Airbus Deutschland Gmbh

Thomas Treimer

Alfred Huber

Ingo Hildebrand

Slawa Babak

Hubert Stützle

Jacek Kogut

An aircraft air conditioning system includes a cyclone unit positioned proximate to at least one discharger, the unit having an inlet opening, which communicates with a fresh air supply line, an intake opening, through which air is sucked in from the aircraft cabin, and at least one outlet opening, which communicates with the at least one discharger. A first, cyclone flow of only fresh air is produced in the cyclone unit during operation of the aircraft air conditioning system, the first cyclone flow tending to draw cabin air into the cyclone unit via the intake opening for mixture with the fresh air, after which a second cyclone flow of the cabin air and fresh air are expelled through the outlet opening and the at least one discharger.

Aircraft air conditioning system with cyclone dischargers

The invention relates to a decompression element for pressure equalization in a cabin of an aircraft, with a decompression element frame, a flap, and a hinge element or at least one bearing element for fitting the flap to the decompression element frame. The hinge element or the bearing element can be produced from a plastics material. A decompression device for decompressing a cabin area includes a decompression device frame, a first opening which enables a flow to take place between a line of an air-conditioning system of the aircraft and the interior space of the decompression device, a second opening which enables a flow to take place between the cabin area and the interior space of the decompression device, and a third opening receiving the decompression element with the flap.

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Laupheim, Germany

Thomas Treimer