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WO/2024/083756A1 |
The present invention relates to a crash handling system (10) for an aircraft, comprising an altitude surveillance system (20), which is adapted to receive altitude data from at least one altitude sensor (22) and to issue an altitude war...
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WO/2024/058619A1 |
The present invention relates to an airship capable of easily switching directions, the airship comprising an aerial vehicle (mother ship) formed in a disc or polygonal shape provided with a jet engine, a rotating body having a jet engin...
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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 ...
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WO/2023/239489A1 |
The present disclosure provides a payload deployment system that is operative to receive and retain a configurable payload. The payload deployment mechanism helps to reduce the drag of the payload and to protect the payload from environm...
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WO/2023/218674A1 |
This flying body comprises: a communication device; a receiver that acquires a current position; a flight controller that controls flight and is able to transmit current position information by using the communication device; a plurality...
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WO/2023/189644A1 |
Provided are a flight device and a flight device control method whereby it is possible to ensure safety even if a defect occurs in a power connection/disconnection unit. A rotor-side power transmission unit 26 of a flight device 10 has...
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WO/2023/169895A1 |
The invention relates to a system for measuring the fatigue (11) of a mechanical structure (10), comprising: - a first force sensor (19.1) capable of generating a first signal (S1) representative of a force applied to a first mechanical ...
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WO/2023/136014A1 |
This flight control device carries out a flight control process for causing an eVTOL to fly. When an EPU abnormality occurs during vertical takeoff, a flight control device (40) performs a during-takeoff process in a flight control proce...
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WO/2023/096414A1 |
A reusable airbag inflator according to an embodiment of the present invention may be provided, the inflator comprising: a gas cartridge mounted with an opening/closing valve which can be opened or closed to discharge compressed gas stor...
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WO/2023/042561A1 |
Provided is a flight device that comprises a plurality of drive sources and that can use, even when any one of the drive sources stops during the flight, another drive source to continue the flight. This flight device 10 is provided wi...
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WO/2023/035086A1 |
A system for detecting smoke in a cargo container in an aircraft cabin is disclosed. The system is exterior to and separate from the cargo container, and may remain in the aircraft cabin when the cargo container is removed. The system co...
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WO/2023/034216A1 |
Force-independent release systems are disclosed. Releasable links are designed for use in connection with inflatable safety devices. Particular examples for use include evacuation slides and/or life rafts on board a passenger transportat...
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WO/2022/255107A1 |
[Problem] To provide a safety device and a flight vehicle provided with a safety device, the safety device not only having excellent safety performance but also allowing for improved accommodation of an ejection object in a container and...
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WO/2022/255000A1 |
[Problem] To provide an actuator capable of achieving a reduced weight compared with conventional actuators while mitigating impact upon actuation, a safety device for ejecting an ejection object, and a flying body equipped with the safe...
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WO/2022/234213A1 |
The invention relates to a seat intended to be fixed to the floor of a vehicle, comprising a seat part incorporating a lower frame, and a backrest incorporating an upper frame secured to the lower frame by at least one fastener (21) that...
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WO/2022/212278A1 |
A system and method for an aircraft evacuation system with hydrogen inflation is disclosed. The system includes an aircraft having an integrated hydrogen-electric engine. A fuel cell stack for powering an aircraft motor of the integrated...
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WO/2022/189877A1 |
The invention relates to an airplane (1) mainly extending along an axis (X-X) between a nose group (11) and a tail group (12). The airplane (1) comprises: i) a fuselage (3) extending axially between the nose group (11) and the tail group...
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WO/2022/173429A1 |
A passenger seat assembly includes a leg, a crushable insert, and a connector assembly. The leg includes an end and a slot extending through the leg proximate to the end, and the slot has a first slot end a second slot end. The crushable...
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WO/2022/168793A1 |
The present invention provides a safety device that can control a landing point when a flight vehicle falls. The safety device is provided in a flight vehicle and comprises: a first parachute that slows the rate of fall and controls the ...
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WO/2022/145410A1 |
This agriculture assistance system is provided with: an unmanned aircraft (70) provided with a sensing device (72); and an agricultural machine (1) capable of traveling through a field. When an abnormality occurs in the unmanned aircraft...
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WO/2022/117453A1 |
An aircraft door architecture comprising: a door (1); an ejector (3); an inflatable evacuation device (4); an emergency energy source (6) connected to the ejector (3) and to the inflatable evacuation device (4); a control unit (9) compri...
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WO/2022/108263A1 |
A flight module control method comprises: an image capturing step for the capturing of a thermal image of at least a portion of a monitored object by an imager of a flying device; a flight path determination step for, on the basis of pre...
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WO/2022/082416A1 |
A deflation device for ejection overload control of a rocket ejection seat. The deflation device comprises single joints (1), a valve seat (4), and an electric initiator (7); the single joints (1) are provided on outer cylinders (10) of ...
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WO/2022/082415A1 |
A method for controlling the ejection overload of a rocket ejection seat, the method comprising: step 1, by means of calculating ballistic performance, obtaining a stroke of a dynamic response index (DRI) at 21ºC and the minimum ejectio...
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WO/2022/086796A1 |
A system and method for evaluating runway conditions that combines known brake control systems with a new runway condition monitoring unit working in conjunction with an anti-skid/brake control unit to improve runway condition evaluation...
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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...
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WO/2022/050031A1 |
The present invention provides a flying device comprising a flight communication unit (24), a device fall determination unit (25, S101), and a flight notification unit (25, S104, S105). The flight communication unit performs wireless com...
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WO/2022/016908A1 |
A helicopter air separation type emergency flight data recording system, comprising: an emergency state analysis system, an ejection system and a cushioning/floating system, wherein the emergency state analysis system is used for determi...
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WO/2022/018790A1 |
The objective of the present invention is to enable easy selection of an unmanned aerial vehicle which is of a plurality of unmanned aerial vehicles autonomously flying and is to be manually operated. An operation terminal device 401 dis...
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WO/2022/009638A1 |
An abnormality warning system (130, 130a) gives a warning of an abnormality in a plurality of motor systems (10) for driving motors (11) each used corresponding to a plurality of rotor blades (30) of an electric aircraft (20). The abnorm...
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WO/2021/233838A1 |
The present invention relates to a metal-polymer laminate structure as well as a method for preparing the same, wherein the metal-polymer laminate structure has an enhanced flame protection function. For the construction of (electric) ve...
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WO/2021/212070A1 |
One method for ejecting a battery from an electric flying vehicle includes monitoring one or more batteries providing power to the electric flying vehicle during a flight, determining when at least one of those batteries is operating as ...
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WO/2021/204679A1 |
A flight jacket (2) comprising a jacket body (4) and a pair of sleeves (6, 8) attached thereto, wherein a restraint cord (12) is mounted on each sleeve extending between a first position at or adjacent the wearer's shoulder and a second ...
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WO/2021/175819A1 |
A leg rest for an aircraft passenger seat, comprising a device, wherein: the device has a housing; the housing has a first and a second housing half; the two housing halves are pivotally connected to one another; the housing is designed ...
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WO/2021/175818A1 |
A leg rest for an aircraft passenger seat, comprising a device, wherein: the device has a housing; the housing has two housing halves; the two housing halves are pivotally connected to one another; the housing is designed such that a lif...
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WO/2021/173803A1 |
A data recording apparatus, data recording system and an orientation determination method thereof is disclosed. The data recording apparatus may include a housing, a wireless communication interface, one or more memories that store execu...
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WO/2021/166839A1 |
An abnormality diagnosis system (130) that diagnoses abnormalities in a plurality of motor systems (10) including a motor (11) for moving a traveling body (20) comprises: a comparison target specification unit (131) that specifies a comp...
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WO/2021/161873A1 |
This propulsion device comprises a gas generator and a plurality of thrusters. The gas generator generates combustion gas when a flying object satisfies emergency conditions. Here, the plurality of thrusters output the combustion gas dow...
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WO/2021/153175A1 |
The objective of the present invention is to realize a configuration for receiving collision risk information from a mobile device such as a drone, generating a corrected path having low collision risk, and performing movement in accorda...
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WO/2021/145191A1 |
[Problem] Provided are a circuit anomaly diagnosis device that can simply and easily diagnose an anomaly in a circuit, a current generation device including the circuit anomaly diagnosis device, an aircraft deployable body ejection devic...
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WO/2021/137975A1 |
An electronic parachute deployment system includes an electronic actuator, a control module, a deployment actuator, and a release mechanism. A parachute is positioned on a payload device, such as a racecar, to slow or stop the payload up...
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WO/2021/123749A1 |
An aircraft passenger suite (100) is provided. The suite (100) comprises an aircraft seat (110) for use by a passenger. The suite (100) also comprises a controller for controlling a number of output states (240) of the suite, the control...
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WO/2021/110572A1 |
An aircraft door comprising means for retaining a deployable evacuation device (6), said means comprising at least: - a beam (8); - a first retention member (10) fixed on a second end (11) of the beam (8) by a detachable clip (16, 17), t...
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WO/2021/093135A1 |
A multi-rotor aircraft (1), comprising a machine frame (11) and a first driving assembly (12), wherein the machine frame (11) comprises a body (111) and two docking parts (112), and the two docking parts (112) are provided on opposite si...
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WO/2021/084872A1 |
Provided is a parachute device capable of reliably opening a parachute. A parachute device (4) has a parachute (400); a parachute accommodating unit (40) that is formed in a tubular shape open at one end and bottomed at the other end a...
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WO/2021/039387A1 |
The present invention pertains to a control device, control method, uncrewed flight vehicle, information processing device, information processing method, and program that are configured so that it is possible to reflect the intention of...
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WO/2021/014712A1 |
The present invention prevents damage to a parachute. A parachute device (4) is characterized by comprising: a parachute (400); a parachute accommodation part (40) that accommodates the parachute; at least one flying body (43) that is ...
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WO/2021/005021A1 |
The invention relates to an emergency opening device of an aircraft door, comprising: - a tubular actuating member (2); - resilient compression means (11); - a member for retaining the tubular actuating member (2), comprising a retaining...
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WO/2021/006339A1 |
[Problem] The present invention addresses the problem of safely moving or landing an aerial vehicle having a plurality of rotor blades when trouble has occurred in a power source. [Solution] An aerial vehicle having a plurality of rotor ...
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WO/2020/204511A1 |
A drone according to an embodiment comprises: a main body; a propulsion unit which is provided outside the main body and generates thrust; a first rotation stabilizing unit which is provided inside the main body or on the top surface of ...
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