Abstract: This disclosure is related to a method for applying insulative coating to a carbon-fiber exposed end of a composite material part using a dispenser device. The dispenser device includes a nozzle discharging a first material or a mixed material obtained by mixing the first material and a second material. The method includes discharging the first material or the mixed material from the nozzle toward the carbon-fiber exposed end, and applying the first material or the mixed material to the carbon-fiber exposed end such that the carbon-fiber exposed end is covered with the insulative coating.

Abstract: An aircraft seat structure comprises: a first seat unit comprising a seat region that includes a seat that can be changed between a seat configuration and a bed configuration, and a protruding region that protrudes adjacent to the seat region in a direction perpendicular to the longitudinal direction of the seat region, which are surrounded by a plurality of partition walls; and a second seat unit comprising a seat region that includes a seat that can be changed between a seat configuration and a bed configuration, wherein the protruding region of the first seat unit and the protruding region of the second seat unit are formed so as to protrude in opposite directions relative to each seat region, and the first seat unit and the second seat unit are arranged in such a manner that longitudinal directions thereof match a front-rear direction of the aircraft.

Abstract: An energy absorbing backshell including a non-metallic core, a non-metallic casing surrounding the non-metallic core, a tube on the top surface of the non-metallic core and non-metallic casing.

Abstract: In providing an aircraft lavatory unit capable of suppressing cost and time for installation in a case where a lavatory unit and an ascending/descending unit are to be installed on the aircraft, the present invention provides an aircraft lavatory unit in which a lavatory area and an ascending/descending area are integrally formed, wherein an ascending/descending mechanism which connects to an upper floor or a ceiling space of the aircraft lavatory unit inside the ascending/descending area is provided on a wall surface dividing the lavatory area and the ascending/descending area.

Abstract: This disclosure is related to a method for applying insulative coating to a carbon-fiber exposed end of a composite material part using a dispenser device. The dispenser device includes a nozzle discharging a first material or a mixed material obtained by mixing the first material and a second material. The method includes discharging the first material or the mixed material from the nozzle toward the carbon-fiber exposed end, and applying the first material or the mixed material to the carbon-fiber exposed end such that the carbon-fiber exposed end is covered with the insulative coating.

Abstract: An aircraft seat unit including: a seat configured to change form between a seat state and a bed state; a right side panel that is arranged upright at a right side of the seat; a left side panel that is arranged to oppose the right side panel; and a back surface panel that is arranged upright at a back surface side of the seat so as to connect the right side panel and the left side panel, wherein the right side panel stores a right side footrest portion in an extendable/storable manner and the left side panel stores a left side footrest portion in an extendable/storable manner.

Abstract: An aircraft seat structure comprises: a first seat unit comprising a seat region that includes a seat that can be changed between a seat configuration and a bed configuration, and a protruding region that protrudes adjacent to the seat region in a direction perpendicular to the longitudinal direction of the seat region, which are surrounded by a plurality of partition walls; and a second seat unit comprising a seat region that includes a seat that can be changed between a seat configuration and a bed configuration, wherein the protruding region of the first seat unit and the protruding region of the second seat unit are formed so as to protrude in opposite directions relative to each seat region, and the first seat unit and the second seat unit are arranged in such a manner that longitudinal directions thereof match a front-rear direction of the aircraft.

Abstract: An aircraft seat structure comprises: a first seat unit comprising a seat region that includes a seat that can be changed between a seat configuration and a bed configuration, and a protruding region that protrudes adjacent to the seat region in a direction perpendicular to the longitudinal direction of the seat region, which are surrounded by a plurality of partition walls; and a second seat unit comprising a seat region that includes a seat that can be changed between a seat configuration and a bed configuration, wherein the protruding region of the first seat unit and the protruding region of the second seat unit are formed so as to protrude in opposite directions relative to each seat region, and the first seat unit and the second seat unit are arranged in such a manner that longitudinal directions thereof match a front-rear direction of the aircraft.

Abstract: An aircraft box seat structure that defines an interior space having a plurality of seat units, the aircraft box seat structure including: an upper panel that is substantially rectangular and that defines an upper surface of the interior space; a pair of opposing side wall panels respectively coupled to two opposing sides of the upper panel; a side wall panel coupled to each of the upper panel and the pair of opposing side wall panels; an entrance side wall panel opposing the side wall panel and coupled to each of the upper panel and the pair of opposing side wall panels; and a partition member disposed substantially parallel to the pair of opposing side wall panels in the interior space and displaceable between a deployed position that divides the interior space into a plurality of private rooms and a housing position in which the plurality of private rooms are connected.

Abstract: An aircraft-installed hand dryer including an air for air conditioning supplied from an air conditioning equipment inside a cabin of an aircraft applied as an air for drying.

Abstract: An aircraft passenger seat (100) is fixed to a floor via a seat track fitting (110), and a reclining assembly of the seat is supported by pipes (130, 132) passed through left and right legs (120) and spreaders (170). A linear actuator (300) operates a reclining motion. A curved arm for deformation is provided to a mount (320) on which the actuator (300) is mounted, and a slit (145) is provided in a link plate (140) to which a rod is connected, and in a state where a forward force F is applied, the curved arm deforms and absorbs the impact. An impact absorbing structure is also provided to the legs (120).

Abstract: A passenger seat 100 for an aircraft, including a seat bottom frame 210, a backrest frame 220 and a headrest frame 230 that constitute a reclining assembly, which are supported by a spreader 170 and pipes 130 and 132 fastened to a floor by seat track fittings 110, the pipes 130 and 132 passing through left and right legs 120. A direct-acting-type damper 300 is attached to the backrest frame 230, and an extension member 400 is attached to the headrest frame 230, whereby a structural design is provided in which the reclining assembly, the direct-acting-type damper and the extension member can be easily replaced.

Abstract: A passenger seat 100 for an aircraft, including a seat bottom frame 210, a backrest frame 220 and a headrest frame 230 that constitute a reclining assembly, which are supported by a spreader 170 and pipes 130 and 132 fastened to a floor by seat track fittings 110, the pipes 130 and 132 passing through left and right legs 120. A direct-acting-type damper 300 is attached to the backrest frame 230, and an extension member 400 is attached to the headrest frame 230, whereby a structural design is provided in which the reclining assembly, the direct-acting-type damper and the extension member can be easily replaced.

Abstract: In order to provide an aircraft galley which is equipped with a sink structure ensuring a work space for crews in a galley and a wide drainage region, an aircraft galley unit according to the present invention includes a hot and cold water supply system, a sink structure, and a work table, wherein the sink structure is formed of a double structure including a first sink in which a portion of the work table is formed as a recessed portion, and a box-shaped second sink provided above the first sink.

Abstract: In order to improve ease of maintenance of an aircraft passenger seat, the aircraft passenger seat 100 is adapted to be changeable between an upright position and a bed mode position at which the backrest is folded forward. A mechanism for locking the seat at each of the positions is provided with lock pins 350 provided on both sides of the backrest, a handle unit 200 mounted to a rear face of the backrest, and two wires 300 for connecting the handle unit 200 and the lock pins 350. A structure for connecting the wires 300 to the handle unit 200 is improved to facilitate the maintenance of the wires and to make the handle unit lightweight.

Abstract: In providing an aircraft lavatory unit capable of suppressing cost and time for installation in a case where a lavatory unit and an ascending/descending unit are to be installed on the aircraft, the present invention provides an aircraft lavatory unit in which a lavatory area and an ascending/descending area are integrally formed, wherein an ascending/descending mechanism which connects to an upper floor or a ceiling space of the aircraft lavatory unit inside the ascending/descending area is provided on a wall surface dividing the lavatory area and the ascending/descending area.

Abstract: In order to provide an aircraft galley which is equipped with a sink structure ensuring a work space for crews in a galley and a wide drainage region, an aircraft galley unit according to the present invention includes a hot and cold water supply system, a sink structure, and a work table, wherein the sink structure is formed of a double structure including a first sink in which a portion of the work table is formed as a recessed portion, and a box-shaped second sink provided above the first sink.

Abstract: An aircraft passenger seat (100) has a seat bottom frame (150), and the seat bottom frame (150) is supported by an eccentric cam (210). A seat back frame (170) which rotates about a support point (250) is provided with a damper mechanism (300). When the seat back frame (170) is tilted forward from an upright position about the support point (250), a gas damper (310) is compressed and prevents rapid tilting. This energy assists force for returning the seat back to the upright position. The eccentric cam (210) rotates and lowers the seat bottom frame (150) so as to prevent cushions from being collapsed. A lock mechanism (400) highly rigidly retains the seat back frame at a bed mode position.