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WO/2005/016749A1 |
A transfer of ordnance units (20) from a first aerial vehicle (10) to a second aerial vehicle (14) performed while both vehicles are airborne. The first aircraft (10) is used as an ordnance storage, ordnance delivery and ordnance supplie...
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WO/2005/005253A1 |
The invention relates to a pod comprising a central pole (1, 8) having a support section (9) which bears the ends of pivot-mounted arms (30). According to the invention, when retracted against the pole (1, 8), opposing free sections (32)...
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WO/2004/113167A1 |
The invention relates to aircraft equipment, namely to means for cargo disposition in an aircraft and for jettison thereof without parachuting. The inventive device comprises pallets arranged in the cargo section of the aircraft, means f...
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WO/2004/110864A2 |
A rig for use in conjunction with a helicopter or other aircraft which allows the aircraft to be quickly converted to use as platform for rappeling. The rig is preferably constructed of stapping materials into relatively plannar main bod...
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WO/2004/108528A2 |
A method and apparatus for aerial fire suppression utilizing a potable fire retardant chemical dispensing system (1), readily adaptable, without extensive aircraft modification, to various makes of aircraft, for dispensing current types ...
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WO/2004/062732A1 |
A lighter-than-air airship system 10, primarily for the purpose of dispensing water over a raging fire, where access by personnel and ground equipment is difficult. The airship system 10 comprises an aerodynamically configured structure ...
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WO/2004/041365A1 |
An apparatus (10) for initiating and dispensing an incendiary comprises a feed mechanism (12) for advancing a line of series connected incendiaries to a dispensing location D; an injection device (14); and a cutter (16). The injection de...
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WO/2004/041642A1 |
An aerial delivery platform (1) comprising a generally flat base (2) for supporting a payload, at least one pair of inflatable airbags (3) mounted underneath the base and capable of inflation during aerial descent, the airbags having a m...
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WO/2004/031033A2 |
A forward restraint apparatus for restraining a load in an aerial delivery system comprising restraining means (16, 18) to provide forward restraint to a load, which restraining means (18) is pivotally connected to a support body to be d...
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WO/2004/022426A1 |
Firefighting bucket (11) suspended from an aircraft by lines (15), has open top (12A) and a valve at base (13). The valve is attachable to the aircraft by remotely actuatable line (16) and independent movement of lines (15-16) may utilis...
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WO/2004/022403A1 |
Device and method for facilitating loading/unloading of goods from a goods wagon (1) comprising least one load-carrying unit (5), and two wagon portions (10). The wagon portions are provided with means for transport on rail, and the load...
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WO/2004/018345A1 |
The invention relates to a device for compensating for pressure drop in a product pipe through which a liquid flows, and a system comprising such a device. The device comprises a collapsible tube portion, which is connectible to the prod...
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WO/2004/018289A1 |
The invention relates to means for seizing objects during missions for rescuing said objects. The inventive method for seizing an object (1) by another seizing object (2) consists in separating a part (3) of the seized object preserving ...
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WO/2004/017096A2 |
The present invention relates generally to a method and devices for the detection of target objects, such as landmines, using the odor characteristics which may be associated with the target objects as a way of detecting their presence. ...
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WO2003053777A9 |
An autonomous guided parachute system for cargo drops that divides the requirements of guidance and soft landing into separate parachutes. Said invention includes a high wing-loaded ram air parachute for guidance, a larger round parachut...
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WO/2004/009444A1 |
The invention relates to a modular galley for an aircraft or train. The modular galley comprises a wall (1) provided with a multiplicity of guides (2) running in the vertical direction with undercuts as well as a multiplicity of essentia...
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WO/2003/104027A2 |
A patrol system comprising a carriage (1) moving along guiding means (21). The carriage includes propulsion means (15), sensors (11) for acquiring data from outside the carriage and control means (4). An automatic safety method comprisin...
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WO/2003/097450A1 |
The invention relates to flying vehicles, that are more light than an air. The apparatus comprises: elements of a framework, bags, which are filled by gas, means for capture of cargo as well as means for release of ballast. The elements ...
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WO/2003/097453A2 |
A system and method for the conversion of fuel tanks, detachably mountable on the exterior of an aerial vehicle, into high volume, high capacity, diverse functionality and aerodynamically efficient airborne stores is disclosed. A convent...
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WO2002040342A9 |
Short-haul escape system (10) includes line (12) for detechable suspension from support member (20) on airborne vehicle (22), load-carrying receptacle (24) attached to end (12B) of line (12), container (16) attachable to airborne vehicle...
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WO/2003/076267A1 |
The invention relates to a system for loading and unloading a unit load (6), such as in particular items of luggage or similar, into a cargo hold (1) of an aircraft, comprising the transport of the unit load (6) to the inner end of the c...
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WO/2003/074924A1 |
The invention relates to an aircraft comprising a number of lifting rotors and propulsion rotors, provided with an electric motor for each rotor and with a power inverter for each motor. The aim of the invention is to provide an aircraft...
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WO/2003/072432A2 |
An integrated cabin pressure control system valve that uses a dual, redundant channel electronic control unit for both control of the valve (204) and to supply alarm, indication, and control signals to the aircraft's avionics system. Eac...
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WO/2003/063966A1 |
A method of retarding fire comprising, packaging a fire retarding substance in a frangible package (25), and dropping the frangible package (25) from a flying aircraft onto the fire whereby to cause the frangible package (25) to rupture ...
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WO/2003/049959A2 |
A multimodal vehicle includes a ground based vehicle (10) with an attached highÂcapacity airfoil parachute (30) for deployment. The ground based vehicle (10) includes a drive system for use on either land, water or both. Furthermore, th...
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WO2002042149A9 |
A system and mechanism for the movement of large, outsized and heavy cargo includes a tow cable (30) connectable at a first end to a towing vehicle (35) , a buoyant lift vehicle (10) comprising an inflatable member (10), a tether cable (...
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WO/2003/020586A1 |
The invention relates to an altitude protection device for an acceleration protection suit (1) that functions according to the hydrostatic principle, comprising a plurality of liquid-filled leads (4). The inventive protection device furt...
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WO/2003/018401A1 |
The invention relates to a flight path planning device for determining path standards for at least one parachute or paraglider (5), which determines an altitude/time corridor (20, 30) as the flying range to be used by the parachute or pa...
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WO/2003/016135A1 |
A sachet (110) for use in the airdrop delivery of aid, the sachet being adapted to contain food, medical supplies or other aid-related contents in use, the sachet (110) comprising opposing flexible walls (114) sealed together to form, in...
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WO/2002/075235A2 |
A stealth airborne suspended operating system, such as imaging sensor (camera 12), dusting sprinkling device etc., for suspension and operation beneath an aircraft (10), the system comprising a suspension device (14) of predetermined len...
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WO/2002/068851A2 |
The invention relates to transportation and/or storage of an object. The inventive device comprises a container (1), a means for arranging an object (2) and a mechanism for displacing said means. The mechanism is embodied in such away th...
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WO/2002/062662A1 |
The invention relates to the aerospace engineering and can be used for jettisoning boost rockets from an aircraft. The inventive device comprises a landing container (3) with an open end (4) provided with a high-pressure source (5). The ...
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WO/2002/055949A1 |
The present invention provides apparatus for launching devices formed from an elongate housing. The apparatus includes a launch housing (1) that defines an elongate cavity (4), with an aperture (6) extending through a first end of the ho...
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WO2001008972A9 |
A locking pin actuating mechanism comprising a housing, a motor (2) in the housing having an output shaft, a flywheel (1) connected to the motor, clutch (5) in the housing connected to the motor and having input and output shafts, clampi...
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WO/2002/046039A1 |
An invention concerns an aircraft self-gripping load clips of the outer free suspension. In the order to decrease the flight time, to simplify significantly piloting of the aircraft when directing and placing the open load clip on a load...
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WO/2002/036426A2 |
An aircraft drainmast assembly (10) including a drainmast (20) for ejection of waste water from an aircraft (12) and a grounding plate (24) for protection against lightning strike currents. The grounding plate is made of an electrically ...
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WO/2002/030744A1 |
An object holding and releasing mechanism (11) for use in combination with a kite (K), a flight string (S) having a first end (FE) for being held by the flyer of the kite and having a second end (SE), and an object (O) to be released aft...
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WO/2002/028708A2 |
An apparatus is for use with a container of liquid that is suspended from an aircraft flying over a ground target area. The container has an outlet through which the liquid is dropped from the container. The apparatus includes a diffuser...
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WO/2002/024529A1 |
This invention relates to a new design and integration approach in the configuration, capability, and side door, hatch, or other removable pressurized plugs, useful for mounting and operating various types of roll on roll off airborne re...
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WO/2002/010000A1 |
An omni directional vehicle with a frame (1) having a round surface about its perimeter with no apparatus mounted on the frame (1) extending beyond the perimeter. Two independent drive wheels (2) located on an axis (120) through the cent...
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WO/2001/086224A1 |
Aircraft (10) carries at least two clusters of barrel assemblies. At least one cluster is oriented normal to the longitudinal axis of aircraft (10) and at least one other cluster is oriented parallel to the longitudinal axis of aircraft ...
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WO/2001/074143A1 |
Arrangement in a bar, which is intended to hang down beneath a helicopter (1) or the like in order to carry equipment, such as saw equipment for tree lopping, which must be manoeuvred by the helicopter. The bar is designed so that if its...
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WO/2001/069058A2 |
A pump system for loading fluid into a tank (22) onboard a translating aircraft (20) includes a substantially rigid tube member (24) having a diving device (40) on the distal end of the tube member. A strut structure (42) may also be pro...
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WO/2001/066413A1 |
The invention relates to aerial cargo means used for transporting equipped large-sized missile carriers to a region which is optimal for launching thereof and also for fueling and launching said carriers from the upper atmosphere to the ...
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WO/2001/052225A1 |
An emergency drop system allows ballasted advertising banner (14) if disconnected from an aircraft to descend slowly to the ground. Banner (14) is suspended below an aircraft by line (4) held taut by ballasted container (24). Static line...
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WO/2001/028852A1 |
A device (10) for attaching a load (12) to a helicopter (14) comprises at least one support cable (20), which itself comprises a first cable section (22), arranged off-centre with respect to a longitudinal axis (24) of the helicopter (14...
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WO/2001/008975A1 |
The invention relates to an aerospace system designed to put payloads into low and medium orbits. In such a system, a launcher (2) provided with a payload (3) is disposed in the fuselage (5) of the mother aircraft (1), within a transport...
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WO/2001/008974A1 |
The invention relates to an aerospace system designed to put payloads into low and medium orbits. After taking off from an aerodrome, a plane comprising the launcher with the payload heads at cruising speed for the launching area, where ...
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WO2000068077B1 |
Apparatus for transporting a load (24) between source and destination locations, comprising an aircraft having a body (11), power plant (12) carried by the body (11) to drive the aircraft both generally vertically and also generally hori...
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WO/2000/076845A1 |
A towed vehicle deployment and retrieval system for attachment to an aircraft (10). The system includes a pylon support (12) that is designed to mount to an aircraft and project outward therefrom. A stores pylon (16) is mounted to the py...
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