| 摘要 |
In order to use the essential characteristic of the gas turbine previously applied for in P3414814.0-13, that is the alternating admission of fuel gas and compressed cooling air to the turbine wheel blades during each rotation of the shaft, also in a radial gas turbine, the turbine spiral housing is divided by two partition walls into two semi-spiral ducts widening in the same direction, that is a fuel gas duct and an air duct. For the purpose of doubling the torque of the above mentioned gas turbine, two gas turbines of this type are combined on the same shaft centre to form a twin turbine engine in such a way that due to the known annular arrangement of their fuel gas ducts on both turbine blade wheels together a 360-degree fuel gas admission is achieved, thereby giving uninterrupted constant torque during each rotation of the shaft. By doubling the air flow, an increase in power, considerable fuel saving and a carbon-free exhaust gas from these gas turbines is achieved. This engine is intended for use in motor vehicles, motor boats, machinery of all types and sports and passenger aircraft.
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