| 摘要 |
A method and device for adding special substances to the gaseous outflow of the jet engine in order to create a“virtual wall”of increased pressure zone behind the jet engine nozzle which can serve as a support for the jet engine gas outflow to push against, thus increasing the thrust power of the jet engine. This increase in acceleration power results in the accelerated movement of the jet engine equipped vehicle or higher fuel efficiency. A device that adds the special substances to the gaseous outflow is proposed. Characteristics of the special substances, which if added into the jet engine gaseous outflow may create a“virtual wall”of increased pressure zone behind the jet engine, are proposed.
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