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WO/2016/207622A1 |
A system comprising: a low observable aircraft (2) having its external surfaces oriented at a limited number of directions; a device (12) mounted to the aircraft (2) outside the external surfaces of the aircraft (2); and a fairing (10) l...
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WO/2016/207623A1 |
An aircraft (2) comprising a launch tube (14) extending along at least part of a length of a wing of the aircraft (2),and through which an item (24) may be launched from the aircraft (2). The launch tube (14) comprises an opening (22) at...
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WO/2016/199132A1 |
An ejector rack is provided for releasably supporting a store, and includes a housing, having a lug engaging and releasing mechanism operative for selectively and releasably engaging the lug, and movable between a lug engaging position a...
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WO/2016/192023A1 |
Systems and methods can control a pumping system (120, 200, 300, 400, 710, 810, 900, 1000, 1200, 1300, 1400, 1500 ). Operating characteristics of a driving apparatus (210, 310, 410, 510, 920, 1030, 1120, 1220, 1510 ) are obtained. The dr...
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WO/2016/192016A1 |
Disclosed are an unmanned aircraft and a spray head structure thereof. The unmanned aircraft comprises an aircraft body, and the spray head structure comprises a spray nozzle, a rotating disk and a brushless electric motor. The brushless...
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WO/2016/192024A1 |
Systems and methods can determine a liquid flow in a spraying system. An amount of liquid that is output from the spraying system during a pump cycle is determined. A number of pump cycles that occur within a given amount of time are mea...
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WO/2016/191382A1 |
A drone apparatus or arrangement is provided. The drone apparatus or arrangement includes a plurality of drone devices, each drone device including an unmanned vehicle configured to be controlled to hover in air at a desired height and m...
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WO/2016/167849A1 |
Various embodiments of the present disclosure provide a helicopter-mediated system and method for launching and retrieving an aircraft capable of long-distance efficient cruising flight from a small space without the use of a long runway.
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WO/2016/159481A1 |
The present invention relates to a drone-type lifesaving equipment dropping device, which comprises: an unmanned aerial vehicle (2) having a propeller (4) and a rotor (3) for rotating the propeller and configured to perform unmanned flig...
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WO/2016/088129A9 |
A fragile substance storage transportation and release device (220) comprises a frame for inserting cartridges (224) to hold the fragile substance; a propulsion unit (222) for propelling the fragile substance out of successive cartridges...
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WO/2016/146918A1 |
The invention relates to a hoisting cable for a helicopter hoist, comprising at least one first electrical conductor (3) built into a non-conductive structure, and at least one second electrical conductor which is electrically isolated f...
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WO/2016/138604A1 |
An agricultural aircraft. Two rotor wing arms (3) are arranged crosswise rotationally and are symmetrical crisscross. The two rotor wing arms (3) can be folded during transportation or storage. Microwave radar (18) and an ultrasonic or l...
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WO/2016/125422A1 |
In the present invention, a helicopter (30) disperses fertilizer to a field while flying. The helicopter (30) is provided with a dispersion unit (33), a fertilization amount map input unit (51), a position information acquisition unit (5...
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WO/2016/126353A1 |
The system includes a snorkel leading from an intake up to a tank borne by an aircraft. A feed pump in the intake draws water up the snorkel to the tank. A polymer gel emulsion reservoir supplies polymer gel upstream of the feed pump for...
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WO/2016/116095A1 |
The invention relates to a heavyweight torpedo for dropping into a body of water outside of a visibility range of a target, comprising a parachute, a parachute-releasing element, and a water-ingress detection element, wherein the parachu...
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WO/2016/113256A1 |
Water scooping apparatus (2) for an aircraft comprising an extendible tubular member (5, 18) having a first end and an opposite end, wherein the first end is pivotally attached to the aircraft (1), a duct (4) for fluidly connecting the e...
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WO/2016/090414A1 |
An automated apparatus, method and system for projecting a control agent toward a recognised target for the purposes of agricultural cultivation or environmental management or various other applications; a source of the control agent ada...
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WO/2016/087822A1 |
The unit (10) uses a resiliently biased electrical connector assembly (16) and/or resiliently biased feet (50) pivotally attached to adjustable sway brace legs (20) to apply an ejection impulse to a store (not shown) after release from a...
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WO/2016/088128A1 |
A method of distributing fragile insects in a distribution involving a wind shear, comprises, encapsulating the insects into a bubble and then releasing the bubble into the wind shear so that the bubble protects the insect from the wind ...
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WO/2016/088127A1 |
A diffuser for distributing insects such as mosquitoes from an aircraft, comprises a distribution tube connected to an insect source at a first end and open to the outside at a second end in a direction away from that of travel of the ai...
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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/2016/070684A1 |
Disclosed is a U-shaped kit for unmanned farm helicopters, comprising a drug kit body (301), wherein the drug kit body has a groove so that it has a cross-section with a U-shaped structure, wherein the U-shaped structure has a U-shaped i...
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WO/2016/064457A1 |
A deployment system (50) for deploying a store from an aircraft includes a lock member (60) that selectively engages the store to the deployment system, an ejector (62) that selectively ejects the store from the deployment system, and a ...
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WO/2016/062176A2 |
Disclosed is an unmanned agricultural helicopter, comprising a fuselage body. The fuselage body comprises a frame. Provided on the frame is a rotor head for fastening a main rotor, the main rotor being disposed on a large blade clip of t...
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WO/2016/060763A2 |
A system and method for identifying a slung load for an aircraft with one or more sensors includes receiving, with a processor via one or more sensors, sensor information related to flight dynamics data for the aircraft; determining, wit...
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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/2016/046823A1 |
A diffuser (10) for distributing spray or insects from an aircraft is mounted on an aircraft and comprises a distribution tube (12) connected to an insect source at a first end and open to the outside at a second end (14) for distributio...
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WO/2016/044248A1 |
A rope deployment mechanism includes a load beam pivotable between an open position and a closed position. Also included is a linkage assembly engaged with the load beam in the closed position and moveable to allow the load beam to pivot...
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WO/2016/037219A1 |
The invention relates to a delivery system for use with an unmanned aerial vehicle ("UAV") to deliver goods to a location. The delivery system includes, a first part including a carrier means for carrying the goods with the UAV and a sen...
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WO/2016/026739A1 |
The invention relates to a lighter-than-air aircraft (1) comprising deballasting means, said deballasting means comprising: at least one tank (2) containing a liquid (3); a system for pressurising the liquid of the at least one tank; and...
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WO/2016/025341A1 |
The disclosure describes an automated aerial vehicle (AAV) and system for automatically detecting a contact or an imminent contact between a propeller of the AAV and an object (e.g., human, pet, or other animal). When a contact or an imm...
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WO/2016/011470A1 |
An anti-rotation sail (8) for suspended rescue equipment (9) for persons on a rotary-wing aircraft (10), having the following features: the anti-rotation sail (8) has a flow-deflecting, non-rigid sail surface (1), wherein the sail surfac...
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WO/2016/011253A1 |
An aerial distribution system and method for deploying items is disclosed. The system includes a box, a lid detachably coupled to the box, a plurality of items within the box, a flexible liner coupled to the box and containing the plural...
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WO/2015/193742A1 |
This invention proposes a method and an apparatus which enables one to combine several autonomous areal vehicles into a larger areal vehicle. In particular, the invention describes an apparatus capable of autonomous flight and consisting...
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WO/2015/161352A1 |
The present innovation relates to an unmanned aerial vehicle (UAV) with self-propulsion, vertical take-off (VTOL), which is actuated and controlled remotely, for the application of pesticides/fertilizers, for manuring, for sowing, and fo...
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WO/2015/162613A1 |
A wall-drawing hovering device (WDHD) is provided. The WDHD comprises an unmanned helicopter configured and operable for flying and hovering while being disconnected from ground. The WDHD further comprises a mobilizing system comprising ...
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WO/2015/154148A1 |
A system for carrying out pest baiting, comprises an unmanned aerial vehicle (UAV) which is controllable to record image data over a predefined flight path, the image data being captured by an image recording device. A computer processin...
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WO/2015/152492A1 |
The present invention relates to an unmanned aerial vehicle for reconnaissance of a scene of a fire and fire suppression, which is suitable to be dispatched to the scene of a fire which a firefighter cannot easily access.
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WO/2015/149108A1 |
A rescue package arrangement for launching from a moving platform such as an aircraft includes a container body externally sized and shaped to be launched from a moving platform using a launch tube and contains a main parachute located w...
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WO/2015/145426A1 |
An aircraft pylon comprising a body for mounting to an aircraft, a suspension mechanism mounted on said body and being configured for attaching thereto a payload, and a moving door configured for selectively covering and uncovering at le...
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WO/2015/136128A1 |
The invention relates to a fire extinguishing device for in-air use, which uses a tank having two separate and related containers, having a mixture of water and foam, together with a chamber to generate the firefighting foam. The device ...
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WO/2015/131037A1 |
An apparatus and a method for the removable retention of a store/ payload to a vehicle comprising: a housing (15) having an elongated base, said base having a first and second distal end; a retention receptacle (14) disposed adjacent sai...
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WO/2015/129767A1 |
Provided is a drop-type fire extinguishing body that enables, at the time of fire extinguishing using a gel fire extinguishing agent, the fire extinguishing agent to be smoothly conveyed and dropped. A drop-type fire extinguishing body (...
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WO/2015/113867A1 |
The present invention relates to an energy absorption device (1) comprising: - a mounting (23), a dissipating element (14) assembled around said mounting (23) and intended to deform plastically when compressed by an impact, - balls (12) ...
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WO/2015/112853A1 |
Reconfigurable payload systems (RPS) and methods of configuring and using the same are disclosed that may be employed to enable external aircraft payloads to be rapidly interchanged or swapped out together with associated internal equipm...
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WO/2015/095948A1 |
The invention relates to the field of delivering goods, and more specifically to methods and systems for automatically delivering goods using an unmanned flying apparatus, including stowing goods on an unmanned flying apparatus, entering...
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WO/2015/080614A1 |
A recovery system used primarily for recovering liquid rocket engines for the purpose of reusing or repeatedly reusing same in the first stage (stage-and-a-half) of a rocket. The technical result of the claimed invention consists in i...
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WO/2015/076886A2 |
Embodiments described herein may help to provide medical support via a fleet of unmanned aerial vehicles (UAVs). An illustrative UAV may include a housmg, a payload, a line-deployment mechanism coupled to the housing and a line, and a pa...
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WO/2015/035288A1 |
A cushioned platform system and an aerial delivery method employ at least one airbag module. The airbag modules are mounted at the underside of a platform which supports the payload. Parallel roller pads are disposed below the at least o...
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WO/2014/191749A1 |
An aerial delivery box (30) for release from an aircraft comprises a hold (31) for a payload; and an impact absorbing zone (32) for protecting the payload of the hold. The hold and the impact absorbing zone are formed of biodegradable ma...
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