The Concept
The SMART turbo
motor was conceived and developed by Daimler Chrysler as a radical
new approach to the drive system for the new City Coupés. This
project aimed at setting new standards in production by focusing
particularly on the weight and therefore the ecological impact of
the car.
The technology implemented by Mercedes-Benz for the
design of this motor made it equally interesting for aircraft
construction:
Ultra
compact, noise-optimized,
complete aluminum construction; dual
ignition concept.
Intensive testing even at continuous full load under all climatic conditions over distances of several million automobile km, and numerous "more than" 1000-hr tests on the testing stations.
The turbo technology with boost control planned from the very beginning of the basic motor concept provides full motor continuous power even at altitudes of 2500m.
The
torque characteristics in combination with the "overboost" ensure
that high power is provided from the very start, even without a
variable pitch propeller.
Fully electronic characteristics control modes and operation monitoring with emergency auxiliary functions ( E-Gas, electronic spark control, mixture control, altitude adaption.....)
State-of–the-art Bosch fuel injection system (carburetor icing not possible), electronically controlled 3-way catalytic converter with Lambda sensor.
What could have been more obvious than to use this motor concept as the basis for a forward-looking airplane engine?