Airbus Operations Gmbh

Focke & Co.

Torben Baumgardt

Ralf-Henning Stolte

Reinhard Hoppe

Ralf Barkmann

Stefan Harms

Carsten Weber

Volker Piezunka

Uwe Wollrab

Christian Mueller

Christina Ott

Remy Reynaud

Thomas Jessen

This disclosure relates to a cooler for an aircraft cooling system. The cooler includes a matrix body in which a plurality of coolant channels are designed and extend from a first surface of the matrix body to a second surface of the matrix body, allowing a coolant to flow through the matrix body. The matrix body of the cooler is designed to form a section of the outer skin of the aircraft.

Cooler for an aircraft cooling system, aircraft cooling system and method for operating an aircraft cooling system

An aircraft cooling system () comprises a cooling element (), which comprises a housing (), a cooling air inlet () formed in the housing () and a plurality of heat exchangers (), which are disposed on lateral surfaces () of the housing () and through which cooling air supplied through the cooling air inlet () may flow. A cooling air supply channel () connects a cooling air supply opening (') formed in a tail section of an aircraft to the cooling air inlet () of the cooling element (). A cooling air outlet channel () connects the heat exchangers () of the cooling element () to a cooling air discharge opening ().

Aircraft cooling system

In order to treat cut tobacco so as to loosen and homogenize the same, a tobacco stream () passes through a plurality of processing stations (), in the region of which the tobacco is loosened, during transportation, with the aid of different processing arrangements. The tobacco stream or main stream here is divided up into a plurality of smaller sub-streams during treatment.

Device for the creating of a homogeneous cut tobacco flow

Growing community of inventors

Stade, Germany

Torben Baumgardt