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WO/1999/047390A1 |
A restraint harness routed in a pulley configuration which operates between fixed points. The fixed points include: a left and right lap belt (22), each attached to the left and right side (21) of the seat respectively and connected toge...
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WO/1999/044865A1 |
A vehicle restraint system for a seated occupant including an inflatable member (18) mounted on a lap belt (16) and restrained by the belt when inflated. The inflatable member (18) is sized and shaped so that one surface (18a) functions ...
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WO/1999/022968A1 |
An electronic crash sensing unit for detecting and discriminating a crash and actuating occupant safety device(s) such as air bags (108, 109). The unit is designed and constructed to operate within an aircraft, but may be used in ground ...
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WO/1999/017986A1 |
One embodiment of a mechanical emergency dual-release mechanism for use in combination with a helicopter external cargo hook system that includes a cargo hook assembly that is operative to jettison an externally-attached cargo includes a...
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WO/1999/017987A1 |
The invention concerns an aircraft seat base (18) comprising mainly a single-piece structure (20) in composite material. An energy-absorbing element, such as an aluminium alloy ring (42), is inserted in a recess (40) formed in the struct...
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WO/1999/010208A1 |
The helmet restraint system (10) of the invention secures the helmet (12) of a driver (D) or passenger occupant of a vehicle (V), such as a race car, to the structural chassis, body (7) or frame (9) of the vehicle (V), independent of the...
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WO/1999/010234A1 |
A method and system for use in identifying the emergency exits (5, 7, 13) of a structure (such as an aircraft (1), building (60), or ship) in the event smoke is present. Laser generators (50) are mounted along pathways (31) inside of the...
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WO/1998/047762A1 |
The invention relates to a safety seat for use in land, air and sea vehicles, comprising a seat part, a back part and a safety belt device (11). Said safety belt device (11) has two safety belts which fit around the shoulders (13) and tw...
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WO/1998/041126A1 |
A seat assembly (20, 20d, 20e, 20f) for mounting within a cabin of an aircraft comprises a seat surface (32) configured to receive and support at least a portion of the body of a human occupant. An air cell module (34, 34a, 34b, 34c, 34d...
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WO/1998/038455A1 |
A chemically activated lighting system is provided which serves to clearly mark an exit door or hatch as an emergency escape route. The system utilizes two chemical agents which when mixed together form a compound which radiates light. T...
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WO/1998/019908A1 |
An emergency egress system (10) for facilitating emergency egress of passengers/crewmembers from an aircraft (4), which egress system (10) includes an egress panel (12), a panel frame (14) disposed about the egress panel (12) and a weath...
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WO/1998/013232A1 |
The invention is a device to prevent oscillations of the helmet (6) worn by car drivers and plane pilots, and features a frame (2) incorporating a guide (3, 4) with means for the essentially vertical installation of said guide in the coc...
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WO/1998/000309A1 |
To protect a vehicle seat from extreme impact loads, as caused especially when running over a mine and by the explosion thus triggered, it is proposed to secure a buckable cylinder (4), advantageously having a series of drillings (5), up...
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WO/1997/028983A1 |
A leg assembly (22) for mounting passenger seats in transport vehicles especially configured to absorb energy, in the event of a survivable crash or other sudden deceleration. The seat legs deform in a controlled manner to prevent loads ...
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WO/1997/025551A2 |
This invention relates to an improved shock-absorber device (6) comprising numerous small hollow flexible walled bodies which are preferably at least paritally gas-filled and are suspended in a liquid or gel medium and confined by a flex...
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WO/1997/022518A1 |
An improved belt buckle (10) is for an aircraft ejection seat having an arm restraint system with arm restraint cables (38) connected for restraining the arms of the seat occupant against certain movement during seat ejection. The seat b...
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WO/1997/014612A1 |
A helicopter safety system provides an increased likelihood of survivability without injury during "survivable" helicopter crashes. The system includes a spinal compression means (212) for precompressing an operator's spine in response t...
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WO/1997/009235A1 |
Device adapted to the ejector seat of an aircraft in order to minimize in the case of an emergency evacuation the risks of traumatisms and their consequences which can often be serious for the air crew. The invention relates to a device ...
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WO/1997/007022A1 |
The proposed method of effecting an emergency escape from an aircraft travelling at between 500 and 600 km/hr involves, first, ejection of the parachute pack (7) by a firing mechanism (6), followed by ejection of the crew member by anoth...
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WO/1996/040556A1 |
The present invention is an environmentally sealed storage and deployment system for inflatable aircraft escape slides (5) which is comprised of an environmentally sealed vacuum bag (1) and an inflatable escape slide (5). Environmentally...
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WO/1996/039062A1 |
The device is directed to a liquid activated buckle release mechanism for safety belt harnesses and restraint devices used in moving crafts such as airplanes, boats, land based vehicles and the like. The buckle (4) includes a latch (63) ...
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WO/1996/035594A1 |
An aircraft crash sensor activates an aircrew safety device upon sensing an impact in any direction to reduce the possibility of injury caused by the crash. The crash sensor includes a triaxial accelerometer (86) to sense accelerations a...
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WO/1996/033093A1 |
An emergency lighting system for an aircraft has photoluminescent strips (16) mounted on the floor rather than a string of electrical lights. This is a better fail-safe since there is no possibility of a failure in power supply. A channe...
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WO/1996/019381A1 |
A hood detonation system for blasting two hoods in a two-seated aircraft is described. It comprises a first detonation cord (3) detonable by means of initiation and attached to the first, front hood (1), and a second detonation cord (4) ...
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WO/1995/033649A1 |
The proposed method involves the inflation using gas of gas-impermeable casings (4) arranged around the ejection seat. The ejection seat comprises a seat (1) arranged in such a way that it can be propelled in space by a motor (2), a cyli...
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WO/1995/015787A1 |
Inflatable construction comprising a supporting element (1) with walls (2, 3) of a flexible fabric material defining an inner compartment (4). The inner compartment is arranged to be filled with gas under such pressure that the material ...
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WO/1994/022714A1 |
An assembly (5) for restraining the upper limbs of an occupant of a seat, particularly an aircraft ejector seat (1), includes a storage unit (65) which is adapted to be fixedly secured to an upper back portion (16) of the seat (1). The s...
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WO/1994/020327A1 |
An aircraft seat frame (1) includes a plurality of upright seat supports (21, 21', 21'') each formed in one piece of heat-conductive material. Heat-generating electronics (20, 20') are thermally coupled to one of the supports (21, 21', 2...
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WO/1994/016287A1 |
A tactiovisual exit finding system is provided with a collection of tactilely and visually recognizable vees (220, 230, 240, 260, 290) to direct occupants of structures, such as aircraft and public buildings, to the nearest appropriate e...
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WO/1994/012806A1 |
An energy absorber has first and second anchorages (18) and is adapted to absorb energy when and only when an applied load along a line of action extending generally through said anchorages exceeds a predetermined limit. The energy absor...
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WO/1993/024347A1 |
The present invention relates to an inflatable air bag apparatus attached to a harness restraint system in a vehicle which inflates if an impact sensor (28) detects an impact. The apparatus includes a bladder (5) attached to the harness'...
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WO/1993/021389A1 |
An inflatable bridge comprises longitudinal, parallel hoses (10) which support or form a walkway (12) and can be inflated by inflating means. The bridge may further comprise a tunnel-forming cover (15) that can be raised and supported by...
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WO/1993/017894A1 |
An airbag crash protection device for paragliders and other personal aircraft. A compressed gas bottle (21) or pyrotechnic gas generator inflates the airbag (11) when the pilot presses a trigger (34) retained in his hand at the end of a ...
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WO/1992/019464A1 |
A leg structure for constituting a seat by mounting a seat bottom (4) and a seat back (5) on a base frame (3) spanning between front and rear beams (1, 2) in which a diagonal member (8) is caused to extend from the front beam (1) support...
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WO/1992/009456A1 |
The invention concerns an impact-protection cell (12) with an impact-sensitive interior (10) and a cell wall (30), exposed to impacts, surrounding this interior. The aim of the invention is to improve the cell so that, in the event of an...
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WO/1991/017085A1 |
With reference to (Fig. 1), an aircraft passenger seat (1) is mounted on a floor (2) of an aircraft and comprises a body support frame (3), and a pair of rear legs (4), and feet (6, 7) for attaching the frame (3) to the floor (2) so as t...
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WO/1991/012989A1 |
Ejection seat rails (4) that guide an ejection seat (2) out of a vehicle (8), wherein the seat (2) has rollers (10) that travel along the rails (4). The rails (4) are constructed such that the rollers (10) simultaneously disengage from t...
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WO/1991/006786A1 |
An energy absorption device comprising: an elongate body (103) arranged along a longitudinal axis to receive an axial impact force at a first end thereof; apparatus arranged adjacent a second end of the body for deformation thereof; die ...
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WO/1990/009923A1 |
Safety enclosures (100) for use in high speed vehicles such as aircraft and high speed trains. The safety enclosures include an enclosure shell (120) which preferably has two shell walls separated by a crash, acoustic, and thermal resist...
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WO/1990/009905A1 |
A front leg (1) is formed of a linear support pole rising upright from a stationary stud (8) and a rear leg (2) is formed of a lower support pole (2a) extending along a diagonal line connecting the upper end portion of the front leg and ...
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WO/1989/012778A1 |
An impact release apparatus provides an important safety protection for the moving and stationing objects by the principle of releasing impact from crash, vibration or earthquake into the space. Said impact release apparatus comprises me...
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WO/1989/002393A1 |
A flying emergency ejection seat for endangered airman to escape from distressed aircraft and to fly cross country in the seat to sanctuary of a more favorable environment for recovery having the following existing state-of-the-art non-f...
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WO/1989/000521A1 |
An inertia responsive mechanism employs a freely mounted inertia mass in combination with a seat belt retractor mechanism (10) wherein the inertia mass (34, 58, 158, 258) is sensitive to vehicle deceleration or to strap acceleration, or ...
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WO/1988/006120A1 |
Spacecraft, satellite, aeroplane and solid rocket booster are provided with similar locking device, comprise the housing (6-41), sleeve (9-42) and the screw clamps (11-15). The housing (6) is composite with thrust ring (7) and sleeve (9)...
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WO/1988/001968A1 |
An aircrew support system for supporting a pilot's head, and optionally his torso, during high g manoeuvres, enabling him to maintain his head in an upright position and thereby increasing his awareness of the situation at all times outs...
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WO/1988/000896A1 |
In order to ensure that a safety device for car passengers will continue to work in an emergency even if the safety device is cut from its distribution voltage (UV), two separate back-up energy storages (12, 15) are provided to supply vo...
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WO/1987/004990A1 |
A packsack or bag for holding a life jacket, providing an easy access thereto, preferably in an aircraft, has the shape of a pipe with an open end (6) and a closed end (7). The closed end (7) forms a flap (8) to receive at least one fixa...
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WO/1987/002813A1 |
Emergency and/or marker lighting, particularly for aircraft in which a surface or part of a surface is provided with luminescent material, applied in such a way as to be invisible under normal lighting conditions with at least one source...
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WO/1987/002438A1 |
A device to be filled with fluid under pressure includes a plurality of low pressure segments (17), ports (14) and a low pressure compartment (13) interconnecting the segments, and a high pressure compartment (11) arranged such that fill...
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WO/1987/000931A1 |
A beacon comprises a container (1), suitably buoyant for deployment on water. An upwardly projecting cylindrical portion (3) contains a radar transponder (6) and is provided with an antenna (5) coupled to a VHF/UHF radio transmitter (7) ...
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