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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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WO/2014/189587A2 |
A method for transporting a cargo load using a carrier aircraft includes: mounting a shield on the cargo load such that the shield is supported by the cargo load to form a protected load; and aerial transporting the protected load as a s...
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WO/2014/186046A2 |
An emergency pod configured for use with a rotary wing aircraft is provided including a rigid, generally hollow shell. The shell includes a movable portion configured to move between a closed position and an open position. An inflatable ...
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WO/2014/179610A1 |
An aerial distribution system and method for deploying items is disclosed. The system includes a bulk shipping container comprised of a single piece of corrugated plastic, cut and folded into a closable box, a plurality of deployment box...
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WO/2014/167163A1 |
The present invention relates to a water discharge device for fire-fighting which enables discharging a large quantity of water from an aeroplane avoiding the dispersion of the water, so that this falls on the ground in a concentrated ma...
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WO/2014/160589A1 |
Modern farming is currently being done by powerful ground equipment or aircraft that weigh several tons and treat uniformly tens of hectares per hour. Automated farming can use small, agile, lightweight, energy-efficient automated roboti...
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WO/2014/140981A1 |
The present technology provides a system and method for tracking payload drops from aircraft. The method includes initiating a payload drop, accurately determining the start of the drop and the end of a drop, determining a drop vector, a...
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WO/2014/133685A1 |
A system and method for deployment operations from an airborne vehicle (104) are presented. A designated location of a target is received at a flight control system coupled to a location tracking guided container (120) comprising an agen...
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WO/2014/117237A1 |
The present invention discloses a suspension and vibration isolation system comprising cable isolators. The cable isolators employ low-friction air-bearing pneumatic cylinders and cables to isolate a suspended payload from vibrations of ...
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WO/2014/032679A1 |
The present invention relates to an automatic system suitable for reducing the speed of rotation of one or more suspended loads, preferably where said rotation is originated by the flow tube located downstream preferably of the blades of...
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WO/2014/009612A1 |
The invention relates to a device for attaching and ejecting a load suspended beneath an aircraft, comprising at least two ejection pistons (4, 5) connected to the load to be attached/ejected, and to a control circuit including a pneumat...
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WO/2013/182761A1 |
The decoy method, of the type in which: an ejectable on-board decoy provided with a decoy charge (13) is enclosed inside a streamlined cylindrical body (9) mounted ejectably on the aircraft (1); the streamlined cylindrical body (9) conta...
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WO/2013/180803A2 |
A vehicle hook-up assembly with a pendant assembly extending from a vehicle. The pendant assembly has an end with a magnetically attractive fitting. A receiver assembly having a magnetic element is attached to a payload. The receiver ass...
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WO/2013/138936A1 |
The present invention provides a capture mechanism for capturing and locking onto the Marman flange located on the exterior surfaces of spacecraft/satellites. The capture mechanism achieves its goal of quickly capturing a target spacecra...
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WO/2013/131122A1 |
A false target deployment system for land, air or water based craft including one or more decoy pods coupleable to pod seats formed in outer peripheral sections of the craft; and fasteners for coupling the decoy pods to the pod seats, wh...
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WO/2013/117784A1 |
The invention relates to a fire extinguishing device which is built into an aircraft, allowing the transport of fire fighting material and the controlled evacuation of same from an aircraft in flight onto the fire-affected area. The devi...
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WO/2013/112896A1 |
A fire suppression apparatus for fighting fires from a vehicle configured for flight is disclosed, comprising a foam and water held in separate containers aboard the vehicle that when mixed forms a fire retardant, a pump driven by an ele...
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WO/2013/102213A1 |
A fire fighting system configured to deliver rescue equipment and fight high rise building fires via pneumatically launched projectiles filled with either rescue equipment or fire suppressant chemicals. The system is composed of several ...
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WO/2012/058677A9 |
An aerial retardant delivery system comprising a retardant tank mountable in the fuselage of an aircraft. The tank includes a pressure opening in fluid communication with the fuselage such that pressure in the fuselage may act on retarda...
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WO/2013/088285A1 |
A soft landing system (10) includes an air cushion structure (12) comprising: a housing portion (14), adapted to house a load (V); a support portion (15), connected to the housing portion (14) and inflatable with fluid under pressure, an...
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WO/2013/087086A1 |
An aircraft (1) is comprising an aircraft body, an aircraft engine and at least one container for containing a fluid is presented. Furthermore, at least one nozzle for releasing the fluid contained in the container into exhaust fumes fro...
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WO/2013/076432A1 |
The invention relates to a method of remineralization and correction of pH for water produced by a fuel cell (P) on board an aircraft, noteworthy in that it consists in diverting part of the water (E1) produced by the cell to at least on...
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WO/2013/076708A1 |
A test apparatus for avionic sensors including a helicopter (2), an avionic sensor test pod (3) equipped with at least one avionic sensor (18, 20) and a cable suspension system (4) connecting the test pod (3) to the helicopter (2).
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WO/2013/076633A1 |
Method for manufacturing a support pylon for avionics made of composite materials, adapted to allow the transport of external loads that cannot be directly supported at the primary or secondary structure of the aircraft. Said loads are r...
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WO/2013/070258A1 |
Water is mixed with fire suppressant polymer in a mixer absent a power source. The mixer receives water through a water inlet with water exhibiting high velocity and associated hydrodynamic force. Such velocity is achieved by locating th...
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WO/2013/066462A2 |
An aircraft store ejector systems and subsystems thereof. Embodiments can include a two-reservoir re-pressurization system wherein a remote reservoir is used to maintain desired pressure in a local ejector reservoir. The system can inclu...
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WO/2013/061563A1 |
A dispersal assistance apparatus provides assistance information to a pilot dropping dispersal matter so that the dispersal is efficiently accomplished when dispersing dispersal matter from an aircraft over a target location on the groun...
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WO/2013/050564A1 |
Disclosed is a passive flying device, in particular for use as a cargo drop system for dropping cargo from aircraft, or as a rescue system for rescue in air emergencies, said device comprising at least two identical wing elements (7) whi...
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WO/2013/024405A1 |
A method of delivering over the air, shelled portions (110) of fluids or granular substances (120) containing effective ingredients, to a target, is provided herein. The method includes the following stages: selecting (630) a type and a ...
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WO/2013/011441A1 |
A retaining device (1) for retaining snow, avalanches, earth, rocks or similar materials, comprising a retaining barrier (3) and a support strut (2) connected to the retaining barrier (3). The retaining device (1) further comprises a fle...
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WO/2012/177785A1 |
An airdrop package (400) for fuel and water is disclosed. A plurality of hollow cylinders (408) are made of combustible firelog material. Closed water container nested within at least some of the plurality of hollow cylinders. The airdro...
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WO/2012/135300A2 |
An aircraft having a cooling system is disclosed. The cooling system can he used to cool a heat emitting component In one form the cooling system is a refrigerant system and includes a relatively high temperature device such as, but not ...
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WO/2012/125127A1 |
An invention concerns a method achieved to provide fully lying for seats groups of public transport vehicles in the space to be allocated for them and a seats group which uses this method.
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WO/2012/104182A1 |
A fuselage segment (12) for an aircraft fuselage comprises a wall (13) with a closed cross section, a first cabin floor (14), a second cabin floor (16), and a cargo hold floor (18). The first cabin floor (14), the second cabin floor (16)...
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WO/2012/082199A1 |
A wireless precision avionics kit is provided for retrofitting aircraft to facilitate communication between the cockpit and modern military stores without hardware or software modifications to the aircraft. The store includes an electric...
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