Polyxeny aircraft additionally provided with hydrofoil
An aircraft and water filling technology, applied in the fields of hydrofoils, ducted propellers, and tilting aircraft, can solve the problems of long-term gliding on the water surface, tip vortex and backflow, and large resistance, and achieve fast and flexible water surface movement capabilities. , The effect of suppressing eddy current and backflow, and increasing the area of the paddle
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Publication Date
- 2019-02-19
Smart Images

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Abstract
Description
technical field
[0001] The present invention relates to the fields of tilting aircraft, hydrofoils and ducted propellers, in particular to a multi-dwelling aircraft, in particular to a multi-dwelling aircraft equipped with hydrofoils. Background technique
[0002] Multi-living aircraft is an aircraft that can operate on water and in the air at the same time, and can take off and land on water. At present, propellers are generally used as propulsion devices in traditional multi-habiting aircraft, but the efficiency of propellers is low and they are easily disturbed by the outside world. Aircraft cannot realize rapid and flexible changes in motion. In addition, the propellers used in traditional multi-habiting aircraft will generate vortex and backflow phenomena at the tips, resulting in low aerodynamic efficiency. Moreover, most traditional multi-habiting aircraft do not have the ability to take off and land vertically on the water surface, so the scope of application is na...
Examples
Embodiment Construction
[0030] In order to make the object, technical solution and effect of the present invention clearer and clearer, the following examples are given to further describe the present invention in detail. It should be pointed out that the specific implementations described here are only used to explain the present invention, not to limit the present invention.
[0031] Such as figure 1 Shown, the polyhedous aircraft of the present invention that installs hydrofoil additionally comprises fuselage 16, the wing 3 on left and right sides of fuselage 16, and left aileron 12 and right aileron are symmetrically installed at the trailing edge place of left and right wing 3 5.
[0032] A hydrofoil device is installed on the abdomen of the lower end of the fuselage 16, and the hydrofoil device includes a group of front hydrofoils 1 and a group of rear hydrofoils 14, and the front hydrofoil 1 is installed on the front part of the fuselage 16 abdomen, so The rear hydrofoil 14 described above i...