CN114103570B - Flying motorcycle - Google Patents
Flying motorcycle Download PDFInfo
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- CN114103570B CN114103570B CN202111440807.3A CN202111440807A CN114103570B CN 114103570 B CN114103570 B CN 114103570B CN 202111440807 A CN202111440807 A CN 202111440807A CN 114103570 B CN114103570 B CN 114103570B
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- vortex spraying
- bracket
- vortex
- spraying devices
- electric telescopic
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60K—ARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
- B60K6/00—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00
- B60K6/20—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs
- B60K6/22—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs
- B60K6/24—Arrangement or mounting of plural diverse prime-movers for mutual or common propulsion, e.g. hybrid propulsion systems comprising electric motors and internal combustion engines ; Control systems therefor, i.e. systems controlling two or more prime movers, or controlling one of these prime movers and any of the transmission, drive or drive units Informative references: mechanical gearings with secondary electric drive F16H3/72; arrangements for handling mechanical energy structurally associated with the dynamo-electric machine H02K7/00; machines comprising structurally interrelated motor and generator parts H02K51/00; dynamo-electric machines not otherwise provided for in H02K see H02K99/00 the prime-movers consisting of electric motors and internal combustion engines, e.g. HEVs characterised by apparatus, components or means specially adapted for HEVs characterised by the combustion engines
Abstract
The invention discloses a flying motorcycle, which belongs to the technical field of aircrafts and comprises a controller, a vehicle body, two first vortex spraying devices, two second vortex spraying devices, two third vortex spraying devices and two fourth vortex spraying devices, wherein the two first vortex spraying devices, the two second vortex spraying devices, the two third vortex spraying devices and the two fourth vortex spraying devices are symmetrically arranged relative to the vehicle body; wheels are arranged at the bottom of the vehicle body; the two first vortex spraying devices and the two second vortex spraying devices are positioned on the front side of the vehicle body; the two third vortex spraying devices and the two fourth vortex spraying devices are positioned at the rear side of the vehicle body; the controller is used for controlling the two first vortex spraying devices to spray air forwards, the two second vortex spraying devices and the two third vortex spraying devices to spray air downwards, and the two fourth vortex spraying devices to spray air backwards. The flying motorcycle has compact structure, can realize stable and rapid running on the ground and in the air, has strong environment adaptability, saves a power system and is safer.
Description
Technical Field
The invention belongs to the technical field of aircrafts, and particularly relates to a flying motorcycle.
Background
The flying motorcycle is a motorcycle which runs on the ground and has the function of flying in the air, namely, the land-air amphibious vehicle on which the motorcycle flies is beneficial to solving the problem of urban traffic jam. At present, most of flying motorcycles adopt fixed wings to run off and land, the flying motorcycles have larger size, and the amphibious conversion function can not be flexibly realized; there are also flying motorcycles which take off and land vertically with multiple rotors, but the ground running power system and the air running power system are independent and cannot be shared, so that the cost of the power system is increased, and the flying motorcycle has slow running and insufficient environment adaptability, for example, even on a pothole road, only the ground running power system works, and the air running power system does not work; when any power fails, namely the corresponding ground or air running function fails, and meanwhile, certain potential safety hazards are brought to the flying motorcycle.
In the prior art, a miniature turbojet engine is adopted as a power source of an aircraft, the miniature turbojet engine has the characteristics of small volume, light weight, large thrust-weight ratio and the like, and the automatic control of starting, acceleration and deceleration, stable operation, stopping and the like of the miniature turbojet engine can be realized through a controller.
Disclosure of Invention
The invention aims to provide a flying motorcycle aiming at the defects, and aims to solve the problems that the existing flying motorcycle is not compact in structure, low in ground and air running, weak in environment adaptability, multiple and incompatible in power systems, potential safety hazards exist and the like. In order to achieve the above purpose, the present invention provides the following technical solutions:
the flying motorcycle comprises a controller, a vehicle body 5, two first vortex spraying devices 1, two second vortex spraying devices 2, two third vortex spraying devices 3 and two fourth vortex spraying devices 4 which are symmetrically arranged relative to the vehicle body 5 respectively; wheels are arranged at the bottom of the vehicle body 5; the two first vortex spraying devices 1 and the two second vortex spraying devices 2 are positioned on the front side of the vehicle body 5; the two third vortex spraying devices 3 and the two fourth vortex spraying devices 4 are positioned at the rear side of the vehicle body 5; the controller is used for controlling the two first vortex spraying devices 1 to spray air forwards, the two second vortex spraying devices 2 and the two third vortex spraying devices 3 to spray air downwards, and the two fourth vortex spraying devices 4 to spray air backwards. As can be seen from the above structure, the two first turbojet devices 1 and the two second turbojet devices 2 are located at the front side of the vehicle body 5, the two third turbojet devices 3 and the two fourth turbojet devices 4 are located at the rear side of the vehicle body 5, and the front side and the rear side represent that the positions of the two first turbojet devices 1 and the two second turbojet devices 2 are forward relative to the positions of the two third turbojet devices 3 and the two fourth turbojet devices 4; the controller can control the two first vortex spraying devices 1 to spray air forwards to enable the vehicle body 5 to generate backward thrust and control the thrust, the air nozzles of the first vortex spraying devices 1 face forwards, the controller controls the two second vortex spraying devices 2 and the two third vortex spraying devices 3 to spray air downwards to enable the vehicle body 5 to generate upward thrust and control the thrust, the air nozzles of the second vortex spraying devices 2 and the third vortex spraying devices 3 face downwards, and the controller controls the two fourth vortex spraying devices 4 to spray air backwards to enable the vehicle body 5 to generate forward thrust and control the thrust, and the air nozzles of the fourth vortex spraying devices 4 face backwards. The flying motorcycle of the present invention has a flat road running mode: wheels arranged at the bottom of the vehicle body 5 run in contact with the ground, the wheels are divided into front wheels and one or two rear wheels, and the flying motorcycle can adopt a handle in the prior art to control the direction of the front wheels so as to realize the steering of the flying motorcycle on the ground; only two fourth vortex spraying devices 4 jet air backwards to generate thrust in the forward direction, and the flying motorcycles can travel forwards at a constant speed or accelerate forwards by adopting different thrust values; only two first vortex spraying devices 1 jet forwards to generate thrust in the backward direction, and the forward running flying motorcycles gradually slow down and brake or the static flying motorcycles travel backwards at a uniform speed or accelerate backwards by adopting different thrust values; the flying motorcycle of the invention has an air running mode: the two second vortex spraying devices 2 and the two third vortex spraying devices 3 jet downwards to generate upward thrust, different thrust magnitudes are adopted to ensure that a flying motorcycle is stably emptied or ascends and descends at a constant speed or ascends and descends at an acceleration, then the two fourth vortex spraying devices 4 jet backwards to generate forward thrust, and different thrust magnitudes are adopted to ensure that the flying motorcycle runs forwards at a constant speed or accelerates forwards or uniformly ascends or uniformly dives or dives at an acceleration; the two first vortex spraying devices 1 jet forwards to generate thrust in the backward direction, and the flying motorcycles gradually slow down and brake or the stationary flying motorcycles uniformly travel backwards or accelerate backwards or uniformly pitch backwards or pitch backwards by adopting different thrust; the flying motorcycle turns in the air, and only the thrust of the two first vortex spraying devices 1 or the thrust of the two fourth vortex spraying devices 4 is required to be different. The flying motorcycle of the invention has a pothole road surface or a water accumulation road surface running mode: when the flying motorcycle is on a hollow road or a water accumulation road, the air flow is transmitted to the controller or the controller is manually identified whether the air flow is on the hollow road or the water accumulation road by adopting the road identification sensor, when the air flow is on the hollow road or the water accumulation road, the two second vortex spraying devices 2 and the two third vortex spraying devices 3 jet air downwards to generate upward thrust so as to ensure that the flying motorcycle is stably emptied, then the two fourth vortex spraying devices 4 jet air backwards to generate forward thrust so as to ensure that the flying motorcycle forwards runs or the two first vortex spraying devices 1 jet air forwards to generate backward thrust so as to ensure that the flying motorcycle backwards runs or gradually decelerates and brakes, thereby avoiding road jolt and ensuring the running stability of the flying motorcycle. When the vehicle body 5 passes over a hollow road surface or a water accumulation road surface and then the two second vortex spraying devices 2 and the two third vortex spraying devices 3 jet air downwards, and the upward thrust is reduced, the vehicle body gradually descends to the wheels arranged at the bottom and then contacts the ground to run. The flying motorcycle has only one set of power system, saves the power system, has strong compatibility, can realize the free conversion of a flat road running mode, an air running mode, a hollow road or a ponding road running mode by adopting eight vortex spraying devices, does not need to arrange wings occupying space and can take off without running, has compact structure, adopts the vortex spraying devices which can be a miniature vortex spraying engine in the prior art, can realize the rapid running on the ground and in the air, has the environment adaptability and has quick response and safety.
Further, a front axle 6 is arranged on the front side of the vehicle body 5, and a rear axle 7 is arranged on the rear side of the vehicle body; the first vortex spraying device 1 is connected with the end part of the front shaft 6 through a first bracket 8; the second vortex spraying device 2 is connected with the end part of the front shaft 6 through a second bracket 9; the third vortex spraying device 3 is connected with the end part of the rear shaft 7 through a third bracket 10; the fourth turbojet device 4 is connected to the end of the rear axle 7 by a fourth bracket 11. As can be seen from the above structure, one end of the front axle 6 is connected with a first bracket 8 and a second bracket 9, and the other end is also connected with a first bracket 8 and a second bracket 9, each first bracket 8 is provided with a first vortex spraying device 1, and each second bracket 9 is provided with a second vortex spraying device 2; one end of the rear shaft 7 is connected with a third bracket 10 and a fourth bracket 11, the other end is also connected with a third bracket 10 and a fourth bracket 11, each third bracket 10 is provided with a third vortex spraying device 3, and each fourth bracket 11 is provided with a fourth vortex spraying device 4; the two first turbojet devices 1, the two second turbojet devices 2, the two third turbojet devices 3 and the two fourth turbojet devices 4 exert forces on the vehicle body 5 through the front axle 6, the rear axle 7.
Further, the device also comprises a synchronous driving mechanism, a front deformation mechanism and a rear deformation mechanism; the first bracket 8 is fixed with the front shaft 6, and the second bracket 9 is hinged with the front shaft 6; the third bracket 10 is fixed with the rear axle 7, and the fourth bracket 11 is hinged with the rear axle 7; the synchronous driving mechanism is used for controlling the front shaft 6 and the rear shaft 7 to synchronously rotate; the front deformation mechanism is used for changing the included angle between the first bracket 8 and the second bracket 9; the rear deformation mechanism is used for changing the included angle between the third bracket 10 and the fourth bracket 11. As can be seen from the above structure, in the flat road running mode of the flying motorcycle of the present invention, when the two fourth vortex spraying devices 4 jet air backward and the thrust in the forward direction cannot be satisfied, for example, in the load situation, the backward deformation mechanism changes the included angle between the third bracket 10 and the fourth bracket 11, so that the air jet ports of the third vortex spraying device 3 and the fourth vortex spraying device 4 face in the same direction, the synchronous driving mechanism controls the rear shaft 7 to rotate, the air jet ports of the two third vortex spraying devices 3 and the two fourth vortex spraying devices 4 face backward, the thrust in the forward direction is greatly improved, and even if any fourth vortex spraying device 4 is damaged, the original idle third vortex spraying device 3 can also ensure that the vehicle body 5 has the power for forward running, so that the flying motorcycle is more reliable; when the two first vortex spraying devices 1 jet forwards and the thrust in the backward direction cannot be met, for example, in the case of sudden braking, the front deformation mechanism changes the included angle between the first bracket 8 and the second bracket 9, so that the air jet ports of the first vortex spraying devices 1 and the second vortex spraying devices 2 face the same direction, the synchronous driving mechanism controls the front shaft 6 to rotate, the air jet ports of the two first vortex spraying devices 1 and the two second vortex spraying devices 2 face forwards, the thrust in the backward direction is greatly improved, and even if any one of the first vortex spraying devices 1 is damaged, the original idle second vortex spraying device 2 can also ensure that the vehicle body 5 has the power for driving backwards or gradually decelerating and braking, so that the vehicle is more reliable; in the air running mode of the flying motorcycle, the rear deformation mechanism changes the included angle between the third bracket 10 and the fourth bracket 11, so that the air nozzles of the third vortex spraying device 3 and the fourth vortex spraying device 4 face the same direction, the front deformation mechanism changes the included angle between the first bracket 8 and the second bracket 9, so that the air nozzles of the first vortex spraying device 1 and the second vortex spraying device 2 face the same direction, the synchronous driving mechanism controls the front shaft 6 and the rear shaft 7 to rotate, the air nozzles of the third vortex spraying device 3 and the fourth vortex spraying device 4 face the rear lower part, and the air nozzles of the first vortex spraying device 1 and the second vortex spraying device 2 face the front lower part, at the moment, even if the second vortex spraying device 2 or the third vortex spraying device 3 is damaged, the flying motorcycle can still continue running and stably drop in the air, and the safety and the reliability of the flying motorcycle are improved.
Further, the synchronous driving mechanism comprises a driving motor 12, a driving gear 13, a driven gear 14, a driving rod 15, a front conical gear 16 and a rear conical gear 17; the driving motor 12 is used for driving the driving gear 13 to rotate; the driving gear 13 and the driven gear 14 are meshed with each other; the driven gear 14 is coaxially fixed on the driving rod 15; the front end of the driving rod 15 is provided with a front bevel gear 16, and the rear end of the driving rod is provided with a rear bevel gear 17; the front shaft 6 is provided with a first bevel gear 18 meshed with the front bevel gear 16; the rear axle 7 is provided with a second bevel gear 19 which meshes with the rear bevel gear 17. As can be seen from the above structure, the driving motor 12 drives the driving gear 13 to rotate, the driving gear 13 drives the driven gear 14 to rotate, the driven gear 14 drives the driving rod 15 to rotate, and the driving rod 15 drives the front bevel gear 16 and the rear bevel gear 17 to rotate, so that the first bevel gear 18 and the second bevel gear 19 rotate, and finally the front shaft 6 and the rear shaft 7 synchronously rotate in the same direction.
Further, the front deforming mechanism includes two front electric telescopic rods 20; the front electric telescopic rods 20, the first brackets 8 and the second brackets 9 are in one-to-one correspondence; one end of the front electric telescopic rod 20 is hinged with the corresponding first bracket 8, and the other end of the front electric telescopic rod is hinged with the corresponding second bracket 9; the rear deformation mechanism comprises two rear electric telescopic rods 21; the rear electric telescopic rods 21, the third bracket 10 and the fourth bracket 11 are in one-to-one correspondence; the rear electric telescopic rod 21 is hinged with the corresponding third bracket 10 at one end and is hinged with the corresponding fourth bracket 11 at the other end. According to the structure, the front electric telescopic rod 20 is shortened, the included angle between the first bracket 8 and the second bracket 9 is reduced, the front electric telescopic rod 20 is extended, and the included angle between the first bracket 8 and the second bracket 9 is increased, so that the change of the included angle between the air injection direction of the first vortex spraying device 1 and the air injection direction of the second vortex spraying device 2 is realized; the rear electric telescopic rod 21 is shortened, the included angle between the third bracket 10 and the fourth bracket 11 is reduced, the rear electric telescopic rod 21 is extended, and the included angle between the third bracket 10 and the fourth bracket 11 is increased, so that the change of the included angle between the air injection direction of the third vortex spraying device 3 and the air injection direction of the fourth vortex spraying device 4 is realized.
Further, the air injection direction of the first turbojet device 1 and the air injection direction of the third turbojet device 3 are always vertical; when the front electric telescopic rod 20 is completely contracted, the air injection direction of the first turbojet device 1 is vertical to the air injection direction of the second turbojet device 2; when the front electric telescopic rod 20 is fully extended, the air injection direction of the first vortex spraying device 1 is the same as the air injection direction of the second vortex spraying device 2; when the rear electric telescopic rod 21 is completely contracted, the air injection direction of the third turbojet device 3 is vertical to the air injection direction of the fourth turbojet device 4; when the rear electric telescopic rod 21 is fully extended, the air injection direction of the third turbojet device 3 is the same as the air injection direction of the fourth turbojet device 4. As can be seen from the above structure, when the front electric telescopic rod 20 is fully extended, the air injection direction of the first turbojet device 1 is the same as the air injection direction of the second turbojet device 2; when the rear electric telescopic rod 21 is fully extended, the air injection direction of the third turbojet device 3 is the same as the air injection direction of the fourth turbojet device 4. Then in the flat road running mode of the flying motorcycle, when the two fourth vortex spraying devices 4 jet backwards and the forward thrust cannot be met, the driving motor 12 drives the front shaft 6 and the rear shaft 7 to synchronously rotate in the same direction, so that the air nozzles of the two third vortex spraying devices 3 and the two fourth vortex spraying devices 4 face backwards, the forward thrust is greatly improved, and even if any fourth vortex spraying device 4 is damaged, the third vortex spraying device 3 can also ensure that the vehicle body 5 has forward running power and is more reliable; when the two first vortex spraying devices 1 jet air forwards and the thrust in the backward direction cannot be met, the driving motor 12 drives the front shaft 6 and the rear shaft 7 to synchronously rotate in the same direction, so that the air nozzles of the two first vortex spraying devices 1 and the two second vortex spraying devices 2 face forwards, the thrust in the backward direction is greatly improved, and even if any one of the first vortex spraying devices 1 is damaged, the second vortex spraying devices 2 can also ensure that the vehicle body 5 has power for backward running or gradual speed reduction braking, so that the vehicle is more reliable; in the air running mode of the flying motorcycle, the driving motor 12 drives the front shaft 6 and the rear shaft 7 to synchronously rotate in the same direction, so that the air nozzles of the third vortex spraying device 3 and the fourth vortex spraying device 4 face to the rear lower side, the air nozzles of the first vortex spraying device 1 and the second vortex spraying device 2 face to the front lower side, and at the moment, even if the second vortex spraying device 2 or the third vortex spraying device 3 is damaged, the flying motorcycle can still continue running and stably fall in the air, and the safety and the reliability of the flying motorcycle are improved.
Further, the front electric telescopic rod 20, the rear electric telescopic rod 21 and the driving motor 12 are respectively electrically connected with a controller. The above structure can be used to control the rotation angle of the driving motor 12, and the angle sensor in the prior art can be used to monitor the rotation angle, so as to realize the synchronous and same-direction rotation angle of the front axle 6 and the rear axle 7. The controller can control the front electric telescopic rod 20 and the rear electric telescopic rod 21 to stretch and retract, so that the jet direction of the first vortex spraying device 1 and the jet direction of the second vortex spraying device 2 are vertical or parallel, and the jet direction of the third vortex spraying device 3 and the jet direction of the fourth vortex spraying device 4 are vertical or parallel.
The beneficial effects of the invention are as follows:
the invention discloses a flying motorcycle, which belongs to the technical field of aircrafts and comprises a controller, a vehicle body, two first vortex spraying devices, two second vortex spraying devices, two third vortex spraying devices and two fourth vortex spraying devices, wherein the two first vortex spraying devices, the two second vortex spraying devices, the two third vortex spraying devices and the two fourth vortex spraying devices are symmetrically arranged relative to the vehicle body; wheels are arranged at the bottom of the vehicle body; the two first vortex spraying devices and the two second vortex spraying devices are positioned on the front side of the vehicle body; the two third vortex spraying devices and the two fourth vortex spraying devices are positioned at the rear side of the vehicle body; the controller is used for controlling the two first vortex spraying devices to spray air forwards, the two second vortex spraying devices and the two third vortex spraying devices to spray air downwards, and the two fourth vortex spraying devices to spray air backwards. The flying motorcycle has compact structure, can realize stable and rapid running on the ground and in the air, has strong environment adaptability, saves a power system and is safer.
Drawings
FIG. 1 is a schematic top view of the present invention in section, with a first vortex spraying device spraying air forward, a second vortex spraying device spraying air downward, and a third vortex spraying device spraying air backward;
FIG. 2 is a schematic front view of the first through fourth turbojet devices of FIG. 1;
FIG. 3 is a schematic top view of the present invention, showing the third and fourth vortex spraying devices spraying air backward;
FIG. 4 is a schematic front view of the first through fourth turbojet devices of FIG. 3;
FIG. 5 is a schematic top view of the present invention, showing the first and second vortex spraying devices spraying air forward;
FIG. 6 is a schematic front view of the first through fourth turbojet devices of FIG. 5;
fig. 7 is a schematic front view of the first to fourth vortex spraying devices, the first and second vortex spraying devices spray air forward and downward, and the third and fourth vortex spraying devices spray air backward and downward;
in the accompanying drawings: 1-first vortex spraying device, 2-second vortex spraying device, 3-third vortex spraying device, 4-fourth vortex spraying device, 5-car body, 6-front axle, 7-rear axle, 8-first bracket, 9-second bracket, 10-third bracket, 11-fourth bracket, 12-driving motor, 13-driving gear, 14-driven gear, 15-driving rod, 16-front bevel gear, 17-rear bevel gear, 18-first bevel gear, 19-second bevel gear, 20-front electric telescopic rod and 21-rear electric telescopic rod.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings and the detailed description, but the present invention is not limited to the following examples.
Embodiment one:
see fig. 1-2. The flying motorcycle comprises a controller, a vehicle body 5, two first vortex spraying devices 1, two second vortex spraying devices 2, two third vortex spraying devices 3 and two fourth vortex spraying devices 4 which are symmetrically arranged relative to the vehicle body 5 respectively; wheels are arranged at the bottom of the vehicle body 5; the two first vortex spraying devices 1 and the two second vortex spraying devices 2 are positioned on the front side of the vehicle body 5; the two third vortex spraying devices 3 and the two fourth vortex spraying devices 4 are positioned at the rear side of the vehicle body 5; the controller is used for controlling the two first vortex spraying devices 1 to spray air forwards, the two second vortex spraying devices 2 and the two third vortex spraying devices 3 to spray air downwards, and the two fourth vortex spraying devices 4 to spray air backwards. As can be seen from the above structure, the two first turbojet devices 1 and the two second turbojet devices 2 are located at the front side of the vehicle body 5, the two third turbojet devices 3 and the two fourth turbojet devices 4 are located at the rear side of the vehicle body 5, and the front side and the rear side represent that the positions of the two first turbojet devices 1 and the two second turbojet devices 2 are forward relative to the positions of the two third turbojet devices 3 and the two fourth turbojet devices 4; the controller can control the two first vortex spraying devices 1 to spray air forwards to enable the vehicle body 5 to generate backward thrust and control the thrust, the air nozzles of the first vortex spraying devices 1 face forwards, the controller controls the two second vortex spraying devices 2 and the two third vortex spraying devices 3 to spray air downwards to enable the vehicle body 5 to generate upward thrust and control the thrust, the air nozzles of the second vortex spraying devices 2 and the third vortex spraying devices 3 face downwards, and the controller controls the two fourth vortex spraying devices 4 to spray air backwards to enable the vehicle body 5 to generate forward thrust and control the thrust, and the air nozzles of the fourth vortex spraying devices 4 face backwards. The flying motorcycle of the present invention has a flat road running mode: wheels arranged at the bottom of the vehicle body 5 run in contact with the ground, the wheels are divided into front wheels and one or two rear wheels, and the flying motorcycle can adopt a handle in the prior art to control the direction of the front wheels so as to realize the steering of the flying motorcycle on the ground; only two fourth vortex spraying devices 4 jet air backwards to generate thrust in the forward direction, and the flying motorcycles can travel forwards at a constant speed or accelerate forwards by adopting different thrust values; only two first vortex spraying devices 1 jet forwards to generate thrust in the backward direction, and the forward running flying motorcycles gradually slow down and brake or the static flying motorcycles travel backwards at a uniform speed or accelerate backwards by adopting different thrust values; the flying motorcycle of the invention has an air running mode: the two second vortex spraying devices 2 and the two third vortex spraying devices 3 jet downwards to generate upward thrust, different thrust magnitudes are adopted to ensure that a flying motorcycle is stably emptied or ascends and descends at a constant speed or ascends and descends at an acceleration, then the two fourth vortex spraying devices 4 jet backwards to generate forward thrust, and different thrust magnitudes are adopted to ensure that the flying motorcycle runs forwards at a constant speed or accelerates forwards or uniformly ascends or uniformly dives or dives at an acceleration; the two first vortex spraying devices 1 jet forwards to generate thrust in the backward direction, and the flying motorcycles gradually slow down and brake or the stationary flying motorcycles uniformly travel backwards or accelerate backwards or uniformly pitch backwards or pitch backwards by adopting different thrust; the flying motorcycle turns in the air, and only the thrust of the two first vortex spraying devices 1 or the thrust of the two fourth vortex spraying devices 4 is required to be different. The flying motorcycle of the invention has a pothole road surface or a water accumulation road surface running mode: when the flying motorcycle is on a hollow road or a water accumulation road, the air flow is transmitted to the controller or the controller is manually identified whether the air flow is on the hollow road or the water accumulation road by adopting the road identification sensor, when the air flow is on the hollow road or the water accumulation road, the two second vortex spraying devices 2 and the two third vortex spraying devices 3 jet air downwards to generate upward thrust so as to ensure that the flying motorcycle is stably emptied, then the two fourth vortex spraying devices 4 jet air backwards to generate forward thrust so as to ensure that the flying motorcycle forwards runs or the two first vortex spraying devices 1 jet air forwards to generate backward thrust so as to ensure that the flying motorcycle backwards runs or gradually decelerates and brakes, thereby avoiding road jolt and ensuring the running stability of the flying motorcycle. When the vehicle body 5 passes over a hollow road surface or a water accumulation road surface and then the two second vortex spraying devices 2 and the two third vortex spraying devices 3 jet air downwards, and the upward thrust is reduced, the vehicle body gradually descends to the wheels arranged at the bottom and then contacts the ground to run. The flying motorcycle has only one set of power system, saves the power system, has strong compatibility, can realize the free conversion of a flat road running mode, an air running mode, a hollow road or a ponding road running mode by adopting eight vortex spraying devices, does not need to arrange wings occupying space and can take off without running, has compact structure, adopts the vortex spraying devices which can be a miniature vortex spraying engine in the prior art, can realize the rapid running on the ground and in the air, has the environment adaptability and has quick response and safety.
Embodiment two:
see fig. 1-2. On the basis of the first embodiment, a front shaft 6 is arranged on the front side of the vehicle body 5, and a rear shaft 7 is arranged on the rear side of the vehicle body; the first vortex spraying device 1 is connected with the end part of the front shaft 6 through a first bracket 8; the second vortex spraying device 2 is connected with the end part of the front shaft 6 through a second bracket 9; the third vortex spraying device 3 is connected with the end part of the rear shaft 7 through a third bracket 10; the fourth turbojet device 4 is connected to the end of the rear axle 7 by a fourth bracket 11. As can be seen from the above structure, one end of the front axle 6 is connected with a first bracket 8 and a second bracket 9, and the other end is also connected with a first bracket 8 and a second bracket 9, each first bracket 8 is provided with a first vortex spraying device 1, and each second bracket 9 is provided with a second vortex spraying device 2; one end of the rear shaft 7 is connected with a third bracket 10 and a fourth bracket 11, the other end is also connected with a third bracket 10 and a fourth bracket 11, each third bracket 10 is provided with a third vortex spraying device 3, and each fourth bracket 11 is provided with a fourth vortex spraying device 4; the two first turbojet devices 1, the two second turbojet devices 2, the two third turbojet devices 3 and the two fourth turbojet devices 4 exert forces on the vehicle body 5 through the front axle 6, the rear axle 7.
Embodiment III:
see fig. 1-7. On the basis of the second embodiment, the device also comprises a synchronous driving mechanism, a front deformation mechanism and a rear deformation mechanism; the first bracket 8 is fixed with the front shaft 6, and the second bracket 9 is hinged with the front shaft 6; the third bracket 10 is fixed with the rear axle 7, and the fourth bracket 11 is hinged with the rear axle 7; the synchronous driving mechanism is used for controlling the front shaft 6 and the rear shaft 7 to synchronously rotate; the front deformation mechanism is used for changing the included angle between the first bracket 8 and the second bracket 9; the rear deformation mechanism is used for changing the included angle between the third bracket 10 and the fourth bracket 11. As can be seen from the above structure, in the flat road running mode of the flying motorcycle of the present invention, when the two fourth vortex spraying devices 4 jet air backward and the thrust in the forward direction cannot be satisfied, for example, in the load situation, the backward deformation mechanism changes the included angle between the third bracket 10 and the fourth bracket 11, so that the air jet ports of the third vortex spraying device 3 and the fourth vortex spraying device 4 face in the same direction, the synchronous driving mechanism controls the rear shaft 7 to rotate, the air jet ports of the two third vortex spraying devices 3 and the two fourth vortex spraying devices 4 face backward, the thrust in the forward direction is greatly improved, and even if any fourth vortex spraying device 4 is damaged, the original idle third vortex spraying device 3 can also ensure that the vehicle body 5 has the power for forward running, so that the flying motorcycle is more reliable; when the two first vortex spraying devices 1 jet forwards and the thrust in the backward direction cannot be met, for example, in the case of sudden braking, the front deformation mechanism changes the included angle between the first bracket 8 and the second bracket 9, so that the air jet ports of the first vortex spraying devices 1 and the second vortex spraying devices 2 face the same direction, the synchronous driving mechanism controls the front shaft 6 to rotate, the air jet ports of the two first vortex spraying devices 1 and the two second vortex spraying devices 2 face forwards, the thrust in the backward direction is greatly improved, and even if any one of the first vortex spraying devices 1 is damaged, the original idle second vortex spraying device 2 can also ensure that the vehicle body 5 has the power for driving backwards or gradually decelerating and braking, so that the vehicle is more reliable; in the air running mode of the flying motorcycle, the rear deformation mechanism changes the included angle between the third bracket 10 and the fourth bracket 11, so that the air nozzles of the third vortex spraying device 3 and the fourth vortex spraying device 4 face the same direction, the front deformation mechanism changes the included angle between the first bracket 8 and the second bracket 9, so that the air nozzles of the first vortex spraying device 1 and the second vortex spraying device 2 face the same direction, the synchronous driving mechanism controls the front shaft 6 and the rear shaft 7 to rotate, the air nozzles of the third vortex spraying device 3 and the fourth vortex spraying device 4 face the rear lower part, and the air nozzles of the first vortex spraying device 1 and the second vortex spraying device 2 face the front lower part, at the moment, even if the second vortex spraying device 2 or the third vortex spraying device 3 is damaged, the flying motorcycle can still continue running and stably drop in the air, and the safety and the reliability of the flying motorcycle are improved.
The synchronous driving mechanism comprises a driving motor 12, a driving gear 13, a driven gear 14, a driving rod 15, a front conical gear 16 and a rear conical gear 17; the driving motor 12 is used for driving the driving gear 13 to rotate; the driving gear 13 and the driven gear 14 are meshed with each other; the driven gear 14 is coaxially fixed on the driving rod 15; the front end of the driving rod 15 is provided with a front bevel gear 16, and the rear end of the driving rod is provided with a rear bevel gear 17; the front shaft 6 is provided with a first bevel gear 18 meshed with the front bevel gear 16; the rear axle 7 is provided with a second bevel gear 19 which meshes with the rear bevel gear 17. As can be seen from the above structure, the driving motor 12 drives the driving gear 13 to rotate, the driving gear 13 drives the driven gear 14 to rotate, the driven gear 14 drives the driving rod 15 to rotate, and the driving rod 15 drives the front bevel gear 16 and the rear bevel gear 17 to rotate, so that the first bevel gear 18 and the second bevel gear 19 rotate, and finally the front shaft 6 and the rear shaft 7 synchronously rotate in the same direction.
The front deformation mechanism comprises two front electric telescopic rods 20; the front electric telescopic rods 20, the first brackets 8 and the second brackets 9 are in one-to-one correspondence; one end of the front electric telescopic rod 20 is hinged with the corresponding first bracket 8, and the other end of the front electric telescopic rod is hinged with the corresponding second bracket 9; the rear deformation mechanism comprises two rear electric telescopic rods 21; the rear electric telescopic rods 21, the third bracket 10 and the fourth bracket 11 are in one-to-one correspondence; the rear electric telescopic rod 21 is hinged with the corresponding third bracket 10 at one end and is hinged with the corresponding fourth bracket 11 at the other end. According to the structure, the front electric telescopic rod 20 is shortened, the included angle between the first bracket 8 and the second bracket 9 is reduced, the front electric telescopic rod 20 is extended, and the included angle between the first bracket 8 and the second bracket 9 is increased, so that the change of the included angle between the air injection direction of the first vortex spraying device 1 and the air injection direction of the second vortex spraying device 2 is realized; the rear electric telescopic rod 21 is shortened, the included angle between the third bracket 10 and the fourth bracket 11 is reduced, the rear electric telescopic rod 21 is extended, and the included angle between the third bracket 10 and the fourth bracket 11 is increased, so that the change of the included angle between the air injection direction of the third vortex spraying device 3 and the air injection direction of the fourth vortex spraying device 4 is realized.
The air injection direction of the first vortex spraying device 1 is always vertical to the air injection direction of the third vortex spraying device 3; when the front electric telescopic rod 20 is completely contracted, the air injection direction of the first turbojet device 1 is vertical to the air injection direction of the second turbojet device 2; when the front electric telescopic rod 20 is fully extended, the air injection direction of the first vortex spraying device 1 is the same as the air injection direction of the second vortex spraying device 2; when the rear electric telescopic rod 21 is completely contracted, the air injection direction of the third turbojet device 3 is vertical to the air injection direction of the fourth turbojet device 4; when the rear electric telescopic rod 21 is fully extended, the air injection direction of the third turbojet device 3 is the same as the air injection direction of the fourth turbojet device 4. As can be seen from the above structure, when the front electric telescopic rod 20 is fully extended, the air injection direction of the first turbojet device 1 is the same as the air injection direction of the second turbojet device 2; when the rear electric telescopic rod 21 is fully extended, the air injection direction of the third turbojet device 3 is the same as the air injection direction of the fourth turbojet device 4. Then in the flat road running mode of the flying motorcycle, when the two fourth vortex spraying devices 4 jet backwards and the forward thrust cannot be met, the driving motor 12 drives the front shaft 6 and the rear shaft 7 to synchronously rotate in the same direction, so that the air nozzles of the two third vortex spraying devices 3 and the two fourth vortex spraying devices 4 face backwards, the forward thrust is greatly improved, and even if any fourth vortex spraying device 4 is damaged, the third vortex spraying device 3 can also ensure that the vehicle body 5 has forward running power and is more reliable; when the two first vortex spraying devices 1 jet air forwards and the thrust in the backward direction cannot be met, the driving motor 12 drives the front shaft 6 and the rear shaft 7 to synchronously rotate in the same direction, so that the air nozzles of the two first vortex spraying devices 1 and the two second vortex spraying devices 2 face forwards, the thrust in the backward direction is greatly improved, and even if any one of the first vortex spraying devices 1 is damaged, the second vortex spraying devices 2 can also ensure that the vehicle body 5 has power for backward running or gradual speed reduction braking, so that the vehicle is more reliable; in the air running mode of the flying motorcycle, the driving motor 12 drives the front shaft 6 and the rear shaft 7 to synchronously rotate in the same direction, so that the air nozzles of the third vortex spraying device 3 and the fourth vortex spraying device 4 face to the rear lower side, the air nozzles of the first vortex spraying device 1 and the second vortex spraying device 2 face to the front lower side, and at the moment, even if the second vortex spraying device 2 or the third vortex spraying device 3 is damaged, the flying motorcycle can still continue running and stably fall in the air, and the safety and the reliability of the flying motorcycle are improved.
The front electric telescopic rod 20, the rear electric telescopic rod 21 and the driving motor 12 are respectively and electrically connected with a controller. The above structure can be used to control the rotation angle of the driving motor 12, and the angle sensor in the prior art can be used to monitor the rotation angle, so as to realize the synchronous and same-direction rotation angle of the front axle 6 and the rear axle 7. The controller can control the front electric telescopic rod 20 and the rear electric telescopic rod 21 to stretch and retract, so that the jet direction of the first vortex spraying device 1 and the jet direction of the second vortex spraying device 2 are vertical or parallel, and the jet direction of the third vortex spraying device 3 and the jet direction of the fourth vortex spraying device 4 are vertical or parallel.
The foregoing description is only of the preferred embodiments of the present invention and is not intended to limit the scope of the invention, and all equivalent structures or equivalent processes using the descriptions and drawings of the present invention or directly or indirectly applied to other related technical fields are included in the scope of the invention.
Claims (2)
1. The flying motorcycle is characterized in that: the device comprises a controller, a vehicle body (5), two first vortex spraying devices (1), two second vortex spraying devices (2), two third vortex spraying devices (3) and two fourth vortex spraying devices (4) which are symmetrically arranged relative to the vehicle body (5); wheels are arranged at the bottom of the vehicle body (5); the two first vortex spraying devices (1) and the two second vortex spraying devices (2) are positioned at the front side of the vehicle body (5); the two third vortex spraying devices (3) and the two fourth vortex spraying devices (4) are positioned at the rear side of the vehicle body (5); the controller is used for controlling the two first vortex spraying devices (1) to spray air forwards, the two second vortex spraying devices (2) and the two third vortex spraying devices (3) to spray air downwards, and the two fourth vortex spraying devices (4) to spray air backwards; a front shaft (6) is arranged on the front side of the vehicle body (5), and a rear shaft (7) is arranged on the rear side of the vehicle body; the first vortex spraying device (1) is connected with the end part of the front shaft (6) through a first bracket (8); the second vortex spraying device (2) is connected with the end part of the front shaft (6) through a second bracket (9); the third vortex spraying device (3) is connected with the end part of the rear shaft (7) through a third bracket (10); the fourth vortex spraying device (4) is connected with the end part of the rear shaft (7) through a fourth bracket (11); the device also comprises a synchronous driving mechanism, a front deformation mechanism and a rear deformation mechanism; the first bracket (8) is fixed with the front shaft (6), and the second bracket (9) is hinged with the front shaft (6); the third bracket (10) is fixed with the rear shaft (7), and the fourth bracket (11) is hinged with the rear shaft (7); the synchronous driving mechanism is used for controlling the front shaft (6) and the rear shaft (7) to synchronously rotate; the front deformation mechanism is used for changing the included angle between the first bracket (8) and the second bracket (9); the rear deformation mechanism is used for changing the included angle between the third bracket (10) and the fourth bracket (11); the synchronous driving mechanism comprises a driving motor (12), a driving gear (13), a driven gear (14), a driving rod (15), a front conical gear (16) and a rear conical gear (17); the driving motor (12) is used for driving the driving gear (13) to rotate; the driving gear (13) and the driven gear (14) are meshed with each other; the driven gear (14) is coaxially fixed on the driving rod (15); the front end of the driving rod (15) is provided with a front bevel gear (16), and the rear end of the driving rod is provided with a rear bevel gear (17); a first bevel gear (18) meshed with the front bevel gear (16) is arranged on the front shaft (6); a second bevel gear (19) meshed with the rear bevel gear (17) is arranged on the rear shaft (7); the front deformation mechanism comprises two front electric telescopic rods (20); the front electric telescopic rods (20), the first brackets (8) and the second brackets (9) are in one-to-one correspondence; one end of the front electric telescopic rod (20) is hinged with the corresponding first bracket (8), and the other end of the front electric telescopic rod is hinged with the corresponding second bracket (9); the rear deformation mechanism comprises two rear electric telescopic rods (21); the rear electric telescopic rods (21), the third brackets (10) and the fourth brackets (11) are in one-to-one correspondence; one end of the rear electric telescopic rod (21) is hinged with the corresponding third bracket (10), and the other end of the rear electric telescopic rod is hinged with the corresponding fourth bracket (11); the air injection direction of the first vortex spraying device (1) is always vertical to the air injection direction of the third vortex spraying device (3); when the front electric telescopic rod (20) is completely contracted, the air injection direction of the first vortex spraying device (1) is vertical to the air injection direction of the second vortex spraying device (2); when the front electric telescopic rod (20) is fully stretched, the air injection direction of the first vortex spraying device (1) is the same as the air injection direction of the second vortex spraying device (2); when the rear electric telescopic rod (21) is completely contracted, the air injection direction of the third turbojet device (3) is vertical to the air injection direction of the fourth turbojet device (4); and when the rear electric telescopic rod (21) is fully stretched, the air injection direction of the third vortex spraying device (3) is the same as the air injection direction of the fourth vortex spraying device (4).
2. A flying motorcycle as claimed in claim 1, wherein: the front electric telescopic rod (20), the rear electric telescopic rod (21) and the driving motor (12) are respectively and electrically connected with the controller.
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| CN103552435B (en) * | 2013-11-18 | 2015-09-02 | 张泽军 | Many sprays self-balancing carplane |
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| CN113427954A (en) * | 2021-08-14 | 2021-09-24 | 北京金璐东方联合物流有限公司 | Flying automobile |
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| WO2009146626A1 (en) * | 2008-06-03 | 2009-12-10 | Zhao Qingtao | Multi-energy direct axis mixed power engine |
| WO2012010021A1 (en) * | 2010-07-19 | 2012-01-26 | Yang zhaoxi | Air-ground double-purpose aircraft |
| RU2016147144A (en) * | 2016-11-30 | 2018-05-30 | Алексей Сергеевич Вишневский | FLIGHT (FLYING VEHICLE) (OPTIONS) |
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