Airbus Operations Gmbh

Peter Grosse-Plankermann

Martin Paetz

Thomas Fink

Dieter Plehn

Ulrike Graeber

Martin Pätz

Holger Becker

Peter Kiron

Thomas Bardenhagen

Uwe Pietz

Markus Goslar

Philipp Junge

Hans-Juergen Poerschke

Martin PÄTZ

A ventilation system () for installation in an aircraft passenger cabin comprises an air supply pipe (), which has a plurality of air outlet openings () disposed in a distributed manner along its longitudinal axis (L). An air chamber housing () is connectable to the air supply pipe () at various positions along the longitudinal axis (L) of the air supply pipe, such that air-conditioning air flowing through the air supply pipe () is supplyable, through an air outlet opening provided in the air supply pipe (), into the air chamber housing (). A connection device () is designed to connect the air chamber housing () to an air supply device () for supplying air-conditioning air into the aircraft passenger cabin.

Ventilation system and aircraft air-conditioning system

A covering system for an interior space of a vehicle comprises at least one surface element and at least one sealing element. The surface element comprises an upper surface and at least one bounding edge extending at an angle to the upper surface. The surface element furthermore comprises at least one recess, which runs at least adjacent to the bounding edge. The sealing element has an extent corresponding at least partly with the at least one bounding edge, and a shape corresponding at least partly with the recess of the surface element.

Covering system for an interior space of a vehicle, a method for covering a region of an interior space of a vehicle, and a vehicle with an interior space, which is covered by the covering system in at least some regions

A cabin structural unit for attaching cabin installation elements is provided for an aircraft. The cabin structural unit is set up in such a way that a cabin installation element is attachable. The cabin structural unit is implemented as self-supporting and fastenable to an aircraft structure.

Self-supporting cabin structure

A system component module () to be mounted in an aircraft cabin () comprises a support (), to which a PSU duct () as well as an individual air supply system () are attached. A fastening device () is designed to fasten the system component module () to a bottom panel () of a luggage compartment () in the aircraft cabin ().

System component module and method for mounting in an aircraft cabin

A seat bench transport device for transporting a bench of seats for a vehicle, comprising a chassis, a retaining rail pair that is arranged on the chassis and including two retaining rails extending parallel to one another for accommodating seat bench feet. The lengthwise sides of these rails that face one another are open at least in sections and the lengthwise sides thereof that face away from one another each have at least one locking section. A displacement mechanism moves the retaining rails transversely relative to one another.

Seat bench transport device

A cabin structural segment is provided for an aircraft that includes, but is not limited to a fuselage structure and a floor structure. The fuselage structure defines an interior and separating it from an environment. The fuselage structure includes, but is not limited to an opening for a door. It is possible to provide via the opening a connection between the interior and the environment. The cabin structural segment is designed to be self-supporting. The cabin structural segment is fastenable exclusively to the floor structure. The cabin structural segment is constructed in such a way that the one cabin structural segment frames the opening.

Self-supporting cabin structural segment

A system for manufacturing a vehicle cabin includes, but is not limited to at least one first installation component, at least one first surface element, and at least one guide element. The first surface element is slidably arranged on the first installation component with the guide element to form a cabin module, and the guide element is lockable in at least one assembly position and at least one operating position. The resultant cabin module in the assembly position includes, but is not limited to outer dimensions enabling incorporation into a fuselage section of a vehicle, so that the cabin module in the operating position can make up at least a section of the cabin in the fuselage section of the vehicle.

System and method for manufacturing a vehicle cabin

A line system for an aircraft cabin has a line channel with a first surface and a second surface facing in an opposite direction with respect to the first surface. The line system also includes at least one conductor running in the line channel a plurality of first plug channels which enable contacting of the at least one conductor through the first surface, and at least one second plug channel which enables contacting of the at least one conductor through the second surface. At and at least one connector plug with an elongated contact pin which contacts the at least one conductor through the second plug channel, the contact pin having a first section situated in the second plug channel and a second section situated outside the second plug channel.

Line system

The invention relates to an aircraft comprising a force transmission element which detachably connects a cabin structural segment to an aircraft primary structure and which comprises a cabin bearing element and a structure bearing element, the cabin bearing element being connected to the cabin structural segment and the structure bearing element being connected to the aircraft primary structure. The force transmission element is designed in such a manner that a force transmission can take place between the cabin structural segment and the aircraft primary structure with at least one degree of freedom of movement.

Growing community of inventors

Neu Wulmstorf, Germany

Peter Grosse-Plankermann