| Document |
Document Title |
|
WO/2021/142557A1 |
An electric jack and an electronic control system thereof, comprising: a support rod hinged to a front end cover, a support disc being disposed at the lower end of the support rod, and the support plate being connected with a bolt after ...
|
|
WO/2021/142970A1 |
Disclosed is a quick launcher for a small unmanned aerial vehicle, the launcher comprising a sliding rail (2), a supporting foot stand (1) mounted at an end of the sliding rail (2) and rotatably connected to the sliding rail (2), a slidi...
|
|
WO/2021/140491A1 |
A computer implemented method for estimating angles of attack (α) and / or sideslip (β) of a flying body comprises the steps of: Providing data or measurements representative of the time derivative of the module of a speed of the flyin...
|
|
WO/2021/138748A1 |
Disclosed is a docking station for use with an unmanned aerial vehicle (UAV). The docking station has a retractable guide apparatus having a retracted state in which the retractable guide apparatus is retracted within the docking station...
|
|
WO/2021/141653A1 |
The present disclosure presents various embodiments of a system for retrieving a fixed-wing aircraft (8030) from free flight using a flexible capture member (8004). The system includes a GPS reference sensor (8020) and a communication li...
|
|
WO/2021/140259A1 |
Camera and lights positioning system for inspecting air-to-air refueling hoses, which comprises a substructure that can be attached to a container or capsule or pod, one or two guidance substructures (13) that enclose the hose, a toroida...
|
|
WO/2021/134999A1 |
A mooring device for airship transfer, comprising a support frame (1) and a travelling assembly (2). The support frame (1) comprises support beams (11) transversely arranged, support rods (13) which are vertically arranged and fixedly co...
|
|
WO/2021/136750A1 |
The invention relates to a method and a computer program product for monitoring a bleed air supply system of an aircraft. At least one sensor (20-22) for monitoring the state of the bleed air supply system (10) by means of the sensor dat...
|
|
WO/2021/134851A1 |
An aircraft engine emissions quantity measurement method and apparatus, relating to the field of aerospace technology. Said method comprises: obtaining four dimensional data and corresponding meteorological data of an aircraft during fli...
|
|
WO/2021/131983A1 |
A takeoff/landing apparatus (100) for a multicopter having a spraying function is provided with: a spraying agent container (81) for receiving a spraying agent; a diluting solution container (82) for receiving a diluting solution for dil...
|
|
WO/2021/130373A1 |
The invention relates to a device for automatically checking the service state of a parachute system for a flying drone. The device comprises an electrical actuator (40) for the deployment mechanism (50) of the parachute (60) and a resis...
|
|
WO/2021/129081A1 |
Provided is an emergency guarantee robot for an unmanned aerial vehicle in a polar region. The robot is of a vehicle body structure. A support table (1) is arranged on the upper side of a chassis of a vehicle body; traveling devices (2) ...
|
|
WO/2021/132372A1 |
This takeoff and landing device (1) for a multicopter (60) comprises: a machine frame (2); a top plate (3) that is supported on the machine frame (2) and has a surface area enabling the takeoff and landing of a multicopter; and a fixing ...
|
|
WO/2021/129352A1 |
An unmanned aerial vehicle base station (100), relating to the technical field of unmanned aerial vehicles. The unmanned aerial vehicle base station (100) comprises an upper housing (10), a lower housing (20), an antenna (30), a function...
|
|
WO/2021/131982A1 |
A multicopter takeoff/landing device (20) comprising: a machine frame (21); and a deployment structure body (22, 221, 222) mounted on the machine frame, the deployment structure body (22, 221, 222) having a plurality of plate members (34...
|
|
WO/2021/130063A1 |
An apparatus and method for adjusting the position of a tool relative to a component using an x-ray backscatter device, including an x-ray backscatter device that is positioned adjacent a first side of a component and configured to emit ...
|
|
WO/2021/126071A1 |
A tether management system is disclosed. The tether management system includes a spool, a tension sensor, a controller and a moveable pulley. The spool is rotatable to reel in and reel out a tether. The tension sensor measures a tension ...
|
|
WO/2021/121803A1 |
The damage assessment device (16) comprises a trolley (4) with a platform (43) carrying a sensor mounting (11) for various non-destructive testing sensors (10) and an additional depth sensor (13) for estimating the depth of a dent, a fle...
|
|
WO/2021/124573A1 |
[Problem] To provide a technology for performing takeoffs and landing with good precision in a takeoff/landing port for a flight vehicle. [Solution] A takeoff/landing system according to the present invention comprises: a flight vehicle ...
|
|
WO/2021/122731A1 |
The invention relates to a contamination protection (10) for the edges of riblet films (2) which are adhered to a surface (1) and have riblets (4) formed on the top side (3') of a film layer (3) and an adhesive layer on the bottom side. ...
|
|
WO/2021/127323A1 |
A longitudinal translatable seal includes a first compartment extending in a longitudinal direction; a second compartment extending in the longitudinal direction forming a sealing surface with the first compartment; and a carriage transl...
|
|
WO/2021/122990A1 |
Multi-rotor hydraulic drone (1) comprising: - a plurality of hydraulic motors (6) each receiving a pressurised fluid, - propellers (5) driven by the hydraulic motors (6), - at least one hydraulic pump (10) driven by at least one motor (1...
|
|
WO/2021/119118A1 |
The technology provides a launch rig structure (300) capable of filling a very large balloon envelope while the balloon is arranged vertically (306). The filled balloon is capable of staying aloft in the stratosphere with its payload for...
|
|
WO/2021/116590A1 |
A first aspect of the invention relates to an impact detection device (3) comprising an impact detector (DC), a wireless communication means (MC), an energy storage means (MS), an autonomous electric power generation means (GE) distinct ...
|
|
WO/2021/117730A1 |
It is desirable to enable an aerial vehicle, such as a drone that performs maintenance and management of an overhead power line, to fly for long periods of time without landing on land and receive electrical energy from the overhead powe...
|
|
WO/2021/116589A1 |
The invention relates to an autonomous impact detection device (3) comprising at least one impact detector (DC); at least one wireless transmission means (MC) configured to transmit the information collected by the impact detector (DC); ...
|
|
WO/2021/118019A1 |
The present invention relates to a landing control device for a drone. The present invention comprises: a drone comprising a leg frame and a charging receiver module on the bottom part and comprising a landing control unit for controllin...
|
|
WO/2021/117296A1 |
The present invention addresses the problem of providing a roof structure with which it is possible to provide a drone port so that a drone can stably land on and take off from an inclined roof, and with which it is possible to protect d...
|
|
WO/2021/105315A1 |
The invention relates to an apparatus for attaching aerodynamically functional films (14.1-5) to surfaces (4) of bodies (1) around which flow occurs and to the use of such an apparatus. The apparatus comprises a self-adhesive, removable ...
|
|
WO/2021/105151A1 |
The invention relates to an avionics network comprising a plurality of avionics components and a configuration monitoring device, which is connected by wire or wirelessly to the plurality of avionics components. The configuration monitor...
|
|
WO/2021/106287A1 |
Provided is a system comprising a calculation device located on the earth and a communication control device that is mounted on a flight vehicle irradiating beams, thereby forming a cell in a target area on the earth and providing a wire...
|
|
WO/2021/100501A1 |
Provided is a takeoff and landing platform for an unmanned aircraft which can vertically take off and land, the takeoff and landing platform comprising: an attachment/detachment unit which an unmanned aircraft can be attached to and deta...
|
|
WO/2021/100908A1 |
The present invention relates to a system for controlling a flashing light for an airfield of an airport, and a method for controlling same. In this regard, the present invention includes: a master timer (100) which receives power from t...
|
|
WO/2021/101389A1 |
A fuelling system (1) for an aircraft comprising a tank (3) comprising a compartment (5) configured to be filled with fuel, a discharge conduit (10) extending from the compartment (5) to an outside of the tank (3), and a sampling arrange...
|
|
WO/2021/099334A1 |
A drone comprising a front section, a wing structure supported by a rotor located behind the front section, and a propeller at the rear, the wing structure comprising two wings rotating with the rotor, the wing structure being able to mo...
|
|
WO/2021/097645A1 |
A landing control method and device, a base station, an unmanned aerial vehicle and a storage medium. The method comprises: establishing a communication connection with an unmanned aerial vehicle that enters a communication coverage regi...
|
|
WO/2021/094667A1 |
The invention relates to a device and method for managing a fleet of information-communicating devices that are able to be reversibly fastened to aircraft turbomachines, comprising: associating (S02) one device of said fleet of devices w...
|
|
WO/2021/096774A1 |
An apparatus for picking, placing, and forming a composite charge over a complex geometry tool comprises a first frame, a second frame, and a plurality of dynamic mechanisms. The first frame is formed from rigid material and includes a f...
|
|
WO/2021/097422A1 |
A system and method of converting engines on a turboprop aircraft, including removing an existing engine and associated propeller from an aircraft fuselage, installing an engine mount adapter assembly to the fuselage, and installing a re...
|
|
WO/2021/097439A1 |
In some embodiments, the present disclosure provides systems and methods enabling unmanned vehicle navigation and delivery including an integrated roofing accessory integrated into a roof, the integrated roofing accessory including at le...
|
|
WO/2021/095701A1 |
The present invention provides safe flight for a flight vehicle even in an area where wireless communications and the like including a position report from the flight vehicle are unavailable. Flight vehicles are controlled with restric...
|
|
WO/2021/095376A1 |
This method is for manufacturing a fan blade rotor 41 which includes an annular rotation support ring 33 around a rotary shaft, a permanent magnet 45 provided side by side with the rotation support ring 33 in the radial direction, and a ...
|
|
WO/2021/092786A1 |
An unmanned aerial vehicle takeoff and landing platform (100), an unmanned aerial vehicle takeoff and landing control method (200), an unmanned aerial vehicle takeoff and landing control device (300), and a machine readable storage mediu...
|
|
WO/2021/094847A1 |
The invention relates to the field of cleaning devices. The device comprises an opening (4) with an edge, at least one cleaning element (6, 7; 19, 20) being provided on a side region of this edge, and a support element for limiting the r...
|
|
WO/2021/096699A1 |
A high visibility safety tag device including a body member and a safety tag member. The body member including a first adhesive element, an elastic element and a second adhesive element. The first adhesive element including an adhesive m...
|
|
WO/2021/094319A1 |
A method of monitoring the condition of an aircraft landing gear (1) shock absorber (9), the shock absorber including at least one spring chamber (18) containing a gas (22), the method comprising: taking a plurality of measurements (40) ...
|
|
WO/2021/087594A1 |
A method is proposed providing for the precision landing of an aircraft. According to this method, radiation is triggered from a plurality of radiation emitters of a radiating unit of a transmitting part; a signal is recorded, by a photo...
|
|
WO/2021/088097A1 |
An aerostat icing characteristic numerical simulation and experimental verification system, comprising an aerostat icing characteristic calculation model and an aerostat icing characteristic experimentation system, the aerostat icing cha...
|
|
WO/2021/082794A1 |
An unmanned aerial vehicle (UAV) airport, a UAV system, a patrol inspection system, a method, a control apparatus, a device, a storage medium, and a UAV cruising system, which relate to the field of UAVs and are used for optimizing the s...
|
|
WO/2021/083791A2 |
The present invention relates to a freight carrier (7) for accommodation in the cargo hold (3) of an aircraft (1), to a system comprising a freight carrier (7) and a fan unit (59), and to a method for loading the cargo hold (3) of an air...
|
