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 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: A cockpit door comprises a hinge 20 provided to one surface and a latch device provided to the other side that can be operated only from the cockpit side. To the inside of a door panel is disposed a reinforcement member 110 formed by laminating multiple layers of sheets with thermoplastic adhesives, the sheets formed by laminating aromatic polyamide fiber onto a honeycomb panel and processing the same into sheet form. A titanium alloy reinforcement plate 400 is disposed to cover the gap G1 between the door body and flap 60. Mounting portions 150 and 160 are provided to the rim of the reinforcement member body 110, and rivet holes 180 are provided thereto. The mounting portion is bent 90 degrees and fixed to the frame by rivets.

Abstract: A washstand unit 10, a waste storage compartment 11, a mirror 12, an upper cabinet 13 and a lighting equipment 14 are disposed on a side panel 5. Fitting concave portions 15 and 16 are formed on the washstand unit 10 for receiving portions of the waste storage compartment 11 and lighting equipment 14. Fitting portions 19, 20 and 21, 22 are formed on the mirror 12 for receiving portions of the upper cabinet 13 and lighting equipment 14. The washstand unit 10, the waste storage compartment 11, the mirror 12, the upper cabinet 13 and the lighting equipment 14 are mounted independently on the side panel 5 without assembling.

Abstract: A cockpit door comprises a hinge 20 provided to one surface and a latch device provided to the other side that can be operated only from the cockpit side. To the inside of a door panel is disposed a reinforcement member 110 formed by laminating multiple layers of sheets with thermoplastic adhesives, the sheets formed by laminating aromatic polyamide fiber onto a honeycomb panel and processing the same into sheet form. A titanium alloy reinforcement plate 400 is disposed to cover the gap G1 between the door body and flap 60. Mounting portions 150 and 160 are provided to the rim of the reinforcement member body 110, and rivet holes 180 are provided thereto. The mounting portion is bent 90 degrees and fixed to the frame by rivets.

Abstract: A washstand unit 10, a waste storage compartment 11, a mirror 12, an upper cabinet 13 and a lighting equipment 14 are disposed on a side panel 5. Fitting concave portions 15 and 16 are formed on the washstand unit 10 for receiving portions of the waste storage compartment 11 and lighting equipment 14. Fitting portions 19, 20 and 21, 22 are formed on the mirror 12 for receiving portions of the upper cabinet 13 and lighting equipment 14. The washstand unit 10, the waste storage compartment 11, the mirror 12, the upper cabinet 13 and the lighting equipment 14 are mounted independently on the side panel 5 without assembling.

Abstract: The object of the present invention is to provide a utility space without decreasing the space for passenger seats, by providing a utility function to a meal service cart and using the meal service cart after finishing the meal service as a bar counter. An in-flight meal service cart 1 includes a box-shaped main body 10 forming a storage space therein, and a utility mechanism (a counter board) 20 equipped so as to be rotatable to the box-shaped main body. The counter board 20 is provided movably between a position of being stored on top of the ceiling board 13 of the main body, and a rotated position of being vertical to the side wall board 12, and when the counter board 20 is in the position of being vertical to the side wall board, it is supported by the opened front and rear doors 17 and 19 in a horizontal condition.

Abstract: An in-flight meal service cart for an aircraft equipped with a box-shaped main body composed of a fireproof material, a plurality of connecting members provided to at least both outer side walls surfaces of the main body, and a cover body composed of cloth for covering at least both side wall surfaces and an upper surface of the box-shaped main body. The cover body is detachable from the main body and is detached from the main body of the meal server, at least during takeoff and landing of an aircraft, so that a fireproof material is exposed as outer wall surfaces. The cover body is a cloth provided at the surface thereof with an advertising function portion for indicating advertising graphic, or advertising phrases.

Abstract: A galley unit 10 for an aircraft is equipped with a utility mechanism (a counter equipment 20 and 200, a decorating wall 131B, and a cabinet 60) provided to at least one wall surface of a box body (closet) 13B, and a cover body (door member 30, cover member 70) with at least its outer wall surfaces made of a special fireproof material. The cover bodies 30 and 70 are construed so as to be movable between a first position for covering the wall surface provided with said utility mechanism, and a second position for opening the wall surface. When the cover bodies are in the first position, outer wall surfaces of the galley unit are all construed from special fireproof material, and the counters 20 and 200 are folded and stored to the side wall surface, and decorators are stored inside the storage space inside the box body.

Abstract: The object of the present invention is to provide a utility space without decreasing the space for passenger seats, by providing a utility function to a meal service cart and using the meal service cart after finishing the meal service as a bar counter.

Abstract: The in-flight meal service cart 1 is equipped with a box-shaped main body 10 composed of a special fireproof material, a plurality of connecting means 110 provided to at least both outer side wall surfaces of the main body, and a cover body 50 composed of cloth for covering at least both side wall surfaces and an upper surface of the box-shaped main body, and the cover body 50 is constituted detachably from said main body 10. And, the cover body 50 is detached from said main body 10 of the meal server at least during takeoff and landing of an aircraft, so that a special fireproof material is exposed as outer wall surfaces 11A, 11B and 13 of the box-shaped main body. The cover body 50 is a cloth provided at the surface thereof with an advertising function portion for indicating advertising graphics, or advertising phrases 60.