Airbus Operations Gmbh

Frank Rahn

Frank Schneider

Hannes Müller

Carsten Ohlfest

Christiane Lindauer

Ole Becker

A shower system for use in aircraft while in flight, the shower system having a feed line through which a stream of water can be supplied to the shower system; a showerhead from which a prepared stream of shower water can exit the shower system and a water stream parameter modification device for modifying at least one parameter of the water stream, said water stream parameter modification device incorporated between the feed line and the showerhead, wherein the water stream parameter modification device comprises at least one valve, which opens when not exposed to any pressure upstream to enable an evacuation of the entire shower system.

Shower system for aircraft

An arrangement for adapting the transportation behavior of material to be conveyed includes a first container, which is coupleable to a first pressure level; a second container, which is coupleable to a second pressure level; a connecting line for transporting material to be conveyed from the first container to the second container; and a pressure reduction device by which a pressure difference between the first container and the second container is controllably variable.

Arrangement for noise reduction in vacuum systems

The present invention relates to an arrangement for adapting the transportation behavior of material to be conveyed, which arrangement comprises a first container, which is coupleable to a first pressure level; a second container, which is coupleable to a second pressure level; a connecting line for transporting material to be conveyed from the first container to the second container; and a pressure reduction device by means of which a pressure difference between the first container and the second container is controllably variable.

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Buxtehude, Germany

Frank Rahn