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Patent Searching and Data


Matches 601 - 650 out of 72,018

Document Document Title
WO/2020/260980A1
An anti-torque rotor (4) is described comprising: a mast (6) rotatable about a first axis (A); a plurality of blades (8) rotatable about respective second axes (B); an element (16) slidable along the first axis (A) with respect to the ma...  
WO/2020/262105A1
At the time of a disaster such as an earthquake, a level difference may occur at a joint of a paved road surface. It is therefore suggested that a flying object (10) is caused to fly to a location at which the possibility of such an occu...  
WO/2020/261149A1
The present invention is related to a flight propulsion system for Vertical Take-Off and Landing (VTOL) and Short Take-Off and Landing (STOL) aircraft, which comprises a two cyclorotors (1, 8), installed in the front and rear portions of...  
WO/2020/262060A1
The present disclosure relates to a mobile body, a control method, and a program that enable safer stopping. A degree-of-safety calculation unit calculates a degree of safety of a flat surface on the basis of flat-surface information abo...  
WO/2020/260269A1
Disclosed is a method of operating a landing gear controller for an aircraft. The method comprises the landing gear controller receiving one or more signals from at least one position sensor. The one or more signals indicate a position o...  
WO/2020/263479A1
A power transfer unit includes a first hydraulic circuit, a second hydraulic circuit fluidly connected to the first hydraulic circuit, a pump and motor assembly fluidly connected between the first hydraulic circuit and the second hydraul...  
WO/2020/260209A1
An automated mechanical machining system (S) for machining a metal panel (P) comprising a first face (F1) and a second face (F2) which is on the opposite side from the first face (F1), the automated mechanical machining system (S) compri...  
WO/2020/264306A1
A fuselage may include a base plate including one or more attachment points for securing the base plate to an unmanned aerial vehicle, a cover removably securable to the base plate, and a cargo compartment disposed in a space between the...  
WO/2020/188604A4
The present invention discloses a VTOL aircraft with retractable wings and TEMCS (trailing edge mounted control surface) mounted tilt-able engines. The aircraft has two hover modes; a first hover mode with retracted wings which allows ta...  
WO/2020/264467A1
A dust cover for an aerospace window that comprises dust cover having an exterior substrate and an interior substrate in a spaced apart relationship with a substantially transparent coupling agent therebetween. The dust cover is disposed...  
WO/2020/222718A3
The invention is related to an ULD apparatus (1) which helps loading cargo packages to ULD pallets used in air transportation, comprises a frame (2) which is in different structures according to the type of the airplane and pallet, forms...  
WO/2020/257883A1
A muffler (40) devised particularly for use with an engine of the type used on unmanned aerial vehicles (UAVs), and a UAV (10) having an engine (30) fitted with the muffler (40). The muffler (40) comprises a body (51) having an interior ...  
WO/2020/263032A1
Disclosed is a paraglider harness that is portable and easy to carry due to removal of the weight and volume of buffer material and is capable of providing both the convenience of being portable and easy to carry, and safety during use b...  
WO/2020/260868A1
Disclosed herein is a method of controlling an aircraft, the aircraft comprising a plurality of actuators (204a, 204b), a plurality of actuator control units (203a, 203b), and a plurality of flight control systems (202a, 202b) for genera...  
WO/2020/260581A1
An aircraft is disclosed, having wings (2) which extend outward from the longitudinal axis and in each of which at least two rotors (3) for generating lift are provided, wherein the rotors (3) are connected to at least one flywheel in or...  
WO/2020/260662A1
Systems and methods for determining parameters suitable for determining an orbit of a satellite using TDOA parameters and several spaced receivers.  
WO/2020/254393A1
The invention relates to a temperature-control device (100) for an aircraft (102), which device has a first layer (104) and a second layer (106) opposite the first layer (104), a heating layer (108), which is arranged between the first l...  
WO/2020/256591A1
The invention relates to robotic systems for operating, lifting and lowering technical equipment on tall engineering structures. The system consists of a drone with a load-carrying platform mounted thereon, a flexible suspension system, ...  
WO/2020/253985A1
Disclosed is an aircraft door comprising: - a first handling arm and a first forearm; - a second handling arm and a second forearm; - a holding device movable between: an immobilising position in which the first forearm and the second fo...  
WO/2020/254386A1
The application relates to a pipe support block for an aircraft fluid system. The pipe support block is arranged to support a pipe on a structural member, such as a bracket. The pipe support has a first part and a second part which toget...  
WO/2020/256173A1
Disclosed are a precise landing method using multiple patterns in an unmanned aerial control system, and a device therefor. Specifically, an aspect of the present invention relates to a precise landing method of an unmanned flying robot ...  
WO/2020/253614A1
Disclosed are a solar floating parking apron and a matching single-blade unmanned aerial vehicle, comprising a parking apron and a single-blade unmanned aerial vehicle. The parking apron is suspended in the air by means of the buoyancy o...  
WO/2020/256629A1
The present disclosure relates to a landing assistance system and method (100) for assisting an airborne vehicle (1) during landing on a landing area (2). The landing assistance system (100) provides the airborne vehicle (1) with light s...  
WO/2020/254973A1
Drone (5) which comprises a plurality of propellers (16) driven by motors (17) supported by at least one structure (18) with a winch (8) provided with a drum which can rotate by means of a motor (22) to unwind or wind a suspended cable (...  
WO/2020/254755A1
The invention relates to an electrical air conditioning system for air-conditioning a cabin (10) of an aircraft comprising a source (11) of fresh air, a dynamic air circulation duct (12), a motorized compressor (13) comprising an air inl...  
WO/2020/256889A2
A process, an article of manufacture, and a product for efficient and cost-effective capture of greenhouse gases and air pollutants directly from the air using an unmanned vehicle including materials reclaimed from the atmosphere. The ma...  
WO/2020/253986A1
Aircraft door comprising a support arm (10) connecting a door leaf (5) and a door frame (13), the locking/unlocking mechanism of which comprises: • a control shaft (17) extending along a substantially vertical axis; • a guide track (...  
WO/2020/253622A1
The present invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a fire-fighting and disaster relief unmanned aerial vehicle, comprising a main fuselage, a fixing frame and a bomb release dev...  
WO/2020/256571A1
A foldable tandem wing aircraft may be fixed for flight and fold for storage, packaging or transporting and otherwise using the aircraft while not in flight is disclosed. An embodiment includes forward and rear wings which folds and unfo...  
WO/2020/256024A1
A satellite constellation formation system forms a satellite constellation (20) having an N number (N being a natural number) of orbital planes (21) having mutually different normal directions. A satellite constellation formation unit fo...  
WO/2020/256505A1
A wheeled wired/wireless charging device is formed in an L shape and has: a wheeled charging connector, equipped with a battery having a body in a hexahedral shape and the like, or a port for connecting the charging connector; a plug and...  
WO/2020/257670A1
An aircraft airfoil having a wave assembly. The airfoil may include a leading edge, a trailing edge position opposite the leading edge, a pressure side extending between the leading edge and the trailing edge, and a suction side extendin...  
WO/2020/254812A1
The invention concerns a deformable aerospace structure comprising a first layer and a second layer spaced from the first layer and defining a space therebetween. The space comprises one or more reinforcement elements extending between t...  
WO/2020/254560A1
Disclosed is an actuation unit (15) for actuating a foldable wing tip portion (9) of a wing (3) for an aircraft (1), the actuation unit (15) comprising a motor (17) configured to be mounted to a fixed wing (5) for an aircraft (1), a driv...  
WO/2020/254754A1
The invention relates to an assembly of heat exchangers comprising a dynamic air flow channel (14) extending in a longitudinal direction and characterised in that it comprises at least two heat exchangers (12a, 12b) which are separated a...  
WO/2020/257443A1
Integrated pultruded composite profiles such as rotor wings and blades for electric vertical take-off and landing aircraft, light helicopters, wind turbines, and other rotor wing applications and integrated design and processing methods ...  
WO/2020/255310A1
A satellite constellation formation system forms a satellite constellation (20) having an N number (N being a natural number) of orbital planes (21) having mutually different normal directions. A satellite constellation formation unit fo...  
WO/2020/253623A1
Provided are a bomb dropping device (32) and a fire rescue drone. The bomb dropping device (32) comprises a cartridge (325) for containing fire extinguishing bombs, a mounting seat (326) and a limiting mechanism (327), wherein the mounti...  
WO/2020/256792A1
A structure for changing the attitude of a spacecraft is provided including an elongated member and a plurality of actuators coupled to the elongated member. The elongated member is coupled to the spacecraft. The elongated member has a l...  
WO/2020/254980A1
Drone (5) which comprises a plurality of propellers (16) driven by motors (17) supported by at least one structure (18), in which a plurality of converters (15) are arranged around the structure (18) to convert electricity to high voltag...  
WO/2020/255472A1
Provided is an arrangement determination apparatus comprising: a target area specifying unit that specifies a target area in which a plurality of frying bodies that irradiate the ground with a beam to form a wireless communication area o...  
WO/2020/254895A1
An anti-torque rotor (4, 4') is described that comprises: a mast (6) rotatable about a first axis (A); a plurality of blades (8) extending along respective second axes (B); a control element (16) sliding along the first axis (A) with res...  
WO/2020/253621A1
The present invention relates to the technical field of unmanned aerial vehicles, and particularly relates to a support frame fitting structure, comprising: a housing provided with a fastening block at a base thereof; a support frame, wh...  
WO/2020/255729A1
This operation assistance device 10 is provided with: a flight control unit 11 which causes a second unmanned aerial vehicle including an image capturing device to fly and follow a first unmanned aerial vehicle operated by an operator, a...  
WO/2020/253974A1
Method of surface protection of fasteners by application of sealant and paint, which comprises the following steps according to the following sequence:positioning a plurality of overcoat nozzles (1) on a rack (2); painting the interior o...  
WO/2020/253987A1
The invention relates to an aircraft door comprising a support arm (6) connected to a support forearm (9) by a first pivot connection (7) about a first pivot axis (8), the support forearm (9) being connected to the leaf (5) by a second p...  
WO/2020/253548A1
A goods receiving and delivering device for unmanned aerial vehicle logistics, comprising: a take-off and landing platform (3A) of a logistics unmanned aerial vehicle; and a bearing bracket (3), provided with the take-off and landing pla...  
WO/2020/257649A1
Various embodiments of a vortex thruster system is described herein that is configured to create at least three discrete thrust levels. In some embodiments, the vortex thruster system is configured to decompose a monopropellant and deliv...  
WO/2020/254921A1
This invention relates to a payload delivery mechanism suitable for use with a drone. The mechanism includes a load carrying and release mechanism which is displaceable between a retaining position, in which at least part of the payload ...  
WO/2020/255283A1
A wireless mobile body 1 comprises a response unit 32 that responds to a call mediated by a voice channel of a mobile communication network, and a control unit 36 that controls the action of the wireless mobile body on the basis of opera...  

Matches 601 - 650 out of 72,018