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Matches 151 - 200 out of 72,018

Document Document Title
WO/2021/055402A1
A portable landing pad (100) for landing of a drone (200) includes a platform (105) having a flat surface for receiving the drone, and multiple global positioning system (GPS) guided lasers (125) positioned at near edges of the platform ...  
WO/2021/051427A1
Disclosed is a pesticide spraying unmanned aerial vehicle with a quick-insertion-type spray pipe, the unmanned aerial vehicle comprising an unmanned aerial vehicle assembly (1), a pesticide barrel (2), an upper connection pipe assembly (...  
WO/2021/051273A1
An electromagnetic flowmeter, comprising: a housing (101); a pipe group, which is arranged in the housing (101) and which comprises at least two pipes (102) which are provided at an interval; a pair of excitation coils (103), which are u...  
WO/2021/053406A1
The invention is related to the field of air vehicles, in particular to unmanned drones with multiple propellers. The folding drone consists of two housings (1, 2), with motors (5, 6) and impellers (7, 8) mounted thereon, which are inter...  
WO/2021/054782A1
An unmanned aerial vehicle for performing a diagnostic flight before executing a flight, according to various embodiments, comprises: a flight body; a sensor module comprising a plurality of sensors; a communication module for wirelessly...  
WO/2020/180371A3
An electrical power system is disclosed for an aircraft having a hybrid-electric propulsion system, which includes a battery assembly for storing energy, an electric motor controller operatively connected to the battery assembly for cond...  
WO/2021/053328A1
An aircraft cabin (100) is disclosed. The aircraft cabin (100) comprises a plurality of pairs of seat units (120) positioned along an aisle (101). Each aisle seat unit (122 A) comprises an aisle seat (125A) and an aisle footwell (126 A) ...  
WO/2021/053320A1
A method for assisting a pilot to navigate an aircraft when taxiing is disclosed. A centre line of a route, conformal to outside scenery, is displayed on an eyes out screen associated with the pilot. A pictorial indication of the alignme...  
WO/2021/052908A1
In order to improve space allocation, reduce weight and increase aerodynamic performance in high-lift devices (20), an actuator arrangement (24) for a fixed leading edge member (26) is proposed. The fixed leading edge member (26) has an ...  
WO/2021/053227A1
The invention relates to an air conditioning unit (1) for an aircraft, comprising an air circuit (10) with an air inlet (110) and an air outlet (120), at least one "positive" closed-loop cooling circuit (20), comprising a heat exchanger ...  
WO/2021/029947A9
A multicopter incorporates a front tiltwing, modular single-circuit motor, hybrid electric-fuel engine, modular injection-molded structures, and operational algorithms to reduce weight, increase efficiency, reduce greenhouse gas footprin...  
WO/2021/053670A1
Damage mitigating apparatus comprises in one embodiment a damage mitigating aerial vehicle that has sensors for detecting flight related characteristics and a communication unit for commanding activation of parachute deploying apparatus ...  
WO/2021/054859A1
The invention relates to parachute technology, more specifically to a component part of parachute systems, and is intended for releasing a load from a parachute upon landing. The technical result of the solution being patented is an incr...  
WO/2021/053929A1
An aerial vehicle comprises a control unit that obtains tilt information about a tilt of a landing point and sets a horizontal speed according to the tilt information.  
WO/2021/053829A1
[Problem] To provide a flying body having a more fundamental structure and provided with safety measures. [Solution] This flying body comprises: a thrust unit comprising a plurality of rotating blades for generating thrust; a tail wing; ...  
WO/2021/050952A1
This present disclosure relates generally to propulsion systems and, more particularly, to adaptive ducted fan propulsion systems for use with aircraft such as unmanned aerial vehicles. Embodiments of ADF systems in accordance with the p...  
WO/2021/049155A1
The present invention strictly manages the number of aircraft that fly on a predetermined flight path in the same time slot. An operation management system 1 comprises: a flight permission determination unit 12 that, by referencing a d...  
WO/2021/050926A1
A plumbing adapter for use in connecting two plumbing interfaces to one another. The plumbing adapter, which is configured to move between multiple positions in order to accommodate any misalignment between the two plumbing interfaces, c...  
WO/2020/201644A3
The present invention relates to the field of aeronautics and more particularly to a high-lift device and an aerodyne comprising such a high-lift device.  
WO/2021/048500A1
The present invention relates to a method for automatically positioning a plurality of drones (10) moving in a swarm (100), each drone comprising an inertial sensor (22), a location module (23) for a satellite positioning system, an alti...  
WO/2021/048497A1
The present invention relates to a system (1) for recharging an unmanned aerial vehicle, comprising: - a base (20), - a supplying boom (21) comprising a tip (23) and first recharging means (24), - a receiving basket (12) comprising an in...  
WO/2021/049734A1
Disclosed are a sterilization device capable of sterilizing an object using plasma and ultraviolet rays, and an airport sterilization system comprising same. The sterilization device may comprise: a first sterilization unit for irradiati...  
WO/2021/048516A1
The invention provides an airborne passive decoy system for use in the radio waveband, the system comprising a controllable aerial propulsion unit and one or more retroreflectors, wherein the one or more retroreflectors are mounted on, c...  
WO/2021/046592A1
The present invention relates to an armed unmanned aerial vehicle ("UAV"), an armed UAV control system, and methods of use thereof. In one form, the armed UAV includes: an elongate body, a pair opposed side rotor arm assemblies extending...  
WO/2021/048329A1
A table arrangement (10) comprises a mounting element (12), which can be fastened to a fastening structure element (102) and defines a mounting plane (E). The table arrangement (10) further comprises a first table element (20) connected ...  
WO/2021/051072A2  
WO/2021/050177A1
In some embodiments, techniques are provided for analyzing time series data to detect anomalies. In some embodiments, the time series data is processed using a machine learning model. In some embodiments, the machine learning model is tr...  
WO/2021/047351A1
Provided in the present application are an infrared imaging unit, an imaging device, and an unmanned aerial vehicle. The infrared imaging unit comprises an infrared detector; and a heat insulation assembly, wherein the heat insulation as...  
WO/2021/047980A1
Retraction of a landing gear assembly (4) on an aircraft (1) is actuated by a hydraulic actuator (12). The actuator (12) includes a piston (28) that travels within a cylinder (26) along a stroke length between a first position correspond...  
WO/2021/048437A1
The present invention pertains an overhead unit (1) for presenting information, gathering information, transferring information, lighting and/or alarm signals in an individualized manner in a carriage or fuselage, comprising a function m...  
WO/2021/013589A9
Disclosed is a method (81) for arranging a set of antennas capable of transmitting or receiving in a radio frequency range in an existing aerodyne implemented either during an initial installation operation, or in a subsequent maintenanc...  
WO/2021/047988A1
A flapping wing aerial vehicle comprises: a first wing and a second wing opposite to the first wing, a support structure to which the wings are coupled, first and second flapping mechanisms for flapping the first and second wings, and an...  
WO/2021/049513A1
According to the present invention, results when agricultural work is performed by a flying object can be easily managed for each agricultural field. This agricultural work support system comprises: a flight acquisition unit (140) that a...  
WO/2020/217000A3
The invention relates to an air inlet (3) for a nacelle (1) that is intended for an aircraft propulsion assembly, comprising an air inlet (3) upstream of an engine (6), which delimits an air inlet passage, a central section (4) designed ...  
WO/2021/048553A1
A packer (200) for application to an aircraft airframe (100), the packer (200) comprising: a sheet of material having a first surface and a second surface opposite to the first surface; and a plurality of voids (208) defined through the ...  
WO/2021/047683A1
A propeller (10), a power assembly (100), and an aircraft (200). The propeller (10) comprises a hub (101) and blades (103) connected to the hub (101), the radius of the hub (101) being R1, and the radius of the propeller (10) being R2. A...  
WO/2021/048201A1
A powerline engagement system (300) for mounting on a drone (200) or configured to form part of a drone to be engaged with a powerline (100) is disclosed. The system comprises a split core gripper (301), which may be a split core current...  
WO/2021/048589A2
It is a fact that the degree of traction and friction is correlated to the self-weight of the tyre and the exerted load. In addition, the more the exerted or supported load, the more difficult it is to roll the tyre on that surface. Ther...  
WO/2021/049156A1
An objective of the present invention is to provide information useful in controlling aircraft for an airspace in which a plurality of aircraft travel. The airspace information provision system 1 comprises: a peripheral turbulence esti...  
WO/2021/011046A9
Systems, devices, and methods including at least one flight control computer (FCC) (113) associated with at least one UAV (108), where the at least one FCC is configured to: determine a direction of travel of the at least one UAV relativ...  
WO/2021/044114A1
Disclosed is an unmanned Aerial Vehicle, UAV (1), comprising a plurality of rotors (5), a camera (3) and an explosive payload (4), wherein the UAV comprises a generally elongate body, and the camera and the payload are arranged substanti...  
WO/2021/044388A1
The present invention relates to improvements to drones and in particular to a tethered drone (10, Fig. 8), which receives an electric current to power on board motors that operate propellers (17c) and is retained in a limited and relati...  
WO/2021/043839A1
Heat exchanger of an air-conditioning system of a cabin of a transport vehicle, comprising: a primary circuit supplied by a first air flow (169), a secondary circuit supplied by a second air flow (168), a casing (161) defining an air-cir...  
WO/2021/045244A1
In the present invention, an unmanned aerial vehicle or a station identify an empty space of the station to determine whether the unmanned aerial vehicle can land in the empty space and to induce landing. A drone according to the present...  
WO/2020/247148A3
An electrically powered vertical takeoff and landing aircraft (EVTOL) includes a payload module, a plurality of electrical power sources, a wing, and a plurality of electric thrust generators. The wing is pivotally attached to the payloa...  
WO/2021/044142A1
There is provided a thermal management apparatus for use with a vehicle comprising: a chassis in thermal contact with one or more first components that require thermal management and one or more second components that require thermal man...  
WO/2021/046558A1
A cargo aircraft configured to carry a portion of its payload in a cargo bay volume enclosed by a moveable nose door and supported by a structural extension of the fuselage that extends forward into the moveable nose door is disclosed. E...  
WO/2021/043334A1
Provided is an unmanned aerial vehicle, comprising a framework (1), a housing component connected to the framework (1), rotation assemblies (3) provided on the framework (1), and arms (2) installed on the framework (1) by means of the ro...  
WO/2021/043524A1
The invention relates to a method for charging a drone by means of a centring and charging device provided with protruding electromechanical charging contacts for rapid and high-power charging of the drone (between 500 and 1,500 watts). ...  
WO/2021/045994A1
Aspects of the disclosure relate to flight termination systems for aerial vehicles having envelopes. For instance, a flight termination system 400 may include one or more heat sources mounted on the top plate 201 and oriented towards env...  

Matches 151 - 200 out of 72,018