| 摘要 |
The filed application is a supplement to my U.S. application Ser. No. 10/757,596 and to my German application No.: 103 02 041.1-13, which represent a basic conception for a novel internal combustion engine with the name: Injector-Centrifuge-Turbine-Engine (ICT-Engine) for road vehicles, and injector-Centrifuge-Jet-Engine (ICJ-Engine) for aircraft. New is the introduction of a supersonic injector in place of the turbine and the rotary compressor, and the introduction of a gas-centrifuge for decomposing of the mixed gases. In particular for aircraft, our presently used turbine-engines suffer from fatal turbine-blades crackings, which often results in aircraft crashes, with hundreds of burnt people. This can be eliminated by the novel engine. But also the automobilists would have a profit, by ca. 30% reduction in fuel consumption, arising from removal of the engine cooling and engine friction. The herewith filed application improves an essential component of the above mentioned novel engine, which is the Combi-Supersonic-Adjusting-Plug-Nozzle, fixing for it the following aims: 1) focusing of the jet stream; 2) increasing of the suction effect; 3) improvement of the design; 4) addition of a four-dimensional (4-D) vectoring; 5) suppression of the engine sound. Also the conventional plug-nozzle will be improved in the same manner, making it compatible with the novel injector-Centrifuge-Turbine/Jet-Engine.
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