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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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; ...
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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 ...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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 ...
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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...
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WO/2018/234071A1 |
The invention relates to a cutting device (20) comprising at least one firing pin retainer (1), at least one locking element (2), a spring (6), a firing pin (7), a percussion cap (9), a charge (13), a cutting element (14), a stop (15) an...
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WO/2018/231842A1 |
Active tethers for controlling UAV flight volumes, and associated methods and systems, are disclosed. A method in accordance with a representative embodiment includes directing a UAV upwardly from a launch site, receiving an indication o...
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WO/2018/229092A1 |
The subject of the invention is an aerodynamic braking device for a payload casing intended to be ejected from a projectile on its trajectory. This braking device comprises at least one parachute connected to the casing by hangers, the p...
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WO/2018/223378A1 |
An unmanned aerial vehicle control method and device, and an unmanned aerial vehicle. The method comprises: acquiring state information about an unmanned aerial vehicle (S101); determining a control instruction according to the state inf...
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WO/2018/216531A1 |
Flight vehicles flying in the stratosphere for the purpose of providing a stratospheric platform are generally known, but it is desirable to provide a technique capable of reducing damage on the ground in the event that a flight vehicle ...
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WO/2018/213920A1 |
A multi-layer bladder construct consisting of a non-stretchable outer covering and a stretchable inner bladder. The outer covering has an inner surface and is made from woven polymer fibers having a warp direction and a weft direction. T...
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WO/2018/212109A1 |
A conventional parachute requires the velocity pressure from a drop in order to open the parachute, and thus, from the beginning to the end of an operation for opening the parachute, drop distance and time are required and therefore use ...
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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...
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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...
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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...
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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...
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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...
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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; ...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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 ...
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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, ...
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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...
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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 ...
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