CN215398048U

CN215398048U - Flying automobile

Info

Publication number: CN215398048U
Application number: CN202121906405.3U
Authority: CN
Inventors: 汪海波; 屈九良
Original assignee: Beijing Jinlu Oriental United Logistics Co ltd
Current assignee: Beijing Jinlu Oriental United Logistics Co ltd
Priority date: 2021-08-14
Filing date: 2021-08-14
Publication date: 2022-01-04
Anticipated expiration: 2031-08-14

Abstract

The utility model provides a flying automobile and relates to the technical field of flying automobiles. The device comprises an automobile body for providing power, a flight empennage arranged on the automobile body, foldable wings for providing cruising lift force of the automobile body, a plurality of turbofan engines capable of adjusting angles and a rotating mechanism; the foldable wings are arranged in the middle of the automobile main body, the turbofan engines are symmetrically arranged at two ends of the automobile main body, and the turbofan engines are connected with the automobile main body through the rotating mechanism. The aircraft can take off vertically and take off in a gliding manner, so that the aircraft can take off and land in various terrains in a matching manner, and the applicability is improved.

Description

Flying automobile

Technical Field

The utility model relates to the technical field of flying automobiles, in particular to a flying automobile.

Background

Since the birth of the first automobile, people have conducted a great deal of research on flying automobiles. In the face of increasingly congested road traffic, all countries are actively developing flying automobiles, which becomes a great trend of future traffic. Currently, flying automobiles developed in various countries are roughly divided into: gliders and rotor-type hovercars. A gliding flying automobile is additionally provided with a pair of wings, a flying tail wing and a propelling device on the basis of the existing automobile body, and a certain run-up distance and a certain takeoff speed are required during takeoff, so that the gliding flying automobile is not suitable for popularization in view of the existing road conditions and environments. The rotor type hovercar achieves the flying purpose by additionally arranging a helicopter rotor on the top of a vehicle body, but the cruising speed and the maneuverability of the rotor type hovercar are far inferior to those of a gliding type hovercar, so that the glider and the rotor type hovercar are combined.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide an aerocar which can take off vertically and take off in a gliding way, so that the aerocar can be adapted to take off and land on various terrains, and the applicability is improved.

The embodiment of the utility model is realized by the following steps:

the embodiment of the application provides a flying automobile, which is used for providing a power automobile main body, a flying tail wing arranged on the automobile main body, a foldable wing used for providing a cruising lift force of the automobile main body, a plurality of turbofan engines capable of adjusting angles and a rotating mechanism; the foldable wings are arranged in the middle of the automobile body, the turbofan engines are symmetrically arranged at two ends of the automobile body, and the turbofan engines are connected with the automobile body through a rotating mechanism.

In some embodiments of the present invention, the rotating mechanism includes a first driving motor, a first transmission member, a second transmission member, a third transmission member, a second driving motor disposed on the first transmission member, a third driving motor disposed on the second transmission member, and a fourth driving motor disposed on the third transmission member, the first driving motor is connected to the automobile body, and an output shaft of the first driving motor is connected to one end of the first transmission member; the other end of the first transmission piece is hinged to one end of the second transmission piece, the other end of the third transmission piece is rotatably connected with the turbofan engine, an output shaft of the second driving motor is connected with the second transmission piece, an output shaft of the third driving motor is connected with the third transmission piece, and an output shaft of the fourth driving motor is connected with the turbofan engine.

In some embodiments of the utility model, the foldable wing includes a plurality of wing links that are in turn hinged using motorized hinges.

In some embodiments of the present invention, the electric hinge includes a fifth driving motor, a planetary reducer, a steering mechanism, a first hinge member, and a second hinge member fitted to the first hinge member; the first articulated element and the second articulated element are respectively connected with two adjacent wing connecting pieces, a steering transmission shaft is arranged on the second articulated element and is connected with the output end of a steering mechanism, the input end of the steering mechanism is connected with the output end of a planetary reducer, and the input end of the planetary reducer is connected with the output shaft of a fifth driving motor.

In some embodiments of the present invention, the steering mechanism includes a support frame, a first gear and a second gear, the first gear and the second gear are disposed on the support frame, the first gear is connected to an output end of the planetary reducer, the first gear is engaged with the second gear, and the second gear is connected to the steering transmission shaft.

In some embodiments of the present invention, the vehicle main body is further provided with a multi-purpose tire mechanism for providing a lift force for the flying vehicle, the multi-purpose tire mechanism comprises a telescopic transmission shaft, a tire main body and a hydraulic push rod, a transmission in the vehicle main body is connected with one end of the telescopic transmission shaft, the other end of the telescopic transmission shaft is hinged with the tire main body, the fixed end of the hydraulic push rod is connected with the telescopic transmission shaft, and the output end of the hydraulic push rod is hinged with the tire main body.

In some embodiments of the utility model, the bottom of the automobile body is further provided with an emergency airbag, a chemical reaction box and an igniter arranged in the chemical reaction box, and the chemical reaction box is communicated with the emergency airbag.

In some embodiments of the utility model, the tire body includes a rim, rotor-type spokes, a hub, and a cover rim disposed on the hub connected to the hub through the rotor-type spokes.

In some embodiments of the utility model, the paddle wheel further comprises a paddle mechanism arranged on the hub, wherein the paddle mechanism comprises an electric telescopic rod, a hydraulic box and a hydraulic telescopic paddle arranged on the hydraulic box; the hydraulic box comprises a box body, a pushing piston and a linear motor arranged in the box body; the fixed end of the electric telescopic rod is connected with the hub, the output end of the electric telescopic rod is connected with the box body, the output shaft of the linear motor is connected with the piston, and the piston is connected with the box body in a sliding manner in the box body; the hydraulic telescopic paddle is communicated with the side wall of the box body.

In some embodiments of the utility model, a thin film solar cell is also provided on the automobile body.

Compared with the prior art, the embodiment of the utility model has at least the following advantages or beneficial effects:

a flying automobile comprises an automobile body for providing power, a flying tail wing arranged on the automobile body, a foldable wing for providing cruising lift force of the automobile body, a plurality of turbofan engines capable of adjusting angles and a rotating mechanism; the foldable wings are arranged in the middle of the automobile body, the turbofan engines are symmetrically arranged at two ends of the automobile body, and the turbofan engines are connected with the automobile body through a rotating mechanism.

For the vertical take-off and gliding take-off modes of the aerocar, the vertical take-off is adopted in the embodiment. The purpose of the method is that if a gliding takeoff mode is adopted on a highway, a straight and long runway needs to be reserved, and no other object can interfere with the start of the aerocar in the midway. The vehicle condition and the road condition on the existing highway can not realize the gliding takeoff, so the vertical takeoff is selected, and the specific implementation mode is that a plurality of turbofan engines capable of adjusting angles are utilized to adjust in the vertical and horizontal directions through a rotating mechanism, so the vertical takeoff purpose is realized. When the flying automobile rises to the preset height of 100 meters, the turbofan engine is adjusted to the horizontal direction from the vertical direction to provide power for cruising of the flying automobile, and the power is matched with the foldable wings arranged in the middle of the automobile main body to finish cruising flight. The turbofan engine adopts a dual-system engine, and aims to use a rotor engine of the dual-system engine even if the turbofan engine is damaged, so that the safety is improved.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings needed to be used in the embodiments will be briefly described below, it should be understood that the following drawings only illustrate some embodiments of the present invention and therefore should not be considered as limiting the scope, and for those skilled in the art, other related drawings can be obtained according to the drawings without inventive efforts.

FIG. 1 is a schematic structural diagram of an aircraft of the present invention;

FIG. 2 is a schematic view of the structure of the utility model for vertical take-off and landing of an aerocar

FIG. 3 is a partial state view of the turbofan engine of the present invention when stowed;

FIG. 4 is a schematic structural view of a rotating mechanism according to the present invention;

FIG. 5 is a schematic view of a foldable wing according to the present invention;

FIG. 6 is a schematic view of the electric hinge of the present invention;

FIG. 7 is a state view of the multi-purpose tire mechanism of the present invention providing lift;

FIG. 8 is a diagram of the multi-purpose tire mechanism of the present invention in operation;

FIG. 9 is a schematic view of the multi-purpose tire mechanism of the present invention in a configuration for providing lift;

FIG. 10 is a schematic view of the assembly of the automobile body, the rowing mechanism and the emergency airbag in the present invention;

FIG. 11 is a schematic structural view of a rowing mechanism in the present invention;

FIG. 12 is a diagram of a flying vehicle in a stationary or driving position;

fig. 13 is a state diagram of a flying vehicle running on the water surface according to the utility model.

Icon: 1. an automobile body; 11. an accommodation hole; 12. an automobile tail fin; 13. a receiving cavity; 2. a turbofan engine; 3. a flight tail; 4. a rotating mechanism; 41. a first drive motor; 42. a first transmission member; 43. a second drive motor; 44. a second transmission member; 45. a third drive motor; 46. a third transmission member; 47. a fourth drive motor; 5. a foldable wing; 51. a wing connection; 52. an electric hinge; 521. a fifth drive motor; 522. a planetary reducer; 523. a first gear; 524. a second gear; 525. a first hinge member; 526. a second hinge member; 6. a multi-purpose tire mechanism; 61. a tire main body; 62. a telescopic transmission shaft; 63. a hydraulic push rod; 7. an emergency air bag; 8. a paddling mechanism; 81. an electric telescopic rod; 82. hydraulic telescopic blades; 83. a hydraulic box; 9. a rotor type spoke.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. The components of embodiments of the present invention generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations.

Thus, the following detailed description of the embodiments of the present invention, presented in the figures, is not intended to limit the scope of the utility model, as claimed, but is merely representative of selected embodiments of the utility model. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, it need not be further defined and explained in subsequent figures.

In the description of the embodiments of the present invention, it should be noted that, if the terms "upper", "lower", "vertical", "horizontal", "inner", "outer", etc. indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings or orientations or positional relationships that are conventionally placed when the products of the present invention are used, the orientations or positional relationships are only for convenience of describing the present invention and simplifying the description, but the terms do not indicate or imply that the devices or elements to be referred to must have specific orientations, be constructed and operated in specific orientations, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used solely to distinguish one from another and are not to be construed as indicating or implying relative importance.

Furthermore, the terms "horizontal", "vertical" and the like do not require that the components be absolutely horizontal or overhanging, but may be slightly inclined. For example, "horizontal" merely means that the direction is more horizontal than "vertical" and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.

In the description of the embodiments of the present invention, "a plurality" represents at least 2.

In the description of the embodiments of the present invention, it should be further noted that unless otherwise explicitly stated or limited, the terms "disposed," "mounted," and "connected" should be interpreted broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood by those skilled in the art according to specific situations.

Example 1

Referring to fig. 1 and fig. 2, a flying automobile is provided for the embodiment, which includes an automobile body 1 for providing power, a flying tail 3 disposed on the automobile body 1, a foldable wing 5 for providing a cruising lift force of the automobile body 1, a plurality of turbofan engines 2 capable of adjusting angles, and a rotating mechanism 4; the foldable wings 5 are arranged in the middle of the automobile body 1, the turbofan engines 2 are symmetrically arranged at two ends of the automobile body 1, and the turbofan engines 2 are connected with the automobile body 1 through the rotating mechanism 4.

In some embodiments of the present invention, for the vertical takeoff and the gliding takeoff of the hovercar, the vertical takeoff is adopted in the present embodiment. The purpose of the method is that if a gliding takeoff mode is adopted on a highway, a straight and long runway needs to be reserved, and no other object can interfere with the start of the aerocar in the midway. The vehicle condition and the road condition on the existing highway can not realize the gliding takeoff, so the vertical takeoff is selected, and the specific implementation mode is that a plurality of turbofan engines 2 capable of adjusting angles are utilized to adjust in the vertical and horizontal directions through a rotating mechanism 4, so the vertical takeoff purpose is realized. When the flying automobile rises to the preset height of 100 meters, the turbofan engine 2 is adjusted to the horizontal direction from the vertical direction to provide power for cruising of the flying automobile, and the power is matched with the foldable wings 5 arranged in the middle of the automobile body 1 to finish cruising flight. Wherein turbofan engine 2 adopts another patent of utility model person, the dual system engine mentioned in application No. 202110438580.2, its dual system engine of its purpose even under turbofan engine 2 the condition that appears damaging, can also use dual system engine's rotor engine, has improved the security from this.

Example 2

Referring to fig. 3 and 4, in the present embodiment, based on the technical solution of embodiment 1, it is proposed that the rotating mechanism 4 includes a first driving motor 41, a first transmission member 42, a second transmission member 44, a third transmission member 46, a second driving motor 43 disposed on the first transmission member 42, a third driving motor 45 disposed on the second transmission member, and a fourth driving motor 47 disposed on the third transmission member 46, the first driving motor 41 is connected with the automobile body 1, and an output shaft of the first driving motor 41 is connected with one end of the first transmission member 42; the other end of the first transmission member 42 is hinged to one end of the second transmission member 44, the other end of the third transmission member 46 is rotatably connected to the turbofan engine 2, the output shaft of the second driving motor 43 is connected to the second transmission member 44, the output shaft of the third driving motor 45 is connected to the third transmission member 46, and the output shaft of the fourth driving motor 47 is connected to the turbofan engine 2.

In some embodiments of the present invention, since the turbofan engine 2, if placed outside the car body 1 during the land driving of the hovercar, increases the occupied area and air resistance of the hovercar, the turbofan engine 2 needs to be housed. Therefore, in the present embodiment, the turbofan engine 2 is accommodated into the front compartment and the rear compartment of the vehicle by using the rotating mechanism 4, wherein the internal engine of the vehicle in the present embodiment is disposed at the rear, so that a space of the front compartment is reserved for placing the turbofan engine 2 disposed at the front end, and the turbofan engine 2 disposed at the rear end is directly placed into the rear trunk. Taking the housing turbofan engine 2 as an example, the first driving motor 41 is used to drive the first transmission member 42 to rotate, so as to control the position of the first transmission member 42 in the axial direction, and the second transmission member 44 and the subsequent components are rotated to the vertical direction under the control of the second driving motor 43. Then the third driving motor 45 controls the third transmission member 46 to put the turbofan engine 2 into the front compartment, as shown in fig. 3. Therefore, the flying automobile can not interfere with other vehicles when running on the road surface, and the safety is improved.

Example 3

Referring to fig. 5, the present embodiment proposes that based on the technical solution of embodiment 1, the foldable wing 5 includes a plurality of wing connectors 51 hinged in sequence by using electric hinges 52.

In some embodiments of the present invention, except that the turbofan engine 2 may cause interference to other vehicles on the road surface when driving on the road surface, the wings of the airplane may also interfere with normal driving of other vehicles due to its long size, in order to avoid this, in this embodiment, the foldable wings 5 are adopted, and the foldable wings 5 are divided into a plurality of wing connecting pieces 51 and connected by the electric hinges 52, so as to achieve the purpose of folding and straightening the wings, thereby saving the occupied area of the flying automobile when driving on the ground. Meanwhile, in order to avoid damage to the wing link 51 caused by road running as much as possible, the storage cavity 13 is provided in the door of the automobile body 1, and the folded wing link 51 is directly put into the door, as shown in fig. 12.

In some embodiments of the present invention, the flight tail 3 may also be of a telescopic structure, and a receiving hole 11 is provided in the car body 1 for receiving the flight tail 3 into the car interior, and then raising the car tail 12 during traveling on a road surface to achieve a shape similar to that of a conventional car, as shown in fig. 12.

Example 4

Referring to fig. 6, the present embodiment proposes based on the technical solution of embodiment 3 that the electric hinge 52 includes a fifth driving motor 521, a planetary reducer 522, a steering mechanism, a first hinge 525 and a second hinge 526 adapted to the first hinge 525; the first hinge element 525 and the second hinge element 526 are respectively connected with two adjacent wing connecting pieces 51, the second hinge element 526 is provided with a steering transmission shaft, the steering transmission shaft is connected with the output end of a steering mechanism, the input end of the steering mechanism is connected with the output end of a planetary reducer 522, and the input end of the planetary reducer 522 is connected with the output shaft of a fifth driving motor 521.

In some embodiments of the utility model, the motorized hinge 52 is provided primarily to allow the wing to fold, and the wing connecting piece 51 is automatically folded by the motor, and because the volume of the wing is small, the rotation of the wing connecting piece 51 during folding needs larger torsion, but the volume of the wing is limited, therefore, the embodiment adopts the way that the planetary reducer 522 is additionally arranged on the fifth driving motor 521, the torque force is increased by utilizing the planetary reducer 522, thereby making the rotation of the wing connection 51 faster and more stable, and at the same time avoiding the exposure of the fifth driving motor 521 and the planetary reducer 522 to the air during folding, in rainy season, water enters to cause damage, and a steering mechanism is arranged, so that the fifth driving motor 521 and the planetary reducer 522 are placed in the wing connector 51, and the service life of the fifth driving motor 521 and the planetary reducer 522 is prolonged.

Example 5

Referring to fig. 6, the present embodiment proposes based on the technical solution of embodiment 4 that the steering mechanism includes a support frame, and a first gear 523 and a second gear 524 disposed on the support frame, wherein the first gear 523 is connected to an output end of the planetary reducer 522, the first gear 523 is engaged with the second gear 524, and the second gear 524 is connected to the steering transmission shaft.

In some embodiments of the present invention, since the rotating mechanism 4 needs to be partially exposed, a simple and stable mechanical structure is adopted, and the specific implementation manner is that the first gear 523 and the second gear 524 are engaged to complete the steering after the power output by the fifth driving motor 521 passes through the planetary reducer 522.

Example 6

Referring to fig. 7, 8 and 9, the present embodiment provides based on the technical solution of embodiment 1 that a multi-purpose tire mechanism 6 for providing a lift force for a flying vehicle is further disposed on a vehicle body 1, the multi-purpose tire mechanism 6 includes a telescopic transmission shaft 62, a tire body 61 and a hydraulic push rod 63, a transmission in the vehicle body 1 is connected to one end of the telescopic transmission shaft 62, the other end of the telescopic transmission shaft 62 is hinged to the tire body 61, a fixed end of the hydraulic push rod 63 is connected to the telescopic transmission shaft 62, and an output end of the hydraulic push rod 63 is hinged to the tire body 61.

In some embodiments of the utility model, when the flying automobile breaks down in the air, so that the turbofan engine 2 cannot work normally and the like, and needs to be urgently landed, the tire is used as the only rotatable component, so that a certain lift force can be provided when necessary, and the situation that the flying automobile is too fast in falling speed and causes damage to people is avoided. Therefore, in the embodiment, the tire extends out of the automobile body 1 by using the telescopic transmission shaft 62, and the rotation of the tire body 61 is pushed by using the hydraulic push rod, so that the tire body 61 is turned upwards, as shown in fig. 9, thereby providing an upward lifting force for the hovercar; when the aircraft is forced to land to a certain height, the aircraft is converted into the original position and is forced to land by matching with wings, as shown in figure 8, the flying automobile slows down the acceleration in the falling process due to the lifting force provided by the multipurpose tire mechanism 6, so that the sliding distance required by forced landing is reduced, and the survival rate of passengers is improved. And the multipurpose tire mechanism 6 in the design scheme can also move transversely or longitudinally, so that the parking at the side position is convenient.

In some embodiments of the utility model, an ejection seat and a parachute matched with the ejection seat can be further arranged, so that escape by the ejection seat is avoided under the condition that power is completely lost when the aerocar is cruising, and the survival probability of air accidents is improved.

Example 7

Referring to fig. 3, the present embodiment proposes based on the technical solution of embodiment 6 that the tire main body 61 includes a rim, a rotor type wheel disc 9, a hub, and an outer tire rim disposed on the hub and connected with the hub through the rotor type wheel disc 9.

In some embodiments of the present invention, the principle of providing the car body 1 with lift force for the main body of the tire is to set the spokes as a rotor structure, and rotate the wheel hub to provide a certain lift force for the car body 1, thereby reducing the falling speed of the hovercar in an unexpected situation.

Example 8

Referring to fig. 10, the present embodiment proposes that based on the technical solution of embodiment 7, an emergency airbag 7, a chemical reaction box and an igniter disposed in the chemical reaction box are further disposed at the bottom of the automobile body 1, and the chemical reaction box is communicated with the emergency airbag 7.

In some embodiments of the present invention, the hovercar may need to be forced to land once it travels over a lake or other relatively wide area of water while cruising. Therefore, the igniter is adopted to ignite the sodium nitride or ammonium nitrate in the chemical reaction box to generate chemical reaction, and a large amount of nitrogen is generated by explosion to quickly fill the emergency air bag 7. Thus, an air cushion is formed at the bottom of the automobile, and when the flying automobile contacts with the water surface, buoyancy is provided for the flying automobile.

Example 9

Referring to fig. 11, the embodiment is provided based on the technical solution of embodiment 8, and further includes a paddling mechanism 8 disposed on the hub, where the paddling mechanism 8 includes an electric telescopic rod 81, a hydraulic box 83, and hydraulic telescopic paddles 82 disposed on the hydraulic box 83; the hydraulic box 83 comprises a box body, a pushing piston and a linear motor arranged in the box body; the fixed end of the electric telescopic rod 81 is connected with the hub, the output end of the electric telescopic rod 81 is connected with the box body, the output shaft of the linear motor is connected with the piston, and the piston is connected with the box body in a sliding manner in the box body; the hydraulic telescopic blades 82 are communicated with the side wall of the box body.

In some embodiments of the utility model, after the flying automobile is forced to land on the water surface or the emergency airbag 7 is opened in the water, in order to achieve emergency safety and keep free navigation in the water, the embodiment adopts the water-rowing mechanism 8 arranged in the hub, so that the water-rowing mechanism 8 provides power for the flying automobile in the water. The specific implementation mode is that after the emergency airbag 7 is unfolded, the electric telescopic rod 81 on the hub extends out the hydraulic box 83, then the hydraulic pressure and the linear motor in the hydraulic box push the piston to raise the pressure in the hydraulic box 83, and as the telescopic blades adopt a form similar to a hydraulic cylinder, the pressure in the hydraulic box 83 extends out the telescopic blades completely, and the telescopic blades rotate under the driving of the hub, so that power is provided for the flying automobile.

Example 10

In this embodiment, based on the technical solution of embodiment 1, it is proposed that the automobile body 1 is further provided with a thin film solar cell.

In some embodiments of the present invention, since the energy is provided to the hovercar by fossil energy alone during the cruising process of the hovercar, and the abnormal condition such as oil leakage can cause the reaction time during the flying process to be short, the present invention adopts the oil-electric hybrid system, and besides the gasoline or diesel oil driving in the prior art, the thin film solar cell is further disposed on the automobile body 1, so as to supply power to the storage battery in the automobile body 1.

In some embodiments of the present invention, a dual system engine (referred to herein as turbofan engine 2) as described in application No. 202110438580.2 is used during use of such a hovercar, whether on the air, land or water, in order to provide sufficient power reserve, climb speed, cruise speed and weight loading capacity for the hovercar, and a user may use different numbers of engines depending on the power level and environmental needs. And because the dual-system engine includes propeller engine and turbofan engine 2, can also adopt different forms of engine types according to the power size and the needs of the environment, wherein can adopt propeller engine, can also adopt turbofan engine 2 alone, can also use propeller engine and turbofan engine 2 to mix, thus reach and can travel in the air on sea and land, its road surface travel state is shown as figure 12, its air travel is shown as figure 1, its surface of water travel is shown as figure 13. In fig. 13, the emergency air cushion and the paddling mechanism 8 are removed, and the vehicle can also run on the road.

In summary, the embodiment of the present invention provides a flying automobile, which includes an automobile body 1 for providing power, a flying tail 3 disposed on the automobile body 1, a foldable wing 5 for providing a cruising lift force of the automobile body 1, a plurality of turbofan engines 2 capable of adjusting angles, and a rotating mechanism 4; the foldable wings 5 are arranged in the middle of the automobile body 1, the turbofan engines 2 are symmetrically arranged at two ends of the automobile body 1, and the turbofan engines 2 are connected with the automobile body 1 through the rotating mechanism 4.

For the vertical take-off and gliding take-off modes of the aerocar, the vertical take-off is adopted in the embodiment. The purpose of the method is that if a gliding takeoff mode is adopted on a highway, a straight and long runway needs to be reserved, and no other object can interfere with the start of the aerocar in the midway. The vehicle condition and the road condition on the existing highway can not realize the gliding takeoff, so the vertical takeoff is selected, and the specific implementation mode is that a plurality of turbofan engines 2 capable of adjusting angles are utilized to adjust in the vertical and horizontal directions through a rotating mechanism 4, so the vertical takeoff purpose is realized. When the flying automobile rises to the preset height of 100 meters, the turbofan engine 2 is adjusted to the horizontal direction from the vertical direction to provide power for cruising of the flying automobile, and the power is matched with the foldable wings 5 arranged in the middle of the automobile body 1 to finish cruising flight. Wherein turbofan engine 2 adopts another patent of utility model person, the dual system engine mentioned in application No. 202110438580.2, its dual system engine of its purpose even under turbofan engine 2 the condition that appears damaging, can also use dual system engine's rotor engine, has improved the security from this.

The above is only a preferred embodiment of the present invention, and is not intended to limit the present invention, and various modifications and changes will occur to those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A flying automobile is characterized by comprising an automobile body for providing power, a flying tail wing arranged on the automobile body, a foldable wing for providing the cruising lift force of the flying automobile, a plurality of turbofan engines capable of adjusting angles and a rotating mechanism; the foldable wings are arranged in the middle of the automobile main body, the turbofan engines are symmetrically arranged at two ends of the automobile main body, and the turbofan engines are connected with the automobile main body through the rotating mechanism.

2. The hovercar as claimed in claim 1, wherein the rotating mechanism comprises a first driving motor, a first transmission member, a second transmission member, a third transmission member, a second driving motor disposed on the first transmission member, a third driving motor disposed on the second transmission member and a fourth driving motor disposed on the third transmission member, the first driving motor is connected with the automobile body, and an output shaft of the first driving motor is connected with one end of the first transmission member; the other end of the first transmission piece is hinged to one end of the second transmission piece, the other end of the third transmission piece is rotatably connected with the turbofan engine, an output shaft of the second driving motor is connected with the second transmission piece, an output shaft of the third driving motor is connected with the third transmission piece, and an output shaft of the fourth driving motor is connected with the turbofan engine.

3. A flying automobile according to claim 1, wherein the foldable wing comprises a plurality of wing connectors hinged in turn by electrically powered hinges.

4. A flying automobile according to claim 3, wherein the electric hinge comprises a fifth driving motor, a planetary reducer, a steering mechanism, a first hinge member and a second hinge member fitted to the first hinge member; the first articulated element and the second articulated element are respectively connected with two adjacent wing connecting pieces, a steering transmission shaft is arranged on the second articulated element and connected with the output end of the steering mechanism, the input end of the steering mechanism is connected with the output end of the planetary reducer, and the input end of the planetary reducer is connected with the output shaft of the fifth driving motor.

5. The flying automobile of claim 4, wherein the steering mechanism comprises a support frame, and a first gear and a second gear which are arranged on the support frame, the first gear is connected with the output end of the planetary reducer, the first gear is meshed with the second gear, and the second gear is connected with the steering transmission shaft.

6. The flying automobile of claim 1, wherein the automobile body is further provided with a multipurpose tire mechanism for providing a lifting force for the flying automobile, the multipurpose tire mechanism comprises a telescopic transmission shaft, a tire body and a hydraulic push rod, a transmission in the automobile body is connected with one end of the telescopic transmission shaft, the other end of the telescopic transmission shaft is hinged with the tire body, a fixed end of the hydraulic push rod is connected with the telescopic transmission shaft, and an output end of the hydraulic push rod is hinged with the tire body.

7. A flying automobile according to claim 6, wherein the tire body comprises a rim, rotor disc spokes, a hub and a cover tyre arranged on the hub, the rim being connected with the hub through the rotor disc spokes.

8. The flying automobile of claim 7, wherein the bottom of the automobile body is further provided with an emergency airbag, a chemical reaction box and an igniter arranged in the chemical reaction box, and the chemical reaction box is communicated with the emergency airbag.

9. The hovercar as claimed in claim 8, further comprising a paddling mechanism arranged on the hub, wherein the paddling mechanism comprises an electric telescopic rod, a hydraulic box and hydraulic telescopic blades arranged on the hydraulic box; the hydraulic box comprises a box body, a pushing piston and a linear motor arranged in the box body; the fixed end of the electric telescopic rod is connected with the hub, the output end of the electric telescopic rod is connected with the box body, the output shaft of the linear motor is connected with the piston, and the piston is in sliding connection with the box body in the box body; the hydraulic telescopic paddle is communicated with the side wall of the box body.

10. The flying automobile of claim 1, wherein the automobile body is further provided with a thin film solar cell.