a saucer-shaped aircraft
An aircraft and dish-shaped technology, applied in the field of aircraft, can solve the problems of the aircraft being unable to take off and land vertically, high noise, slow flight speed, etc., and achieve the effects of low noise, high noise and good maneuverability.
Inactive Publication Date: 2017-08-08
SHANXI UNIV
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Problems solved by technology
[0003] The purpose of the present invention is to solve the technical problems that the existing aircraft cannot take off and land vertically, the flight speed is slow and the noise is large, and a saucer-shaped aircraft is provided.
Method used
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Embodiment Construction
[0012] As shown in the accompanying drawings, a kind of saucer aircraft in the present embodiment comprises base 1, dish rotor 2, motor 4, inner frame 5, inner frame coil 6, inner frame shaft 7, vertical magnetic field coil 8, outer frame 9. Outer frame coils 10, outer frame shafts 11, support bases 13 and horizontal magnetic field coils 12, the two outer frame shafts 11 are arranged in the middle of the front and rear sides of the outer frame 9, and the outer frame 9 is installed through the two outer frame shafts 11 On the two support seats 13 of the base 1, and the outer frame shaft 11 can rotate on the support seat 13 to drive the outer frame 9 to rotate, and the two inner frame shafts 7 are arranged at the bottom of the inner frame 5 left and right sides, and the inner frame 5 is installed on the outer frame 9 through two inner frame shafts 7, and the two inner frame shafts 7 can rotate on the outer frame 9 to drive the inner frame 5 to rotate, the motor 4 is installed in ...
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The invention belongs to the technical field of aircrafts, and particularly relates to a saucer type aircraft. The technical problems that an existing aircraft cannot achieve vertical take-off and landing and is low in flight speed and large in noise are solved. The saucer type aircraft comprises a base, a saucer-shaped rotary wing, a motor, an inner frame, an inner frame coil, an inner frame shaft, a vertical magnetic field coil, an outer frame, an outer frame coil, an outer frame shaft, a supporting base and a horizontal magnetic field coil. According to the saucer type aircraft, gyroscopic precession is reasonably utilized for adjusting the rotating shaft direction of a saucer-shaped spiral paddle, vertical take-off and landing and hovering can be achieved, and high-speed or low-speed flight in air can be conveniently achieved by adjusting the rotating speed and inclination angle of the saucer-shaped spiral paddle. Procession of the inner frame and that of the outer frame are in rotating fit for use, 360-degree comprehensive rapid and any steering can be achieved, and the maneuverability is good. The saucer-shaped rotary wing is adopted for replacing a traditional helicopter spiral paddle, so that noise brought by rotation of the traditional helicopter spiral paddle is avoided.
Description
technical field [0001] The invention belongs to the technical field of aircraft, and in particular relates to a saucer-shaped aircraft. Background technique [0002] At present, there are no more than two types of practical aircraft: one is a fixed-wing aircraft, that is, a common aircraft, which uses the thrust generated by the propeller or engine to drive the body to slide for a certain distance. The advantage of aerodynamic lift-off is that the flight speed is fast and the load capacity is large; the disadvantage is that it must have a taxiing runway and cannot take off and land vertically. Another rotorcraft is the common helicopter, which has the advantages of vertical take-off and landing and hovering in the air; the disadvantage of slow flight speed and loud noise. Contents of the invention [0003] The purpose of the invention is to solve the technical problems of the existing aircraft that cannot take off and land vertically, the flight speed is slow and the nois...
Claims
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IPC IPC(8): B64C39/00
CPCB64C39/001
Inventor 樊民革
Owner SHANXI UNIV