Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 1 - 50 out of 1,002

Document Document Title
WO/2024/048196A1
This flying body includes a parachute and a sensor device that detects the flight state of the flying body, and the flying body is provided with: an ejection device capable of ejecting the parachute; and a controller that determines whet...  
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/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...  
WO/2023/228921A1
[Problem] To provide a safety device that can be easily mounted to a flying object without requiring linking of a link member to the flying object, and a flying object equipped with the safety device. [Solution] A safety device 100 compr...  
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...  
WO/2023/184945A1
Disclosed is a parachute system for planetary exploration. The parachute system (100) for planetary exploration is provided with sensors (40) and repair structures (50) on a parachute body, and the impact strength of dust particles is mo...  
WO/2023/184946A1
A repair system (50) for repairing a parachute for planet detection, the repair system comprising a folding member (53) and a fuse (54). The fuse is provided in the folding member. The fuse receives a sensing signal reflecting the impact...  
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/2023/184947A1
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/2023/153120A1
Provided is an information processing device comprising: a prediction result acquisition unit that acquires a prediction result regarding the weather in the stratosphere; and a flight path determination unit that determines, on the basis...  
WO/2023/148446A1
The invention relates to a parachute comprising a canopy (2) having a leading edge (3) and a trailing edge opposite to the leading edge (3), suspension lines (5) each having a first end (6) attached to the leading edge (3) and a second e...  
WO/2023/140159A1
[Problem] To provide a parachute that can be deployed more quickly than conventional ones, a safety device having the parachute, and an aerial vehicle having the safety device. [Solution] An umbrella body 40 of a parachute has a substant...  
WO/2023/126930A1
A method is provided for operating a parachute-payload system with respect to a predetermined target zone location. The method includes: providing the parachute-payload system; constructing a predicted descent trajectory for the parachut...  
WO/2023/096907A1
Parachutes which have a generally circular skirt or hem, such as semi-hemispherical, extended gore, or any variant of axisymmetric parachutes and cruciform parachutes with arms attached are disclosed with a plurality of vertical slits lo...  
WO/2023/089735A1
[Problem] The present invention provides a flying object with which any decrease in flight efficiency while the flying object is cruising can be minimized while safety is improved. [Solution] This flying object is provided with a safety ...  
WO/2023/084303A1
A system (10) for enabling descent control of a payload (50) is provided. The system includes drag generating units (20) coupled to open canopies (30). The open canopies are coupled together by a connector (40) to support a payload. The ...  
WO/2023/080249A1
[Problem] To provide a safety device, and a flying body provided with the safety device. [Solution] A safety device 100 is provided with an actuator 1, an ejection object 16 to be ejected in one direction (upward direction in fig. 1) by ...  
WO/2023/076232A1
Devices, such as aerodynamic kites used in kiteboarding (also known as kitesurfing), handheld aerodynamic wings used in wing foiling and wing surfing, and paddles used in paddleboarding, for generating a force for powering a user on an a...  
WO/2023/068041A1
[Problem] To provide: a safety device which enables rapid expansion of a float, which has sufficient buoyancy at the time of contact with water, and which has reduced weight compared to prior art; and an aircraft comprising this safety d...  
WO/2023/059820A1
Embodiments of the invention provide a carrier for the organization and delivery of payload when used in conjunction with a motorized vehicle. The carrier comprises a housing defining an interior; at least one holder, wherein the interio...  
WO/2023/016023A1
Disclosed is a parachute, comprising: a parachute body (100), the parachute body (100) being formed by splicing 2N pieces of canopies, and the parachute body (100) being hemispherical after being opened; suspension lines (200), there bei...  
WO/2023/279032A1
Exemplary embodiments include systems and method for making a membrane surface having an axis of revolution using first and second mandrel having precise and accurate working surfaces. The systems and methods may also use gore material t...  
WO/2022/266597A1
An Intermediate Load Attachment Platform (ILAP) for attaching a cargo load to at least one main parachute, the ILAP protects a release mechanism disposed at least partially therein, the release mechanism is coupled to a drogue mechanism,...  
WO/2022/261864A1
A control method and apparatus for an unmanned aerial vehicle system, and an unmanned aerial vehicle system and a storage medium. The unmanned aerial vehicle system comprises an unmanned aerial vehicle and a parachute mounted on the unma...  
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...  
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...  
WO/2022/237973A1
The invention relates to a flight state system (20) for ascertaining the flight state of a paraglider (50, 50') which comprises a canopy (51) with two canopy ends (52) and which carries a load (53) when operated as intended. The flight s...  
WO/2022/240685A1
Systems and methods to cut a closing loop to deploy a parachute. The system includes a cutter with a body with a cutter opening that extends through the body and a blade that is movable across the cutter opening. Processing circuitry is ...  
WO/2022/213448A1
An air-dropped underwater vehicle, comprising a vehicle body. The vehicle body comprises a cabin (1); retractable/extendable wings are mounted on the vehicle body; each wing comprises a retraction/extension framework mechanism (7) and a ...  
WO/2022/195459A1
A system for payload delivery and drone recovery, wherein the system functions with the use of a lightweight parachute and a directional control module. The system can include a drop system for payload delivery, wherein the drop system r...  
WO/2022/184086A1
An unmanned aerial vehicle system, and a parachute module and a folding structure, a mold thereof and a parachute opening method therefor. The folding structure is folded back and forth along a vertical folding line in an outwardly radia...  
WO/2022/182912A1
The technology relates to payload separation during descent of an aerial vehicle. A flight termination system (FTS) for a lighter than air (LTA) vehicle can include a first, a second, and a third mechanical actuation system. The first me...  
WO/2022/171974A1
A line management apparatus and a paramotor comprising the same A line management apparatus for a flexible wing, which comprises a canopy and a line system comprising one or more lines for connecting the canopy to a vehicle, the apparatu...  
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 ...  
WO/2022/157496A1
A canopy attachment yoke, comprising: first and second support bars, each having a first end and a second end, wherein the respective first ends are configured for attachment to at least one support line of a canopy and the respective se...  
WO/2022/139264A1
The present invention relates to a paraglider canopy and a paraglider comprising the paraglider canopy. The paraglider canopy according to an embodiment of the present invention comprises: an upper wing including a first upper wing havin...  
WO/2022/123211A1
A method for monitoring a flexible wing, which comprises a canopy (1) and a line system (6) for attaching the canopy (1) to a vehicle (2), the method comprising operating the wing and measuring during the operation, using one or more sen...  
WO/2022/109735A1
Disclosed is an apparatus and method for operating a gliding parachute/kite. The gliding parachute/kite has a wing with a flexible material, and a set of suspension lines adapted for coupling a load to the wing, such that the coupling is...  
WO/2022/101525A1
The invention discloses a procedure for manufacturing an inflatable structure, where the structure comprises at least one body (1) formed by a piece of thermoplastic polymer fabric (2) configured to house an air chamber (3), such that th...  
WO/2022/104123A1
A strap that may be used to secure equipment (e.g., a bag) to the parachute harness of a parachutist. The strap may provide adjustability of an effective strap length to assist in positioning the suspended equipment relative to the parac...  
WO/2022/092395A1
Provided is an acoustic sensor device which, for confirming the location of a missing person, is airdropped from a drone, lands on the ground and collects and transmits a sound event. The acoustic sensor device according to an embodiment...  
WO/2022/072551A1
Rescue parachute deployment systems (RPDSs) and related techniques are provided to improve the safety and operational flexibility of unmanned aerial vehicles (UAVs). An RPDS includes a canopy assembly (168), a rotor guard (680, 682) disp...  
WO/2022/047344A1
Methods of reducing wing type parachute (1) opening shock during a parachute drop, and parachute systems with reduced opening shocks are disclosed, the opening force reduction is achieved by dynamic braking, i.e. dynamically adjusting th...  
WO/2022/040539A1
The technology relates to techniques for drogue deployment for a lighter than air (LTA) vehicle descent. A drogue deployment system for an LTA vehicle descent can include a drogue comprising a drogue parachute coupled to a carrier. A spr...  
WO/2022/031377A2
An aircraft emergency parachute deployment system (AEPDS) is disclosed. The AEPDS includes a parachute assembly coupled with an aircraft, a ballistic rocket assembly coupled to a top portion of the parachute assembly by a lanyard, an act...  
WO/2022/006905A1
A separable aircraft protection device, method and system. The separable aircraft protection device comprises: a protection device (11), and an unmanned aerial vehicle flight module (12), a fixing module (13), and a control module (14) s...  
WO/2021/250746A1
[Problem] To provide a flying object with which the falling body can be adjusted to a predetermined orientation and a parachute can be deployed more normally. [Solution] The present disclosure relates to a rotorcraft. The rotorcraft acco...  
WO/2021/251548A1
The present invention relates to a drone parachute and, more specifically, to a drone parachute in which a natural convection current is generated through holes formed in a body part so that a parachute is released naturally, and thus is...  
WO/2021/247999A1
A shock absorber assembly, particularly for attenuating shocks transmitted to a person's body, especially to reduce shock to a paratrooper's body during a tethered cargo tandem jump. Specialized elastic absorber units are disposed betwee...  

Matches 1 - 50 out of 1,002