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Patent Searching and Data


Matches 901 - 950 out of 2,077

Document Document Title
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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...  
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...  
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).  
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...  
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...  
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...  
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...  
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...  
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 ...  
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...  
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...  
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 ...  
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.  
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)...  
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...  
WO/2012/077115A2
An add-on sling-load system capable of being attached to a host that comprises a load provided with at least two slices arranged in a predetermined configuration and preferably a stack and a controlled coupling mechanism configured to at...  
WO/2012/066027A1
The present invention creates a connection arrangement, having: a fuselage portion (2); a wing portion (3) which is mounted on the fuselage portion in an upper region thereof; a first Z-coupling element (6) which couples the wing portion...  
WO/2012/067558A1
The present invention regards a pyrotechnic countermeasure (15, 25) dispensing system (1) comprising a set of contacting members (27, 27') of a launching electronic circuitry (19). A first magazine (A) is mountable in said housing (23) i...  
WO/2012/065584A2
The invention relates to an aircraft (1), in particular for inspecting and/or maintaining the structural condition of building structures such as wind power plants (8) having wind turbines (9) with several rotor blades (10). The aircraft...  
WO/2012/045929A1
The present invention relates to the field of devices for airdropping a load from a flying vehicle, wherein specifically the aim of the invention is to provide a device for securing/releasing a first element (65) capable of supporting a ...  
WO/2012/042079A1
The invention relates to the use of the device from the air, allowing fires to be extinguished efficiently, reducing both the time and cost of extinguishing the fires, the device being essentially characterized in that it includes: a cra...  
WO/2012/037595A1
A load attachment system for a helicopter including a load attachment coupling mounted to a helicopter, the load attachment coupling having a load point associated therewith forward of the standard hook attachment and below the centre of...  
WO/2012/028155A1
The force back technology is stands on thermodynamic theories to prove the steam power in fire fighting (1), it assume that fire like any matter in life have a center and certain equilibrium (2). The invention highlighting new applicatio...  
WO/2012/028374A1
In order to be able to airdrop cargo items during a flight, use is made of cargo gates which secure the cargo items and release them at a given time. The present application describes an improved cargo gate. This cargo gate for holding a...  
WO/2011/154325A1
Fire fighting device (1) designed to be fixed under a helicopter (50), said helicopter having landing gear (51) and an external load hook (58), said fire fighting device comprising a frame (2), a fluid reservoir (4), an adjustable fluid ...  
WO/2011/152702A1
A remotely controlled flying apparatus (200) utilized for crop-spraying and crop monitoring purposes is disclosed. The present indention comprises a microcontroller (110) electronically coupled to an inertia measuring means(120). A contr...  
WO/2011/137335A1
A sonar buoy includes a fuselage having a tube-like shape, one or more wings coupled to the fuselage, an engine coupled to the fuselage and operable to propel the sonar buoy through flight, and a guidance computer operable to direct the ...  
WO/2011/113144A1
An aerial fire suppression system mountable to a helicopter fuselage is provided. The system having a tank divided into at least two compartments by a barrier. The base of each compartment having an outwardly opening door. The system als...  
WO/2011/098832A1
A system wherein control of a safety-critical system operation is effected by sending a plurality of keywords via a low integrity transmission means.  
WO/2011/092397A1
The system (1) comprises an outer container (15) which is fixed, directly and fully, in the hold of the transport aeroplane (AC), and in which there is an inner container (4) that can be moved longitudinally and brought from a first carr...  

Matches 901 - 950 out of 2,077