Air-ground amphibious manned carrier aircraft
An aircraft, ground and air technology, applied in the field of manned aircraft, can solve the problems of large rotor size and inconvenient driving, and achieve the effects of high safety, ease of congestion, and high practicability
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specific Embodiment approach 1
[0019] Specific implementation mode one: combine Figure 1 to Figure 6 Illustrate the present embodiment, a kind of land-air amphibious manned and loaded aircraft, it comprises vehicle body 1, control box 2 and some ducted rotors 3, control box 2 is arranged on the top of vehicle body 1, and each ducted rotor 3 all comprises Guard ring and several evenly distributed propeller blades, it also includes vertically arranged rotor shaft 4, one or more horizontally arranged rotor brackets 5, each of the two ends of each rotor bracket 5 is horizontally fixed to a ducted rotor 3 , each rotor bracket 5 includes a fixed rod 51 and two telescopic rods 52, the two telescopic rods 52 are respectively slidably connected to the two ends of the fixed rod 51 along the length direction of the fixed rod 51, and the middle part of each rotor bracket 5 is respectively The rotor shaft 4 is rotatably fixed on the top of the control box 2. When the aircraft is running on the ground, several rotor bra...
specific Embodiment approach 2
[0028] Specific implementation mode two: combination Figure 1 to Figure 6 Illustrate the present embodiment, a kind of land-air amphibious manned and loaded aircraft, it comprises vehicle body 1, control box 2 and two ducted rotors 3, control box 2 is arranged on the top of vehicle body 1, each ducted rotor 3 It includes a retaining ring and several evenly distributed propeller blades, and it also includes a vertically arranged rotor shaft 4, two horizontally arranged rotor supports 5 arranged parallel to each other, and each rotor support 5 includes a fixed rod 51 and a telescopic rod 52 One end of the fixed rod 51 is rotatably fixed on the top of the control box 2 through the rotor shaft 4, the ducted rotor 3 is fixed on one end of the telescopic rod 52, and the other end of the telescopic rod 52 is slidably connected along the length direction of the fixed rod 51. At the other end of the fixed rod 51, when the aircraft is flying, the two ducted rotors 3 are symmetrically a...
specific Embodiment approach 3
[0034] Specific implementation mode three: combination Figure 1~6To illustrate this embodiment, the rotor shaft 4 includes a plurality of coaxial and rotatably fixed tube shafts 41, the rotor shaft 4 is rotatably fixed above the control box 2, and each tube shaft 41 is provided with an internal The number of the ring gear 42 and the tube shaft 41 is consistent with the number of the rotor bracket 5, and one rotor bracket 5 is fixedly connected with a tube shaft 41. The control box 2 is provided with a motor 21, and several tube shafts 41 pass through the gear pair 43 in turn. Connect with motor 21. Designed in this way, the gear pair includes some gears and some internal gear rings that mesh with each other. For example, when the aircraft is provided with two rotor brackets 5, the motor drives the bottom internal gear ring to rotate through a gear, thereby driving the bottom tube. The shaft rotates, and the uppermost tube shaft is rotated by meshing with the uppermost intern...
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