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Matches 1 - 50 out of 962

Document Document Title
WO/2018/190319A1
The flight vehicle (1A) is provided with: a lift-generating member (1110) disposed on an airframe (1201) in a deployable manner; manipulation mechanisms (1111, 1112), which are connected to the lift-generating member (1110) and are for m...  
WO/2018/182448A1
The invention relates to methods for rescuing the crew of a light helicopter in the event of an emergency involving loss of control in uncontrolled freefall. The technical result of the invention is a more effective method for rescuing t...  
WO/2018/158686A1
A remote piloted aircraft (1) comprising a secondary flight assembly (4) adapted to intervene in case of failure of the aircraft (1) or in an emergency, said secondary flight assembly (4) being provided with an additional control unit (5...  
WO/2018/154603A1
The present subject matter relates to an apparatus (100) that use of a tuft of numerous wires as a drag enhancing system for spacecrafts (102). When these ultra-thin wires are used in high numbers and deployed on-board a spacecraft, they...  
WO/2018/149255A1
The present invention relates to intelligent warehousing technology. Provided in the present disclosure are a parachute system and a safety protection method for an unmanned aerial vehicle. The parachute system for an unmanned aerial veh...  
WO/2018/142319A1
A device (1) is described for braking the fall of a load comprising a sling (2) and a braking element (3, 30), said sling (2) comprising a first end (21) constrainable to an anchoring point; a second end (22) constrainable to said load; ...  
WO/2018/144915A1
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 descent-restraint system. The control system detec...  
WO/2018/098774A1
An apparatus, method and device for controlling forced landing. The method for controlling forced landing comprises: obtaining a signal for indicating power loss or partial power loss of an unmanned aerial vehicle; and when the signal fo...  
WO/2018/093608A1
A pneumatic parachute deployment system is disclosed. In various embodiments, a pneumatic parachute deployment system as disclosed herein includes a bladder configured to control a parachute's expansion in at least one dimension, and an ...  
WO/2018/093607A1
A cinched parachute is disclosed. In various embodiments, a cinched parachute as disclosed herein includes a canopy comprising one or more sections of canopy material, and a device integrated with the canopy that controls dimensions of t...  
WO/2018/080877A1
A distributed parachute system is disclosed. In various embodiments, a parachute is at least partially deployed along one or more dimensions. A deployment mechanism configured to deploy the parachute is provided. The distributed parachut...  
WO/2018/080876A1
A parachute deployment system is disclosed. In various embodiments, the system includes an interface configured to receive sensor information; a parachute load limiting device; and a parachute load limiting device state controller. The p...  
WO/2018/029119A1
The invention concerns a rotary-wing aerodyne (10), said aerodyne comprising: - a motor (35); - a structure (11) supporting at least one passenger seat; - a rotor (14) arranged above said structure (11) and linked to the motor by a hollo...  
WO/2018/019075A1
Disclosed in the present invention is an aircraft having an air crash lifesaving function. The aircraft comprises a nose, a passenger cabin and wings disposed on the left side and the right side of the passenger cabin. The wings and the ...  
WO/2018/014064A1
The invention relates to a device (1) for ejecting a parachute, comprising a housing (2) with an ejection opening (3), wherein the housing (2) is suitable for at least partially accommodating the parachute. In order to achieve a robust, ...  
WO/2018/013368A1
Techniques to deploy a parachute are disclosed. In various embodiments, a first projectile is configured to be propelled in a first direction, causing the parachute to be deployed. A second projectile configured to be propelled in a seco...  
WO/2018/012768A1
Disclosed are a system and method for sensing and controlling the crash of an unmanned aerial vehicle. The system includes a crash sensing device detachably mounted on an unmanned aerial vehicle and configured to sense a crash situation ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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 ...  
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 ...  
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...  
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: ...  
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...  
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...  
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 ...  
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 ...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  

Matches 1 - 50 out of 962