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Patent Searching and Data


Matches 151 - 200 out of 57,454

Document Document Title
WO/2022/079398A1
The invention relates to a discharge valve (1) for an aircraft, comprising: a cylindrical body (2) having an inlet (3) and an outlet (4), a first valve (5), a second valve (6) arranged inside the body (2), the first and the second valve ...  
WO/2022/081830A1
In a method for routing communications through a constellation (100) of a plurality of CubeSats orbiting a planet and responsive to a ground controller, the ground controller determines optimal tunnels (210) that include inter-satellite ...  
WO/2022/081242A1
Carbide-based fuel assembly includes outer structural member of ceramic matrix composite material, the interior surface of which is lined in higher temperature regions with an insulation layer of porous refractory ceramic material. A con...  
WO/2022/081035A1
An air curtain device and an air circulation system are provided. The air curtain device includes a main body, an air supply opening configured to receive air, an armrest air jet aperture configured to discharge the received air, and a h...  
WO/2022/077079A1
The present invention patent application relates to a method using real pressure, temperature and mass data obtained from real telemetry to control the mixing ratio by altering the temperature set in its tanks, wherein, for the purposes ...  
WO/2022/079254A1
The present invention relates generally to a system for automatically positioning a drone (1) on a take-off/landing site (2) which comprises a landing area defined by an outer boundary, the system being designed to position a drone (1), ...  
WO/2022/077123A1
There is provided a system for accurate localization and tracking of one or more UAVs. The system comprises a wheeled chassis; at least three pose detecting sensors disposed on the wheeled chassis and configured to operably measure the p...  
WO/2022/073892A1
Disclosed is a supersonic speed attenuator (2) for an air inlet (5) of an aircraft power plant (8), comprising a conical external wall (20) with a tapered end (21) upstream and an internal dividing wall (22) that delimits, with the conic...  
WO/2022/077036A1
A kite (10) which includes a canopy (12) comprising an upper sail (14) and a plurality of rib bridles (26) arranged substantially at an inclined angle relative the upper sail (14), wherein the rib bridles (26) are further connectable to ...  
WO/2022/073465A1
An unmanned aerial vehicle arm mechanism, comprising an upper unmanned aerial vehicle arm (1) and a lower unmanned aerial vehicle arm (2), wherein first slots (3) are arranged on two sides of the lower unmanned aerial vehicle arm (2); in...  
WO/2022/074327A1
Disclosed are a device (24) and a method for diagnosing an engine control unit (16) of an aircraft, said device comprising an autonomous and mobile electronic diagnostic unit (26) and connecting means (28) for connecting the unit to an e...  
WO/2022/076736A1
The present invention comprises a novel autorotation safety device consisting of at least one compressed air tank that is configured to release high velocity air, either autonomously or through the actions of a pilot, into a thrust produ...  
WO/2022/074063A1
The invention relates to an architecture of a braking system for aircraft (1000), comprising a brake (20); an electromechanical actuator (30) associated with a power module (33) connected to a digital communication module (34) by a first...  
WO/2022/073543A1
The invention relates to a hybrid electric drive system (10) for multi-motor aircraft (20). The hybrid electric drive system comprises at least a first and a second hybrid electric drive unit (31, 32), each of which comprises: an interna...  
WO/2022/074405A1
A propulsion system for an aircraft having a two stage contra-rotating fan system to generate thrust. The contra-rotating fan system is surrounded by an aerodynamic duct, having the power train within the duct.  
WO/2022/076040A1
An apparatus providing continuous tilt and variable pitch for rotors on a fixed wing VTOL aircraft. An actuator on a housing rotates a first pivot point on a motor mount to tilt a motor to horizontal and vertical positions. Simultaneousl...  
WO/2021/250330A9
Disclosed is an electrically supplied power chain for a single-propeller aeroplane, characterised in that, upstream, the power chain comprises a supply stage with batteries (12), photovoltaic panels (14) and an electric generator (11) th...  
WO/2022/076288A1
The present disclosure provides compositions, articles thereof, and methods of forming compositions. In at least one aspect, a composition includes (1) an epoxy, (2) an amino or amido hardener, (3) a polyaniline, (4) a dopant selected fr...  
WO/2022/075523A1
The present embodiments relate to a drone and a drone delivery method. The drone can determine can a final product delivery point on the basis of a three-dimensional address corresponding to a specific area of a building, and can horizon...  
WO/2022/073563A1
The present invention relates to a method for inspecting a facility (1), the method comprising at least the following automatically performed steps: • detecting (100a) optical data of at least one facility part (12, 13) of the facility...  
WO/2022/074470A1
A simplex Flight Control Computer (FCC) to be used in a flight control system comprising the simplex Flight Control Computer and at least one neighboring flight control computer is disclosed. The simplex flight control computer comprises...  
WO/2022/075530A1
The present invention relates to an automatic vessel recognition and monitoring system using artificial intelligence image processing, and a method for providing same. More specifically, the present invention provides an automatic vessel...  
WO/2022/075165A1
[Problem] To provide technology capable of realizing safe flight by a flying body without limiting the flight range of the flying body. [Solution] An autonomous mobile device according to the present technology comprises a moving part, a...  
WO/2022/075968A1
Described is a seat track stud for attaching a passenger seat to a seat track having a first stud member, a second stud member, and a pin. The first stud member includes a base portion with at least one flanged edge, a first securing por...  
WO/2022/076101A1
Provided herein are various improvements to launch vehicle payload systems, such as employed to launch and deploy secondary payloads into orbit. In one example, a system includes a fairing configured to encase a payload within an envelop...  
WO/2022/074306A1
This invention discloses a system for detecting the path of moving objects. It comprises: - a first network of N1 telescopes which each have a field angle of M1 degrees and are orientated to cover an arc of C° in a plane P1, M1 being be...  
WO/2022/074322A1
Disclosed are a device (24) and a method for diagnosing an engine control unit (16) of an aircraft, said device comprising an autonomous and mobile electronic diagnostic unit (26) and connecting means (28) for connecting the unit to an e...  
WO/2022/076084A2
Combined moderator-propellant technologies allow a dual-purpose fluid to act as both a nuclear moderator as well as a propellant in a nuclear reactor system, such as a nuclear thermal propulsion (NTP) system. By increasing the mass effic...  
WO/2022/074040A1
Disclosed is a system for protecting an outer surface of an aircraft from icing, comprising at least two fuel cells (112, 212), characterised in that it comprises a first and a third liquid circuit (114, 214) each circulating a coolant f...  
WO/2022/073616A1
A conveyor arrangement (106) for airborne battery replacement between an aerial supply vehicle (102) having a store (108) of replacement batteries (114) suitable to power electric aerial vehicles (104) and an electric aerial vehicle (104...  
WO/2022/074839A1
[Problem] To provide an unmanned rover which, while being compact and lightweight, has improved travel performance on uneven ground and is not readily damaged. [Solution] An unmanned rover comprising a main body part, a pair of wheels wh...  
WO/2022/068041A1
A spraying assembly and a movable platform having same. The spraying assembly comprises: a plurality of liquid storage tanks (10), the plurality of liquid storage tanks (10) being in communication with one another at the bottom to form a...  
WO/2022/067687A1
An operation structure identification method and apparatus for an agricultural plant protection unmanned aerial vehicle, a control method for an agricultural plant protection unmanned aerial vehicle, and a device. The method comprises: a...  
WO/2022/068056A1
A manipulator for an unmanned aerial vehicle. The unmanned aerial vehicle (600) comprises a battery (620) detachably arranged in a battery compartment (610); the manipulator comprises a base (100), a mechanical arm (200), a clamping mech...  
WO/2022/071891A1
The present invention relates to a system for detecting a foreign object on a runway. The system includes a thermal camera having a first field of view and adapted to capture a thermal image of an area of interest on the runway, a visibl...  
WO/2022/072551A1
Rescue parachute deployment systems (RPDSs) and related techniques are provided to improve the safety and operational flexibility of unmanned aerial vehicles (UAVs). An RPDS includes a canopy assembly (168), a rotor guard (680, 682) disp...  
WO/2022/071104A1
A motor-driven movable body (510) comprises an output shaft (531) and a plurality of motors (571, 572) for driving the output shaft. This motor-driven movable body executes multiple drive control for assigning at least two of the plurali...  
WO/2022/070851A1
[Problem] To make it easy to set the flight path of a flight vehicle on site. [Solution] A method relating to the control of a flight vehicle, said method including: acquiring information about an image captured by an uncrewed flight veh...  
WO/2022/071830A1
The invention relates to space-based information systems for comprehensive Earth monitoring. The present space-based system comprises compact and lightweight spacecraft which interact with distributed ground control centres for receiving...  
WO/2022/069834A1
The invention relates to a turbine engine module of longitudinal axis X, comprising an unducted propeller (2) intended to be rotated around the longitudinal axis X by a power shaft (10, 11) which is connected at least to a rotor member (...  
WO/2022/072465A1
The present embodiment discloses a mobile security system for managing pedestrian activities from a perimeter of a venue to a point of entry to the venue as well as pedestrian entry into the venue is provided. The security system include...  
WO/2022/072430A1
Systems and methods for controlling satellites are provided. In one example embodiment, a computing system can obtain a request for image data. The request can be associated with a priority for acquiring the image data. The computing sys...  
WO/2022/069749A1
A spacecraft, for example a satellite, or a part thereof having a coating comprising a 2D material on an outer surface thereof is described. The 2D material comprises one or more elements, excluding C, N and S, in an amount of at least 5...  
WO/2022/068059A1
A liquid storage assembly, a spraying device and a movable platform. The liquid storage assembly comprises a liquid storage body (10) and a liquid level meter (20), wherein the liquid storage body (10) and the liquid level meter (20) are...  
WO/2022/070371A1
A propeller guard 2 comprises a propeller guard body 10 that is configured so as to surround the propeller 30 of a flight vehicle 20, and a repulsive member 40 having a first end and a second end, protruding from the propeller guard body...  
WO/2022/069957A1
An armed aerial platform (100) includes a weapon for firing a projectile from a barrel (102) that defines a weapon axis (104). The weapon is supported by a single-axis gimbal mechanism (116) within a central vertical slot (112) in a rigi...  
WO/2022/070375A1
This propeller guard 2 comprises: a propeller guard body 10 configured to surround a propeller 30 of a flight vehicle 20; and a repulsion mechanism 40 which has a first end section 45 and a second end section 46 and protrusively formed o...  
WO/2022/069101A1
A cover panel for an aircraft, comprising: a first region, a second region for forming an overlap with a second panel, and a ramp, wherein at least a portion of the ramp is between the first and second regions, wherein the ramp includes ...  
WO/2022/067492A1
An aerial vehicle, comprising: a main body fuselage (6); a front base (1) connected to the front portion of the main body fuselage (6); a rear base (8) connected to the rear portion of the main body fuselage (6); multiple external ducts ...  
WO/2022/069835A1
The invention relates to a turbomachine module having a longitudinal axis X, comprising a shroudless propeller (2) which is rotated about the longitudinal axis X by a drive shaft (9, 10), which is connected at least to a compressor rotor...  

Matches 151 - 200 out of 57,454