An unmanned powered delta-wing aircraft
An unmanned and delta-wing technology, which is applied in the field of aircraft, can solve the problems of affecting the payload of the aircraft, reducing the time of the aircraft in the air, and increasing the weight of the whole machine, so as to increase the payload and the time of the air, shorten the sliding distance, The effect of improving safety
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Embodiment 1
[0050] see Figure 1 to Figure 9 , The unmanned powered delta-wing aircraft of the present embodiment is mainly composed of a body 1, a delta wing 2, a power system 3, a flight control system, an operating system 6 and a landing gear system 7.
[0051] see Figure 1 to Figure 9 , the body 1 is a frame structure made of metal materials or engineering plastics, and all components on the machine are arranged on the body 1 . Wherein, the delta wing 2 is arranged above the body 1 , the power system 3 is arranged at the tail of the body 1 , and the operating system 6 and the landing gear system 7 are arranged at the bottom of the body 1 .
[0052] see Figure 1 to Figure 6 and Figure 9 , the delta wing 2 is mainly composed of a triangular frame 21 and a tower 22, wherein the triangular frame 21 includes a keel 211, a crossbeam 212 and two leading edge beams 213, and the two leading edge beams 213 and the crossbeams 212 are fixedly connected to each other , forming a triangle; t...
Embodiment 2
[0075] see Figure 11 , the difference between this embodiment and Embodiment 1 is that in this embodiment, the operating system 6 includes a dispensing device, and the dispensing device is connected to the front bottom of the body 1 through a mounting bracket, so that the aircraft of this embodiment It can be used for pesticide spraying operations, and the spraying device is provided with a spray rod.
[0076] In this embodiment, other implementations other than the above are carried out with reference to Embodiment 1.
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