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WO/2009/039787A1 |
A safety rescue aircraft is provided, which scheme can be adapt to a fixed-wing aircraft and a rotorcraft. In the case of large or medium sized aircraft, at least two channel shaped floors are provided. When the aircraft is in danger, pr...
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WO/2009/036551A1 |
A high capacity passenger airplane is provided with a plurality of fuselages (1, 2, 3) releasably mounted on it wings section (5). Each fuselage has an outer shell (17) with a plurality of passenger cabins (20) mounted in tandem within t...
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WO/2009/031022A1 |
Flotation systems including separately packed floats (1) and life rafts (6) are disclosed. Such systems, advantageously used for helicopters or other vessels, attach rafts to exterior covers (3,4) of the floats. Thus, if not needed, or i...
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WO/2009/019603A2 |
The invention relates to a security device for protecting the users and the flying crew in case of technical or human failure onboard an aircraft in all the critical evolution phases of the airplane. The invention relates to a new mode f...
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WO/2009/013502A1 |
The invention provides an anti bomb cell for use with an aircraft for saving the aircraft from destruction in the event of a bomb, wherein the anti bomb cell takes the form of a luggage or cargo storage container capable of storing lugga...
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WO/2008/147339A1 |
This invention is related to a mechanical, electronic and pneumatic system, which will be activated in emergency situations of possible falling down of the aircraft. At this system pilot and passenger cabins (1) will be separated from th...
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WO/2008/127143A1 |
The invention relates to a device for rescuing people in emergency situations. The inventive device comprises a knapsack which is provided with means for fixing it to the back of a rescued person, a part of which is designed in the form ...
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WO2007096689B1 |
Emergency system of Airplane parachute with cusion means if air plane needs make a stop on the way or need . temporary Landing on the way, This system work for Airplane can landing at Emergency on flying tinm. This parachute system are b...
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WO/2008/110343A1 |
The invention relates to an escape path marking for an aircraft, having a plurality of photoluminescent elements (12, 30, 36, 44, 84, 88, 100, 102, 54, 56, 70, 72, 80, 104, 106), which glow in the dark and of which each has a carrier ele...
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WO/2008/110344A1 |
Flight path marking for aircraft, which has an afterglowing photoluminescing material which is placed in several elements on the floor, characterized in that at least one element has a bent shape.
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WO/2008/100711A2 |
Systems and methods for multi-exit evacuation for aircraft are disclosed. In one embodiment, an inflatable evacuation slide for emergency evacuation includes two coupled inflatable portions. The first inflatable portion (112), which incl...
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WO/2008/054401A2 |
A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the ai...
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WO/2008/034992A1 |
The invention relates to a method for locking and unlocking a separation door (5) that separates the cockpit (2) from the cabin (5) of an aircraft (1), comprising : a lock system (12) electrically controlled for locking the door; a contr...
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WO/2008/019697A1 |
Suspending a body in air or reducing its weights by a balloon filled of light nonflammable gas which is charged by a compressed gas in a tank during any emergency. Regaining the gas in the tank happens by an engine and a valve that allow...
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WO/2007/137360A1 |
A head support device is described for providing support to a person (18) travelling in a vehicle, the device comprising a first side restraint (14), a second side restraint (16) and a support (26) defined between the first and second si...
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WO/2007/118035A2 |
In general, the invention is directed to methods and articles for inspecting aircraft life vests using radio frequency identification technology (RFID). In one embodiment, a tamper evident, RFID-enabled package is described, the package ...
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WO/2007/115882A1 |
The invention concerns a device and a method for standby power supply on board an aircraft, capable of powering the aircraft "essential" electrical system. Said device comprises a separately energized synchronous machine (MSI) associated...
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WO/2007/092015A1 |
A passenger aircraft (10) that has a fuselage shell (80) assembly releasably housing a passenger capsule assembly (20). An ejection mechanism is selectively actuated, in emergency situations, to exert a force of predetermined magnitude, ...
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WO/2007/068845A1 |
Device for supplying oxygen to occupants of an aircraft comprising an oxygen source (1) at a first pressure (HP) known as a high pressure, a first oxygen supply line (3) at a second pressure known as an intermediate pressure (IP), first ...
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WO/2007/068169A1 |
A safety air-bag, a safety seat and a lifesaving system for airplane are provided. The lifesaving system includes a lifesaving air-bag (1), which is provided on a seat before inflation and can envelop the user after inflation. A safety a...
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WO/2007/031320A1 |
A system for selective emergency evacuation of persons from a first level (I) to a second level (II) located above the first level (I) or to a third level (III) located under the first level comprises for evacuation to the upper level a ...
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WO/2007/003075A1 |
A improved seat for a vehicle and a plane includes a concave in the middle of the rear end of the seat portion and the other concave in the backrest corresponding to the concave without changing the connections of the seat, the angle adj...
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WO/2006/123048A1 |
The invention relates to a device for establishing contact between an aircraft and a receiving surface (100). The inventive device comprises: at least one inflatable bag (5) which is associated with intake and discharge means (15) for an...
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WO/2006/122626A1 |
The invention relates to a seat, in particular air passenger seat, with seat components, such as a seat part (10) and a backrest (12) with a housing shell (20), which is part of the backrest (12) or which at least partially includes the ...
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WO/2006/105587A1 |
The invention relates to a releasable fastening system (10). The releasable fastening system (10) includes a fastening means having a pair of legs (12), at least part of the legs (12) being adapted for movement towards and away from a ch...
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WO/2006/102817A1 |
A glide type safety airplane comprises of the detachable gliding part and the bearing part. The connection between said two parts is achieved by the electromagnetic coupling. When encountering the emergency accidents, this glide type saf...
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WO/2006/069434A1 |
An emergency electrical power generating apparatus (50) for use with a turbofan engine comprises an electrical generator (52) and a clutch assembly (54). The clutch assembly (54) connects the electrical generator (52) with a fan assembly...
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WO/2006/036137A1 |
An aircraft occupancy, here a helicopter with a seat chassis mounted on a set of rails of any type, ideally as I have demonstrated on load bearing triple monorails with one hundred sixty-eight circumventing roller trucks attached to the ...
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WO/2006/032883A1 |
An aircraft emergency lighting system operable to guide passengers to an exit in an emergency comprises a plurality of units (102) having communication devices (103) arranged to communicate wirelessly with a master controller (107). Each...
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WO/2006/005550A1 |
In a commercial aircraft with a main deck (2) and a lower deck (5, 6), at least one passenger cabin (16, 16’) is also provided on the lower deck. The fuselage diameter lies on the order of a wide-body aircraft, and an energy-absorbing ...
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WO/2005/113285A1 |
An impact-G-force, vector-modifying seat structure in a vehicle, which seat structure introduces, in a forward crash situation, and in a generally vertical plane, a special forward, the upward, and then rearward rotation of the base of t...
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WO/2005/105569A1 |
The present invention relates to a water activated inflator and a method of air deployment of a water activated inflatable device. A gas cylinder opening device for opening a sealing mechanism of the gas cylinder is disposed in the housi...
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WO/2005/097263A1 |
The inventive method for evacuating persons from highly populated objects (buildings, constructions, aircrafts, ships, trains and buses) consists in ejecting people-carrying platforms (1) from said objects and after ejection, in quickly ...
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WO/2005/085061A1 |
A flotation device for maintaining an aircraft in a floating and stable condition is provided. The flotation device comprises at least one flotation bladder mounted to the aircraft and an inflation mechanism for inflating the flotation b...
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WO/2005/080126A1 |
The invention relates to a land, air or sea vehicle comprising a transport compartment for receiving cargo and/or seats that are mounted in the vehicle for conveying personnel, at least one row of seats, which are arranged next to one an...
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WO/2005/028245A1 |
The invention relates to a safety seat for land vehicles, aircraft or sea vessels, consisting of a harness (10) that is suspended from fixed points of the vehicle and that supports a vehicle occupant. Fabric retaining belts (17, 19, 21, ...
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WO/2005/023607A1 |
The invention relates to a position securing system (1) for either sitting or standing-up people in landcraft and aircraft (2). Said system comprises a harness (3) constituted by a two-part lap belt (4), two thigh belts (6), a rear belt ...
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WO/2005/016750A2 |
The invention relates to a circuit for supplying oxygen to aircraft passengers. According to the invention, the line (5) used to supply pressurised oxygen to the passenger masks (6) comprises a motorised pressure regulator (8) which can ...
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WO/2005/016456A2 |
A pilot seat ejection system for use in a number of environments, can be designated for automatic operation. A microprocessor, or other on-board computer, uses avionic sensors to sense an irreversible catastrophe or dangerous situation, ...
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WO/2005/012088A2 |
A method and system for ejection operation in an aircraft are provided. The system allows selection of one of two modes of ejection: ejecting through the canopy; and jettisoning the canopy before ejection. The system includes an ejection...
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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/2004/110864A2 |
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/2004/106155A1 |
What is described is a locally yielding structure (1) with high energy absorption for aeronautical applications, the said structure being substantially closed and substantially rigid, characterized in that at least one wall (3) of the sa...
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WO/2004/106769A1 |
The present invention refers to an apparatus for absorbing energy attenuating a force caused by an impact. In particular it refers to a triggering system for the plastic collapse of a metal structural element, particularly suitable for a...
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WO/2004/078588A1 |
The invention relates to an advantageous design of aircraft, such as passenger or cargo transport aircraft. The invention also relates to a system for loading and unloading aircraft of this type at airports. The invention additionally re...
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WO/2004/074096A1 |
A fire protection apparatus (90, 92) for an oil cooler (26) in an aircraft auxiliary power unit compartment (10) adapted to at least partially cover the oil cooler to thereby at least partially block flames from directly impinging the oi...
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WO/2004/043749A1 |
A pretensioner (6) for tightening an occupant restraint, such as a seatbelt (16), against an occupant on a vehicle. The pretensioner has a locking reel (8) which is activated when a signal is sent by a crash sensing device (2). When such...
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WO/2004/043784A1 |
A protection system for aircraft comprises two parachutes (1,2) mounted to the upper part of the aircraft body. A third parachute (3) is mounted at the tail of the aircraft. The lower part of the aircraft comprises containers (4,5) holdi...
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WO/2004/039643A1 |
A vehicle seat (1) including an arrangement (11) for resisting loads applied to the vehicule seat (1) which comprises a seat base (3) and a seat back (2); said arrangement (11) including a link mechanism (13, 14, 15) connected between th...
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WO/2004/024560A1 |
The invention relates to a vehicle seat for equipment with shoulder belts (24) connected to the seat backrest (21), comprising an energy absorbing device (1) acting on the seat backrest, wherein said energy absorbing device comprises def...
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