The invention provides a tailless flying wing layout plane with a split type wing tip, relating to the technical field of plane structure design, and being used for course regulation of the tailless flying wing layout plane. An upper wing tip and a wing are in shaft driving connection by means of an upper rotary shaft; a lower wing tip and the wing are in shaft driving connection by means of a lower rotary shaft; the upper rotary shaft drives the upper wing tip to deflect; the lower rotary shaft drives the lower wing tip to deflect; by matching with the upper rotary shaft and the lower rotary shaft, the wing is provided with a driving device for controlling the upper rotary shaft and a driving device for controlling the lower rotary shaft. According to the tailless flying wing layout plane with the split type wing tip, under the premises of not damaging the basic appearance of the plane and not adding additional parts, by means of local deflection of the split type wing tip, the course stability of the body of the tailless flying wing layout plane can be effectively increased, and the course operation stability is improved; in case of needing high stealth performance in defense penetration and the like, the plane is quickly converted into a high stealth structure by closing the wing tips.
Tailless flying wing layout plane with split type wing tip
2015-11-11
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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