| Document |
Document Title |
|
WO/2023/191013A1 |
[Problem] Provided are: a parachute which can be increased in size at low cost, and the strength of which can be more improved than conventional, regardless of having a relatively small number of panels; and a safety device and a flying ...
|
|
WO/2023/183983A1 |
An unmanned fixed wing vertical take-off and landing aircraft, comprising: an elongate fuselage defining a longitudinal axis, the fuselage having a nose and a tail; a pair of rearward swept fixed wings, each wing having a root end respec...
|
|
WO/2023/188266A1 |
This aircraft comprises: a body; a plurality of arms which are connected to the body; a plurality of motors which are disposed on the leading ends of the plurality of arms; and a plurality of propellers which are rotated by the plurality...
|
|
WO/2023/187283A1 |
The present invention relates to a method (10) for allocating requests for observations of geographical areas (ZG) to be made to a plurality of satellites (30), the method comprising the steps of: - (S10) breaking down each geographical ...
|
|
WO/2023/187284A1 |
The invention relates to a suspension assembly for a turbomachine (10), the assembly comprising: • - a beam (12) for the attachment thereof to an aircraft pylon (13), the beam (12) comprising a first portion (12a) and a second portion ...
|
|
WO/2023/188270A1 |
This aircraft comprises a first communication unit that performs first wireless communication, a second communication unit that performs second wireless communication different from the first wireless communication, and a control unit th...
|
|
WO/2023/184947A1 |
A monitoring and repairing method for a parachute system (100) for planetary exploration. The method comprises the steps of: a sensor (40) sensing the impact force of dust and generating a sensing signal; an electrode in a fuse (54) rece...
|
|
WO/2023/184150A1 |
Provided in the embodiments of the present disclosure is an aircraft. The aircraft comprises a frame and a driving device, wherein a wing fixed supporting rod, a wing rotary supporting rod, and a wingtip supporting rod are arranged on th...
|
|
WO/2023/187298A1 |
The invention relates to a propulsion assembly for an aircraft, comprising a nacelle (24) which comprises a fan compartment (48), a front cowling (34) forming an air inlet, and an intermediate section (36) including at least one intermed...
|
|
WO/2023/187597A1 |
Disclosed is an air transporter (10) for ocean freight containers, which is a device comprising propellors (20) that enable same to fly to reach an unloading area on a cargo ship and to lift the containers (40) to carry them to a holding...
|
|
WO/2023/184653A1 |
The present invention provides an automatic filling apparatus for an unmanned aerial vehicle rocket booster, comprising a supporting bracket, wherein a raising/lowering module for adjusting a rocket booster to move up and down is fixedly...
|
|
WO/2023/190327A1 |
This vehicle comprises: a front seat 2 the posture of which can be changed between a first posture in which a seating surface faces forward and a second posture in which the seating surface faces rearward; a rear seat 3 that is arranged ...
|
|
WO/2023/182127A1 |
Provided is a flying apparatus in which inner ends of arms can be rigidly connected to an airframe. A flying apparatus 10 comprises an airframe 11, arms 12, and rotors 13. The arms 12 each have a first arm part 121 and a second arm par...
|
|
WO/2023/178687A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a main body (10), first rotation portions (20), and first arms (30). The first arms (30) can rotate around the first rotation portions (20) relative to the mai...
|
|
WO/2023/178490A1 |
A control method for an unmanned aerial vehicle, the method comprising: acquiring a state of a base station, wherein the base station provides an accommodation space for an unmanned aerial vehicle and is used for the unmanned aerial vehi...
|
|
WO/2023/181027A1 |
A deployment system pivotably deploys panel elements between a stowed configuration and a deployed configuration. Actuator(s) associated with each pair of panel elements include a first bracket mountable to one panel element, a second br...
|
|
WO/2023/180267A1 |
The invention relates to a propelled vehicle (D1; D2) comprising: an electrical power source (SE), a chassis (C), a first shaft (A1) supporting a propulsion unit (P) and mounted such that it can rotate on the chassis about a first axis (...
|
|
WO/2023/181036A2 |
A system and method for autonomously landing a Vertical Take-Off and Landing (VTOL) aircraft on a landing surface is provided. At least one primary sensor is mounted to the VTOL aircraft. A processing circuitry is configured to repeatedl...
|
|
WO/2023/181355A1 |
An information processing device 2X comprises a data acquisition means 32X and a maneuver detection means 33X. The data acquisition means 32X acquires time-series data that represents the position and time at which a space object having ...
|
|
WO/2023/180612A1 |
Disclosed is a method for carrying out tasks on infrastructure, which is implemented using a system of uncrewed vehicles, preferably drones, which comprises a base vehicle (1) and at least one host vehicle (2). The base vehicle (1) moves...
|
|
WO/2023/180449A1 |
The invention relates to a vehicle, which can be used either as an aircraft or ground effect vehicle or as an aircraft and ground effect vehicle, comprising a fuselage (4) and at least two front wings (2), wherein the fuselage (4), when ...
|
|
WO/2023/180381A1 |
The present invention relates to an electrically driven ducted fan engine (10), comprising a housing (12) with an inner housing wall (12a), defining a substantially cylindrical inner space (14) and a longitudinal axis (L), an inlet openi...
|
|
WO/2023/180838A1 |
A method of 3D motion reconstruction of outdoor, highly flexible moving subjects with multiple cameras on drones is described herein. A multi-drone capturing system is used to remove the restriction of a dedicated virtual reality shootin...
|
|
WO/2023/178477A1 |
A vibration reduction structure (10), comprising a first support (12), a plurality of groups of vibration reduction members (18), a second support (14), and a third support (16), wherein the second support (14) is connected to a head por...
|
|
WO/2023/178512A1 |
The present invention relates to the technical field of plant protection, and in particular to a mobile platform (10). The mobile platform (10) comprises: a body (100); a container (200), the container (200) being provided with a liquid ...
|
|
WO/2023/179037A1 |
An outer duct nozzle of an aerial turbofan engine. A notch (3) is formed in an engine nacelle rear edge (4) on the outer side of an engine pylon (2), a flow guide curved surface (7) matching the notch (3) in shape is provided on the oute...
|
|
WO/2023/126936A9 |
The present subject matter provides a combination system for manipulating an electrical potential of a plurality of plants and manipulating an electrical charge of particles that interact with at least one plant of which electrical poten...
|
|
WO/2023/183167A1 |
A method for managing propellant in a spacecraft is disclosed. The method includes storing liquid propellant in a tank under an operating pressure controlled using a product of chemical decomposition of the propellant. The method may inc...
|
|
WO/2023/178456A1 |
The present invention relates to a tensegrity-type membrane structure, the aim of which is to provide a structure that levitates by means of a vacuum chamber and that can be used for the transport of cargo and/or people. The invention wo...
|
|
WO/2023/183522A1 |
An electrically operated window shade system includes a frame that is mounted on the outer side of the inner wall of an aircraft cabin. A cassette is mounted in the frame and includes one or more motors and drive systems and one or two s...
|
|
WO/2023/178688A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises a housing (10), a heating component (20), a heat sink (30) and an arm assembly (40). The housing (10) is provided with an air inlet (11) and an air outlet (12)...
|
|
WO/2023/181029A1 |
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/2023/181354A1 |
An information processing device 2X is provided with a data acquisition means 32X and an abnormality degree calculation means 33X. The data acquisition means 32X acquires time-series data representing the luminous intensity of a space ob...
|
|
WO/2023/183515A1 |
Provided in this disclosure is a dual-motor propulsion assembly, and corresponding methods of operation, that is configured for use in an electric aircraft. Dual-motor propulsion assembly provides redundant systems by including verticall...
|
|
WO/2023/180646A1 |
The invention relates to a method (100) for controlling the orbit of a satellite, which method comprises: - determining (102) a manoeuvre plan (PMA) comprising at least one previous manoeuvre (PM1) of the previous manoeuvre plan (PPMA), ...
|
|
WO/2023/182089A1 |
The purpose of the present invention is to improve the accuracy of three-dimensional surveying if sloping ground is included in the target region for surveying. A control device according to the present technology comprises: a point cl...
|
|
WO/2023/180270A1 |
The invention relates to a propelled vehicle including: a chassis, a first shaft comprising a crown that is rotationally symmetrical about a first axis and rotatably mounted on the chassis about the first axis of rotation, a first drive ...
|
|
WO/2023/179403A1 |
Disclosed in embodiments of the present disclosure are a capturing system and method for a spatial target. The capturing system comprises a plurality of capturing devices, a conveying device, a transmitting device, and a speed reduction ...
|
|
WO/2023/181490A1 |
An electric fan comprising: an electric motor having an output shaft extending along an axis and a cylindrical housing centered on the axis; an inner duct provided on the downstream side of the electric motor; a plurality of blades mount...
|
|
WO/2023/183267A2 |
The present invention pertains to a system and method for transportation of goods, service, marketable securities or other valuable payloads optionally utilizing a carrier or smart carrier to contain a payload and using artillery for tra...
|
|
WO/2023/181829A1 |
The present invention realizes a transport system that has high transport reliability and is simplified. The transport system (100) comprises: a deposit place (3) for depositing baggage (200); a supply device (1) for supplying a tray (9)...
|
|
WO/2023/180166A1 |
The present invention relates to a device for automatically locking an adjusting member comprising an outer element (2), secured to a mechanical system, provided on its inner wall with an internal thread and intended to receive a movable...
|
|
WO/2023/177986A1 |
Described herein are apparatuses and methods for use therewith that can be used to remove dust and other types of particulates from a solar array of a spacecraft, a lander, a rover, or the like. Such an apparatus can include a main body ...
|
|
WO/2023/175127A1 |
Protective envelope for a portion (2 to 7) of an aircraft body (1), comprising a framework (23) and a fabric (24), the fabric (24) being mechanically coupled to the framework (23) and extending around the framework (23) such that, in a d...
|
|
WO/2023/178121A1 |
A calibration of an unmanned aerial vehicle is performed without the use of a magnetometer. The unmanned aerial vehicle generates a first acceleration vector in a navigation frame of reference and a second acceleration vector in a GPS fr...
|
|
WO/2023/177774A1 |
A vehicle for travelling on a road and in the air is provided, comprising a fuselage extending from a forward to a rear end along a horizontal longitudinal roll axis, a pair of main wings mounted on the rear end of the fuselage, a pair o...
|
|
WO/2023/176782A1 |
Provided is a flying apparatus in which the engine can be effectively cooled during flight. The flying apparatus 10 is provided with an airframe 19, a rotor 14, an engine 30, and a cooling unit 11 for cooling the engine 30. The cooling...
|
|
WO/2023/178180A2 |
The present disclosure provides cargo systems for unmanned aircraft systems ("UAS") such as drones, and method of using same to deliver (e.g., load, transport, and unload) cargo.
|
|
WO/2023/178175A2 |
Exemplary disclosed embodiments include systems, methods, and devices for a ground maneuvering system for aircraft. The systems, methods, and devices may include a ground maneuvering system including at least one processor in communicati...
|
|
WO/2023/173202A1 |
A brake assembly is suitable for use in conjunction with a wheel having a rim rotatably mounted to an axle. The brake assembly includes a rotor configured to rotate about the axis with the rim. The rotor has a first frustoconical rotor s...
|
