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JP2011069344A |
To reduce the number of fatal accident due to a fall of an aircraft going into a spin.Three valves are fitted to each of engines of an aircraft and a combat plane to reduce the number of fatal accident due to a fall of an aircraft going ...
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JP4647172B2 |
An emergency supplementary vision device comprises a collapsible tube made of airtight material and having an expanded form and a compact stowed form; first and second clear members disposed at respective first and second ends of the tub...
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JP2011504772A |
The present invention provides test equipment (40, 42, 44, 46) for testing an aircraft oxygen system control device (30) comprising one or more detector signal inputs for receiving detector signals representative of one or more condition...
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JP2011504832A |
A flight management verification apparatus adapted to verify at least one flight management, wherein the flight management in use outputs a warning, disables an aircraft and/or inhibits the activation thereof in response to a power fail ...
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JP2010274703A |
To provide a shock absorbing structure capable of sufficiently absorbing shock energy even when a force is applied in a direction perpendicular to a crushing direction.The shock absorbing structure 3 includes a movable bottom plate 7 on ...
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JP2010537944A |
A filter material for generating oxygen and/or hydrogen gas from a source having a porous boron doped carbon film with diRuthenium/diRuthenium molecules in direct contact with the porous boron doped carbon film, a synthetic film having a...
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JP4584738B2 |
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JP2010535347A |
The marker has elongated segments having a light module (12) arranged on a carrier module (10). The light module has a transparent plastic material, in which photoluminescence pigments e.g. strontium aluminate, dysprosium oxide and europ...
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JP2010208479A |
To provide an impact reduction apparatus for an aircraft by which the impact acting on a boarding space is reduced even in the case in which the airframe comes into contact with the ground in the crash of the aircraft in such a way that ...
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JP4541656B2 |
The seat has a backrest structure (3) and a squab structure (2) mounted to pivot with respect to the backrest. The backrest structure is connected to the support structure (5) by a pivot connection (10) and a leg rest (4) is connected by...
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JP4520901B2 |
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JP2010169115A |
To provide an energy absorbing structure for developing a high breaking load while reducing a peak load when impact is applied thereto.The energy absorbing structure 1 includes a honeycomb core 3 having a plurality of cells 2, and a plur...
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JP2010163046A |
To provide an impact absorbing structure for efficiently absorbing an impact irrespective of a posture of an aircraft when the aircraft lands. The impact absorbing structure 2 includes an energy absorbing member 24 for absorbing energy w...
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JP4478594B2 |
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JP4457959B2 |
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JP4407957B2 |
A mechanism (10) arms, disarms, and activates an airplane emergency evacuation system having a slide with one end connected to a girt bar (16). The mechanism includes floor fittings (18) mountable below and at each edge of the airplane d...
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JP2010500214A |
The invention relates to a storage box (13) in which is received a protective mask (4) adapted to be applied on the face of an aircraft crewmember, said storage box further comprising signaling means (19) activable upon occurrence in the...
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JP2009542394A |
The invention relates to a respiratory gas supply circuit (1) for an aircraft carrying passengers and crewmembers (30), comprising a source of breathable gas (R1, R2), at least one supply line (2) connected to said pressurized source, a ...
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JP2009542393A |
The invention relates to a respiratory gas supply circuit (1) for an aircraft carrying passengers and crewmembers (30), comprising a source of breathable gas (R1, R2), at least one supply line (2) connected to said pressurized source, a ...
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JP4345917B2 |
A gas generation method and apparatus capable of use in an aircraft, generates oxygen with at least one On Board Oxygen Generating System (OBOGS) and generates an inert gas with at least one On Board Inert Gas Generating System (OBIGGS) ...
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JP2009534136A |
The invention relates to a system to deliver a respiratory gas to crew members in a cabin of an aircraft. The system includes at least one respiratory mask, an ambient air inlet for admission of ambient air into the respiratory mask, a s...
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JP2009534238A |
The invention relates to a breathing apparatus for providing a respiratory gas to a crewmember in a cabin of an aircraft, said breathable apparatus comprising an air inlet (5) for admission of ambient air in said breathing apparatus, an ...
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JP4329998B2 |
A breathing gas supply system for supplying breathable gas in an aircraft includes an oxygen enriching apparatus which is operable in at least two modes to provide product gas with varying oxygen concentrations. A first feed line feeds m...
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JP2009520621A |
A cargo aircraft has a load-bearing floor bearing one or more cargo containers secured by conventional means. The cargo deck is sub-divided by one or more bulkheads with rearwards-directed airbags that are inflated under emergency condit...
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JP2009519071A |
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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JP4260124B2 |
An aircraft seat which can receive the load of a sitting person with only a back plate member, using no seat back frame, thus eliminating the need for sacrificing the sitting space, which results from the existence of the seat back frame...
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JP4260628B2 |
A breathing gas supply system for an aircraft includes a plurality of oxygen concentrating apparatus, each of which in use, is operable to supply oxygen enriched gas to a breathing gas supply. Each oxygen concentrating apparatus includes...
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JP2009514740A |
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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JP2009514728A |
The invention relates to a breathing apparatus for an aircraft crew member, said apparatus comprising at least one breathing mask (620) provided with a demand regulator (810), said demand regulator being linked through a feedline to a ce...
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JP2009062041A |
To provide a method and arrangement for adjusting nitrogen and oxygen concentrations within regions of an aircraft.The method includes separating nitrogen from ambient air onboard an aircraft thereby establishing a high-concentration nit...
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JP4240260B2 |
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JP4190249B2 |
A conventional fire detection system initially detects the existence of a fire, and initiates a fire alarm. Either automatically or by crew action, Halon(RTM) extinguishant, liquefied under pressure, is piped (3) from a supply vessel (2)...
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JP4160314B2 |
A rescue vehicle (1) having a compartment (2) for receiving a movable stretcher (15) having two mushroom-shaped pins (23, 24) located at a front end and a rear end respectively of the stretcher (15). The compartment (2) has a lateral ope...
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JP4154151B2 |
An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slo...
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JP4155081B2 |
A vertical takeoff and landing apparatus is excellent in the maneuverability and postural stability of its airframe, serves to protect a pilot from an impact when landing, and can make extremely stable flight when hovering near a buildin...
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JP4138136B2 |
A seatbelt system is provided with a retractor, which has a retractor base provided with side plates, a bobbin, a locking member prevented from rotation in a webbing-withdrawing direction in an event of an emergency, a shaft integrally c...
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JP2008525266A |
A wire-strike system (1) including; a wire cutter with at least one pair of electrodes (5, 6), electrically insulated from each other and mounted to an outer surface of an aircraft (2). The electrodes (5, 6) being connectable to a power ...
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JP2008505790A |
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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JP4054066B2 |
A leg assembly 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 at it...
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JP4026746B2 |
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JP4026749B2 |
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JP4014015B2 |
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JP4003852B2 |
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JP3916016B2 |
To prevent an air flow from being introduced from the rear side or from leading out of the inside space to outside in an cover type emergency escape unit. This cover type emergency escape unit is equipped with a seat 1 and a cover 6 supp...
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JP3916015B2 |
To protect the pilot's body when the cover of an emergency escape unit is closing. This emergency escape unit is equipped with a seat 1, a cover 6 supported by a part of the seat 1 and an escape drive handle 20. The cover 6 is made in th...
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JP2007501041A |
The circuit has an oxygen supply line (5) connected to a pressurized oxygen source (1). A pressure regulator operates in response to a pressure control signal provided by an electronic control unit (9). A cabin pressure sensor (12) provi...
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JP2006528042A |
A mask, designed to cover the wearer's nose and mouth and having a semi-supple edge for an improved seal, a tube for delivering a breathable gas mixture from a source, and inlet and outlet valves, incorporates a thin inner filter to let ...
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JP2006523111A |
A storage device ( 50 ) for emergency equipment ( 2, 17, 19 ) for aircraft flight crew. The storage device ( 50 ) is adapted so that the emergency equipment ( 2, 17, 19 ) in the stored position presents at least one grip surface ( 21 ) t...
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JP2006518297A |
A fire protection apparatus for an oil cooler in an aircraft auxiliary power unit compartment adapted to at least partially cover the oil cooler to thereby at least partially block flames from directly impinging the oil cooler in the eve...
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JP2006160233A |
To allow a delta wing-fuselage plane to exert its characteristics at a high speed and secure the buoyancy and maneuverability sufficiently even at a low speed.The delta wing-fuselage plane is given characteristics as a middle to high spe...
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