Fixed-wing form-switchable aerocar capable of being used for intercity navigation and mode switching system

Abstract

The invention provides a fixed-wing form-switchable flying car capable of being used for intercity navigation. The fixed-wing form-switchable flying car comprises three modules, namely an intelligent cabin module, a car chassis module and an aircraft body module. The switchable form comprises two modes, namely an automobile mode and an airplane mode; meanwhile, the invention further provides a mode switching system of the automobile, the mode switching system is used for switching two modes of the fixed-wing form-switchable flying automobile, the fixed-wing aircraft is adopted in the mode switching system, and the mode switching system is easy to maintain, low in manufacturing cost, high in safety, high in load capacity, high in comfort, high in speed, long in endurance and more suitable for long-distance intercity navigation.

Description

Technical Field

[0001] The present invention belongs to the technical field of flying cars, and in particular relates to a fixed-wing switchable flying car and a mode switching system that can be used for inter-city navigation. Background Art

[0002] The purpose of transportation is to move people or goods from one place to another safely, quickly, conveniently and comfortably. With the continuous progress of society, traditional transportation can no longer meet people's requirements for travel efficiency and convenience. As a new type of transportation, flying cars that can switch their forms can effectively alleviate highway congestion, improve travel efficiency, and provide a new possibility for future transportation.

[0003] The country is currently vigorously developing the low-altitude economy. The low-altitude economy refers to a comprehensive economic form that mainly uses civil manned and unmanned aircraft, and is driven by multi-scenario low-altitude flight activities such as manned and cargo operations, and radiates and drives the integrated development of related fields.

[0004] At present, the low-altitude economy mainly focuses on eVTOL (multi-rotor helicopters), supplemented by helicopters and traditional fixed-wing aircraft. However, mainstream aircraft can only fly in the sky, not on the ground, and can only serve as a supplement to urban / inter-city public transportation. They have a small load capacity, a short range, and a slow speed. They cannot meet the needs of inter-city navigation, nor can they solve the problem of the last 5-10-20 kilometers and the problem of using a car at the destination. A small number of flying cars have the functions of both flying and driving, but because they need to take into account both flying and driving modes at the same time, such flying cars need to carry two systems at the same time, namely the air flight system and the ground driving system, which leads to a complex structure, increased weight, increased energy consumption, low loading capacity, low speed, and reduced range. They are not suitable for inter-city navigation and cause a huge waste of energy, that is, carrying a useless system at any time.

[0005] The switchable flying car can be freely combined into car mode or airplane mode through the mode switching system. You can choose to combine the smart cockpit module with the car chassis module into car mode, or you can choose to combine the smart cockpit module with the aircraft body module into airplane mode. In car mode, it is a complete 4-7-seat electric new energy vehicle that meets the daily household use and can meet the short-distance transportation needs within the city or between cities. In airplane mode, it is a complete fixed-wing aircraft that can meet the long-distance transportation needs between cities. It has the advantages of both cars and airplanes, but without the disadvantages of combining the two. Summary of the invention

[0006] Technical solution: To solve the above technical problems, the present invention has made improvements compared with the current mainstream eVTOL of flying cars, which mostly adopt the form of multi-rotors. The aircraft mode in the present invention adopts the form of a fixed-wing aircraft. Compared with multi-rotor aircraft, fixed-wing aircraft have a simple structure, simple maintenance, low cost, high safety, high load capacity, high comfort, high speed, and long endurance, and are more suitable for intercity navigation over longer distances.

[0007] The present invention provides a fixed-wing switchable-form flying car that can be used for intercity navigation. The specific technical solution is as follows: It includes an intelligent cockpit module, a car chassis module, and an aircraft body module; the switchable form includes two modes, a car mode and an aircraft mode; in the car mode, it is composed of the intelligent cockpit module and the car chassis module; in the aircraft mode, it is composed of the intelligent cockpit module and the aircraft body module; among them, the bottom of the intelligent cockpit module is detachably connected to the car chassis module, and the bottom of the intelligent cockpit module is detachably connected to the aircraft body module.

[0008] As an improvement, in the car mode, it is a 4- to 7-seat electric vehicle, and the electric vehicle is either automatically intelligent-driven or manually driven; in the aircraft mode, it is a fixed-wing propeller or jet aircraft for intercity navigation, and the aircraft is either automatically intelligent-driven or remotely controlled.

[0009] As an improvement, it further includes a flight assistance module, which is detachably connected to the top of the intelligent cockpit module, and the flight assistance module includes a parachute.

[0010] As an improvement, in the car mode, the user drives the car to a general airport and parks in the designated area at the entrance of the hangar in the general airport; after the user leaves, through the mode switching system, the intelligent cockpit module automatically separates from the car chassis module, and then the intelligent cockpit module docks with the aircraft body module to switch to the aircraft mode; in the aircraft mode, the user takes the aircraft and flies to the general airport at the destination and lands in the designated area at the entrance of the hangar in the general airport; after the user leaves, through the mode switching system, the intelligent cockpit module automatically separates from the aircraft body module, and then the intelligent cockpit module docks with the car chassis module to switch to the car mode.

[0011] As an improvement, a connecting mechanism, a docking mechanism and a connecting hole are all provided in plurality; the connecting mechanism is a block structure with an internal threaded hole, in which a bolt can be installed; the docking mechanism is an axial structure with an internal threaded hole protruding from the outer side of the block structure, in which a bolt can be installed; the connecting hole is a hole with an internal threaded hole; the connecting mechanism and the connecting holes are installed in matching numbers and positions on the bottom of the smart cockpit module and on the chassis of the automobile chassis module to complete the detachable connection of the smart cockpit module and the automobile chassis module; the connecting mechanism and the docking mechanism are installed on the bottom of the smart cockpit module and on the inside of the cabin of the aircraft body module, and the number and positions are matched to complete the detachable connection of the smart cockpit module and the aircraft body module.

[0012] That is to say, in the present invention, preferably, the connecting mechanism and the docking mechanism, the connecting mechanism and the connecting hole can be threadedly connected by installing bolts in the internal threads, so as to realize the detachable connection between the smart cockpit module and the automobile chassis module, and the smart cockpit module and the aircraft fuselage module.

[0013] As a specific implementation of the present invention, the positions of the connecting mechanism and the docking mechanism may also be interchangeable. Specifically, the connecting mechanism is installed on the aircraft body module.

[0014] As an improvement, it also includes a plurality of positioning blocks and a plurality of fixing grooves, wherein one positioning block and one fixing groove, or one positioning block, or one fixing groove is installed on one side of a connecting mechanism or a docking mechanism, to assist in the initial alignment of the connecting mechanism and the docking mechanism, and the initial alignment of the connecting mechanism and the connecting hole;

[0015] When the connection mechanism and the docking mechanism, the connection mechanism and the connection hole are accurately positioned by bolt connection, there is no need to perform initial alignment of the positioning block, the fixing groove, the positioning block and the fixing groove.

[0016] That is to say, in the present invention, the initial alignment is first performed by cooperating with the positioning block and the fixing groove, and then the alignment is performed through the connecting hole and the connecting mechanism, and the connecting mechanism and the docking mechanism, which can reduce the time of direct alignment.

[0017] As a specific embodiment of the present invention, the matching method can be set as follows: a positioning block is installed at the bottom of one side of the connecting mechanism and protrudes downward; a fixing groove and a positioning block are set at the upper and lower positions but not through and are installed on one side of the connecting hole, and the positioning block protrudes downward; a fixing groove is installed on one side of the docking mechanism; thereby realizing that a positioning block and a connecting mechanism are detachably connected to a fixing groove and a connecting hole of a positioning block;

[0018] It is also possible to realize that a fixing groove and a connecting hole of a positioning block can be detachably installed with a docking mechanism of a fixing groove.

[0019] Preferably, the smart cockpit module and the automobile chassis module are connected / separated: the positioning block and the fixing groove are docked; the connecting mechanism and the connecting hole are docked, and then the automatic screw locking machine on the intelligent handling robot is used to tighten / release with bolts passing through the connecting hole (on the automobile chassis module) and the connecting mechanism (at the bottom of the smart cockpit module).

[0020] Preferably, the intelligent cockpit module and the aircraft body module are connected / separated by: the positioning block and the fixing groove are docked; the connecting mechanism and the docking structure of the aircraft body module are docked, and then the bolts and the connecting mechanism provided by the aircraft body module are used to tighten / release.

[0021] As an improvement, the smart cockpit module includes: steering system, seats, entertainment system, and power system; the automobile chassis module includes a frame, steering system, driving system, braking system, battery power system, and luggage rack; the aircraft body module includes a fuselage, wings, tail, landing gear, power unit, and positioning monitoring system, wherein the positioning monitoring system includes at least one of radar, ADS-B, and ADS-C.

[0022] At the same time, the present invention also provides a mode switchable system for a fixed-wing switchable flying car that can be used for inter-city navigation, the system being used for switching between the two modes of the above-mentioned fixed-wing switchable flying car, comprising a lifting-type intelligent transport robot AGV and a retractable fixed boom; the lifting-type intelligent transport robot AGV is used for positioning, moving, docking, transporting and lifting the entire vehicle and the separated automobile chassis module in automobile mode, and the entire vehicle and the separated aircraft fuselage module in airplane mode; the retractable fixed boom is installed on the top of the airport hangar, and is used to separate or dock the intelligent cockpit module from the automobile chassis module or the aircraft fuselage module.

[0023] As an improvement, the lifting-type intelligent handling robot AGV includes an intelligent automobile handling robot AGV and an intelligent aircraft handling robot AGV; the intelligent automobile handling robot AGV is used to dock or separate the intelligent cockpit module and the automobile chassis module, and also includes an automatic screw locking machine for automatically screwing the screws in or out during docking or separation; the intelligent aircraft handling robot AGV is used for handling and lifting the aircraft body module in the aircraft mode as a whole or in a separated state.

[0024] As an improvement, the retractable fixed boom includes an automatic clamp, a boom, and a positioning system. One end of the positioning system is connected to a fixed seat and fixed on the top of an airport hangar, and the other end is connected to the boom. The boom is a retractable structure, and an automatic clamp is installed at the bottom through a connecting block, which can move up and down. The automatic clamp includes a fixed plate and a clamp. The fixed plate is installed vertically to the boom, and two clamps are independently fixed at both ends of the fixed plate. The clamp can be opened and closed to clamp objects to be lifted.

[0025] Advantages: The technical solution provided by the present invention and this application has at least the following advantages compared with current pure electric vehicles, multi-rotor flying cars, etc.:

[0026] 1. A major reason affecting the popularization of pure electric vehicles currently is the range anxiety of pure electric vehicles. The current mainstream approach is to increase the battery capacity, but a large battery will inevitably lead to an increase in price and weight, which is very wasteful in daily use. However, for the vehicle mode in this embodiment, it only needs to meet commuting within the city and short-distance travel between cities. When traveling longer distances, the aircraft mode can be selected. Therefore, usually only a smaller battery needs to be carried, which can effectively reduce the vehicle purchase cost, reduce energy consumption, and reduce range anxiety.

[0027] 2. In order to meet the needs of users, the current vehicle chassis often needs to take into account styles such as sports / comfort / off-road, etc. As a result, it is neither sporty nor comfortable, and the actual effect is greatly reduced. Replacing the entire vehicle chassis can make the tuning of the vehicle chassis more pure. Users can choose a chassis suitable for themselves according to their needs. When they want to experience other styles, they can directly replace it.

[0028] 3. Replacing the entire vehicle chassis can also better detect and maintain the vehicle chassis equipment, increasing safety.

[0029] 4. Compared with self-driving travel, this embodiment is faster and more comfortable because the flight distance is equivalent to the ground driving distance, but because the flight speed is faster and there is no congestion.

[0030] 5. Compared with high-speed rail travel, this embodiment is more convenient. There is no need to transfer (from public transportation to the high-speed rail station), and it solves the problem of the last 5 - 10 kilometers and the vehicle use problem at the destination.

[0031] 6. Compared with air travel, this embodiment is also more convenient. The general airport required for this embodiment has a smaller area and can be built closer to the urban area than large airports. Moreover, there is no need to change boarding passes, go through security checks, etc. at the airport, and there is no need to carry luggage back and forth. One only needs to arrive at the airport according to the pre-arranged time, and it solves the problem of the last 10 - 30 kilometers and the vehicle use problem at the destination.

[0032] 7. Compared with current multi-rotor aircraft such as eVTOL, the aircraft mode in this case adopts the form of a propeller fixed-wing aircraft. Fixed-wing aircraft have a simpler structure, easier maintenance, higher safety, higher comfort, faster speed, and longer endurance compared to multi-rotor aircraft, and are more suitable for longer-distance commuting.

[0033] 8. Compared with current multi-system aircraft that can be driven and flown, it is lighter in weight and lower in energy consumption. BRIEF DESCRIPTION OF THE DRAWINGS

[0034] Figure 1Schematic diagram of the intelligent cockpit module of the present invention.

[0035] Figure 2 Schematic diagram of the vehicle chassis module of the present invention.

[0036] Figure 3 Schematic diagram of the aircraft fuselage module of the present invention; among which 3-1 is an enlarged view near the positioning block three, and 3-2 is an enlarged view near the docking mechanism one.

[0037] Figure 4 Schematic diagram of the flight assistance module; among which 4-1 is a partial structural schematic diagram of the luggage rack of the automatic latch fixing system in the unlocked state; 4-2 is a partial structural schematic diagram of the luggage rack of the automatic latch fixing system in the locked state.

[0038] Figure 5 Schematic diagram of the retractable fixed boom.

[0039] Figure 6 Schematic diagram of the lifting type intelligent vehicle handling robot AGV.

[0040] Figure 7 Schematic diagram of the lifting type intelligent aircraft handling robot AGV.

[0041] Figure 8 Schematic diagram and flow chart of the overall structure of the switchable form flying car; 1a is a schematic diagram of the aircraft mode, and 1b is a schematic diagram of the car mode.

[0042] Figure 8-1 Schematic diagram of Workflow 1 in Embodiment 2, among which 8-1a is that the intelligent handling robot AGV moves autonomously towards the vehicle in the designated area under the command of the mode switching system; 8-1b is that the throttle and brake of the vehicle chassis module pass through the automatic cover plate at the bottom of the intelligent cockpit module and enter the cockpit; 8-1c is that the intelligent cockpit module and the vehicle chassis module are fastened together by bolts; 8-1d is that the positioning block at the bottom of the intelligent cockpit module is docked with the positioning groove at the top of the vehicle chassis module; 8-1e is that the user parks the vehicle in the designated area.

[0043] Figure 8-2 Schematic diagram of Workflow 2 in Embodiment 2, among which 8-2a is that the automatic gripper at the bottom of the retractable boom grips the flight assistance module; 8-2b is that the intelligent handling robot lifts the vehicle and moves towards the boom; 8-2c is the vehicle chassis positioning block; 8-2d is that the docking groove of the intelligent handling robot docks with the positioning block of the vehicle chassis module.

[0044] Figure 8-3Schematic diagram of Workflow 3 in Embodiment 2. 8-3a shows the automatic latch fixing system locking the luggage rack; 8-3b shows the automatic screw locking machine releasing the bolt for docking and locking; 8-3c shows the intelligent vehicle handling robot lifting the vehicle and docking with the boom; 8-3d shows the boom clamping the auxiliary flight module, the automatic latch fixing system of the auxiliary flight module locking the luggage rack, and the intelligent handling robot lifting the vehicle chassis module.

[0045] Figure 8-4 Schematic diagram of Workflow 4 in Embodiment 2. 8-4a shows the boom clamping the flight auxiliary module, and the flight auxiliary module fixing the luggage rack; 8-4b shows the automatic cover at the bottom of the cockpit closing; 8-4c shows the state where the intelligent robot lifts the vehicle chassis module and leaves.

[0046] Figure 8-5 Schematic diagram of Workflow 5 in Embodiment 2. 8-5a shows the intelligent robot lifting the aircraft and moving it towards the boom; 8-5b shows the schematic diagram of the intelligent robot docking the docking slot with the positioning block at the bottom of the aircraft fuselage.

[0047] Figure 8-6 Schematic diagram of the docking of the intelligent cockpit module and the aircraft fuselage module in Workflow 6 of Embodiment 2.

[0048] Figure 8-7 Schematic diagram of the intelligent robot lifting the aircraft and moving it towards the designated flight waiting area in Embodiment 2.

[0049] Figure 8-8 Schematic diagram of Workflow in Embodiment 2. 8-8a shows the aircraft in the flight waiting area, waiting for the user to board and take off; 8-8b shows the state diagram of the intelligent robot moving to the work waiting area.

[0050] In the figure: 1 - intelligent cockpit module; 11A - cockpit; 11B - luggage rack; 11C - automatic cover; 12B - connecting mechanism 1; 12C - positioning block 1; 12D - nose.

[0051] 2 - vehicle chassis module; 21A - chassis; 21B - tire; 21C - throttle; 21D - brake; 22A - fixing slot 1; 22B - connecting hole; 22C - positioning block 2.

[0052] 3 - aircraft fuselage module; 31A - fuselage; 31B - wing; 31C - power system; 31D - tail; 31E - landing gear; 32A - fixing slot 2; 32B - docking mechanism 1; 32C - positioning block 3.

[0053] 4 - flight auxiliary module; 41A - parachute; 41B - top radar; 41C - card slot; 42A - boom clamping area; 42B - automatic latch fixing system.

[0054] 5 - Telescopic Fixed Boom; 51B - Boom; 51C - Positioning Device; 52B - Automatic Claw

[0055] 6 - Lifting Type Intelligent Vehicle Handling Robot AGV; 61A - Universal Wheel 1; 61B - Lifting Mechanism 1; 61C - Positioning Device 1; 62A - Docking Slot 1; 62B - Docking Structure; 62D - Base; Docking Mechanism 2 62B

[0056] 7 - Lifting Type Intelligent Aircraft Handling Robot AGV; 71A - Universal Wheel 2; 71B - Lifting Mechanism 2; 71C - Positioning Device 2; 72A - Docking Slot 2 Detailed Implementation Manner

[0057] The technical solutions in the embodiments of the present invention will be clearly and completely described below, so that those skilled in the art can better understand the advantages and features of the present invention, and thus make a clearer definition of the protection scope of the present invention. The embodiments described in the present invention are only a part of the embodiments of the present invention, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present invention without creative work belong to the protection scope of the present invention.

[0058] As Figure 8 shown, the present invention provides a fixed - wing convertible flying car that can be used for inter - city navigation, including an intelligent cockpit module 1, an automobile chassis module 2, and an aircraft body module 3; the convertible form includes two modes, an automobile mode and an aircraft mode; in the automobile mode, it is composed of the intelligent cockpit module 1 and the automobile chassis module 2; in the aircraft mode, it is composed of the intelligent cockpit module 1 and the aircraft body module 3; wherein the bottom of the intelligent cockpit module 1 is detachably connected to the automobile chassis module 2, and the bottom of the intelligent cockpit module 1 is detachably connected to the aircraft body module 3.

[0059] The flying car of the present invention will be introduced and described in detail below with reference to the accompanying drawings of the specification.

[0060] Specifically, the intelligent cockpit module 1 is used to carry passengers, goods, etc. The automobile chassis module 2 is used to provide power for the intelligent cockpit module 1 to travel on land. The aircraft body module 3 is used to provide lift and power for the intelligent cockpit module 1 during take - off, in - air flight, and landing.

[0061] See Figure 1As shown in the figure, the intelligent cockpit module includes: a steering system, seats, an entertainment system, a power system, cockpit 11A, a luggage rack 11B, an automatic cover 11C, a first connecting mechanism 12B, a first positioning block 12C, and a nose 12D; the steering system is used to turn the steering wheel to adjust the direction, the seats are generally 4 to 7 seats, and the entertainment system includes games, videos, recordings, etc.; the power system is used to provide the required electrical energy. The cockpit 11A is the body of the current automobile, generally in a box structure.

[0062] The luggage rack 11B is fixedly installed on the top of the cockpit 11A, generally 1 - 4 rods with a spaced design or a rack assembled by rods, and is used to place luggage. Moreover, multiple noses 12D are provided and fixedly installed on the luggage rack 11B, and are used as the brackets to be lifted when the vehicle mode is changed to the flight mode.

[0063] The automatic cover 11C is in a retracted state in the vehicle mode and is used for the driving system of the vehicle chassis module 2, including the throttle and the braking system including the brakes, which extend into the intelligent cockpit module 1; it is in a closed state in the aircraft mode.

[0064] Furthermore, at the bottom of the intelligent cockpit module, that is, at the end point positions of the bottom surface of the cockpit 11A, the first connecting mechanism 12B, the first positioning block 12C, and the nose 12D are installed; among them, the first connecting mechanism 12B is in a block structure, the top surface is a horizontal plane, and it is installed at the bottom of the cockpit 11A; one end of the bottom surface protrudes downward to form a first positioning block 12C, and a through hole with a threaded inner side is provided at the other end of the bottom surface; the first positioning block 12C is in an inverted frustum of a pyramid structure and is integrally formed with the first connecting mechanism 12B.

[0065] See Figure 2 As shown in the figure, the vehicle chassis module 2 includes: a chassis 21A, tires 21B, a steering system, a driving system including a throttle 21C, a braking system including brakes 21D, a battery power system, a suspension system, etc. Among them, the chassis 21A is a base with a cavity structure in the middle and is used to install the intelligent cockpit module 1; the tires 21B are installed at the bottom of the chassis 21A and are used for the normal operation of the vehicle.

[0066] The present invention adopts a steer - by - wire operating system for the steering system. This system enables the steering systems of the intelligent cockpit module 1 and the vehicle chassis module 2 to be connected without mechanical connection, relying only on electrical connection and communication connection, and can achieve lower latency and more precise control.

[0067] The throttle 21C of the driving system and the brakes 21D of the braking system of the vehicle chassis module 2 can move back and forth within a certain range to adapt to intelligent cockpits with different functions and sizes, increasing versatility.

[0068] Furthermore, the vehicle chassis module is also equipped with one or more positioning systems such as the Beidou satellite navigation system, GPS (Global Positioning System), GLONASS (Global Navigation Satellite System), etc. Combining with on-board sensors, calculators, artificial intelligence algorithms, and cloud computing systems, precise path planning and autonomous driving can be achieved. Regarding the structures of the driving system, braking system, battery power system, suspension system, etc., they are conventional existing systems. The main focus is on enabling those skilled in the art to achieve the normal operation of the vehicle in this invention, so they will not be elaborated here.

[0069] The vehicle chassis module further includes: connection blocks, fixing groove 1 22A, connection hole 22B, and positioning block 2 22C. Specifically, the fixing groove 1 22A, connection hole 22B, and positioning block 2 22C are all designed on the connection blocks; there are multiple connection blocks, which are detachably installed at multiple end positions of the cavity structure of the vehicle chassis module for docking with the intelligent cockpit module 1. Preferably, as shown in Figure 3 In [the figure], four connection blocks can be provided and detachably installed at the four end positions of the cavity structure of the vehicle chassis module for docking with the intelligent cockpit module 1.

[0070] Furthermore, on one side of the top of the connection block, there is a fixing groove 1 22A, whose structure is adapted to that of the positioning block 1 12C for snap-in installation of the positioning block 1 12C; the connection hole 22B is provided at the other end of the connection block and is a through hole with internal threads for adaptively installing with the corresponding bolt of the connection structure 1 12B of the intelligent cockpit module; the positioning block 2 22C is an inverted frustum pyramid structure protruding downward at the bottom of the other side of the fixing groove 22A.

[0071] See Figure 3 As shown in [the figure], the aircraft body module 3 includes the body 31A, wings 31B, tail wing 31D, landing gear 31E, and power plant 31C. The body 31A is the main structure of the aircraft with a cabin in the middle; there are two wings 31B, symmetrically installed on both sides of the cabin; the power plant 31C is installed on one side of the connection position between the wing 31B and the cabin for providing flight power for the aircraft; the tail wing 31D is installed at the tail end of the cabin; the landing gear 31E is installed at the bottom of the front end of the cabin.

[0072] As a specific embodiment of the present invention, the overall length of the aircraft is 10 meters, the wingspan is 15 meters, and the height (including the tail wing) is 3 meters. The entire body is made of composite materials to reduce weight. The wings 31B and the tail wing 31D can provide lift and control for the aircraft during takeoff, in-air flight, and landing.

[0073] The aircraft body module 3 further includes a second solid groove 32A, a first docking mechanism 32B, and a third positioning block 32C; the second solid groove 32A is a groove structure in the shape of an inverted frustum of a pyramid, installed on the inner side of the cabin of the airframe 31A, and there are multiple of them, and the quantity, position, and shape are all matched with the first positioning block 12C of the intelligent cockpit module 1; the first docking mechanism 32B is arranged on one side of the second fixed groove 32A, preferably an automatic screw locking machine, and is used for detachable threaded connection with the first connecting mechanism 12B of the intelligent cockpit module 1. The third positioning block 32C is a hemispherical structure protruding downward and is installed on the inner side of the cabin.

[0074] As another specific embodiment of the present invention, the power device 31C of the aircraft body module adopts 2 (or more than 2) electric motors, and the power of each electric motor is not less than 200 kilowatts. A 3-blade composite material propeller is used, which can provide power for the aircraft during takeoff and cruise, meet the takeoff / landing of the aircraft at a 2B general airport, and a cruising speed of about 350 - 400 kilometers per hour, and improve flight safety.

[0075] Furthermore, the aircraft adopts an extended-range power system. The aircraft carries a battery with a power of not less than 100 kilowatts to supply power to the whole aircraft. A micro gas turbine generator is used, and environmentally friendly energy such as green ammonia is used to charge the battery to meet the flight range of the aircraft of not less than 1000 kilometers.

[0076] In order to obtain a faster flight speed and a longer flight range, the aircraft mode can also adopt a jet power system.

[0077] In the present invention, the landing gear 31E of the aircraft body module 3 is opened during the mode switching, takeoff, and landing stages of the aircraft to provide the aircraft with ground support and taxiing capabilities. It is retracted during the flight stage to reduce flight resistance.

[0078] The first docking mechanism 32B of the aircraft body module 3, for example, can be an automatic screw locking machine, which includes a bolt and a driving component. The bolt has an external thread, and the driving component is mechanically connected to the bolt. The driving component is used to drive the bolt to rotate around its own central axis.

[0079] Furthermore, threaded holes are provided on the four sides of the bottom of the intelligent cockpit module 1 and are flatly arranged on the first connecting mechanism 12B of the intelligent cockpit module. After the first docking mechanism 32B and the first connecting mechanism 12B are aligned, the driving component drives the bolt to tighten in the threaded hole of the first connecting mechanism 12B, realizing the connection between the first docking mechanism 32B and the first connecting mechanism 12B, and further realizing the fastening of the intelligent cockpit module 1 and the aircraft body module 3.

[0080] When it is necessary to separate the intelligent cockpit module 1 and the aircraft fuselage module 3, the driving component drives the bolt to reverse out of the threaded hole of the connecting mechanism 12B, realizing the separation of the docking mechanism 32B and the connecting mechanism 12B, and further realizing the release of the intelligent cockpit module 1 and the aircraft fuselage module 3.

[0081] The connection or separation between the intelligent cockpit module 1 and the aircraft fuselage module 3 adopts a threaded fastening and releasing mechanism, that is, through the cooperation of the bolt and the Automatic Screw Feeding and Driving System, the connection and separation are realized; the threaded fastening and releasing mechanism has a simple and reliable structure, high connection strength, and good durability and maintainability.

[0082] In the present invention, the aircraft fuselage module 3 is also equipped with one or more positioning systems such as the Beidou satellite navigation system, GPS (Global Positioning System), GLONASS (Global Navigation Satellite System), etc. Combined with on-board sensors, calculators, artificial intelligence algorithms and cloud computing systems, under the command of the air traffic control system (ATC) and the ground control system, it can take off, fly automatically and land precisely along the planned path.

[0083] The aircraft fuselage module 3 is also equipped with a radar, as well as one or more air positioning and surveillance systems such as ADS-B (Automatic Dependent Surveillance-Broadcast) and ADS-C (Automatic Dependent Surveillance-Broadcast), cooperating with the air traffic control system (ATC) to increase flight safety.

[0084] As one of the specific implementation manners of the present invention, the automotive chassis module 2 and the aircraft fuselage module 3 are also respectively integrated with electrical components such as an autopilot system and an electric control system, and electrical connectors are respectively arranged between the intelligent cockpit module 1 and the automotive chassis module 2 and the aircraft fuselage module 3, so as to realize the electrical connection and communication connection between the intelligent cockpit module 1 and the automotive chassis module 2 or the aircraft fuselage module 3.

[0085] The automotive chassis module 2 and the aircraft fuselage module 3 are also equipped with a detection component for detecting the docking state between the intelligent cockpit module 1 and the automotive chassis module 2 or the aircraft fuselage module 3. The detection component includes one or more of an image sensor, a laser sensor, an infrared position sensor, and a metal proximity sensor.

[0086] SeeFigure 4 As shown, in airplane mode, there is an additional flight assistance module 4, which includes: an intelligent cockpit parachute pack 41A, a top-mounted radar 41B, a card slot 41C, a boom clamping area 42A, and an automatic bolt fixing system 42B.

[0087] This flight assistance module is a plate-like structure with a dome. The intelligent cockpit parachute pack 41A is installed on one side of the top of the module, and the top-mounted radar 41B is installed on the other side of the top of the module; the card slot 41C is set at the bottom of the module and is a pair of symmetric channels, which are detachably installed in a matching manner with the overhead luggage rack on the top of the intelligent cockpit module 1; the boom clamping area 42A is set at the top of the module, and when switching to flight mode, the telescopic boom claw clamping part of the hoisting device can be clamped. The automatic bolt fixing system 42B is used to complete the locking through the cooperation with the nose on the top after the overhead luggage rack on the top of the intelligent cockpit module 1 is slidably installed, and the flight assistance module is detachably connected to the top of the intelligent cockpit module.

[0088] As one of the specific embodiments of the present invention, in car mode, it is a 4-7 seat electric new energy vehicle suitable for daily household use, applicable to daily urban or short-distance intercity road driving, and can be either automatically intelligent driving or manual driving.

[0089] As another specific embodiment of the present invention, in airplane mode, it is a fixed-wing propeller or jet aircraft that can be used for intercity navigation, suitable for rapid intercity navigation, and the aircraft is either automatically intelligent driving or remotely controlled driving.

[0090] In the switchable form flying car of the present invention: in car mode, it does not need to carry systems such as the fuselage, wings, tail, landing gear, and power device included in the aircraft body module 3, which can reduce weight, reduce size, reduce energy consumption, increase endurance and economy. In airplane mode, it does not need to carry systems such as the frame, tires, steering system, driving system, braking system, and battery power system included in the car chassis module 2, which can reduce weight, reduce flight resistance, reduce energy consumption, and increase speed, range, and economy.

[0091] Furthermore, through the mode switching system, the switchable form flying car can automatically switch to car mode or airplane mode, and can quickly realize ground driving or flying in the air, meeting both the needs of daily commuting and rapid intercity navigation.

[0092] Specifically, the mode switching system of the fixed-wing transformable flying car for intercity navigation includes a lifting intelligent transfer robot AGV and a telescopic fixed boom; the lifting intelligent transfer robot AGV is used for positioning, moving, docking, handling, and lifting the whole vehicle in car mode, the separated car chassis module, the whole machine in aircraft mode, and the separated aircraft body module; the telescopic fixed boom is installed on the top of the airport hangar and is used to separate or dock the intelligent cockpit module with the car chassis module or the aircraft body module.

[0093] Furthermore, the telescopic fixed boom cooperates with the lifting intelligent transfer robot AGV to connect / separate the intelligent cockpit module with the car chassis module or the aircraft body module through positioning, moving, (lifting mechanism) lifting, docking, handling, fastening / releasing, automatically switching between car mode and aircraft mode.

[0094] See Figure 5 As shown, the telescopic fixed boom 5 is fixed to the top of the airport hangar and includes an automatic gripper 52B, a boom 51B, and a positioning system 51C. One end of the positioning system 51C is connected to the fixed seat and fixed to the top of the airport hangar, and the other end is connected to the boom; the boom 51B is a telescopic structure, and an automatic gripper 52B is installed at the bottom through a connecting block and can move up and down; the automatic gripper 52B includes a fixing plate and grippers; the fixing plate is perpendicularly installed to the boom, and two grippers are independently fixed at both ends of the fixing plate; the grippers can open and close to clamp the object to be lifted and are adapted to clamp with the boom clamping area 42A of the aircraft auxiliary module.

[0095] See Figure 6 As shown, the lifting intelligent car transfer robot AGV6 includes: a robot main body, a universal wheel 61A, a lifting mechanism 61B, a positioning device 61C, etc.

[0096] Specifically, the robot main body is a box structure, and a lifting mechanism 61B is installed in the middle of the upper end face. Four universal wheels 61A are independently installed at the bottom four end points of the lower end face; the positioning device 61C is installed on the side of the box structure for positioning; the lifting mechanism 61B includes a base, a lifting arm, and an end face. The base is fixedly installed on the upper surface of the robot main body structure; the lifting arm is cross-installed through a hinge, one end is at the base, and the other end is installed at the end face, and can move up and down under the action of a motor; connectors are installed at the four ends of the end face, and the connectors are used to dock and separate the intelligent cockpit module 1 from the car chassis module 2 and the intelligent cockpit module 1 from the aircraft body module 3.

[0097] See Figure 6As shown, when the connecting piece is used to dock and separate the intelligent cockpit module 1 and the vehicle chassis module 2, the connecting piece includes a base 62D, a first docking groove 62A, and a second docking mechanism 62B; the first docking groove 62A is installed on one side of the upper end surface of the base 62D, and its structure is a regular quadrangular pyramid structure, which is adapted in shape, size, quantity, and position to the corresponding inverted quadrangular pyramid structure positioning block; the second docking mechanism 62B is installed on one side of the first docking groove 62A, and can be an Automatic Screw Feeding and Driving System, which is used to automatically screw-connect with the through holes to be connected through bolts.

[0098] Figure 7 As shown, it is an intelligent aircraft handling robot, including a robot main body, a second universal wheel 71A, a second lifting mechanism 71B, a second positioning device 71C, etc. Among them, the designs of the robot main body, the second universal wheel 71A, the second lifting mechanism 71B, and the second positioning device 71C are Figure 6 the same as those of the intelligent vehicle handling robot in [reference], and this part will not be elaborated here. Only the connecting pieces are different, as follows:

[0099] The connecting piece of the intelligent aircraft handling robot only includes a base and a second docking groove 72A. The second docking groove 72A is installed on the upper end of the base through a support rod, and the opened slot is adapted in position, shape, and size to the third positioning block 32C of the aircraft body module 3 for installation.

[0100] Through Figure 6 - Figure 7 As shown, the connection or separation between the intelligent cockpit module 1 and the vehicle chassis module 2 adopts a threaded fastening and release mechanism, that is, through the cooperation of bolts and an automatic screw locking machine, connection and separation are realized. The threaded fastening and release mechanism has a simple and reliable structure, high connection strength, and good durability and maintainability.

[0101] In the present invention, the mode-switchable system further includes a positioning system. Specifically, through one or more positioning technologies such as Wi-Fi positioning, Bluetooth Beacons, or Ultra-Wideband (UWB), the intelligent cockpit module 1, the vehicle chassis module 2, the aircraft body module 3, the boom, and the lifting intelligent handling robot AGV can locate each other.

[0102] As a specific implementation manner of the present invention, the positions of the intelligent cockpit module 1, the vehicle chassis module 2, the aircraft body module 3, and the boom are relatively fixed and stationary during docking / release.

[0103] As another specific embodiment of the present invention, the lifting intelligent transport robot AGV moves autonomously to the bottom of the intelligent cockpit module 1, the automobile chassis module 2, the aircraft body module 3 or the fixed boom through electromagnetic guidance, magnetic tape guidance, or QR code guidance plus inertial navigation.

[0104] As another specific embodiment of the present invention, the lifting intelligent transport robot AGV is also communicatively connected with the boom, the intelligent cockpit module 1, the automobile chassis module 2, and the aircraft body module 3. The lifting intelligent transport robot AGV can receive position signals emitted by the fixed boom, the intelligent cockpit module 1, the automobile chassis module 2, and the aircraft body module 3 in real time, thereby increasing the automatic docking accuracy of the lifting intelligent transport robot AGV with the boom, the intelligent cockpit module 1, the automobile chassis module 2, and the aircraft body module 3.

[0105] As another specific embodiment of the present invention, the lifting-type intelligent transport robot AGV is divided into a lifting-type intelligent automobile transport robot AGV and a lifting-type intelligent aircraft transport robot AGV, both of which have the functions of positioning, moving, lifting / docking, but their lifting height, lifting weight, lifting mechanism position, docking groove shape, etc. are all different.

[0106] Example 1

[0107] In the present invention, the docking mechanism 2 62B of the intelligent automobile handling robot AGV, such as an automatic screw locking machine, and the docking mechanism 1 32B of the aircraft body module 3, such as an automatic screw locking machine, which is arranged horizontally on the docking surface, have the same function, the same size, and similar effect.

[0108] The similarities are that the intelligent cockpit module 1 and the automobile chassis module 2 or the aircraft body module 3 can be connected, tightened or released by bolts. The difference is that the bolts of the docking mechanism 32B (automatic screw locking machine) of the aircraft body module 3 are mechanically connected to the drive assembly, and the two are (mechanically) connected as one, and the bolts are directly connected to the connection mechanism 12B at the bottom of the intelligent cockpit module 1, without other connection components or mechanisms. The bolts and drive assembly of the automatic screw locking machine of the intelligent automobile handling robot AGV are only connected by magnetic force (not integrated), and with the help of the drive assembly, the bolts directly penetrate the connection hole 22B of the automobile chassis module and connect to the connection mechanism 12B at the bottom of the intelligent cockpit module 1.

[0109] When the smart cockpit module 1 and the vehicle chassis module 2 are connected and tightened, the bolts will be separated from the drive assembly. When the smart cockpit module 1 and the vehicle chassis module 2 are separated by releasing the bolts, the drive assembly will be separated from the smart cockpit module and the vehicle chassis module with the bolts.

[0110] The bolt holes of the bottom connecting mechanism 12B of the intelligent cockpit module 1 and the internal threads of the connecting holes 22B passing through the vehicle chassis module 2 are the same, continuous, and connected, enabling the threaded fasteners to be smooth when released or tightened without jamming.

[0111] The relative positions of the bottom positioning blocks 12C of the intelligent cockpit module 1 and the connecting mechanism 12B are fixed (and the distances are the same), the relative positions of the top fixing grooves 22A and the connecting holes 22B of the vehicle chassis module 2 are fixed, the relative positions of the top fixing grooves 32A of the docking surface of the aircraft body module 3 and the docking mechanism 32B are fixed, and the relative positions of the docking grooves 62 of the intelligent vehicle handling robot AGV and the automatic screw locking machine 62B are fixed, and the center point distances between each pair are the same.

[0112] When the positioning block is successfully docked with the fixing groove / docking groove, the connecting mechanism, the connecting hole, and the docking mechanism are automatically aligned.

[0113] Embodiment 2

[0114] The full working process of the morphing flying car in the present invention with the help of the mode switching system includes:

[0115] See Figure 8-1 As shown, in the car mode, after the user parks the whole vehicle at a designated position near the entrance of the general airport hangar, the user turns off the engine and leaves the vehicle. Under the command of the mode switching system, the intelligent vehicle handling robot AGV communicates with the vehicle chassis module, accurately positions through its own positioning device and the positioning device of the vehicle chassis module, and autonomously and precisely moves under the vehicle chassis module in the car mode.

[0116] There are also four inverted frustum-shaped positioning blocks 22C protruding from the bottom corners of the vehicle chassis module, which are adapted to the shape of the docking groove 62A at the top of the lifting mechanism of the intelligent vehicle handling robot AGV. The lifting mechanism of the intelligent vehicle handling robot AGV rises, and the docking groove 62A at the top of the lifting mechanism docks with the inverted frustum-shaped positioning block 22C protruding from the bottom of the vehicle chassis module. After the docking is completed, the lifting mechanism continues to rise to lift the whole vehicle (tires) in the car mode off the ground to a set height. Under the action of gravity, the inverted frustum-shaped positioning block 22C protruding from the chassis is accurately docked and limited with the docking groove 62A at the top of the lifting mechanism of the intelligent vehicle handling robot AGV.

[0117] See Figure 8-2 As shown, under the command of the mode switching system, the intelligent vehicle handling robot AGV communicates with the fixed boom, accurately positions through its own positioning device and the positioning device of the fixed boom, and autonomously and precisely moves while holding the whole vehicle in the car mode under the fixed boom.

[0118] The lifting mechanism of the intelligent vehicle handling robot AGV continues to lift until the set height is reached.

[0119] See Figure 8-3 As shown, an automatic gripper 52B is provided at the bottom of the telescopic fixed suspension rod, and the automatic gripper 52B grips the suspension rod clamping area 42A at the top of the flight assistance module. A card slot 41C for docking with the luggage rack at the top of the intelligent cockpit module is provided at the bottom of the flight assistance module, and an automatic pin fixing system 42B is provided at the four corners.

[0120] After the telescopic fixed suspension rod is lowered to the set height, the card slot at the bottom of the flight assistance module docks with the luggage rack at the top of the intelligent cockpit module, and the automatic pin fixing system 42B at the four corners of the bottom of the flight assistance module automatically inserts and locks the luggage rack. The bottom of the flight assistance module 3 and the top of the intelligent cockpit module 1 are as closely fitted as possible to reduce drag and wind noise during flight.

[0121] After the automatic pin fixing system 42B of the flight assistance module locks the luggage rack at the top of the intelligent cockpit module 1, each associated system between the intelligent cockpit module and the vehicle chassis module is automatically separated one by one, including but not limited to: the electrical components such as the power system of the intelligent cockpit module are automatically separated from the corresponding system of the vehicle chassis module. The steering wheel inside the intelligent cockpit module automatically retracts into the driver's console to increase the space of the intelligent cockpit module. The automatic cover 11C at the bottom of the intelligent cockpit module closes.

[0122] The suspension rod grips the flight assistance module, and the flight assistance module locks the intelligent cockpit module 1. The intelligent vehicle handling robot AGV holds up the vehicle chassis module 2, and the intelligent cockpit module 1 and the vehicle chassis module 2 are connected together by bolts.

[0123] The docking mechanism two 62B of the intelligent vehicle handling robot AGV, for example, can be an automatic screw locking machine to rise and release the bolts connecting the intelligent cockpit module 1 and the vehicle chassis module 2. The nuts of the bolts connecting the intelligent cockpit module 1 and the vehicle chassis module 2 contain magnetism, and the unscrewed bolts will automatically be received into the sleeve of the docking mechanism two 62B, for example, an automatic screw locking machine. The docking mechanism two 62B of the intelligent vehicle handling robot AGV, for example, can be an automatic screw locking machine to lower to the set height.

[0124] The lifting mechanism of the intelligent vehicle handling robot AGV descends to the set height, and the vehicle chassis module 2 is completely separated from the intelligent cockpit module 1 under the action of gravity.

[0125] See Figure 8-4 As shown, the intelligent vehicle handling robot AGV holds up the vehicle chassis module 2 and moves it to the vehicle chassis module self-inspection area for self-inspection in preparation for the next use.

[0126] See Figure 8-5As shown, the boom clamps the flight assistance module, the flight assistance module locks the intelligent cockpit module 1, and the fixed boom rises to a set height. The intelligent aircraft handling robot AGV lifts the aircraft body module 3 (the landing gear is in the open state at this time) to the fixed boom.

[0127] See Figure 8-6 As shown, the lifting mechanism of the intelligent aircraft handling robot AGV rises, and the second fixing groove 32A on the top of the aircraft body module 3 is docked with the second inverted quadrangular platform positioning block 22C protruding from the bottom of the intelligent cockpit module.

[0128] The docking mechanism 62B inside the aircraft body module 3 can be, for example, raised by an automatic screw lock, and the top of the docking mechanism has bolts, which are connected and fastened with the connecting mechanism 12B of the smart cockpit module 1. After the smart cockpit module 1 is connected and fastened with the aircraft body module 3, each associated system of the smart cockpit module 1 and each associated system of the aircraft body module 3 are automatically connected one by one, including but not limited to: electrical connection, which can supply power to the smart cockpit module; communication connection, real-time transmission of relevant data, including: speed, mileage, remaining energy, energy consumption, endurance, etc.

[0129] Then, the automatic clamp 52B at the bottom of the boom is released; the boom rises to a set height (without affecting the movement of the entire machine in the airplane mode held by the intelligent aircraft handling robot AGV).

[0130] like Figure 8-7 As shown, the intelligent aircraft handling robot AGV lifts the entire aircraft in aircraft mode and moves it to a fixed position near the hangar exit.

[0131] like Figure 8-8 As shown, the lifting mechanism of the intelligent aircraft handling robot AGV is lowered to the set height, and the whole machine in the aircraft mode stands on the ground relying on the landing gear. The intelligent aircraft handling robot AGV automatically moves to the work waiting area and waits for the next work.

[0132] The user boards the plane with the help of the staff (using the boarding stairs). After boarding is completed, the plane automatically drives to the runway and prepares to take off. It should be noted that with the help of the mode switching system, switching from airplane mode to car mode, or replacing a chassis of different nature for car mode, is similar to the process of switching from car mode to airplane mode, which will not be described in detail here.

[0133] The above-mentioned embodiments only express several implementation methods of the present invention, and the descriptions thereof are relatively specific and detailed, but they cannot be understood as limiting the scope of the invention patent. It should be pointed out that, for ordinary technicians in this field, several variations and improvements can be made without departing from the concept of the present invention, and these all belong to the protection scope of the present invention. Therefore, the protection scope of the patent of the present invention shall be subject to the attached claims.

Claims

1. A fixed-wing flying car with switchable configurations that can be used for inter-city navigation, characterized by: The invention comprises an intelligent cockpit module (1), an automobile chassis module (2), and an aircraft body module (3); the switchable form comprises two modes, namely, an automobile mode and an aircraft mode; the automobile mode comprises an intelligent cockpit module (1) and an automobile chassis module (2); the aircraft mode comprises an intelligent cockpit module (1) and an aircraft body module (3); wherein the bottom of the intelligent cockpit module (1) is detachably connected to the automobile chassis module (2), and the bottom of the intelligent cockpit module (1) is detachably connected to the aircraft body module (3).

2. The fixed-wing switchable flying car for inter-city navigation according to claim 1 is characterized in that: The car mode is an electric car with 4 to 7 seats, which can be driven automatically or manually. The airplane mode is a fixed-wing propeller or jet aircraft used for inter-city navigation, which can be driven automatically or remotely.

3. The fixed-wing switchable flying car for inter-city navigation according to claim 1 is characterized in that: It also includes a flight assistance module, which is detachably connected to the top of the smart cockpit module, and the flight assistance module includes a parachute.

4. The fixed-wing switchable flying car for inter-city navigation according to claim 1 or 2, characterized in that: In car mode, the user drives the car to the general airport and parks in the designated area at the hangar door of the general airport; after the user leaves, the mode switching system automatically separates the smart cockpit module from the car chassis module, and then the smart cockpit module docks with the aircraft body module to switch to airplane mode; in airplane mode, the user takes an airplane to the destination general airport and parks in the designated area at the hangar door of the general airport; after the user leaves, the mode switching system automatically separates the smart cockpit module from the aircraft body module, and then the smart cockpit module docks with the car chassis module to switch to car mode.

5. The fixed-wing switchable flying car for inter-city navigation according to claim 1 is characterized in that: The invention comprises a connecting mechanism, a docking mechanism and a connecting hole, all of which are provided in plurality; wherein the connecting mechanism is a block structure with an internal thread opening, and the docking mechanism is an axial structure with an internal thread opening protruding from the outer side surface of the block structure; the connecting hole is a hole with an internal thread opening; the connecting mechanism and the connecting hole are installed at the bottom of the intelligent cockpit module (1) and on the chassis of the automobile chassis module (2) in a matching manner in terms of quantity and position, so as to complete the detachable connection between the intelligent cockpit module (1) and the automobile chassis module (2); the connecting mechanism and the docking mechanism are independently installed at the bottom of the intelligent cockpit module (1) and on the inner side of the cabin of the aircraft body module (3), so as to complete the detachable connection between the intelligent cockpit module (1) and the aircraft body module (3) in a matching manner in terms of quantity and position.

6. The fixed-wing switchable flying car for inter-city navigation according to claim 5 is characterized in that: It also includes a plurality of positioning blocks and a plurality of fixing grooves, wherein one positioning block and one fixing groove, or one positioning block or one fixing groove is installed on one side of a connecting mechanism or a docking mechanism, and is used to assist in the initial alignment of the connecting mechanism and the docking mechanism, and the initial alignment of the connecting mechanism and the connecting hole; When the connection mechanism and the docking mechanism, the connection mechanism and the connection hole are accurately positioned by bolt connection, there is no need to perform initial alignment of the positioning block, the fixing groove, the positioning block and the fixing groove.

7. The fixed-wing switchable flying car for inter-city navigation according to claim 1 is characterized in that: The smart cockpit module includes: steering system, seats, entertainment system, power system, and luggage rack; the automobile chassis module includes a frame, steering system, driving system, braking system, battery power system, and Beidou satellite navigation system; the aircraft body module includes a fuselage, wings, tail, landing gear, power unit, and positioning monitoring system, wherein the positioning monitoring system includes at least one of radar, ADS-B, and ADS-C.

8. A mode switchable system for a fixed-wing flying car with switchable form that can be used for inter-city navigation, characterized by: The mode-switchable system is used for switching between two modes of the fixed-wing switchable flying car described in any one of claims 1 to 7, and comprises a lifting-type intelligent transport robot AGV and a retractable fixed boom; the lifting-type intelligent transport robot AGV is used for positioning, moving, docking, transporting and lifting the whole vehicle and the separated automobile chassis module in automobile mode, and the whole vehicle and the separated aircraft fuselage module in airplane mode; the retractable fixed boom is installed on the top of the airport hangar, and is used to separate or dock the intelligent cockpit module with the automobile chassis module or the aircraft fuselage module; when the positioning of the intelligent transport robot is sufficiently accurate, the positioning block and / or the fixing groove are not used for initial alignment.

9. A mode switchable system for a fixed-wing switchable flying car that can be used for inter-city navigation according to claim 8, characterized in that: The lifting-type intelligent handling robot AGV includes an intelligent automobile handling robot AGV and an intelligent aircraft handling robot AGV; the intelligent automobile handling robot AGV is used to dock or separate the intelligent cockpit module and the automobile chassis module, and also includes an automatic screw locking machine for automatically screwing in or out the screws during docking or separation; the intelligent aircraft handling robot AGV is used for handling and lifting the aircraft body module in the aircraft mode as a whole or in a separated state.

10. According to claim 8, a mode switchable system for a fixed-wing switchable flying car that can be used for inter-city navigation is characterized by: The retractable fixed boom includes an automatic clamp, a boom, and a positioning system. One end of the positioning system is connected to a fixed seat and fixed on the top of an airport hangar, and the other end is connected to the boom. The boom is a retractable structure, and an automatic clamp is installed at the bottom through a connecting block, which can move up and down. The automatic clamp includes a fixed plate and a clamp. The fixed plate is installed vertically to the boom, and two clamps are independently fixed at both ends of the fixed plate. The clamp can be opened and closed to clamp objects to be lifted.

Images