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JP2023511703A |
In one aspect, described herein is an aircraft capable of carrying a payload of at least 400 pounds. One embodiment has four rotor systems, each independently driven by an electric motor or other source of torque. Each of the rotor syste...
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JP7241504B2 |
Systems and methods are provided for aircraft fire extinguishing with heated tubing. One example is a fire extinguishing system that includes a container configured to store a fire extinguishing agent, a tube configured to transport the ...
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JP7231393B2 |
In an example, a system includes a first controller for controlling a first-flight-control surface, a second controller for controlling a second-flight-control surface, and a first override system including a mechanical linkage between t...
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JP7224271B2 |
Provided is a parachute device capable of reliably opening a parachute. A parachute device includes a parachute, a parachute accommodation section formed in a tubular shape including an opening at one end and a bottom at another end, the...
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JP2023023283A |
To provide a safety device whose number of components is reduced more than before so as to be reduced in weight and simplified in manufacturing work, and provide a flight body equipped with the safety device.A safety device 100 comprises...
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JP2023019321A |
To provide a control apparatus having sufficient redundancy.There is provided, according to one aspect of the present invention, a control apparatus that controls driving of a plurality of drivers. The control apparatus comprises a plura...
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JP7215286B2 |
To attenuate an impact force at the time of collision.A flight vehicle 1 comprises: a body 2; a thrust generation part 10 that generates thrust for flying in the air; and a variable part 15 that connects the body 2 and the thrust generat...
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JP2023502477A |
The present invention is an aircraft seat comprising an actuator and a motion transmission device (22), - a frame (26) comprising at least one supporting surface (34, 38) and one braking surface (36, 40); - a drive (28) rotatable relativ...
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JP7208533B2 |
To provide an unmanned flying body which achieves redundancy without increasing a rotary wing.An unmanned flying body includes a flight controller 19 for determining rotation numbers of a plurality of motors 15 to 18 for rotationally dri...
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JP2023008884A |
To provide a vehicle comprising: an internal cabin; multiple passenger service units (PSUs) within the internal cabin; and an emergency oxygen system within the internal cabin.A vehicle includes an internal cabin. Multiple passenger serv...
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JP2023002486A |
To provide a system and a method for effectively and efficiently suppressing fire within a lavatory of a commercial aircraft.A fire suppression system (200) for an enclosed space, such as within a lavatory (100) of a vehicle, includes a ...
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JP7191090B2 |
[Summary][Problem] Provided are a flying object operating device, a malfunction preventing method for a flying object operating device, a flying object thrust generating device, a parachute or paraglider deploying device, and an airbag d...
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JP2022185549A |
To assist deceleration and descent of an aircraft and cushioning of descent impact force, and guarantee safety of an aircraft and occupants in the aircraft.A lifesaving system includes an aircraft body, wherein an openable/closable safet...
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JP2022185561A |
To solve the technical problem that there is no device for assisting deceleration and descent of an aircraft and cushioning of a descent impact force in an aircraft, and safety of an aircraft and occupants in the aircraft cannot be surel...
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JP2022184249A |
To provide a safety device which has excellent safety performance, is also capable of improving storability of injected objects in a container, and of securing more diversity of fitting positions to a flying body than conventional, and a...
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JP7179065B2 |
The present disclosure relates to a cargo protection method, device and system, and a non-transitory computer-readable storage medium, relating to the technical field of unmanned aerial vehicles. The method of the present disclosure incl...
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JP7177635B2 |
A method for detecting tampering with a stowage container can include configuring the stowage container, the stowage container comprising a container housing and a barrier, wherein edges of the barrier overlap edges of the container hous...
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JP7177636B2 |
A stowage container including a barrier such as a door or access panel and a breach detector for monitoring and/or detecting a breach of the barrier. The breach detector includes an indicator assembly having a slot that can be positioned...
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JP7174661B2 |
A communication management device provided in a flight vehicle that communicates with a base station management device that manages a plurality of base stations, includes: a first communication unit that transmits and receives control si...
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JP7166070B2 |
An inerting system for aircraft including a gas circuit with successively at least one air inlet, a compressor and an air separation module. The air separation module includes an outlet for oxygen-enriched gas and an outlet for inerting ...
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JP2022167542A |
To provide a multicopter that can perform emergency landing stably from any altitude.A multicopter 1 includes: an airframe 11; a battery 31 capable of discharging power for flying the airframe 11; and an engine power generation unit 12 f...
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JP7164633B2 |
A flight information acquisition unit periodically acquires flight information (information indicating flight status, including the position and flight direction of the host aerial vehicle) of a drone. A flight irregularity determination...
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JP2022165886A |
To provide a tail unit remote control device that enables a tail unit to be operated by a command transmitted by radio, when a failure suddenly occurs in an airplane in flight or when air piracy or a terrorist explosion disenables functi...
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JP2022160365A |
To solve the problem in present methodologies for aircraft protection that are insufficient in suppressing thermal runaway events in high-energy density batteries such as lithium-ion cells.Systems are for suppressing adverse exothermic r...
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JP2022144833A |
To suppress damage and wear of a sliding-down part of an evacuation chute.An evacuation chute 1 includes a sliding-down part 11 and a sliding-down seat 50. The sliding-down part 11 is put into a using state expanded by supplying gas insi...
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JP7137222B2 |
To provide a rotorcraft that can improve flight efficiency.A propeller includes at least one fixed-pitch blade and at least one variable-pitch blade. A motor component includes a motor for rotating the propeller. A flying body includes: ...
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JP7134837B2 |
To provide a safety device for an air vehicle which enables reduction of swinging during operation compared to a conventional safety device, and to provide an air vehicle including the safety device for the air vehicle.An injection devic...
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JP7132765B2 |
A method and system for managing a control system having triple redundancy for an aircraft. The method comprises receiving a group of messages from a transmitting lane in a controller including three lanes in which a first lane failure h...
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JP7128155B2 |
A device is provided for preventing a parachute from being damaged. A parachute device (4) includes a flying body (43) including a parachute (400), a parachute accommodation section (40) configured to accommodate the parachute, at least ...
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JP2022124061A |
To provide a technology that can reduce a descending speed of an air vehicle when the air vehicle descends unexpectedly without providing an air resistance layer on a surface of a fuel container.An air vehicle includes: a rotor; a motor ...
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JP2022120777A |
To provide a system and a method for safely, efficiently and effectively separating a canopy from a fuselage of an aircraft during an ejection procedure.A canopy for an aircraft includes a pivot assembly 140 including a first hinge 142 a...
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JP7118976B2 |
An aerial vehicle safety apparatus (100) includes a safety mechanism (10), a drive mechanism, an ejection mechanism, and a control mechanism. The safety mechanism (10) is used for securing safety of at least one of an aerial vehicle (30)...
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JP2022118547A |
To provide a safety device that can control the landing point of a flying object in the event of a crash.A safety device of the present invention is a safety device that is installed on a flight vehicle, the safety device comprising: a f...
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JP2022117762A |
To provide an airbag base fabric for a small aircraft, which is lightweight, highly airtight and excellent in cut resistance. and an airbag for a small aircraft.There is provided an airbag base fabric for a small aircraft having a fiber ...
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JP7104071B2 |
A degree-of-abnormality specification unit 202 specifies a degree of abnormality that corresponds to a detection value detected in a flight body 10. A parameter specification unit 203 specifies a derivation parameter for deriving a fligh...
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JP2022104736A |
To properly cope with any anomaly of an unmanned flying object in a case where an agricultural machine and the unmanned flying object work in a field in collaboration.An agricultural support system includes an unmanned flying object havi...
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JP7094421B1 |
To provide a control system capable of guiding an evacuation target person to which position (height) it is necessary to evacuate when a tsunami occurs. A control system 10 has a predicted tsunami information acquisition unit 11a for acq...
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JP7089623B2 |
Provided is a crash detection device, a method of detecting a crash of a flying object, a parachute or paraglider deployment device, and an airbag device that can improve the reliability in terms of safety. A device detecting a crash of ...
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JP7086083B2 |
An aerial vehicle safety apparatus (100) includes an expandable object (10), an ejection apparatus, a bag-shaped member (50), and a gas generator. The expandable object (10) is wound or folded in a non-expanded state and generates at lea...
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JP2022083949A |
To provide an unmanned aircraft which can transport another unmanned aircraft, which becomes uncontrollable during flight, to a place where the same can land without harming people or equipment and can be safely collected.An unmanned air...
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JP7079659B2 |
To provide a power storage device and a method of controlling the same, and a moving body control system that can speedily specify a position where a moving body becomes abnormal so as to ensure safety in such a case.A power storage devi...
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JP7075693B2 |
An unmanned aerial vehicle and a battery, possible to be disabled when a phenomenon to cause a functional disorder, are provided. The battery includes a battery pack having a battery cell, sensors detecting a phenomenon that impairs a fu...
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JP7072488B2 |
To provide a measurement system capable of reducing labor and time for measurement using an unmanned flight body.A measurement system 1 is attached to an unmanned flight body 10 and performs measurement by an observation part 11 for obse...
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JP7071544B2 |
A flight information acquisition unit repeatedly acquires the respective flight status of a plurality of drones in flight. A flight irregularity determination unit determines whether or not the drones are flying in a manner deviated from...
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JP7068126B2 |
Provided is an abnormality detection device for a rotary wing unit. The rotary wing unit includes a plurality of rotary wings that is coaxially disposed. The abnormality detection device includes a controller configured to acquire at lea...
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JP7058290B2 |
When a specified flight-incapable parameter does not meet a safety standard, a flight control unit 203 controls a flight body 10 so as to perform an operation that corresponds to the reason the parameter exceeded the safety standard. It ...
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JP2022058014A |
To provide a propeller guard which inhibits flying from being stopped when an air vehicle moving in a vertical direction collides with an object.A propeller guard 10 includes: an upper frame 12 provided on an uppermost surface of the pro...
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JP2022058015A |
To provide a propeller guard which inhibits flying from being stopped when an air vehicle moving in a vertical direction collides with an object.A propeller guard 10 includes: an upper frame 12 provided an uppermost surface of the propel...
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JP7046633B2 |
An example unit load device inerting system includes a nitrogen generation system, a first conduit coupled to the nitrogen generation system to carry nitrogen, an inlet located downstream of the first conduit and attached to a unit load ...
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JP7046923B2 |
An aerial vehicle (1A) includes a lift generation member (1110) provided in an airframe (1201) in an expandable manner, a manipulation mechanism (1111, 1112) connected to the lift generation member (1110) and configured to manipulate the...
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