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WO/2024/155744A1 |
A landing gear system includes forward and aft structures, each carrying inboard and outboard rotating arms below the structure, the arms each holds a double bogies that, together, form a quad double bogie arrangement. Each structure inc...
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WO/2024/153921A1 |
Two propellant component tanks are integrated and arranged concentrically such that a first tank is contained within but separated from and surrounded by a second tank. A common wall between the tanks acts as an outer wall of the first t...
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WO/2024/155749A1 |
A Vertical Take Off and Landing (VTOL) aircraft is described. The VTOL aircraft has a landing and takeoff configuration form factor suitable for landing and takeoff at a space-constrained location. The VTOL aircraft includes safety featu...
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WO/2024/153713A1 |
An runway incursion detection and warning system (100) for monitoring at least one entity (200), said system comprising airfield signaling devices (801.1), wherein the one or more airfield signaling devices (801.1) each comprise a sensor...
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WO/2024/153627A1 |
A method and system for calculating the accumulated damage on a component of an aircraft, the method comprising determining the weight of the aircraft at a predetermined point of a flight cycle, calculating, based at least partially on t...
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WO/2024/153888A1 |
The present disclosure relates to a method for controlling the speed of an engine assembly (2) of an aircraft (1), comprising updating (S70, S80) the speed setpoint (Nc) of the engine assembly (2) as a function of the current state-of-ch...
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WO/2024/153883A1 |
The invention relates to an aircraft comprising: - drive units, - at least one battery (B1, ..., BM) of the drive units, - at least one electrical generation source that is connected to each battery (B1, ..., BM) and comprises at least o...
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WO/2024/152080A1 |
A lighting system for an accessible space comprising: a plurality of light members each capable of selectively emitting a white light or a blue light in accordance with a determined mode of operation; wherein each of the light members ar...
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WO/2024/153885A1 |
The invention relates to an aircraft comprising: - drive units, - a plurality of batteries (B1, ..., BM) of the drive units, - at least one electrical generation source that is connected to one or more batteries (B1, ..., BM) and compris...
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WO/2024/155655A1 |
A power distribution control approach employs power distribution buses that are controllably energized and de-energized to control which aerial vehicle systems received power based on the applicable operational mode. A method of controll...
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WO/2024/155126A1 |
The present disclosure relates to a 5G or 6G communication system for supporting a higher data transmission rate. According to an embodiment of the present disclosure, safe drone communication or urban air mobility communication can be p...
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WO/2024/154415A1 |
A propulsion device (15) comprises a propeller (20) and an EPU (50). The EPU (50) includes a motor device (60), an inverter device (80), and an EPU housing (55). The motor device (60) includes a motor (61) and is driven to propel an eVTO...
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WO/2024/155537A1 |
A crankcase for a UAV internal combustion engine, comprising a crankcase housing comprising a crankcase chamber, a fuel injection port extending through said crankcase housing to said crankcase chamber, and a fuel diverter comprising a d...
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WO/2024/153297A1 |
The invention relates to a captive balloon support structure assembly (1) comprising a captive balloon which is filled with a lifting gas having a lower density than the ambient air and is kept floating at a specific altitude above the g...
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WO/2024/153647A1 |
The invention relates to a timer device for activating a spacecraft passivation system. The timer device (2) is made up of a control device (4) coupled to a dosimeter (6). The dosimeter is capable of characterizing a dose of radiation to...
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WO/2024/155878A1 |
Embodiments provide mechanisms for coupling rotor blade pitch to propulsion system tilt angle in an aircraft, and more specifically in electric aircrafts. A system may include a tiltable propulsion system configured to move between a fir...
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WO/2024/153887A1 |
The present disclosure relates to a method for controlling the speed of an engine assembly (2) of an aircraft (1). The engine assembly (2) comprises at least a combustion engine (21) and an electric machine (22) mechanically coupled to t...
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WO/2024/153886A1 |
The invention relates to an aircraft comprising: - drive units, - a plurality of batteries of the drive units, - at least one electrical generation source connected to one or more batteries and comprising at least one electrical converte...
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WO/2024/154655A1 |
[Problem] To provide a winch system capable of easily carrying out control of a fuselage suspended by a cable and control of the cable. [Solution] A winch system according to the present disclosure comprises: an electric winch connected ...
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WO/2024/155261A1 |
The present invention relates to a body (2) on the air vehicle; a cockpit (K) that located on the body (2); a canopy (3) that located on the body (2) so as to move relative to the body (2), that allowing access to the cockpit (K) and pro...
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WO/2024/153884A1 |
The invention relates to an aircraft comprising: - drive units, - at least one battery of the drive units, - at least one electricity generation source connected to each battery and comprising at least one electrical converter, and - a p...
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WO/2024/150155A1 |
A proprotor-driven powered-lift aircraft (PPLA) has at least four proprotors, each of which, in rotation, sweeping a respective annulus of radial extent re that covers, by axis- orthogonal projection, a collective length of 2.1 x re of p...
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WO/2024/151846A1 |
A fluid distribution system that uses a hovering distribution device and methods for using such a system are provided. In one example, the system may include a reel that provides a hose for the hovering distribution device. The hovering ...
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WO/2024/149950A1 |
The invention relates to a method for determining an emergency landing plan for an aerial drone, comprising the steps of: applying (2) a main neural network to map data so as to determine at least one candidate area on an emergency landi...
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WO/2024/150013A1 |
A power supply unit for a launch vehicle is disclosed. The power supply unit comprises a protective housing and, within the housing, a control module and a battery holder configured to receive a plurality of replaceable lithium-ion batte...
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WO/2024/151242A1 |
The present invention relates to a door (2) located movably on an air vehicle; at least one pin (3) located fixedly as an extension on the air vehicle; at least one hook (4) located as a hook on the door (2) and enabling the pin (3) to b...
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WO/2024/149902A1 |
A method of operating an aerial vehicle (1), the aerial vehicle (1) comprising a plurality of propulsion units (4, 5) arranged to be pivotable about at least one axis along an angular position and configured to generate a thrust force an...
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WO/2024/151716A1 |
A docking system for use with in-space structures includes a first connector attached to a first in-space structure and a second connector attached to a second in-space structure. The first connector includes a first housing that defines...
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WO/2024/149059A1 |
An unmanned and towbarless aircraft traction control system and an intelligent tractor, relating to the technical fields of aircraft ground movements and human-machine collaboration. The traction control system comprises an aircraft ligh...
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WO/2024/149887A1 |
The invention relates to an optical output system (10) for an aircraft (100) for the graphical output of data, the optical output system (10) comprising a planar output device (20) for the graphical output of data and a data interface de...
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WO/2024/152035A1 |
In one possible embodiment, a propeller adapter is provided which includes a base having at least one fastener hole therethrough and a propeller alignment boss extending upward from the base. Opposing capture walls extend upward from the...
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WO/2024/151253A1 |
A valve includes a first seal seat, a second seal seat, and a flow path for a fluid across the first seal seat. A seal is sealed against the first seal seat and the second seal seat. An actuator is adjacent the first seal seat and is ope...
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WO/2024/152031A1 |
Systems, devices, and methods for determining a placement of a gas collection well based on gathered trace gas data and/or wind speed data including to achieve enhanced gas production: gathering trace gas data over an area of interest (1...
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WO/2024/149580A1 |
Safety system (1) for a boarding bridge (10, 100) and the bridge comprising it. The system comprises a processing unit (13) for examining a telescoping movement of the boarding bridge (10, 100), a first sensor (11) for measuring a first ...
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WO/2024/119106A3 |
Drone roosts, storage facilities, and/or drone delivery mailbox systems can be used to aid in drone deliveries and/or drone deployment. A roost can include a top hatch, a conveyor belt, a drone storage wheel with at least one drone stora...
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WO/2024/150951A1 |
The present invention relates to a brightness control device for NVIS switch lighting using a microcontroller and, more specifically, to a brightness control device for NVIS switch lighting using a microcontroller which precisely control...
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WO/2024/151243A1 |
The present invention relates to at least one body (G) on an air and/or space vehicle; at least one door (2) on the body (G); at least one handle (3) on the door (2), which allows the door (2) to move; a transfer element (6) which is loc...
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WO/2024/148958A1 |
Disclosed is a dual-mode hydraulic servo actuator. The actuator comprises: an oil intake pipeline and an oil return pipeline, wherein the oil intake pipeline is distributed to a servo valve (6) and a first-stage modal selection valve (7)...
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WO/2024/151241A1 |
The present invention relates to a body (G) on an air vehicle; at least one door (2) on the body (G); a locked position (K) in which the door (2) is stationary on the body (G); a free position (S) in which the door (2) is located movably...
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WO/2024/151137A1 |
The present invention relates to a thrust generation apparatus for an unmanned aerial vehicle such as a drone, and more specifically, to a low-noise thrust generation apparatus which generates a similar level of thrust as a typical prope...
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WO/2024/152015A2 |
A system and method for flight control of an aircraft, the flight control system including a plurality of flight components coupled to an aircraft, wherein the plurality of flight components includes a plurality of redundant control surf...
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WO/2024/151705A1 |
A rotor assembly includes a rotor mast, motor, and a rotor hub. The rotor mast may connect to the motor and to the rotor hub. The rotor mast may be rotatable about a first axis. A plurality of blades may be connected to the rotor hub. Th...
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WO/2024/149799A1 |
An electrical propulsion unit (EPU) for an aircraft includes a DC:AC power electronics converter and a transverse flux electrical machine. The transverse flux electrical machine includes a rotor that is drivingly coupled to a rotating sh...
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WO/2024/152011A1 |
A structure of an electric aircraft is disclosed. The structure may include a wing (104), wherein the wing (104) is a single component that runs from a left side of the electric aircraft to a right side of the electric aircraft. The wing...
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WO/2024/151435A1 |
A system, methodology, and computer program identified herein as an in-time aviation safety management system (IASMS) configured to monitor an aviation ecosystem for adverse or off-nominal conditions. Once detected, the IASMS assesses th...
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WO/2024/150071A1 |
Systems and methods of the present disclosure may use a satellite operations center (SOC) to determine a satellite anomaly indicative of a problem with a health or status of satellite. The SOC may generate a satellite anomaly ticket reco...
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WO/2024/152016A1 |
A system for cross-channel communication for effectors (120B, 120) in an electric aircraft (248) is presented. The system may include a flight component (104, 532) of an electric aircraft (248). The system may include a plurality of effe...
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WO/2024/149953A1 |
The invention relates to tooling (20) for visually inspecting an aircraft turbomachine part (10), said part (10) having an annular shape about an axis (X) and comprising an annular attachment flange (14) which is oriented in the radial d...
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WO/2024/151835A1 |
A system of an electric aircraft (200) with pitch control using an elevator (108) is presented. The electric aircraft may include the elevator (108) configured to deflect and a lift lever (112, 600) configured to generate a lift command ...
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WO/2024/149667A1 |
The invention relates to a drive device (30) for an aircraft with a casing device (1) for air guiding, characterised in that the casing device (1) surrounds the drive device (30) at least partially in the peripheral direction, wherein th...
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