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WO/2021/072414A3 |
A cabin pressure sensor system (100) for an aircraft including a plurality of air pressure sensors (104) positioned within an aircraft environment, an indication device (106), a central processing unit (CPU) (102) electrically coupled to...
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WO/2021/115166A1 |
When a flying object comprising an illuminance sensor (500) measures illuminance by means of the illuminance sensor (500) in flight, since an angle formed between an incident direction of sunlight and a flight direction of the flying obj...
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WO/2021/119564A1 |
Methods and devices for confirmation of successful delivery by an unmanned aerial vehicle (UAV) are disclosed. A UAV is configured to navigate to a delivery destination, authenticate a receiving zone at the delivery destination, release,...
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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...
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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 ...
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WO/2021/114578A1 |
A telescopic wing mechanism with continuously variable wingspan is composed of an inner wing section (1), an outer wing section (3), a middle wing section (2) nested between the inner wing section and the outer wing section, as well as a...
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WO/2021/119603A1 |
A fractal unmanned aircraft system (200) includes a first module(100), a second module (100) and a third module, (100) each having a top member (120) and a first thruster (130) affixed thereto. Each module (100) is laterally coupled to e...
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WO/2021/117105A1 |
A cooling apparatus (100) cools an electronic device (2) or other heat-generating device mounted on a satellite or other such carrier. The cooling apparatus (100) is provided with an annular refrigerant flow path (10) formed by sequentia...
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WO/2021/115635A1 |
An overall efficiency of an actuator system can be monitored to determine the health of the actuator system. A ratio between the output power of the actuator system and the input power of the actuator system is monitored over time. Degra...
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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...
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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); ...
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WO/2021/118401A1 |
The invention relates to rocket and aircraft technology. A device for the high-speed intercontinental transportation of passengers is configured in the form of an aircraft provided with extendable landing gear, aerodynamic control surfac...
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WO/2021/114198A1 |
A management method and device. The method is applied to a management device for a movable platform, and comprises: acquiring identification information of a currently configured battery in a movable platform (S301); acquiring an electri...
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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...
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WO/2021/119598A1 |
Disclosed herein are apparatus embodiments and methods for using same that facilitate occlusion of a lumen in a subject. In a particular example, the apparatus is configured for occluding a portion of the lower GI tract (e.g. colon). Fur...
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WO/2021/064300A8 |
Functional professional drone which is remote-controlled by a user and the electronic control unit (500) of which communicates with the electronic control unit for piloting the drone (300), characterised in that the mechanical architectu...
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WO/2021/119346A1 |
A method for controlling application of agrichemical products, comprises acquiring remotely sensed digital image data: developing a prescription to apply at least one agrichemical product in a variable manner based on at least the digita...
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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...
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WO/2021/115167A1 |
A determination apparatus, comprising a circuit. The circuit is configured to: acquire first illuminance measured, in a first time period, by an illumination sensor (500) comprised in a flight body; acquire at least one first variation o...
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WO/2021/116248A1 |
The invention relates to a hybrid fuel system (10) for an aircraft comprising a first subsystem (12) for a first fuel and a second subsystem (14) for an additional second fuel, said second subsystem comprising a circuit (52) of a carrier...
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WO/2021/117388A1 |
Provided are a mobile unit, a control device, and an imaging method with which it is possible to reduce image data. The mobile unit is provided with: a mobile unit body; an imaging device attached to the mobile unit body to capture an im...
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WO/2021/115175A1 |
An image processing apparatus. The apparatus processes an image photographed by a photographing part comprised by an aerial vehicle surrounded by a frame body. An image processing part of the image processing apparatus determines a first...
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WO/2021/118363A1 |
An aerial vehicle (1) comprising; at least three support arms (2) for interconnecting at least three motors (3); at least one battery module (5); at least one of the support arms (2) is configured for supporting the at least one battery ...
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WO/2021/118364A1 |
A light emitting device (1) for a vessel. The device (1) comprises a support structure (5), and two or more light sources (10) attached to different portions of the support structure (5) separated from each other and configured to emit l...
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WO/2021/118391A1 |
The invention relates to the field of aviation, and specifically to pilotless aircrafts of vertical take-off and landing. A multicopter-type aircraft comprises a plurality of rotors with propellers and a motor, an onboard computer and a ...
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WO/2021/116606A1 |
System (11) for balancing at least one parameter to be balanced of an electric motor of a propulsion system (1), in particular of an aircraft, comprising at least two electric motors (3, 4) and a propulsion member (2) driven in rotation ...
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WO/2021/118937A1 |
Systems, devices, and methods including an unmanned aerial vehicle (UAV) (101); one or more inner wing panels (107) of the UAV; one or more outer wing panels (109) of the UAV; at least one inboard propeller (140) attached to at least one...
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WO/2021/118397A1 |
The invention relates to space engineering, and more particularly to spacecraft that can be used individually or in a constellation for monitoring and warning of disasters, providing global Internet coverage and other purposes, and which...
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WO/2021/117933A1 |
A system for monitoring and extinguishing fire using an unmanned aerial vehicle according to one embodiment of the present invention comprises: an unmanned aerial vehicle which scans a fire section from the air, and drops or scatters a f...
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WO/2021/118925A1 |
A system for in-flight stabilization including a plurality of flight components mechanically coupled to an aircraft, wherein the plurality of flight components includes a first flight component and a second flight component opposing the ...
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WO/2021/118928A1 |
Systems, devices, and methods for: an unmanned aerial vehicle (UAV); at least one sensorless motor comprising a set of windings and a rotor; at least one propeller connected to the at least one sensorless motor; a microcontroller in comm...
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WO/2021/117681A1 |
A static electricity eliminating device (10) has: a first conductor (11) electrically connected to at least a part of a static electricity elimination target object 1; and a dielectric shell (15) that forms, between the shell and the fir...
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WO/2021/116566A1 |
The invention relates to a blade pivot (2) with adjustable orientation for a turbomachine fan hub, comprising a stud (4) having means (10) for retaining a fan blade root and coupling means for transmitting a torque, a roller bearing (14)...
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WO/2021/114667A1 |
Disclosed are an airborne nitrogen generator integrating air flushing and membrane separation and a method of use therefor, which belong to the technical field of aviation systems. The airborne nitrogen generator can effectively increase...
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WO/2021/116694A1 |
A pressure altering surface for use in an airspeed measurement system of an aircraft, the pressure altering surface comprising a fluid engaging exterior surface, the fluid engaging outer surface having a portion that is substantially dom...
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WO/2021/117054A1 |
Electric flying vehicle with outer rotor in wheel motor is comprises a brushless motor with propeller in centre of the wheel to fly like a quad copter, and outer rotor coupled with tire will be compact and efficient wheel-mounted electri...
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WO/2021/115660A1 |
The invention relates to a propulsion system (150) comprising a nacelle (202) with an air channel (208) along a longitudinal direction X, an electric motor (108), the output of which drives a propeller (110), and a fuel cell (250) compri...
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WO/2021/112158A1 |
A flight control system (1) for an unmanned aerial vehicle comprising a total station (2) for tracking an unmanned aerial vehicle (3) having a reflector 7 mounted thereon and the reflector and acquiring measurement data including three-d...
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WO/2021/109311A1 |
A ground effect based rotorcraft comprises a fuselage (1), a rotor system (2), ground effect wings (3), side end plates (4), an empennage (5), an engine (22), and a transmission and tilting system (23). The ground effect wings (3) are sy...
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WO/2021/113331A1 |
A multiple hoist system is used with an unmanned aerial vehicle (UAV) for delivering parcels. An example of the multiple hoist system comprises two or more hoists that are independently operable, meaning that a first hoist can lower or r...
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WO/2021/109312A1 |
A morphing aircraft, comprising a fuselage (1), an inner variable wing segment (2), an outer variable wing segment (3), a high-speed wing segment (4), and a morphing mechanism (6). The inner variable wing segment (2) is rotatably connect...
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WO/2021/109529A1 |
A flying car, comprising a body (6) and wheels (4). First wing bays (3) and a second wing bay (5) are arranged on the body; folding wings (8) are respectively arranged in the first wing bays and the second wing bay; the folding wing comp...
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WO/2021/111097A1 |
The present invention provides an unmanned aerial vehicle (100) comprising: a flight system (4) for producing thrust to manoeuvre the unmanned aerial vehicle (100). The flight system (4) comprises: one or more flight rotors (42) defining...
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WO/2021/112954A2 |
A tiltrotor has a range of motion between a forward flight position and a hovering position, where a pylon and the tiltrotor are coupled via a telescoping actuator, a rigid bottom bar, and a fixed hinge that is attached between the rigid...
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WO/2021/110358A1 |
A thermally insulated container for storing a scoopable frozen confectionery and serving a scoop thereof to a consumer, and suitable for mounting within a service cart, the container comprising: a thermally insulated housing having at le...
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WO/2021/110572A1 |
An aircraft door comprising means for retaining a deployable evacuation device (6), said means comprising at least: - a beam (8); - a first retention member (10) fixed on a second end (11) of the beam (8) by a detachable clip (16, 17), t...
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WO/2021/071599A3 |
Nuclear propulsion fission reactor structure has an active core region including fuel element structures, a reflector with rotatable neutron absorber structures (such as drum absorbers), and a core former conformal mating the outer surfa...
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WO/2021/112940A1 |
An integrated electric propulsion assembly includes a stator including at least a first magnetic element generating first magnetic field. The assembly includes a propulsor with an integrated rotor, the propulsor further including a hub r...
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WO/2021/110489A1 |
The invention relates to a deployable structure (10) comprising a segmented structure (20) comprising N assemblies (21) of n articulated adjacent elementary panels (22), the assemblies being joined two by two by a connection panel (24). ...
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WO/2021/064374A9 |
A propulsion management system for an aircraft, an aircraft comprising such a propulsion management system and a method of decelerating an aircraft. The aircraft comprises an air propulsion system having one or more propellers. The propu...
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