| Document |
Document Title |
|
WO/2024/032907A1 |
An electric vertical take-off and landing aircraft comprises a fuselage (1) and a tilt wing (7). The tilt wing (7) is tiltable relative to the fuselage (1) in a range of tilt wing angles. Control surfaces (13) are arranged at the tilt wi...
|
|
WO/2024/033594A1 |
The invention relates to a method for assisting with propulsion by detecting a failure of a turboshaft engine of an aircraft operating in a nominal mode, the aircraft comprising a deactivated assistance motor, which method comprises a st...
|
|
WO/2024/033590A1 |
The invention relates to a propeller (10) for an aircraft turbine engine, this propeller (10) having: - a hub (12), - vanes (14), - bearings (46, 48) for guiding the roots (18) of the vanes (14) into orifices (12a) in the hub (12), and -...
|
|
WO/2024/033166A1 |
A device for subdividing a passenger cabin (1) of an aircraft, comprising a wall element (2). The wall element (2) has a fastening element so that it can be fastened to at least one element of the passenger cabin (1) in such a way that t...
|
|
WO/2024/031120A1 |
A locking device (1) for locking a pivotably mounted door (21) of a container (20) in the closed position, with a housing (2), at least one hook (3) for hooking into a holder shaft (26), and an actuating handle (4) for unlocking the hook...
|
|
WO/2024/033468A1 |
A computerized system of controlling a bag-drop process via a mobile device is provided. The system is arranged to create a virtual zone in front of a bag-drop station using signal emitter(s) located at the bag-drop station. Signals emit...
|
|
WO/2024/033273A1 |
According to one aspect, the present disclosure relates to a device for reducing the electric charge of a space vehicle, the device comprising: a substrate (201) made of a conductor or semiconductor which is configured to be electrically...
|
|
WO/2024/035714A1 |
A compact and lightweight, drone delivery device propelled by an electric ducted air propulsion system. The device is called an ArcSpear Electric Jet Drone System and is relatively di f ficult to track in flight ( stealth), relatively fa...
|
|
WO/2024/034498A1 |
Provided is a robot arm in which a first sensor detects the posture of a flying robot. The robot arm has a control unit that controls a second drive module, on the basis of a detection signal from the first sensor, and that thereby cause...
|
|
WO/2024/035019A1 |
The present invention relates to a low-impact landing system for a rotary wing aircraft for reducing landing impact transmitted to an airframe (11) upon landing of a rotary wing aircraft (10), comprising: a landing platform (110) having ...
|
|
WO/2024/034419A1 |
This protection device comprises an outer shell container, a protective body, and a driving unit. The protective body is provided with: frame assemblies that each include at least two frames which are disposed at a distance from each oth...
|
|
WO/2024/033589A1 |
The invention relates to an electrical system (100) having: - an electric circuit (102) having a electrically insulating flat support (104) and two electric conductors (106, 108) secured to the flat support, the two electric conductors (...
|
|
WO/2024/033430A1 |
The invention relates to a passenger seat device comprising a stand unit (14a; 14b), a leg support module (20a; 20b) which is pivotally mounted on the stand unit (14a; 14b), a bearing module (29a; 29b) which is designed to adjust the leg...
|
|
WO/2024/030996A1 |
An aircraft air conditioning system comprises intakes ram air from outside the aircraft, and uses a heat exchanger to pretreat (preheat or precool) some of the ram air. The system further includes a heat recovery unit that uses the cabin...
|
|
WO/2024/028671A1 |
Aircraft (1) capable of hovering comprising a fuselage (2), at least one rotor (3a, 3b, 4) that is rotatable with respect to the fuselage (2), electrical drive means adapted to rotate the rotor (3a, 3b, 4) and electrically powered by a b...
|
|
WO/2024/029430A1 |
[Problem] To provide a parachute having a float that can exhibit greater long-term buoyancy than is conventional, without being damaged during deployment, and a safety device and a flying body comprising the same. [Solution] A parachute ...
|
|
WO/2024/028571A1 |
An aircraft landing gear assembly comprising an oleo-pneumatic shock absorber (50) comprising an outer cylinder (52) and sliding tube (54) movable between a compressed position and an extended position, further comprising a sprung elemen...
|
|
WO/2024/030357A1 |
This invention relates to intelligent structural and spatial three-dimensional (3D) real time guidance and training security process. Previously, when police or other law enforcement authorities are dispatched to an ongoing criminal site...
|
|
WO/2024/028016A1 |
A hydrogen fuel delivery system (300) comprises a fuel line (312) having an inlet (315) and an outlet (316), a liquid fuel pump (307) configured to provide a flow of liquid hydrogen fuel from a hydrogen fuel storage tank (308) to the fue...
|
|
WO/2024/028573A1 |
An aircraft landing gear shock absorber strut (50) comprising: an outer cylinder (52) and a sliding tube (54) being movably mounted within the outer cylinder so as to be movable between a compressed position and an extended position, fur...
|
|
WO/2024/028572A1 |
An aircraft landing gear shock absorber strut (50) comprising: an outer cylinder (52) defining an oleo chamber (O) for containing pressurised oleo-pneumatic shock absorber fluid; a sliding tube (52) including a piston head (56) movably m...
|
|
WO/2023/139459A9 |
The present disclosure includes an apparatus (10) for drone landing or drone dropping or wiring down of a package adjustable to a window and/or balcony sill (20) of a building. The present solution thereby innovatively overcomes the desc...
|
|
WO/2024/028817A1 |
A system for generating magnetic fields in one or more axis, the system system comprising a primary electromagnet comprising a first coil having a first axis a first secondary electromagnet comprising a second coil having a second axis, ...
|
|
WO/2024/030530A1 |
An energy harvesting system including a conductor that conducts a first current, a transformer that outputs a second current based on the first current flowing through the conductor, an energy storage device, and a rectifier connected be...
|
|
WO/2024/028739A1 |
An unmanned aerial vehicle (UAV) comprising a rotor module comprising a coaxially arranged rotor having a substantially vertical axis of rotation and a laterally extending rotor housing, a battery located below the rotor module, a shaft ...
|
|
WO/2024/028200A1 |
A method of applying a herbicide to a flood field (1). The method comprises providing an unmanned aerial vehicle (UAV) (2), and flying the UAV (2) along a plurality of substantially parallel spray flight paths (31). The method also compr...
|
|
WO/2024/028858A1 |
An energy attenuation system for a seating system (having a bucket and a frame includes at least one energy attenuation component operatively coupled with a fuse system. The energy attenuation component includes first and second ends sec...
|
|
WO/2024/028710A1 |
The present disclosure provides an aerofoil profile (200) for an aerodynamic element such as a wing, turbine blade, fin, etc. that facilitates the aerodynamic element to keep the boundary layer attached to its top surface with increasing...
|
|
WO/2024/028553A1 |
The invention relates to a turboprop (10) comprising: - a turbine (12) mechanically connected to an input (21) of a reducer (20); - a tail shaft (30) bearing a variable-pitch propeller (31); - a rotary electric machine (46); and - an ele...
|
|
WO/2024/024655A1 |
This hydrogen storage tank for a hydrogen aircraft includes an outer tank, an inner tank, a first strap, and a second strap. The inner tank is disposed inside the outer tank with a space therebetween, and has a shape having a longitudina...
|
|
WO/2024/025491A1 |
The invention relates to motor groups consisting of electric motors for use in electric aircraft and the propulsion system that drives and manages them. Every electric motor has a propeller on the outside, while the rotor and stator inte...
|
|
WO/2024/021319A1 |
A turntable type lifting airport device for a relative motion air kinetic energy aviation aircraft. A plurality of relative motion air kinetic energy reversal thrust generating devices (3) are provided on the periphery of a lower portion...
|
|
WO/2024/023409A1 |
The invention relates to a power supply assembly (1) for a plasma thruster (2) of a spacecraft (100) for controlling a keeper current (Ikeeper) supplied to a keeper electrode (22) of the plasma thruster. The power supply assembly takes i...
|
|
WO/2024/022748A1 |
An effector data connector (22) for data connection of an effector (10) to a firing platform (2). The effector data connector (22) contains a data storage module (34) for recording firing data in order to increase safety during the use o...
|
|
WO/2024/022821A1 |
The present invention relates to a clamping device (6) for fitting a sheet (2) of a flexible material, wherein the clamping device comprises a sealing-strip rail (3) and a sealing-strip body (1), wherein the sealing-strip rail has a guid...
|
|
WO/2024/021399A1 |
The present invention provides an all-electric propulsion satellite orbit transfer method based on autonomous task planning, comprising: step S1, a ground telemetry, tracking, and control system formulates an orbit transfer strategy, and...
|
|
WO/2024/022208A1 |
Disclosed in the present invention is a large-area flexible solar cell wing capable of unfolding in two steps. The solar cell wing comprises a lifting mechanism, an extension mechanism, flexible solar cell arrays capable of unfolding in ...
|
|
WO/2024/025730A1 |
A propeller includes a rotatable hub and at least two propeller blades coupled to the rotatable hub. Each of the propeller blades is formed from a combination of a first material having a negative Poisson's ratio (NPR) and a second mater...
|
|
WO/2024/024991A1 |
The present invention is to provide a remotely drone-controlled, battery-loaded surfboard, in which a plurality of batteries are loaded inside the surfboard, and a guide tube is suspended from the bottom of a drone in the air and has bui...
|
|
WO/2024/023971A1 |
The core part of this invention is in introducing the third body (bodies) launched from the servicing spacecraft. The third body, which can be an unsophisticated and disposable device, should be equipped with the double capabilities of d...
|
|
WO/2024/021135A1 |
Provided in the embodiment of the present application is an aircraft, comprising: a center body; two arm assemblies, which are respectively arranged on opposite sides of the center body, and each of which is provided with a proximal end ...
|
|
WO/2024/024815A1 |
This robot arm has a base end connected to a flying robot, and a tip connected to an end effector. At a plurality of locations between the base end and the tip of the robot arm, first joints that rotate about an axis parallel to a pitch ...
|
|
WO/2024/023410A1 |
The invention relates to an annular enclosure (10) for an intermediate stage of a multi-stage aerospace launcher, the annular enclosure (10) comprising at least two segments (12) together forming a ring defining an axial direction (DA), ...
|
|
WO/2024/023462A1 |
The invention relates to a method for monitoring a propulsion system (102) of an aircraft (100), comprising: - computing a margin of a parameter (NG, T4x) of a thermal chain (TH), this margin being taken as margin (PMD1, PMT1) of the the...
|
|
WO/2024/023316A1 |
The invention relates to a thermal management system (1, 1a, 1b, 41, 51, 61) comprising a fluid cooling circuit (2) comprising a cooling channel (3) in a thermal load (4), a cooling pump (5) arranged to circulate cooling fluid inside the...
|
|
WO/2024/025163A1 |
The present invention relates to a drone station having a function of guiding a drone to a correct position, the drone station comprising: a take-off/landing pad where a drone takes off and lands; and a plurality of landing skid movement...
|
|
WO/2024/021640A1 |
A control method and apparatus, an aircraft, a mobile platform, and a storage medium. The control method comprises: controlling a driving assembly of the aircraft to drive a wing assembly of the aircraft to move relative to a central bod...
|
|
WO/2024/022837A1 |
A deceleration platform for aerial delivery of payloads into water is described. The deceleration platform comprises an upper flexible support for supporting a payload and a lower flexible sheet having a cross-sectional shape which is co...
|
|
WO/2024/022556A1 |
The present invention relates to a propulsion system (1) for an aircraft (50), having a first propulsion unit (11) which has a first power generator (21) for outputting a first electric power (P1) and a first thrust unit (31) connected t...
|
|
WO/2024/022304A1 |
An inlet cone. The inlet cone comprises a body (2) and a nose cone portion (1), wherein the body (2) comprises an outer wall (21), and the nose cone portion (1) is connected to an end of the outer wall (21); an outer surface of the nose ...
|
