Combined type aircraft adopting rotors and vector propulsion system
A technology of vector propulsion and propulsion system, which is applied in the field of combined aircraft of rotor and vector propulsion system, can solve the problems of increasing the weight of the aircraft, affecting the effective load, etc., and achieves the effects of reasonable load distribution, high utilization rate, and improved lift-to-drag ratio.
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[0051] Figure 1 to Figure 3 Shown is an embodiment of the rotor and vector propulsion system combined aircraft provided by the present invention. figure 1 The aircraft 8000 includes a fuselage 8200, which can be used as a lifting body, and a cabin body 8211 is arranged on the fuselage 8200, and the cabin body 8211 can be used to carry people and / or loads. The fuselage 8200 is used as a lifting body to connect with other multiple lifting bodies, specifically as follows: the first side lifting body 8202 and the fourth side lifting body 8209 are respectively arranged on both sides of the fuselage 8200, the first side lifting body 8202 and the fourth side lifting body The fuselage 8209 connects the fuselage 8200 with the first side lifting body through the first front lifting body 8201 and the second front lifting body 8210 arranged at the front end and the first rear lifting body 8203 and the second rear lifting body 8208 arranged at the rear end. 8202 and the fourth side lift ...
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