Airbus Operations Gmbh

Sabrina Moje

Matthias Breuer

Uwe Schneider

Dirk Humfeldt

Paul Vine

A separating device for separating two zones of a passenger cabin equipped with overhead luggage bins comprising a movable shell comprising a curtain element made of a flexible material and being dimensioned and shaped so as to be capable of at least partially covering an area extending below an overhead luggage bin with its movable shell being in its closed position in a direction substantially perpendicular to a longitudinal axis of the overhead luggage bin. The curtain element has a first edge adapted to face the movable shell of the overhead luggage bin when the separating device is mounted in the passenger cabin. The separating device further comprises a holder supporting a first end of the first edge of the curtain element and a fixing device adapted to fix a second end of the first edge of the curtain element to the movable shell of the overhead luggage bin.

Separating device for separating two zones of a passenger cabin equipped with overhead luggage bins comprising a movable shell

An aircraft luggage system comprising a luggage compartment which comprises an upper side directed towards a ceiling of an aircraft when the luggage compartment is assembled in the aircraft, a lower side directed towards a floor of the aircraft, a rear side directed towards an outer contour of the aircraft, and two side faces connect the upper side to the lower side. The lower side of the luggage compartment is rigidly connected to the side faces and the rear side of the luggage compartment. A flap, movable between a closed position and an open position, is configured to make an inner space of the luggage compartment accessible or to close it. At least one additional luggage compartment is arranged adjacent to at least one of the upper side and the lower side of the luggage compartment.

Aircraft luggage system having a luggage compartment and an additional luggage compartment

An aircraft interior door assembly () for selectively increasing usable space within an aircraft lavatory () adjacent a passenger doorway area () of the aircraft or in the passenger doorway area () adjacent the lavatory () comprises a door element () and a door element supporting structure (). The door element () is rotatably mounted to the door element supporting structure () so as to be at least rotatable between first and second closed positions relative to the door element supporting structure (). The door element () has the same configuration in both of its closed positions. A door rotation space which is encompassed by the door element () when positioned in its first and second closed positions or rotated through by the door element () when rotated between its first and second closed positions is part of the aircraft lavatory interior space, when the door element () is in its first closed position, and is part of the passenger doorway area (), when the door element () is in its second closed position.

Aircraft interior door assembly

A flight attendant seat comprises a carrier device having a first surface, a seat element movably coupled to the carrier device, and a backrest element movably coupled to the carrier device and operatively coupled to the seat element. The seat is movable between an operative position, permitting the use of the seat by a flight attendant, and an inoperative position in which the seat element and the backrest element are positioned, relative to the carrier device, such that they do not protrude from the carrier device first surface. The seat may be positioned in such a way, relative to a passenger seat or a row of passenger seats, that the rear side of the backrest element faces towards the rear side of a backrest of the passenger seat or the rear side of a backrest of at least one passenger seat belonging to the row of passenger seats.

Flight attendant seat, arrangement having a flight attendant seat, and aircraft area

An aircraft system component carrier system includes at least one aircraft system component carrier module, at least one aircraft system component that is fastened via an aircraft system component holder to the aircraft system component carrier module, and an aircraft structural element of a fuselage upper shell, to which element the aircraft system component carrier module is fastened via a structural holder in such a way that the aircraft system component carrier module, the aircraft system component and the aircraft structural element form an assembly group that is capable of being handled independently.

Aircraft system component carrier system and mounting method

An aircraft system component carrier module includes a carrier element which is arc-shaped at least in sections and is configured, when the module is mounted in an aircraft, to extend at least in some sections substantially in the direction of the ribs of an aircraft structure over at least a section of a crown area of an aircraft cabin. The module includes a transverse carrier element which is configured, when the module is mounted in an aircraft, to extend in the crown area of an aircraft cabin substantially perpendicularly to a longitudinal axis of the cabin. The module further includes a structure holder for fastening the module to the aircraft structure, an aircraft system component holder for fastening at least one of the aircraft system components to the module and an attaching device, connected to the transverse carrier element, for attaching an aircraft luggage compartment to the module.

Aircraft system component carrier module and system

A luggage system includes a luggage compartment having a base body and a flap which is movable between a closed position and an open position and is configured to make accessible or close an interior space of the base body. The flap includes a first flap element facing the interior space of the base body and a second flap element facing away from the interior space of the base body, wherein an installation space for components which are to be installed in the region of the luggage compartment is provided between the first and the second flap element.

Luggage system having a component installation space

An aircraft area comprises a first rib forming a component of an aircraft primary structure and extending in an arc shape along an outer contour of the aircraft area. A second rib is arranged at a distance from the first rib and parallel to the first rib, also forms a component of the aircraft primary structure and extends in an arc shape along the outer contour of the aircraft area. A luggage compartment is arranged between the first and the second rib such that a portion of a first side face of the luggage compartment that faces the first rib is arranged opposite a side face of the first rib that faces the luggage compartment, and/or that a portion of a second side face of the luggage compartment that faces the second rib is arranged opposite a side face of the second rib that faces the luggage compartment.

Aircraft area comprising a luggage compartment

An aircraft monument for installation in an aircraft cabin comprising a first functional module, a second functional module and a side wall for delimiting the first module from at least one of a region of the aircraft cabin adjacent to the first module and a region of the aircraft monument adjacent to the first module. The side wall is movable between a first and a second operational position and comprises a first side-wall region separating the first and second functional modules and in the second operational position, the side wall is displaced in the direction of the second module relative to its position in the first operational position, so that a movement of the side wall from its first operational position into its second operational position results in an enlargement of a base area of the first module and a corresponding diminution of a base area of the second module.

Modifiable aircraft monument

An aircraft monument for installation in an aircraft cabin including a first functional module, the first functional module including a side wall for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module and/or from a region of the aircraft monument adjacent to the first functional module. The side wall is movable between a first and a second operational position and comprises a side-wall region which merely in the second operational position of the side wall serves for delimiting the first functional module from a region of the aircraft cabin adjacent to the first functional module, so that a movement of the side wall out of its first operational position into its second operational position results in an enlargement of a base area of the first functional module.

Expandable aircraft monument

A security door comprises a frame structure, having a lateral surface in which a plurality of doorways are constructed. A first doorway has a first width along an inner circumference of the frame structure, and lateral surface portions delimiting the first doorway in a first direction and a second direction, opposing the first direction, along the inner circumference of the frame structure have a second width. A lock element is received in the frame structure and comprises a first segment, movable along the frame structure inner circumference relative to the frame structure, and a second segment, movable independently of the first segment along the inner circumference relative to the frame structure. The first segment is dimensioned so that, in a position in which it closes the first doorway, it also closes a second doorway adjacent to the first doorway in the first direction along the frame structure inner circumference.

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Hamburg, Germany

Sabrina Moje