Bionic aircraft
A bionic aircraft and shock absorber technology, applied in the field of bionic aircraft, can solve the problems of clumsy flying attitude, poor attitude control, complicated structure, etc., and achieve the effects of rapid and agile change, reasonable aerodynamic pattern, and favorable take-off.
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Embodiment 1
[0039] Embodiment 1: the structure of the present invention is as figure 1 Shown, on the top of the body (1), the tandem parallelogram retractable main wings (2, 3) are assembled bilaterally symmetrically, and the bidirectional parallelogram parallelogram retractable flat empennage (4) is assembled at the rear of the body (1). The underside of the body (1) is assembled into landing gear shock absorbers (40, 41, 42) arranged at three points, and landing gear wheels (5, 6, 7) are assembled on one end of the shock absorbers (40, 41, 42) respectively. , the cockpit (8), the safety umbrella storehouse (9), are assembled on the top of the body (1), the cockpit (8) is before the safety umbrella storehouse (9), and the solid rocket flying aid (10) is assembled on the body (1) ), its axis forms an included angle of 10 to 15 degrees below the central axis of the body (1), the spout faces to the rear and downward, the machine head (11) is assembled in front of the body (1), and the trans...
Embodiment 2
[0063] Embodiment 2: Fig. 7, Figure 8 , Figure 9 Shown are three views of this embodiment, Figure 8 is a front view, and Figure 7 is a top view, Figure 9 It is a left side view, and the present embodiment is to increase a fixed wing of assembling above the center of gravity of the bionic aircraft described in embodiment 1; Delta wing (or rectangular wing), flat tail (4) is refitted into vertical tail (182), horizontal tail (178,179) combined empennage, rudder (183), elevator (180,181).
[0064]Fix assembly with bar member (190,191,192,193) between the triangle fixed wing (189) and the body (1), and one end of dragline (196,197,200,201) is fixedly installed on support bar ( 194), the other end is respectively fixed on the top of the three corners of the triangular fixed wing (189) and the middle position of a side, and one end of the dragline (192, 193, 199, 202) is respectively fixed on the triangular fixed wing (189). Below the middle position of fixed wing (189) belo...
Embodiment 3
[0067] Embodiment 3, Figure 10 , Figure 11 , Figure 12 Shown are three views of this embodiment. Figure 11 is the main view, Figure 10 is a top view, Figure 12 is the left view. In this embodiment, the fixed delta wing above the body (1) of Embodiment 2 is refitted into two streamlined airbags arranged symmetrically in the form of two osprey boats with equal volume and weight. The airbag is supported by a ring skeleton made of aluminum-magnesium alloy or carbon fiber of different sizes. There is a longitudinal opening under each airbag, and a group of gas nozzles are installed at the opening of the lower end of each airbag to fill the airbag with hot gas; or use a sealed The airbag is filled with helium inwardly to provide part of the lift to the aircraft, and the other part of the lift is provided by the main wings (2, 3). When the aircraft is not loaded, it is lighter than the air, and when it is loaded, it is slightly heavier than the air. The thrust of the aircr...
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