摘要 |
The hollow propeller (1) has internal combustion, which is controlled via its shaping. The propeller is simple, and functions without engine, impeller, fuel pump, or moveable part. The hollow blades function as combustion chamber and gas discharge nozzle. The propeller interior is curved, so that a gas stream passing through the blades, is divided into pressure and underpressure zones. Air/fuel is automatically taken-in through the underpressure zone, and the mixture automatically ignites at the continuous combustion. The divided flow directs explosion impulses, heat movement of molecules, recoil, and sound waves in direction of rotation. USE/ADVANTAGE - All-blade propeller functioning as turbine works with all fuels, low energy consumption, low noise.
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申请人 |
WERDING, HANS J., 4520 MELLE, DE |
发明人 |
WERDING, HANS J., 4520 MELLE, DE |