Airbus Operations Gmbh

Martin Paetz

Peter Grosse-Plankermann

Thomas Fink

Ulrike Graeber

Peter Kiron

Markus Goslar

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 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 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.

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Hamburg, Germany

Martin Paetz