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Matches 1 - 50 out of 1,080

Document Document Title
WO/2020/170603A1
Provided is a parachute device which can quickly and reliably deploy a parachute even when an air stream effect cannot be immediately achieved during flight or descent of a flight device. A parachute device (4) is characterized by bein...  
WO/2020/167915A1
A device to orient a riser of a parachute. The device can include a twist body that is includes a slot through which the riser passes. The slot includes a twist to change the orientation of the riser from a relatively high-profile orient...  
WO/2020/167901A1
A device to orient a riser of a parachute. The device can include a twist body that is includes a slot through which the riser passes. The slot includes a twist to change the orientation of the riser from a relatively high-profile orient...  
WO/2020/167214A1
This disclosure relates to a system and method for an inflatable motorcycle outfit. The system comprises an inflatable trouser, an inflatable jacket, a pair of inflatable boots, one or more inflatable canopies. The system is flat when wo...  
WO/2020/076419A3
A preferred break point is provided in the airframe, where there is a ballistic parachute system which includes a rocket which sits in a rocket canister and a canopy which sits in a canopy canister. The airframe includes a composite mate...  
WO/2020/157490A1
A thermally insulated package 100 for transporting a temperature sensitive payload by unmanned aerial vehicle. The thermally insulated package comprises a payload retention volume 150, at least one layer of insulation 121, 122 surroundin...  
WO/2019/209540A3
A parachute vent reefing system is disclosed. The parachute vent reefing system includes a plurality of attachment members disposed about a vent portion of a parachute canopy and a keeper routed between each attachment member of said plu...  
WO/2020/136429A2  
WO/2020/136752A1
The purpose of the present invention is to provide an unmanned aerial vehicle which, during an emergency of the aircraft, can quickly alert the people below of the emergency. This unmanned aerial vehicle 1 is provided with: an aircraft 2...  
WO/2020/116826A1
The present invention relates to a fall prevention device for a drone, for preventing damage from an impact caused by falling of an unmanned aerial vehicle such as a drone, wherein the fall prevention device is coupled to a drone which i...  
WO/2020/107091A1
The invention relates to the field of heavier-than-air aircraft, aeroplanes and unmanned aircraft, and more particularly to emergency rescue systems. The aim of the invention is achieved by means of an aircraft consisting of a propulsion...  
WO/2020/043987A3
The invention relates to a device for disconnecting by means of a mechanical action, comprising at least one mechanical connection piece (5), in particular a spring-loaded buckle (5), connected to at least one trigger means (6) via at le...  
WO/2020/104816A1
An aerial vehicle comprising: a source of thrust, for propelling the vehicle forwards; and a canopy attachment arrangement having at least one securement point for at least one line of a canopy securable to the vehicle in use for providi...  
WO/2020/089660A1
An energy absorbing device provided at the parachute riser strap of an aircraft, UAV, etc., adapted to reduce the otherwise high forces resulting from the weight of the aircraft, the speed of descent and, ultimately, the speed of impact,...  
WO/2020/066391A1
[Problem] To provide a flying body provided with a deployment device of a lift generation member, the flying body configured so as to make automatic avoidance of a collision with an obstacle easier than heretofore. [Solution] A flying bo...  
WO/2020/043987A2
The invention relates to a device for disconnecting by means of a mechanical action, comprising at least one mechanical connection piece (5), in particular a spring-loaded buckle (5), connected to at least one trigger means (6) via at le...  
WO/2020/039424A1
According to at least one example a launch system is provided, including a carrier vehicle and at least one payload vehicle. The payload vehicle includes a payload propulsion system and aerodynamic lift surfaces designed for providing th...  
WO/2020/022582A1
The present invention relates to a solar panel management apparatus for monitoring a plurality of solar panels and cleaning foreign substances off the solar panels, while freely moving around in a solar power plant. The present invention...  
WO/2019/202257A3
The invention relates to a system for launching a paraglider canopy (30) from the stratosphere, comprising: - a stratospheric balloon (3); - a launch ramp (10) connected to the stratospheric balloon, the launch ramp extending between a f...  
WO/2020/016946A1
With conventional UAVs, it is difficult to achieve flight of adequate reliability in terms of flight distance, safety, etc. Provided is a multi-rotor helicopter (10) having: a fuselage (11); a flight motor unit (100) that has a flight mo...  
WO/2020/004426A1
[Problem] To provide: an ejection device in which a reduction in weight is achieved without a reduction in the ejection speed of an ejected object; and a flying body provided with the ejection device. [Solution] This ejection device 100 ...  
WO/2019/241725A1
A hover-capable aircraft includes a body including a tubular strut, a first rotor assembly rotatably coupled to the body and positioned about the strut, wherein the first rotor assembly includes a first plurality of circumferentially-spa...  
WO/2019/220077A1
The present invention provides a payload activation device,comprising: a housing; a cord, disposed within the housing, arranged to be coupled at a first end to an activation mechanism within a payload; and a retardation device coupled to...  
WO/2019/209540A2
A parachute vent reefing system is disclosed. The parachute vent reefing system includes a plurality of attachment members disposed about a vent portion of a parachute canopy and a keeper routed between each attachment member of said plu...  
WO/2019/202257A2
The invention relates to a system for launching a paraglider canopy (30) from the stratosphere, comprising: - a stratospheric balloon (3); - a launch ramp (10) connected to the stratospheric balloon, the launch ramp extending between a f...  
WO/2019/202533A1
An apparatus an unmanned aerial vehicle recovery system is provided. The apparatus includes a base to mount to an unmanned aerial vehicle. The apparatus further includes a housing to engage the base. In addition, the apparatus includes a...  
WO/2019/181989A1
[Problem] To provide a flying object operation device that is capable of improving reliability of safety, a malfunction prevention method for the flying object operation device, a flying object thrust generation device, a parachute or pa...  
WO/2019/179924A1
The invention relates to a flexible wing (100) comprising a canopy (1) and a plurality of guys (2) connected to the canopy (1), said canopy (1) comprising an upper wall (11) and a lower wall (12), defining an inner volume, at least one a...  
WO/2019/168316A1
A paradrone is disclosed. A paradrone according to an embodiment of the present invention comprises a canopy and a servomotor portion. The canopy comprises: a parafoil; a transverse canopy frame coupled to the parafoil so as to support t...  
WO/2019/166423A1
This device for unlocking a system for closing a container by means of a tie (12), such as a rope or strap, in particular a tie tensioned between closing eyelets, comprises a cutting tool (O) capable of cutting the tie in order to unlock...  
WO/2019/149283A1
A parachute ejecting mechanism for an unmanned helicopter comprises: a parachute cylinder (1); a parachute cover (2) mounted on the parachute cylinder (1); a parachute bag (3) located in the parachute cylinder (1); a high-pressure gas cy...  
WO/2019/144202A1
An unmanned aerial vehicle ("UAV") damage mitigation system includes a drone housing (12), a processor (20), a memory (22), an inertial measurement unit ("IMU")(34), and associated electronics configured to determine if the drone (10) is...  
WO/2019/139073A1
The purpose of the present invention is to improve safety of a flying device when dropped down. Provided according to a typical embodiment of the present invention is a flying device (1), comprising: an airframe unit (2); a lift force-ge...  
WO/2019/127351A1
A parachute (200) and an unmanned aerial vehicle having same. The parachute (200) comprises a cylinder (1), a parachute body (2) received in the cylinder (1), and a power mechanism (3) and a trigger mechanism (4) cooperating with the pow...  
WO/2019/106342A1
A canopy (1) control system comprising: • a yoke (5), configured to be pivotably securable to a vehicle (2) and securable to a line system (6) of a canopy (1) in use, such that the yoke pivots with respect to the vehicle in a first dir...  
WO/2019/092914A1
This flying object safety device (90) is provided with a deployable body (86) and an ejection device (88). The ejection device (88) has: a container (80) that accommodates the deployable body (86) and has an opening provided at one end; ...  
WO/2019/090277A1
Embodiments of the present invention enable a user of a drone to operate it more quietly. Embodiments of the present invention relate to such a system, apparatus, and a method of and for a drone that may be quiet, that can fly far while ...  
WO/2019/081031A1
The invention is related to a device (2), a wingsuit (8), a system and a method for performing a flight-like jump. For securing the trajectory of a user (7) performing the flight-like jump, a guiding element (3, 4) and an elongated secur...  
WO/2019/078094A1
[Problem] To provide a crash detection device, a flying body crash detection method, a parachute or paraglider deployment device, and an airbag device capable of improving safety reliability. [Solution] This flying body crash detection d...  
WO/2019/077365A1
An emergency landing apparatus (100) for an aircraft and a method of operating the emergency landing apparatus is provided. The emergency landing apparatus comprises: one or more rocket motors (30) arranged to eject efflux in order to pr...  
WO/2019/061781A1
A gimbal (10) and an unmanned aerial vehicle. The gimbal (10) comprises a pitch shaft arm (11), a roll shaft arm (12), and a first drive device for driving the pitch shaft arm (11). The roll shaft arm (12) comprises a main body (121), a ...  
WO/2019/044125A1
This flying body comprises: a fuselage; a canopy capable of adjusting the speed of a fall when falling; a brake cord having one end connected to the canopy; a winding device (20) which is provided on the fuselage and allows the other end...  
WO/2019/041069A1
A flying robot, comprising a flying robot body and a damping device body (9). Both left and right sides of the damping device body (9) are equipped with a chest fixing plate (1) and a back fixing plate (4), and an arm fixing column (2) i...  
WO/2019/039062A1
A flight vehicle safety device (100) is equipped with a safety mechanism (10), a drive mechanism, an ejection mechanism, and a control mechanism. The safety mechanism (10) is used to ensure the safety of a flight vehicle (30) and/or an o...  
WO/2019/039063A1
A flight vehicle safety device (100) is equipped with a deployable body (10), an ejection mechanism, a bag-shaped member (50), and a gas generator. The deployable body (10) is wound or folded in an undeployed state, and generates dynamic...  
WO/2019/035378A1
A spacecraft (100) includes a principal airframe (6), a parachute (1), which is an air brake structure, and a jetting nozzle (5). The air brake structure is provided farther on one side in a traveling direction with respect to the princi...  
WO/2019/032865A1
An aerial vehicle comprises: an electric power supply device, a motive power device, and a protective device disposed in an aerial vehicle body. The electric power supply device is configured to supply electric power to the motive power ...  
WO/2019/030116A1
The invention relates to a safety system for an unmanned flying object (1), flown by a user on the ground, the safety system making it possible to reduce the risks of the flying object (1) falling in the event of failure. The safety syst...  
WO/2019/001941A1
A device for securing (3) at least one sling (E) for transporting a load under a helicopter, the securing device (3) comprising at least a first strap (31) and at least a second strap (32), a connection mechanism (33) configured, in the ...  
WO/2019/003405A1
Provided is a landing apparatus which guides an unmanned aircraft to avoid obstacles and the like and lands the unmanned aircraft at a low-risk spot. The landing apparatus has a dangerous object position detecting device, a movement targ...  

Matches 1 - 50 out of 1,080