Flaperon
The invention relates to especially relates to a flaperon, belonging to the field of designing of airplane structures. The flaperon comprises a flap aileron (2), a retreat driving mechanism, a deflection driving mechanism and a watt connecting rod (5). According to the invention, the retreat driving...
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| Hauptverfasser: | , , , , , , , , , , , , , , |
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| Format: | Patent |
| Sprache: | chi ; eng |
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| Zusammenfassung: | The invention relates to especially relates to a flaperon, belonging to the field of designing of airplane structures. The flaperon comprises a flap aileron (2), a retreat driving mechanism, a deflection driving mechanism and a watt connecting rod (5). According to the invention, the retreat driving mechanism and the deflection driving mechanism are designed, and the watt connecting rod (5) is employed for connecting the retreat driving mechanism with the deflection driving mechanism, so the flaperon has an assistant lift enhancement function via left/right synchronous retreat and deflection and roll controlling capability via left/right differential deflection thereon. The flaperon provided by the invention has strong lift enhancement capability and roll controlling efficiency, does not increase the complexity of a flight control system and plays an active role in simplifying control surface configuration of short-distance taking-off and landing airplanes and ship-borne fixed-wing airplanes.
本发明涉及飞机结构设计领域，特别 |
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