Water-air amphibious annular wing aircraft based on thrust vector nozzles and navigation control method of water-air amphibious annular wing aircraft
A technology of thrust vector and control method, which is applied in flight direction control, unmanned aircraft, aircraft, etc., can solve problems such as poor reliability and complicated adjustment mechanism of water and air amphibious vehicles, and achieve low resistance, wide application range and Application scenarios, the effect of large lift-to-drag ratio
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Embodiment 1
[0053] The present embodiment provides a water-air amphibious ring-wing aircraft based on a thrust vectoring nozzle, including:
[0054] The fuselage adopts ring-shaped wings and adopts a design without rudder surfaces;
[0055] A plurality of thrust vectoring power arrays are arranged on the fuselage at regular intervals, the thrust vectoring power arrays include at least one thrust vectoring power unit, and the total number of thrust vectoring power units on the aircraft is 3 to 12.
[0056] Specifically, when the number of thrust vectoring power units included in the thrust vectoring power array is 2 or more, the thrust vectoring power units included therein are fixedly connected through the cover body 9, for example, when one The thrust vectoring power array includes 3 thrust vectoring power units, these 3 thrust vectoring power units can be stacked with one upper part and two lower parts, or the three thrust vectoring power units are fixedly connected in sequence, and the...
Embodiment 2
[0062] see figure 1 and figure 2 , the present embodiment provides a thrust-vectoring nozzle-based water-air amphibious ring-wing aircraft, the thrust-vectoring nozzle-based water-air amphibious ring-wing aircraft includes a thrust vectoring ring-wing layout fuselage and four thrust vectoring power arrays , and arranged in an X-shaped distribution with equal arc lengths on the ring-wing fuselage, and each thrust vector power array has a thrust vector power unit, which specifically includes: when the aircraft is in a horizontal state, from the head of the aircraft To the tail is the visual direction, then define:
[0063] The thrust vector power array located on the upper side of the ring wing’s horizontal symmetry axis and on the right side of the vertical symmetry axis is the first thrust vector power array 1, which is defined to be located on the upper side of the ring wing’s horizontal symmetry axis and to the left of the vertical symmetry axis The thrust vectoring power...
Embodiment 3
[0071] see Figure 6 , this embodiment provides a water-air amphibious ring-wing aircraft that adopts a rectangular layout. The layout of the rectangular ring-shaped wing is directly divided into upper, lower, left, and right parts according to the rectangular sides, and each part is directly stretched through the airfoil section. , different adjacent airfoils are fixed through the cover body of the thrust vectoring power unit, the thrust vectoring power arrays are respectively arranged on the four corners of the rectangle, and each thrust vectoring power array has a thrust vectoring power unit.
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