Daimler Chrysler Ag

Eads Deutschland Gmbh

Nord-micro Elektronik Feinmechanik Ag

Hermann Wandel

Herbert Zippold

Roland Lang

Manfred Palik

Helmut Sommer

Heinz Meister

Michael Jost

Horst Odebrecht

Ronald Gerbig

Robert Fischer-Wilk

Sensor structure of a flow body protruding into a current for carrying out measurements of flow states, containing a structural part () with at least two measuring orifices (), to which transfer lines () are coupled, which guide the flow medium from the measuring orifices () to a pressure converter system () for the purpose of determining the flow states. The outer shell () of the structural part () contains two areas (), which are arranged behind each other viewed in the direction of flow, wherein the first area () has greater thermal conductivity than the second area (). Within the first area () heating elements () are arranged on the structural part (), and are connected with a temperature control circuit with the temperature on the surface of the first area () as a control variable.

Sensor structure and sensor arrangement for measuring flow data on a flow body

An aircraft pitot and static pressure sensing device and an aircraft having the sensing device, more particularly a fighter aircraft, include a plurality of pressure sensors disposed in a radome of the aircraft. In addition, a plurality of air intake ports is provided in the radome. The air intake ports are connected through connecting passages to the pressure sensors.

Aircraft pitot and static pressure sensing device and aircraft having

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Unterhaching, Germany

Hermann Wandel