| 摘要 |
A flying vehicle having a supporting body (which is especially rotationally symmetrical) and having at least one drive unit (which is preferably arranged coaxially on the supporting body), for example a drive motor (engine) having a propeller, and having a cabin as well as a control section, an annular gap being performed between the supporting body and the drive unit and its supporting structure, through which annular gap an airflow is passed downwards, at least two guide-blade rims (9, 10) (which are arranged at a distance one above the other and have in each case two or more, especially adjustable, guide blades (11) (guide vanes)) being provided in the annular gap (4) and immediately above it respectively. <IMAGE>
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