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WO/2018/009252A1 |
Methods, devices, and systems for deploying cargo for high altitude, low opening (HALO) deployments are disclosed. The method comprises the steps of coupling a parachute deployment device to the cargo, adjusting the valve to determine ra...
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WO/2017/219201A1 |
An unmanned aerial vehicle (100). The unmanned aerial vehicle (100) comprises an unmanned aerial vehicle main unit (1), multiple rotors (2), and a parachute (4). The unmanned aerial vehicle main unit (1) is connected to the rotors (2). T...
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WO/2017/219202A1 |
An unmanned aerial vehicle (100) comprising an unmanned aerial vehicle main unit (1), multiple rotors (2), a photographing device (4), and a parachute (6). The unmanned aerial vehicle main unit (1) is connected to the rotors (2) and to t...
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WO/2017/207570A1 |
This invention relates an unmanned aerial vehicle (UAV) apparatus (20) having a frame structure (7), a plurality of primary arm structures (8) extending from the frame structure (7), a driving system (10) for driving the UAV apparatus, a...
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WO/2017/199237A1 |
A system for the measurement of weather comprises a sensor configured to sense data comprising data indicative of the geometrical configuration of a flexible airfoil of an air vehicle, and a controller configured to extract data indicati...
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WO/2017/199236A1 |
A safety system for a parachute comprises at least a sensor configured to sense data indicative of the geometrical configuration of a canopy of the parachute, and at least a controller configured to extract data indicative of the geometr...
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WO/2017/181260A1 |
A kite control bar having a tensioning member anchored to the bar end float and secured to the trim line. The tensioning member is capable of expanding and contracting. The tensioning member has a default state which is either an expande...
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WO/2017/180780A1 |
Described herein are features for a riser release flaring system for parafoils and other descent flight vehicles for controlled descent and landing of the flight vehicle. The descent flight vehicle may have a payload suspended by a canop...
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WO/2017/164666A1 |
An embodiment relates to an unmanned aerial vehicle comprising: a body; an imaging device mounted in the body; a sensing unit for sensing a current state of the body; and a controller communicating with the imaging device and the sensing...
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WO/2017/158234A1 |
An object of the invention is a launching device for launching an object from a launch pad, wherein said apparatus comprises a frame (1) affixed to the launch pad, a push element (2) for pushing an object detached from the launch pad, a ...
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WO/2017/151483A1 |
A system and method is provided for shortening specific suspension lines near the center of a ram air parachute in order to distort the airfoil section only in the center section of the canopy. This distortion of the center section resul...
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WO/2017/144178A1 |
The invention relates to a safety system for a paraglider strap assembly, comprising an impact protection element that is formed by molded foam and/or an airbag filled using dynamic pressure, and comprising an emergency parachute that is...
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WO/2017/136906A1 |
This invention patent is aimed at innovating personal locomotion by free uni-steerable flight with new technologies using clean propulsion energies. The invention is characterised by a new concept of individual aerial locomotion, innovat...
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WO/2017/139803A1 |
An aircraft includes an airframe parachute system. The parachute system includes an ejector assembly, a switch assembly, a projectile object and a mechanical connector. The ejector assembly includes an inflatable cushion. The switch asse...
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WO/2017/127413A1 |
A parafoil system having an adjustable trim angle during flight to control glide slope and descent speed of a parafoil is provided. The parafoil system may include a pulley cluster comprising first and second variable trim pulleys, each ...
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WO/2017/121985A1 |
An air safety device comprising a shaped inflatable bag having a frame with a plurality of inflatable channels (5), the frame defining the shape of the bag when inflated. A source of compressed gas is provided for inflating the channels ...
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WO/2017/123591A1 |
Aspects herein provide for an apparel item (100, 1200, 800) having an integrated parachute structure (2112, 212, 912) and a set of intake ducts (120, 1220, 1222, 122, 124, 126, 1710, 2012, 816, 818). The parachute structure (2112, 212, 9...
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WO/2017/097292A1 |
The invention relates to an automatic deployment mechanism for a parachute assembly that can be fastened to a person, the parachute assembly comprising a main parachute and a spare parachute. The automatic deployment mechanism includes: ...
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WO/2017/095076A1 |
According to the present invention, a GPS guided parafoil aerial delivery system comprises: a parachute part; an automatic guidance device unit connected to the lower part of the parachute part so as to fly to a target point through a fu...
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WO/2017/086234A1 |
Provided is an unmanned airplane which enables prevention of exacerbation of accidental damage sustained by rotor blades following a crash resulting from an in-flight collision with an obstacle. This unmanned airplane is provided with mu...
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WO/2017/078227A1 |
The subject matter of the present invention relates to providing a maritime recovery device of an unmanned aerial vehicle, the maritime recovery device enabling an unmanned aerial vehicle to be recovered at sea regardless of the size of ...
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WO/2017/073310A1 |
The image capture system for shape measurement comprises: an imaging device (20) for capturing an image of a structure; a flying body (2); an onboard control device (10) for controlling the imaging device (20) and the flying body (2) in ...
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WO/2017/075245A1 |
An improved slider for use with a parachute, particularly a ram-air type parachute, is provided. The slider includes a generally rectangular piece of material having grommets in the corners through which the suspension lines of the parac...
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WO/2017/066662A1 |
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automati...
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WO/2017/066649A1 |
Disclosed is a technique for landing a drone using a parachute. The technique includes a parachute deployment system (PDS) that can deploy a parachute installed in a drone and land the drone safely. The parachute may be deployed automati...
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WO/2017/062686A1 |
A food container is disclosed that includes a food compartment and a seal-on cover. The food compartment has an outer rim that circumscribes a volume. The food compartment outer rim has tear tab guides that extend outward from the rim. T...
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WO/2017/036080A1 |
A parachute equipped autogyro comprises: a fuselage body (1), a rotor device (2), a propeller device (3), and a parachute device (4). The fuselage body (1) comprises a cockpit (5) and a tail rudder (6). A control system is arranged at a ...
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WO/2017/034174A1 |
A drone according to an embodiment may comprise: a support table; a main unit spaced from the support table and formed above the support table; a connecting portion for connecting the main unit and the support table; and a propulsion uni...
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WO/2017/026354A1 |
Provided are a loss prevention device that makes it possible to efficiently search for and retrieve an unmanned aircraft that has gone missing, an unmanned aircraft that is provided with the loss prevention device, and an unmanned aircra...
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WO/2017/022805A1 |
The present invention establishes a technology for accurately monitoring and managing small aircraft that frequently fly. A small aircraft 1 is provided with: an aircraft ID storage unit 201 that stores an aircraft ID that uniquely ident...
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WO/2016/204803A1 |
A system and method for resisting an uncontrolled descent or uncontrolled flight condition of an aerial vehicle. The system includes a control system, sensors, an inflation device, and a deployable, inflatable assembly. The control syste...
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WO/2016/191140A1 |
An unmanned aerial vehicle includes a closely integrated emergency recovery and operation systems for an unmanned aerial vehicle with built-in levels of redundancy and independence to maximize the likelihood of a controlled velocity land...
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WO/2016/182750A1 |
A safety and recovery system 10 for an unmanned aerial vehicle 12 including parachute holder 14 mountable to aerial vehicle 12. Parachute 18 is disposed in parachute holder 14. An actuator 16 is engaged with parachute holder 14. A flight...
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WO/2016/180172A1 |
Disclosed is a coaxial two-layered parachute (10) comprising an inner layer of inflation sac body (20) and an outer layer of parachute cover (30) provided on a coaxial centreline, and a bearing article (T) connected below the inner layer...
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WO/2016/160628A1 |
An atmospheric balloon descent system includes a system housing having a drogue chamber containing a drogue chute and a parachute chamber containing a parachute. The parachute coupled with the drogue chute with a drogue tether. A riser t...
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WO/2016/153720A1 |
A balloon system is provided including a balloon envelope, a payload secured to the balloon envelope, a first parachute positioned within a parachute container, the parachute container secured to the payload, a first bridle line having a...
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WO/2016/145130A1 |
A parafoil for operation at high altitudes, in low density air, or at low airspeeds, and methods for opening same. Some versions of the parafoil comprise flexible members connected to the parafoil canopy. When the parafoil canopy is in a...
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WO/2016/142573A1 |
The object of the invention is a method to replace the control signal of an operation organ of a remote controlled flying apparatus with another signal. The signal to be replaced (a, b, etc., y, z, etc.) is a signal to be sent from the s...
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WO/2016/141928A1 |
The invention relates to a method and a device for an intelligent parachute rescue system for manned and unmanned aerial vehicles (14), wherein no pyrotechnic propellants are used, but compressed air (4a) extracted from a pressure bottle...
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WO/2016/141231A1 |
A system for quickly locating and retrieving flight data of an aircraft after an aircraft mid-air mishap comprises: a flight data recorder; a tracking device comprising at least one camera; a rapid ejection system for ejecting the flight...
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WO/2016/128584A1 |
The invention relates to a paraglider (10) comprising a canopy (12) having a top sail (14) and a bottom sail (16), wherein the canopy (12) is subdivided into several elongated chambers (18) having a longitudinal axis. Each chamber (18) h...
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WO/2016/081753A1 |
IA canopy tracking device for a skydiving system kit is provided. The canopy tracking device includes a tracking device mounted to or embedded in a riser. The tracking device remains powered off until a cut-away system of the skydiving k...
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WO/2016/079493A1 |
A parachute arrangement comprising a parachute having a canopy, a plurality of shroud lines coupled to the canopy, and a plurality of connectors (23) coupled to the shroud lines for attachment to a load; and a packaging (10) for the para...
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WO/2016/067489A1 |
An electric multicopter (100) that has a plurality of propellers (1). The multicopter (100) is provided with an electric motor (2), at least one main battery (3), a generator (4), an engine (5), and a battery status detection unit (71). ...
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WO/2016/059286A1 |
The object of this invention is a method to shoot an object from a flying apparatus. Into an flying apparatus, into certain part of it, like a container (2) that consists at least of a bottom (3) and a shell (4) a spring (6) will be plac...
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WO/2016/049383A1 |
The present disclosure provides danger avoidance apparatuses and related methods, such as for use to avoid avalanches. An apparatus may include a container configured to couple to a user, a lift providing mechanism, a descent control mec...
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WO/2016/025444A1 |
Various embodiments of the present disclosure relate to a parachute deployment system for an unmanned aerial vehicle (UAV). In some examples, the parachute deployment system includes a base attached to the unmanned aerial vehicle, a depl...
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WO/2015/199567A1 |
Method and apparatus for bailing with logic ballistic parachute for special, short, complex falls in helicopters, aircrafts and land vehicles and aerial braking The invention comprises a group of principles and methods associated so that...
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WO/2015/194979A1 |
This invention provides a conical troop parachute with a multi-gore canopy made of pieces of cloth of a varied air-permeability, delimited by an air- permeability boundary, where side edges of the gores are sewn together and attached via...
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WO/2015/165021A1 |
Embodiments of the present invention provide an air vehicle protection control method and apparatus, and an air vehicle. The method comprises: detecting a flight state of an air vehicle; when the flight state of the air vehicle is detect...
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