CN110789281A

CN110789281A - Flying automobile

Info

Publication number: CN110789281A
Application number: CN201911232202.8A
Authority: CN
Inventors: 杨忠; 田小敏; 张曌; 王逸之
Original assignee: Jinling Institute of Technology
Current assignee: Jinling Institute of Technology
Priority date: 2019-12-05
Filing date: 2019-12-05
Publication date: 2020-02-14

Abstract

The invention provides a flying automobile, which comprises an automobile body and wheels, wherein a first wing cabin and a second wing cabin are arranged on the automobile body, folding wings are respectively arranged in the first wing cabin and the second wing cabin, the folding wings comprise a first folding shaft, a second folding shaft and a third folding shaft, the first folding shaft, the second folding shaft and the third folding shaft are sleeved, a motor box is connected to the third folding shaft, the motor box is rotatably arranged relative to the third folding shaft, a propeller is arranged above the motor box, a propeller driving motor is arranged in the motor box, the propeller is arranged in a folding way relative to a propeller groove, so that the flying automobile can be folded into the first wing cabin and the second wing cabin quickly when running on the ground, the first folding shaft, the second folding shaft, the third folding shaft, the propeller and the motor box are folded tightly, and the parts of the folding wings cannot extend out when running on the ground, the safety and the service life of the folding wing are ensured.

Description

Flying automobile

Technical Field

The invention relates to the technical field of aircraft design, in particular to a flying automobile.

Background

In recent years, with the rapid development of modern social economy, a great number of private cars of large and medium-sized cities are increased, the traffic pressure is increased day by day, traffic jam frequently occurs, a series of energy problems, environmental problems and the like are caused, and how to effectively solve the traffic problems existing in modern cities becomes a big problem.

For this reason, those skilled in the art have studied a variety of hovercars, such as four hovercars with ducted rotors, a hovercar with foldable wings, a hovercar with two ducted fans placed inside the body, and the like. However, although four hovercars with ducted rotors can provide lift force and forward power by simultaneously controlling the rotating speed and the direction of the four ducts, the hovercars are excessively heavy in structure and complex to operate; the wings of the aerocar with the foldable wings are folded and furled on two sides when the aerocar runs on the ground and unfolded when the aerocar needs to fly, but the folding and furling of the wings after landing are troublesome and can not be completely furled, so that the wings are easy to damage by bruising.

Disclosure of Invention

The purpose of the invention is as follows: the invention aims to provide a flying automobile aiming at the defects in the prior art, and solves the technical problems that in the prior art, the folding and furling of wings after the wings fall are troublesome, the wings cannot be furled completely, and the wings are easy to damage due to collision.

The technical scheme is as follows: in order to achieve the purpose, the invention provides a flying automobile, which comprises an automobile body and wheels, and is characterized in that: the aircraft body is provided with a first wing cabin and a second wing cabin, the first wing cabin is provided with two wing cabins which are respectively positioned at the two sides of the aircraft body, the second wing cabin is positioned above the fuselage, the first wing cabin and the second wing cabin are respectively provided with a folding wing, the folding wing comprises a first folding shaft, a second folding shaft and a third folding shaft, the first folding shaft, the second folding shaft and the third folding shaft are sleeved and arranged, the first folding axis having a dimension greater than a dimension of the second folding axis, the second folding axis having a dimension greater than a dimension of the third folding axis, the third folding shaft is connected with a motor box which is arranged in a rotating way relative to the third folding shaft, the motor box is characterized in that a propeller is installed above the motor box, a propeller driving motor is arranged in the motor box, and the propeller is arranged in a folding mode relative to the propeller groove.

Preferably, the first folding shaft is provided with a folding wing mounting hole, and the folding wings are respectively mounted in the first wing cabin and the second wing cabin through the folding wing mounting hole.

Preferably, the end of the first folding shaft is arc-shaped, a plurality of protrusions are arranged in the arc-shaped circumferential direction, arc-shaped grooves are respectively arranged in the first wing cabin and the second wing cabin, a plurality of dents are arranged in the circumferential direction of the grooves, the end of the first folding shaft is mounted in the arc-shaped grooves, and the protrusions are embedded in the dents.

Preferably, a motor box groove is formed in the third folding shaft, and the motor box is rotatably placed in the motor box groove.

Preferably, the side surfaces of the motor box are respectively provided with a propeller groove, and the propellers are foldable and placed in the propeller grooves.

Preferably, the wheel is provided with a mudguard, the mudguard comprises a front mudguard and a rear mudguard, the front mudguard is arranged behind the wheel in the rotation direction, and the rear mudguard is arranged in front of the wheel in the rotation direction.

Preferably, the body is further provided with a glass window, a front lamp and a steering lamp, the glass window is semicircular and is located above the body, and the front lamp and the steering lamp are provided with two pairs and are located on two sides of the glass window respectively.

Preferably, a trunk and a tail lamp are arranged behind the fuselage, and a trunk key hole for opening the trunk is formed in the trunk.

Compared with the prior art, the invention has the following beneficial effects:

the invention arranges the folding wings in the first wing cabin and the second wing cabin, so that the folding wings can be quickly folded into the first wing cabin and the second wing cabin when the aerocar runs on the ground, and the first folding shaft, the second folding shaft, the third folding shaft, the propeller and the motor box are tightly folded to ensure that no folding wing extends out of the surface of the aerocar when the aerocar runs on the ground, thereby ensuring the safety and the service life of the folding wings, when the aerocar needs to fly, the folding wings are quickly unfolded, the first folding shaft is unfolded towards the outer surfaces of the first wing cabin and the second wing cabin, the second folding shaft extends out from the first folding shaft, the third folding shaft extends out from the second folding shaft, the motor box is unfolded from the motor box groove on the third folding shaft, the propeller is unfolded from the propeller groove, and the unfolding is quick and orderly, the preparation work of the aerocar in the preparation takeoff phase is less, and the takeoff is faster.

Drawings

FIG. 1 is a schematic perspective view of a flying vehicle according to the present embodiment;

FIG. 2 is a structural diagram illustrating a ground driving state of the hovercar in the embodiment;

FIG. 3 is a structural diagram illustrating a flight state in the hole of the flying automobile in this embodiment;

fig. 4 is a schematic perspective view of the propeller of this embodiment.

List of reference numerals: 1. a headlamp; 2. a turn signal light; 3. a first wing tank; 4. a wheel; 5. a second wing tank; 6. a body; 7. a glass window; 8. folding the wing; 9. a tail light; 10. a trunk; 11. a key hole; 12. a rear fender; 14. A front fender; 15. folding wing mounting holes; 16. a first folding shaft; 17. a second folding shaft; 18. a third folding shaft; 19. a propeller; 20. a motor case; 21. a propeller groove; 22. a protrusion; 181. and a motor box groove.

Detailed Description

The present invention will be further illustrated with reference to the accompanying drawings and specific embodiments, which are to be understood as merely illustrative of the invention and not as limiting the scope of the invention. It should be noted that the terms "front," "back," "left," "right," "upper" and "lower" used in the following description refer to directions in the drawings, and the terms "inner" and "outer" refer to directions toward and away from, respectively, the geometric center of a particular component.

As shown in fig. 1-4, the hovercar comprises a fuselage 6 and wheels 4, wherein a first wing cabin 3 and a second wing cabin 5 are arranged on the fuselage 6, the first wing cabin 3 is provided with two sides respectively located on the fuselage 6, the second wing cabin 5 is located above the fuselage 6, folding wings 8 are respectively arranged in the first wing cabin 3 and the second wing cabin 5, each folding wing 8 comprises a first folding shaft 16, a second folding shaft 17 and a third folding shaft 18, the first folding shaft 16, the second folding shaft 17 and the third folding shaft 18 are sleeved and arranged, the size of the first folding shaft 16 is larger than that of the second folding shaft 17, the size of the second folding shaft 17 is larger than that of the third folding shaft 18, a motor box 20 is connected to the third folding shaft 18, the motor box 20 is rotatably arranged relative to the third folding shaft 18, a propeller 19 is installed above the motor box 20, a propeller driving motor is arranged in the motor box 20, and the propeller 19 is arranged in a folding mode relative to the propeller groove 21.

In this embodiment: still be provided with glass window 7, headlight 1 and indicator 2 on the fuselage 6, glass window 7 is the semicircle form and is located fuselage 6 top, headlight 1 and indicator 2 are provided with two pairs and are located the both sides of glass window 7 respectively.

In this embodiment: 6 backs of fuselage are provided with trunk 10 and tail lamp 9, be provided with trunk 10 key hole 11 that is used for opening trunk 10 on the trunk 10.

In the above structure: the invention provides a flying automobile which comprises an automobile body 6 and wheels 4, wherein a first wing cabin 3 and a second wing cabin 5 are arranged on the automobile body 6, the first wing cabin 3 is provided with two folding shafts 16, a second folding shaft 17 and a third folding shaft 18 which are respectively positioned at two sides of the automobile body 6, the second wing cabin 5 is provided with one folding shaft positioned between a glass window 7 and a trunk 10, folding wings 8 are respectively arranged in the first wing cabin 3 and the second wing cabin 5, the folding wings 8 comprise a first folding shaft 16, a second folding shaft 17 and a third folding shaft 18 which are sleeved, a motor box 20 is connected onto the third folding shaft 18, the motor box 20 is rotatably arranged relative to the third folding shaft 18, a propeller 19 is arranged above the motor box 20, a propeller driving motor is arranged in the motor box 20, the propeller 19 is arranged in a folding manner relative to a propeller groove 21, and folding wings 8 are arranged in the first wing cabin 3 and the second wing cabin 5, so that the folding wings 8 can be quickly folded to the first wing cabin 3 and the second wing cabin 5 when the flying automobile runs In the wing cabin 5, the first folding shaft 16, the second folding shaft 17, the third folding shaft 18, the propeller 19 and the motor box 20 are tightly folded to ensure that no part of the folding wing 8 extends outside on the surface of the hovercar when the hovercar runs on the ground, so that the safety and the service life of the folding wing 8 are ensured when the hovercar runs, when the hovercar needs to fly, the folding wing 8 is rapidly unfolded, the first folding shaft 16 is unfolded towards the outsides of the first wing cabin 3 and the second wing cabin 5, the second folding shaft 17 extends from the first folding shaft 16, the third folding shaft 18 extends from the second folding shaft 17, the motor box 20 is unfolded from a motor box groove 181 on the third folding shaft 18, then the propeller 19 is unfolded from the propeller groove 21, the unfolding is rapid and orderly, the preparation work of the hovercar in the takeoff preparation stage is ensured to be less, and the hovercar can more rapidly take off

In this embodiment: the first folding shaft 16 is provided with mounting holes for folding wings 8, and the folding wings 8 are respectively mounted in the first wing cabin 3 and the second wing cabin 5 through the mounting holes for folding wings 8.

In the above structure: the first folding shaft 16 is provided with a mounting hole for the folding wing 8, and the folding wing 8 is respectively mounted in the first wing cabin 3 and the second wing cabin 5 through the mounting hole for the folding wing 8, so that the folding wing 8 is mounted and fixed.

In this embodiment: the tip of first folding axle 16 is circular-arc, is provided with a plurality of archs 22 along circular-arc circumferencial direction, be provided with circular-arc recess in first wing cabin 3 and the second wing cabin 5 respectively, be provided with a plurality of indents along the circumferencial direction of recess, the tip of first folding axle 16 is installed in circular-arc recess, arch 22 imbeds in the indent.

In the above structure: the end part of the first folding shaft 16 is arc-shaped, a plurality of protrusions 22 are arranged in the circumferential direction of the arc-shaped end part, grooves matched with the arc-shaped end parts are respectively arranged in the first wing cabin 3 and the second wing cabin 5 for installing the folding wings 8, a plurality of dents are arranged on the circumference of each groove, when the arc-shaped end part of the first folding shaft 16 is installed in each groove, the protrusions 22 are embedded into the dents, and when the flying automobile is ready to take off, the arc-shaped end part of the first folding shaft 16 rotates in each groove, so that the first folding shaft 16 is unfolded.

In this embodiment: the third folding shaft 18 is provided with a motor box groove 181, and the motor box 20 is rotatably placed in the motor box groove 181.

In the above structure: be provided with the motor case groove 181 that is used for placing motor case 20 on third folding shaft 18, motor case groove 181 is rotatable setting for third folding shaft 18, and when the hovercar was gone on ground, motor case 20 rotated, made it receive and release in motor case groove 181, and when the hovercar was prepared to take off, motor case 20 rotated, made it transfer to suitable position in motor case groove 181 fast, guaranteed that the hovercar takes off rapidly in order.

In this embodiment: the side surfaces of the motor box 20 are respectively provided with a propeller groove 21, and the propellers 19 are foldable and placed in the propeller grooves 21.

In the above structure: the side face of the motor box 20 is provided with a plurality of propeller grooves 21 for placing the propellers 19, the propellers 19 are arranged above the motor box 20 and can be arranged in a folding mode relative to the motor box 20, when the flying automobile runs on the ground, the propellers 19 stop rotating and turn over downwards to enable the propellers to be stored in the propeller grooves 21, when the flying automobile is ready to take off, the propellers 19 turn over upwards from the propeller grooves 21 to a designated position to start rotating, and the flying automobile can take off quickly and orderly.

In this embodiment: install the fender on wheel 4, the fender is including preceding fender 14 and rear fender 12, preceding fender 14 is installed at wheel 4 rotation direction's rear, rear fender 12 is installed in wheel 4 rotation direction's place ahead.

In the above structure: the wheels 4 are provided with mud guards which comprise a front mud guard 14 and a rear mud guard 12, and the front mud guard 14 and the rear mud guard 12 are respectively arranged in front of and behind the wheels 4 to prevent muddy water from scattering on a bottom plate of the aerocar when the aerocar runs on the ground.

The technical means disclosed in the invention scheme are not limited to the technical means disclosed in the above embodiments, but also include the technical scheme formed by any combination of the above technical features.

Claims

1. A flying automobile comprises an automobile body (6) and wheels (4), and is characterized in that: be provided with first wing cabin (3) and second wing cabin (5) on fuselage (6), first wing cabin (3) are provided with two both sides that are located fuselage (6) respectively, second wing cabin (5) are located fuselage (6) top, be provided with folding wing (8) in first wing cabin (3) and second wing cabin (5) respectively, folding wing (8) including first folding axle (16), second folding axle (17) and third folding axle (18), first folding axle (16), second folding axle (17) and third folding axle (18) cup joint the setting, the size of first folding axle (16) is greater than the size of second folding axle (17), the size of second folding axle (17) is greater than the size of third folding axle (18), be connected with motor case (20) on third folding axle (18), the motor case (20) rotates the setting for third folding shaft (18), screw (19) are installed to motor case (20) top, be provided with screw driving motor in motor case (20), screw (19) are for screw groove (21) folding setting.

2. A flying automobile as claimed in claim 1, wherein: the foldable wing aircraft is characterized in that a mounting hole of a foldable wing (8) is formed in the first foldable shaft (16), and the foldable wing (8) is mounted in the first wing cabin (3) and the second wing cabin (5) through the mounting hole of the foldable wing (8).

3. A flying automobile as claimed in claim 2, wherein: the tip of first folding axle (16) is circular-arc, is provided with a plurality of archs (22) on the circular-arc circumferencial direction of edge, be provided with circular-arc recess in first wing cabin (3) and the second wing cabin (5) respectively, be provided with a plurality of indents on the circumferencial direction of edge recess, the tip of first folding axle (16) is installed in circular-arc recess, arch (22) embedding indent.

4. A flying automobile as claimed in claim 1, wherein: a motor box groove 181 is arranged on the third folding shaft (18), and the motor box (20) can be rotatably placed in the motor box groove 181.

5. A flying automobile as claimed in claim 1, wherein: the side surfaces of the motor boxes (20) are respectively provided with a propeller groove (21), and the propellers (19) are arranged in the propeller grooves (21) in a foldable mode.

6. A flying automobile as claimed in claim 1, wherein: install the fender on wheel (4), the fender is including preceding fender (14) and rear fender (12), the rear in wheel (4) rotation direction is installed in preceding fender (14), the place ahead in wheel (4) rotation direction is installed in rear fender (12).

7. A flying automobile as claimed in claim 1, wherein: still be provided with glass window (7), front car light (1) and indicator (2) on fuselage (6), glass window (7) are the semicircle form and are located fuselage (6) top, front car light (1) and indicator (2) are provided with two pairs and are located the both sides of glass window (7) respectively.

8. A flying automobile as claimed in claim 7, wherein: fuselage (6) rear is provided with trunk (10) and tail lamp (9), be provided with trunk (10) key hole (11) that are used for opening trunk (10) on trunk (10).