Flying saucer with rotor
阅读说明：本技术 一种具有旋翼的飞碟 (Flying saucer with rotor ) 是由 杨定生 于 2020-08-13 设计创作，主要内容包括：本发明公开了一种具有旋翼的飞碟,包括本体、以及布设在本体上的第一环形旋翼和第二环形旋翼,所述第一环形旋翼和第二环形旋翼的旋转方向相反,所述第一环形旋翼和第二环形旋翼产生的升力均朝上,所述环形旋翼包括套设在本体外侧的机架、布设在机架上的且套设在本体外侧的可旋转的翼环和沿翼环周向均匀布设的多个翼板；所述翼环可从水平状态调整到倾斜状态。本发明其能源转化及使用效率高,故障率低,且易于大型化和小型化。(The invention discloses a flying saucer with a rotor wing, which comprises a body, a first annular rotor wing and a second annular rotor wing, wherein the first annular rotor wing and the second annular rotor wing are arranged on the body, the rotating directions of the first annular rotor wing and the second annular rotor wing are opposite, the lifting forces generated by the first annular rotor wing and the second annular rotor wing are upward, and each annular rotor wing comprises a rack, a rotatable wing ring and a plurality of wing plates, the rack is sleeved with the outer side of the body, the rotatable wing ring is arranged on the rack, and the wing rings are uniformly arranged along the circumferential direction of the wing ring; the wing ring is adjustable from a horizontal position to an inclined position. The invention has high energy conversion and use efficiency, low failure rate and easy large-scale and miniaturization.)
1. A flying saucer with rotor, its characterized in that: the lifting wing comprises a body, a first annular rotor wing and a second annular rotor wing, wherein the first annular rotor wing and the second annular rotor wing are arranged on the body, the rotating directions of the first annular rotor wing and the second annular rotor wing are opposite, the lifting forces generated by the first annular rotor wing and the second annular rotor wing are upward, each annular rotor wing comprises a rack, a rotatable wing ring and a plurality of wing plates, the rack is sleeved with the outside of the body, the rotatable wing ring is arranged on the rack and sleeved with the outside of the body, and the wing plates are uniformly arranged along the circumferential; the wing ring is adjustable from a horizontal position to an inclined position.
2. A flying saucer having a rotor as claimed in claim 1, wherein: the body comprises a first ring bone, a second ring bone, a third ring bone and a fourth ring bone which are sequentially arranged from top to bottom, and a plurality of vertical bones which are used for connecting the first ring bone, the second ring bone, the third ring bone and the fourth ring bone in series, wherein the vertical bones are uniformly arranged along the circumferential direction of an inner ring of each ring bone;
the frame of the first annular rotor wing comprises an inner ring and an outer ring, the inner ring is horizontally sleeved on the outer side of a second ring bone, the inner ring is supported on the second ring bone through two first rotating shafts, the two first rotating shafts are positioned at two ends of the diameter of the inner ring, and the inner ring can be adjusted to be in an inclined state from a horizontal state relative to the second ring bone through the two first rotating shafts;
the outer ring is horizontally sleeved outside the inner ring, the outer ring is supported on the inner ring through two second rotating shafts, the two second rotating shafts are located at two ends of the diameter of the outer ring, and the straight line where the two first rotating shafts are located is perpendicular to the straight line where the two second rotating shafts are located; the outer ring can be adjusted from a horizontal state to an inclined state relative to the inner ring through two second rotating shafts;
the frame of the second annular rotor wing has the same structure as the frame of the first annular rotor wing;
the outer ring of the first ring rib is universally hinged with two electric push rod devices, the radian of a first ring rib section between the two electric push rod devices is 90 degrees, the telescopic end of one electric push rod device is universally hinged with the inner ring of the first ring rotor wing, and the telescopic end of the other electric push rod device is universally hinged with the outer ring of the first ring rotor wing;
the outer lane universal type of third ring bone articulates there are two electric putter devices, two the radian of third ring bone section between the electric putter device is 90, one of them the flexible end of electric putter device is articulated with the inner ring universal type of second annular rotor, another the flexible end of electric putter device is articulated with the outer loop universal type of second annular rotor.
3. A flying saucer having a rotor as claimed in claim 2, wherein: the frame further comprises a plurality of gears, and the wing ring is driven to rotate by the plurality of gears; the plurality of gears are uniformly distributed along the circumferential direction of the outer ring and can be adjusted to an inclined state along with the outer ring from a horizontal state, the plurality of gears are all meshed with the inner ring of the wing ring, the upper side and the lower side of each gear are uniformly provided with a limiting cover plate, a cavity is formed between two teeth of each gear, one cavity of each gear is meshed with one tooth of the inner ring of the wing ring, and the wing ring is fixed on the plurality of gears; at least one of the gears is a driving gear driven by a driving mechanism to rotate.
4. A flying saucer having a rotor as claimed in claim 3, wherein: the wing ring gear assembly further comprises a shell covering the body, the shell is provided with a notch exposing a gear part, and each gear is meshed with the wing ring through the part exposed from the notch.
5. A flying saucer having a rotor as claimed in claim 2, wherein: an electromagnetic track is distributed along the outer side surface of the outer ring; the inner ring of the wing ring is provided with a plurality of magnets, and the wing ring is driven to rotate through the electromagnetic change of the electromagnetic track.
Technical Field
The invention belongs to the technical field of aircrafts, and particularly relates to a more stable and durable aircraft.
Background
The existing aircraft mainly comprises a fixed wing aircraft and a helicopter, and the lift force of the existing aircraft is formed by the difference between the air pressure flowing at the upper part of the wing and the air pressure flowing at the lower part of the wing. The fixed wing aircraft (jet aircraft) is used for providing forward thrust by jetting air backwards through an engine, and in the forward high-speed movement process of the aircraft, the lift force is formed by the pressure difference formed by the air when the air flows at the upper part and the lower part of the wing; the helicopter drives the rotor at the top to rotate at a high speed through the engine, the air pressure difference flowing between the upper part of the rotor and the lower part of the rotor forms lift force, and meanwhile, the rotor pushes air downwards to form certain upward reaction force.
The helicopter main rotor wing adopts a transmission shaft positioned in the center of the main rotor wing to drive the rotor wing to rotate so as to form an upward lifting force, the front, back, left and right steering is realized by changing the angle of the main rotor wing, and the reaction force of the main rotor wing is counteracted by the thrust generated by the rotation of the tail rotor wing; meanwhile, horizontal hinges, vertical hinges, axial hinges and the like are adopted on the main rotor wing to control the problems of uneven left and right lifting forces, uneven front and back lifting forces, ground resonance prevention and the like generated during flight.
In the existing aircraft, a fixed wing aircraft needs a longer runway to take off, so that an airport runway needs to be built; in order to avoid the disadvantages of the fixed-wing aircraft, the helicopter has many disadvantages such as low energy conversion and use efficiency, high failure rate, difficulty in upsizing, and the like.
The low energy conversion and use efficiency is mainly reflected in that: 1. the weight of the helicopter body is increased by components such as a tail beam, a tail rotor power device, a tail rotor transmission device and the like of the helicopter; even if the unmanned aerial vehicle with multiple rotors is adopted, the components such as a horn for connecting the rotors and the body, a plurality of power devices and the like are also required to be added, and the weight of the body is also increased; 2. in order to avoid uneven front-back, left-right lifting force, a certain flexible material (or a horizontal hinge, a vertical hinge, an axial hinge and other devices) is adopted in the rotor wing, the up-down waving caused by uneven lifting force is avoided, and the energy conversion and the waste in use are caused; 3. the rotor wing of the helicopter has small area and is difficult to be enlarged, and the lift force is generated little;
the high failure rate is mainly reflected in that: all bearing points and core stress points of the traditional helicopter are a transmission shaft positioned in the center of a rotor wing and the root part of the wing near the periphery of the transmission shaft, and the transmission shaft bears the weight of the whole helicopter body and also bears the task of transmitting the power of an engine to the rotor wing; on the other hand, a steering system of the airplane, horizontal hinges, vertical hinges and axial hinges which are arranged for avoiding uneven front, back, left and right lifting forces are all arranged on the periphery of the transmission shaft and the transmission shaft; the failure rate of the helicopter is 2 times higher than that of a fixed-wing aircraft due to the complex structure and the single stress point;
it is difficult to make the size large and to make the size small: the difficult upsizing is mainly because the front, back, left and right lifting forces of the rotor wing are not uniform (flexible materials are needed or devices such as horizontal hinges, vertical hinges, axial hinges and the like are arranged), the core stress points are concentrated on a transmission shaft, aerodynamic interference and the like, and compared with the fixed-wing airplane, the largest helicopter'm 12' produced by the former Soviet Union has the advantages that the
Disclosure of Invention
The technical problem to be solved by the present invention is to provide a flying saucer with a rotor, which has high energy conversion and utilization efficiency, low failure rate, and is easy to be upsized and miniaturized.
In order to solve the technical problems, the invention adopts the technical scheme that: a flying saucer with rotors comprises a body, a first annular rotor and a second annular rotor, wherein the first annular rotor and the second annular rotor are arranged on the body, the rotating directions of the first annular rotor and the second annular rotor are opposite, the lifting forces generated by the first annular rotor and the second annular rotor are upward, the annular rotors comprise a rack, a rotatable wing ring and a plurality of wing plates, the rack is sleeved outside the body, the rotatable wing ring is arranged on the rack and sleeved outside the body, and the wing plates are uniformly arranged along the circumferential direction of the wing ring; the wing ring is adjustable from a horizontal position to an inclined position.
The flying saucer with the rotor wing comprises a body, a first ring bone, a second ring bone, a third ring bone and a fourth ring bone which are sequentially arranged from top to bottom, and a plurality of vertical bones which are formed by connecting the first ring bone, the second ring bone, the third ring bone and the fourth ring bone in series, wherein the vertical bones are uniformly arranged along the circumferential direction of an inner ring of each ring bone;
the frame of the first annular rotor wing comprises an inner ring and an outer ring, the inner ring is horizontally sleeved on the outer side of a second ring bone, the inner ring is supported on the second ring bone through two first rotating shafts, the two first rotating shafts are positioned at two ends of the diameter of the inner ring, and the inner ring can be adjusted to be in an inclined state from a horizontal state relative to the second ring bone through the two first rotating shafts;
the outer ring is horizontally sleeved outside the inner ring, the outer ring is supported on the inner ring through two second rotating shafts, the two second rotating shafts are located at two ends of the diameter of the outer ring, and the straight line where the two first rotating shafts are located is perpendicular to the straight line where the two second rotating shafts are located; the outer ring can be adjusted from a horizontal state to an inclined state relative to the inner ring through two second rotating shafts;
the frame of the second annular rotor wing has the same structure as the frame of the first annular rotor wing;
the outer ring of the first ring rib is universally hinged with two electric push rod devices, the radian of a first ring rib section between the two electric push rod devices is 90 degrees, the telescopic end of one electric push rod device is universally hinged with the inner ring of the first ring rotor wing, and the telescopic end of the other electric push rod device is universally hinged with the outer ring of the first ring rotor wing;
the outer lane universal type of third ring bone articulates there are two electric putter devices, two the radian of third ring bone section between the electric putter device is 90, one of them the flexible end of electric putter device is articulated with the inner ring universal type of second annular rotor, another the flexible end of electric putter device is articulated with the outer loop universal type of second annular rotor.
The flying saucer with the rotor wing, the frame further comprises a plurality of gears, and the wing ring is driven to rotate by the plurality of gears; the plurality of gears are uniformly distributed along the circumferential direction of the outer ring and can be adjusted to an inclined state along with the outer ring from a horizontal state, the plurality of gears are all meshed with the inner ring of the wing ring, the upper side and the lower side of each gear are uniformly provided with a limiting cover plate, a cavity is formed between two teeth of each gear, one cavity of each gear is meshed with one tooth of the inner ring of the wing ring, and the wing ring is fixed on the plurality of gears; at least one of the gears is a driving gear driven by a driving mechanism to rotate.
The flying saucer with the rotor wing further comprises a shell covering the body, the shell is provided with a notch exposing a gear part, and each gear is meshed with the wing ring through the part exposed from the notch.
According to the flying saucer with the rotor wings, the electromagnetic tracks are distributed on the outer side surface of the outer ring; the inner ring of the wing ring is provided with a plurality of magnets, and the wing ring is driven to rotate through the electromagnetic change of the electromagnetic track.
Compared with the prior art, the invention has the following advantages:
1. according to the invention, the first annular rotor wing and the second annular rotor wing are arranged in opposite rotating directions, so that the reaction force generated by rotation can be counteracted, the body is prevented from rotating, and the stability of the body is ensured.
2. The wing rings are adopted to drive the plurality of wing plates, so that compared with the traditional helicopter shaft drive, the wing plate drive mechanism can disperse the acting points at the root parts of the wing plates, reduces force concentration, is more stable and durable, and has low failure rate, reliability and stability and good use effect.
3. The present invention eliminates the need for a tail section such as a helicopter, and the transmission efficiency can be significantly enhanced, and is easy to be upsized and miniaturized.
4. The invention can make the aircraft have the function of moving in four directions, namely front, back, left and right, by using the frame which can be adjusted from a horizontal state to an inclined state.
The technical solution of the present invention is further described in detail by the accompanying drawings and embodiments.
Drawings
Fig. 1 is a schematic structural diagram of
Fig. 2 is a schematic side view of the internal structure of
Fig. 3 is a schematic top view of the internal structure of
Fig. 4 is a schematic view of the connection of the second ring bone with the inner ring and the outer ring in
Fig. 5 is a schematic structural diagram of the first ring bone or the third ring bone in
Fig. 6 is a schematic structural view of a gear according to
Fig. 7 is a schematic top view of the structure of embodiment 2 of the present invention.
Fig. 8 is a schematic view of an assembly of an electromagnetic track and a magnet according to embodiment 2 of the present invention.
Description of reference numerals:
1-body; 2-a first annular rotor; 3-a second annular rotor;
4-wing ring; 5-wing plate; 6-first annulus bone;
7-second ring bone; 8-third ring bone; 9-fourth ring bone;
10-vertical bones; 11-inner ring; 12-an outer ring;
13-a first shaft; 14-a second shaft; 15-an electric push rod device;
16-a bump; 17-a gear; 18-a housing;
19-an electromagnetic track; 20-magnet.
Detailed Description
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