the motion of a movable body, on the basis of a ratio between a first distance from a reference body...  
WO/2020/210800A1
An aircraft engine mounting system to retrofit an aircraft engine from one aircraft type to another in a manner suitable for approved flight. The system includes a circular member having longitudinal securement members extending therefro...  

Matches 451 - 500 out of 70,945