CN218258708U

CN218258708U - Electronic VTOL manned unmanned aerial vehicle

Info

Publication number: CN218258708U
Application number: CN202222820597.7U
Authority: CN
Inventors: 李坤煌
Original assignee: Shenzhen High Innovation Technology Co ltd
Current assignee: Shenzhen High Innovation Technology Co ltd
Priority date: 2022-10-24
Filing date: 2022-10-24
Publication date: 2023-01-10
Anticipated expiration: 2032-10-24

Abstract

The utility model provides an electronic VTOL manned unmanned aerial vehicle, including aircraft nose, fuselage, wing and tail, the fuselage is equipped with manned cabin, be equipped with seat, human-computer interaction control cabinet, navigation and flight control unit in the manned cabin, human-computer interaction control cabinet with navigation all with flight control unit electricity is connected and is used for sending flight command to flight control unit, first screw group, second screw group and third screw group are installed to the left and right both sides symmetry respectively to the wing, be equipped with on the tail and be V style of calligraphy fin, the fourth screw group is installed to the symmetry on the fin, thereby flight control unit is used for the control motor to drive the screw motion, provides economic efficient trip scheme for masses, need not professional navigating mate, adopts intelligent navigation, and the airline is independently flown, accurate location, and unique power distribution design has increased substantially unmanned aerial vehicle's security, convenient and fast.

Description

Electronic VTOL manned unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field, in particular to electronic VTOL manned unmanned aerial vehicle.

Background

With the development of unmanned aerial vehicles, high-speed communication, artificial intelligence and smart cities, the concept of urban air traffic is gradually increased, the urban air traffic refers to the provision of various air flight services inside large cities or between city circles and cities by using full-automatic urban unmanned aerial vehicles, the urban air traffic uses the unmanned aerial vehicles as cores to exploit urban airspace resources, 2.5D traffic with the existing underground, ground and overhead carriers is expanded into a novel 3D three-dimensional traffic mode, the urban unmanned aerial vehicles greatly expand traffic capacity, an effective mode is provided for solving the bottleneck problem of urban operation, the urban unmanned aerial vehicles can play a great role in multiple scenes in cities in the future, such as urban operation services (traffic evacuation, emergency rescue and the like), commercial services (low-altitude sightseeing, fast goods transportation, cold chain transportation) and public traffic services (passenger transportation), application demands on the background of urban operation and management, and demands on the novel unmanned aerial vehicles are greatly promoted.

The domestic tourism industry is rapidly developed, and more tourism is carried out in holidays along with the continuous improvement of the living standard of people. Most of domestic scenic spots are mainly outdoor close nature (mountains, islands, canyons and grasslands) and urban sightseeing, and low-altitude sightseeing in the scenic spots is more and more popular due to extraordinary experience, so that the scenic spots are key items for tourism development of future scenic spots. When high-altitude experience projects in scenic spots are realized by manned helicopters or fixed-wing airplanes, the airplanes need to be equipped with drivers with flight qualifications. In view of the shortage and high culture cost of domestic navigation flight drivers, the cost of pilots is high, so that the price of low-altitude sightseeing experience items is high, and the popularization is difficult to achieve. Scenic spots with low-altitude sightseeing requirements are mostly in mountainous areas, canyons, urban areas and the like, and the terrains in the places are complex, so that professional runways and airports with enough areas are difficult to construct. Meanwhile, most of the existing mountainous areas and canyon scenic areas adopt cableways for tourism and sightseeing passenger transport. However, the cableway cable car has a slow running speed, is long in queuing time in busy tourism seasons, particularly in golden weeks, and causes large-area detention of tourists, and the experience feeling is poor.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an electronic VTOL manned unmanned aerial vehicle aims at solving the technical problem that can not realize nimble, swift, safe various demands of city air traffic and scenic spot sightseeing among the prior art.

In order to solve the technical problem, the utility model discloses a technical scheme be: the utility model provides an electronic VTOL manned unmanned aerial vehicle, includes aircraft nose, fuselage, wing and tail, the wing sets up the left and right both sides of fuselage, tip and afterbody along axial direction are located respectively to aircraft nose, tail, the fuselage is equipped with manned cabin, be equipped with seat, human-computer interaction control platform, navigation in the manned cabin, human-computer interaction control platform with navigation all with flight control unit electricity is connected and is used for sending the flight command to flight control unit, first screw group, second screw group and third screw group are installed to the left and right both sides symmetry respectively to the wing, be equipped with on the tail and be V style of calligraphy fin, the fourth screw group is installed to the symmetry on the fin, thereby flight control unit is used for the control motor to drive the screw motion.

Furthermore, first screw group installs at the left and right both sides tip of wing, first screw group and second screw group are located collinear, first screw group and fourth screw group are the tilting screw, the tilting screw is by tilting motor drive.

Furthermore, the third propeller group is arranged in the middle of the left side and the right side of the wing, and the third propeller group is respectively provided with an upper blade and a lower blade.

Furthermore, the first propeller group and the second propeller group are powered by a first battery module, the third propeller group and the fourth propeller group are powered by a second battery module and a third battery module respectively, and each single battery module can be charged or replaced.

Furthermore, spoilers are further arranged on the left side and the right side of the wing, and elevators are further arranged on the tail.

Furthermore, the number of the seats is four, and the seats are arranged in two rows in the manned cabin.

Furthermore, a luggage rack is further arranged in the manned cabin and used for placing luggage.

Furthermore, a landing gear is arranged on the lower surface of the manned cabin and comprises a damping unit and a roller.

Furthermore, the aircraft nose still is equipped with airspeed head.

Furthermore, cabin doors are arranged on two sides of the passenger cabin, and the cabin doors are gull wing doors or scissor doors.

The beneficial effects of the utility model reside in that: an electric vertical take-off and landing manned unmanned aerial vehicle can be used for air traffic, scenic spot sightseeing and replacing a cable car to transport passengers. Its fuselage is equipped with manned cabin, be equipped with seat, human-computer interaction control cabinet, navigation and flight control unit in the manned cabin, for masses provide economic efficient trip scheme, need not professional navigating mate, the passenger selects near the fixed point of taking off and land of destination at the human-computer interaction control cabinet, can take at ease, adopts intelligent navigation, and the airline is independently flown, through accurate location, and is safe swift. First screw group, second screw group and third screw group are installed to the wing left and right both sides symmetry respectively, be equipped with on the tail and be the V style of calligraphy fin, the fourth screw group is installed to the symmetry on the fin, thereby flight control unit is used for the control motor to drive the screw motion, unique power distribution design, the comprehensiveness of aircraft has been increased substantially, can accomplish various flight actions through adjusting different drive arrangement's rotational speed respectively at the flight in-process, convenient control, can hover, the side is flown and is switched over smoothly between flight states such as rotatory, maneuverability with control the performance good.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings required for the embodiments or the prior art descriptions will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art to obtain other drawings without inventive labor.

Fig. 1 is a schematic view of a three-dimensional structure of an electric vertical take-off and landing manned unmanned aerial vehicle of the utility model;

fig. 2 is a top view of the electric vertical take-off and landing manned unmanned aerial vehicle in vertical flight;

FIG. 3 is a perspective view of the electric vertical take-off and landing manned unmanned aerial vehicle in vertical flight;

FIG. 4 is a perspective view of the electric vertical take-off and landing manned unmanned aerial vehicle in horizontal flight;

fig. 5 is the utility model relates to an electronic VTOL manned unmanned aerial vehicle fuselage local schematic diagram.

Description of reference numerals:

10. a machine head; 101. a pitot tube; 20. a body; 201. a landing gear;

202. a seat; 203. a cabin door; 204. a luggage rack; 30. an airfoil;

301. a first propeller group; 302. a second propeller group; 303. a third propeller group; 304. a spoiler; 40. a tail; 401. a fourth propeller group; 402. an elevator.

Detailed Description

Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below by referring to the drawings are exemplary intended for explaining the present invention, and should not be construed as limiting the present invention.

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.

Furthermore, the terms "first", "second" and "first" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of that feature. In the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.

In the present invention, unless otherwise expressly stated or limited, the terms "mounted," "connected," and "fixed" are to be construed broadly and may, for example, be fixedly connected, detachably connected, or integrally formed; can be mechanically or electrically connected; either directly or indirectly through intervening media, either internally or in any other relationship. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.

As shown in fig. 1-5, the embodiment of the utility model provides an electronic VTOL manned unmanned aerial vehicle, including aircraft nose 10, fuselage 20, wing 30 and tail 40, wing 30 sets up the left and right both sides of fuselage 20, aircraft nose 10, tail 40 locate fuselage along axial direction's tip and afterbody respectively, fuselage 20 is equipped with the manned cabin, be equipped with seat 202, human-computer interaction control platform, navigation and flight control unit in the manned cabin, the human-computer interaction control platform with navigation all with flight control unit electricity is connected and is used for sending the flight command to flight control unit, first screw group 301, second screw group 302 and third screw group 303 are installed to the left and right both sides symmetry respectively, be equipped with on the tail 40 and be the V style of calligraphy fin, the symmetry is installed fourth screw group 401 on the tail, thereby flight control unit is used for the control motor to drive the screw motion. Its fuselage is equipped with manned cabin, be equipped with seat, human-computer interaction control cabinet, navigation and flight control unit in the manned cabin, for masses provide economic efficient trip scheme, need not professional navigating mate, the passenger selects near the fixed point of taking off and land of destination at the human-computer interaction control cabinet, can take at ease, adopts intelligent navigation, and the airline is independently flown, through accurate location, and is safe swift. First screw group, second screw group and third screw group are installed to the wing left and right both sides symmetry respectively, be equipped with on the tail and be the V style of calligraphy fin, the fourth screw group is installed to the symmetry on the fin, thereby flight control unit is used for the control motor to drive the screw motion, unique power distribution design, the comprehensiveness of aircraft has been increased substantially, can accomplish various flight actions through adjusting different drive arrangement's rotational speed respectively at the flight in-process, convenient control, can hover, the side is flown and is switched over smoothly between flight states such as rotatory, maneuverability with control the performance good.

Further, as shown in fig. 3 and 4, the first propeller group 301 is installed at the end portions of the left and right sides of the wing, the first propeller group 301 and the second propeller group 302 are located on the same straight line, the first propeller group 301 and the fourth propeller group 401 are inclined propellers, and the inclined propellers are driven by an inclinable motor. Can realize not receiving the restriction in place at quick VTOL under any environment, can hover in order to satisfy the take off and land demand under the various scenes in city in the realization of co-altitude to make unmanned aerial vehicle can obtain great horizontal thrust at the level in-flight process through the tilting screw, improve the airspeed. When the inclined propeller is in a vertical state, the airplane can hover, fly sideways, fly backwards, vertically ascend and descend and the like; when the inclined propeller is in a horizontal state, the airplane is equivalent to a fixed-wing airplane and can fly at high speed and in a long distance. Adopt the tilting screw, combine together fixed wing unmanned aerial vehicle and many rotor unmanned aerial vehicle's advantage, a tractor driver bimodulus possesses many rotor unmanned aerial vehicle VTOL, fixed point ability of hovering and the ability that fixed wing unmanned aerial vehicle cruised at a high speed simultaneously.

Further, as shown in fig. 2, the third propeller group 303 is installed in the middle of the left side and the right side of the wing, and the third propeller group is provided with an upper blade and a lower blade, so that the performance and the safety of the airplane are greatly improved.

Further, the first propeller group 301 and the second propeller group 302 are powered by a first battery module, the third propeller group 303 and the fourth propeller group 401 are powered by a second battery module and a third battery module, respectively, and each single battery module can be charged or replaced. The battery module is independently for supplying power for the motor, adopts the passive bus that can dismantle to allow when normal operating to stride the bus and share the electric current, and can not lead to single point trouble, redundant high-pressure system design to provide the highest level safety. The electric energy is adopted to provide power, hydrocarbon fuel is not used, zero emission is achieved, the helicopter is more environment-friendly, and noise is 100 times quieter than that of a helicopter. The noise is only 65dBA in the hovering state and only 40dBA in the forward flight.

Further, as shown in fig. 2, spoilers 304 are further disposed on the left and right sides of the wing, and an elevator 402 is further disposed on the tail. The spoilers are used for assisting in providing high-lift power for taking off and landing and increasing aerodynamic drag on the ground or in flight, and the maneuverability of the airplane is improved. The elevator is used for controlling the direction of the empennage control surface to drive the fuselage cabin body to carry out dive flight or upward-dive flight.

Further, as shown in fig. 5, the number of the seats is four, and the seats are arranged in two rows in the passenger plane cabin. The visual field of the passenger can be guaranteed, the passenger has higher sightseeing experience in the unmanned aerial vehicle, the cruising ability of the unmanned aerial vehicle is integrated, the whole unmanned aerial vehicle is compact in structure, the space utilization rate is high, and the occupied area is small.

Further, as shown in fig. 5, a luggage rack is further provided in the passenger compartment for placing luggage. Unmanned aerial vehicle wholly constructs compactly, and space utilization is high, reaches better passenger and experiences.

Further, as shown in fig. 1 and 5, a landing gear 201 is disposed on a lower surface of the passenger cabin, and the landing gear includes a damping unit and a roller. Support whole unmanned aerial vehicle and be used for taking off to descend or ground slides and when descending buffering, improve passenger's comfort level.

Further, as shown in fig. 1 and 3, the handpiece is also provided with a pitot tube 101. For deriving aircraft speed by measuring the dynamic pressure of the airflow. Make unmanned aerial vehicle overall structure compact, space utilization is high, and area is little.

Further, as shown in fig. 5, cabin doors 203 are further provided at both sides of the passenger cabin, and the cabin doors are gull wing doors or scissor doors.

To sum up, the utility model provides a pair of electronic VTOL manned unmanned aerial vehicle can be used to air traffic, scenic spot sightseeing and replaces the cable car and transports passenger. Its fuselage is equipped with manned cabin, be equipped with seat, human-computer interaction control cabinet, navigation and flight control unit in the manned cabin, for masses provide economic efficient trip scheme, need not professional navigating mate, the passenger selects near the fixed point of taking off and land of destination at the human-computer interaction control cabinet, can take at ease, adopts intelligent navigation, and the airline is independently flown, through accurate location, and is safe swift. The unique power distribution design greatly improves the safety of the airplane, various flight actions can be completed by respectively adjusting the rotating speeds of different driving devices in the flight process, the control is convenient, the flying states such as hovering, side flying, rotating and the like can be smoothly switched, and the maneuvering performance and the control performance are good. The whole structure is compact, the space utilization rate is high, and the occupied area is small. Adopt the tilting screw, combine together fixed wing unmanned aerial vehicle and many rotor unmanned aerial vehicle's advantage, a tractor driver bimodulus possesses many rotor unmanned aerial vehicle VTOL, fixed point ability of hovering and the ability that fixed wing unmanned aerial vehicle cruised at a high speed simultaneously.

The above mentioned is only the embodiment of the present invention, and not the limitation of the patent scope of the present invention, all the equivalent transformations made by the contents of the specification and the drawings, or the direct or indirect application in the related technical field, are included in the patent protection scope of the present invention.

Claims

1. The utility model provides an electronic VTOL manned unmanned aerial vehicle, includes aircraft nose, fuselage, wing and tail, the wing sets up the left and right both sides of fuselage, tip and afterbody along axial direction are located respectively to aircraft nose, tail, a serial communication port, the fuselage is equipped with manned cabin, be equipped with seat, human-computer interaction control platform, navigation and flight control unit in the manned cabin, human-computer interaction control platform with navigation all with flight control unit electricity is connected and is used for sending the flight command to flight control unit, first screw group, second screw group and third screw group are installed to the wing left and right both sides symmetry respectively, be equipped with on the tail and be V style of calligraphy fin, fourth screw group is installed to the symmetry on the fin, thereby flight control unit is used for controlling the motor and drives the screw motion.

2. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 1, wherein the first propeller group is installed at the left and right side ends of the wing, the first propeller group and the second propeller group are located on the same straight line, the first propeller group and the fourth propeller group are inclined propellers, and the inclined propellers are driven by an inclined motor.

3. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 1, wherein the third propeller group is installed in the middle of the left side and the right side of the wing, and the third propeller group is respectively provided with an upper blade and a lower blade.

4. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 1, wherein the first propeller group and the second propeller group are powered by a first battery module, the third propeller group and the fourth propeller group are powered by a second battery module and a third battery module respectively, and each individual battery module can be charged or replaced.

5. The unmanned aerial vehicle for vertically electric taking off and landing according to claim 1, wherein spoilers are further disposed on left and right sides of the wing, and elevators are further disposed on the tail.

6. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 1, wherein the number of the seats is four, and the seats are arranged in two rows in the manned cabin.

7. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 1, wherein a luggage rack is further arranged in the manned cabin for placing luggage.

8. The electric VTOL manned unmanned aerial vehicle of claim 1, wherein the lower surface of the manned cabin is provided with landing gear, and the landing gear comprises a damping unit and rollers.

9. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 1, wherein the aircraft nose is further provided with an airspeed head.

10. The electric vertical take-off and landing manned unmanned aerial vehicle of claim 6, wherein cabin doors are further provided on two sides of the manned cabin, and the cabin doors are gull wing doors or scissor doors.