CN114852331A - Manned flying automobile with form intelligence - Google Patents
Manned flying automobile with form intelligence Download PDFInfo
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- CN114852331A CN114852331A CN202210678769.3A CN202210678769A CN114852331A CN 114852331 A CN114852331 A CN 114852331A CN 202210678769 A CN202210678769 A CN 202210678769A CN 114852331 A CN114852331 A CN 114852331A
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- 238000013461 design Methods 0.000 claims abstract description 22
- 230000004927 fusion Effects 0.000 claims abstract description 19
- 238000013016 damping Methods 0.000 claims abstract description 9
- 239000000725 suspension Substances 0.000 claims abstract description 9
- 238000006073 displacement reaction Methods 0.000 claims abstract description 4
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 17
- 239000004917 carbon fiber Substances 0.000 claims description 17
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 17
- 229910000838 Al alloy Inorganic materials 0.000 claims description 13
- 230000001681 protective effect Effects 0.000 claims description 10
- 230000003014 reinforcing effect Effects 0.000 claims description 5
- 239000012780 transparent material Substances 0.000 claims description 4
- 239000011521 glass Substances 0.000 claims description 3
- 230000002349 favourable effect Effects 0.000 claims description 2
- 230000006872 improvement Effects 0.000 description 9
- 238000005265 energy consumption Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000013585 weight reducing agent Substances 0.000 description 4
- 229910000851 Alloy steel Inorganic materials 0.000 description 3
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 3
- 230000007547 defect Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 230000010354 integration Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000004134 energy conservation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 230000000877 morphologic effect Effects 0.000 description 1
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- 230000004083 survival effect Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C37/00—Convertible aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
Abstract
The invention relates to the technical field of hovercars, in particular to a manned hovercar with intelligent form, wherein the hovercar adopts a flight driving fusion frame design with an integrated topological structure, a main flight structure adopts a multi-rotor type layout and a four-shaft eight-propeller aircraft structure, and a ground driving structure adopts an Ackerman steering and Macpherson suspension damping type chassis structure; judging based on signals acquired by a laser displacement sensor deployed on the flying automobile, and starting flying operation of the flying automobile when the ground runs and is congested; and after the flight operation is finished, the aerocar performs landing operation, and after the landing operation is finished, the aerocar starts ground driving operation.
Description
Technical Field
The invention relates to the technical field of aerocars, in particular to a manned aerocar with intelligent form.
Background
The most obvious difference between the flying automobile and the common automobile is that the flying automobile has the function of flying in the air. With the rise of urban air traffic concepts in recent years, an electric vertical take-off and landing aircraft which is used for solving the problem of urban traffic congestion and only has an air flight function is also called a flying car, and the connotation of the flying car concept is expanded to be a carrier with an air-ground amphibious function or used for urban air traffic.
The prior technical scheme comprises the following steps:
due to the development of modern science and technology, the aerocar can be mainly divided into three categories, namely a folding wing aerocar, a multi-rotor aerocar and a self-rotor aerocar.
1. The aerocar taking off and landing vertically adopts a foldable wing design. When the automobile runs on a highway, the wings can be folded at two sides of the automobile body, the propellers are folded in the fairing, and the automobile can run on the highway like a common civil automobile. In flight mode, the wings and propellers are deployed. The wheels are contracted in the fairing inside the vehicle body, so that the resistance of the wheels during flying is reduced. The flight mode employs the principles of tiltrotor aircraft. During taking off, the double engines are in certain included angle with the horizontal line, so that the double engines can take off and land vertically, and after reaching a certain height, the double engines are gradually rotated to be horizontal to provide continuous power. In addition, the vertical take-off and landing function is realized, the safety coefficient is higher, and the requirement on a take-off field of a road surface is low. But adopt the rotor structure that verts to lead to its cost higher, energy consumption than greatly increased, use cost is high, and is fit for the masses little.
2. The multi-rotor type aerocar adopts the principle of external symmetrical propellers, offsets torque force while providing enough lift force, has the capability of vertical take-off and landing, and is not limited to take-off and landing fields any more. The unmanned aerial vehicle can fly by a planned air route in advance, the limitation on the operation capacity of passengers is low, the misoperation probability is low, and the safety is high. But compared with other flying automobiles, the flying automobile has the advantages of high use cost, low speed, large energy consumption, small voyage and high maintenance cost. Is only suitable for traffic in a small range and short distance
3. The design of the self-rotor aerodyne integrates the functions of an automobile and a motorcycle, and the self-rotor aerodyne can normally run on a road after being folded. After the rotor wing is unfolded, thrust is provided through the propeller at the tail of the collective body, the self-rotating rotor wing rotates to generate lift force, and the running takeoff of 170m is needed. The novel automobile flight control device is high in flight speed and low in requirement on the field, meets the daily requirement of people on automobiles and flight, and has certain practicability. But does not have hovering capability, a vertical take-off and landing function.
In addition, the existing flying automobile has the defects of high manufacturing cost, greatly increased energy consumption ratio, high use cost, small application range and heavy weight due to the limitation of design and technology, cannot meet the requirement of complex scene landing, and has no way of passing through complex terrains in mountains and countries when executing specific tasks, so that the existing flying automobile cannot be effectively applied to the field of military.
Disclosure of Invention
The existing aerocar has the defects of high manufacturing cost, greatly increased energy consumption ratio, high use cost, small size and heavy weight due to the design and technical limitations, cannot meet the requirement of complex scene landing, and has no way of passing through mountains and rural complex terrains when executing a specific task, so that the aerocar cannot be effectively applied to the military field.
The invention aims to overcome the defects of the prior art and provides a manned aerocar with intelligent form. The flying automobile adopts a flying driving fusion frame design with an integrated topological structure, a main flying structure adopts an aircraft structure with multi-rotor type layout and four-shaft eight-propeller, and a ground driving structure adopts a chassis structure with Ackerman steering and Macpherson suspension damping modes; judging based on signals acquired by a laser displacement sensor deployed on the flying automobile, and starting flying operation of the flying automobile when the ground runs and is congested; and after the flight operation is finished, the aerocar performs landing operation, and after the landing operation is finished, the aerocar starts ground driving operation.
As an improvement of the manned aerocar, the fan-shaped expandable protection duct is arranged around the propeller, and comprises a fan-shaped expandable protection duct inner ring and a fan-shaped expandable protection duct outer ring which are connected through a slide rail, wherein the fan-shaped expandable protection duct inner ring is positioned on the inner side of the fan-shaped expandable protection duct outer ring.
As an improvement of the manned hovercar, when the hovercar starts flying operation and rises to a set height, the inner ring of the fan-shaped expandable protection duct rotates out of the outer ring of the fan-shaped expandable protection duct, so that the propeller is protected from being influenced by other objects and the pneumatic performance of the propeller is improved;
when the hovercar starts the landing operation and descends to the set height, the inner ring of the fan-shaped expandable protection duct rotates to enter the outer ring of the fan-shaped expandable protection duct, and the propeller executes the fixed position propeller stopping operation, so that the transverse size of the hovercar is shortened, and the hovercar is favorable for running in a single lane.
As an improvement of the manned flying automobile, the flying and driving fusion frame uses carbon fiber tubes as a frame, the carbon fiber tubes are connected through aviation aluminum alloy, and the chassis functional component and the covering piece are directly arranged on the frame.
As an improvement of the manned flying automobile, the flying driving fusion frame comprises an auxiliary frame body, wherein the auxiliary frame body is connected with an aviation aluminum alloy in a pin positioning and bolt locking mode through a carbon fiber pipe on a chassis in a Macpherson suspension damping mode.
As an improvement of the manned flying automobile, the flying and driving fusion frame comprises a frame body, and a triangular reinforcing rib carbon fiber pipe is connected with a linking point at the front lower part of the frame body.
As an improvement of the manned aerocar, the eight propellers are not arranged on the same plane, the front propeller is positioned below the front glass of the car body, and the rear propeller is positioned on the car body.
As an improvement of the manned aerocar, the layout of the motor power source of the aerocar adopts a non-square parallel non-coplanar central symmetry structure.
As an improvement of the manned aerocar, the aerocar comprises a roof window, an upper window and a lower window which are arranged on the left side and the right side, and the windows are made of transparent materials, such as but not limited to acrylic plates made of transparent materials.
Compared with the prior art, the invention has the advantages that:
1. aiming at complex terrains including but not limited to urban road surfaces and special road surface conditions, the aerocar provides a topological integration design of four shafts and eight propellers for vertical take-off and landing, and can overcome the problem that the existing aerocar is difficult to switch land and air; the fan-shaped expandable protective duct and fixed position propeller stopping solve the problem that the transverse dimension is too long to normally go on the road;
2. the aerocar can normally pass through a complex road surface in the process of ground driving, so that a driver can conveniently observe the surrounding environment and safely drive the aerocar in the process of ground driving, and the aerocar can be ensured to drive in a single lane of a normally paved road surface without hindering the driving of other vehicles by the ground driving;
3. the aerocar provided by the invention has the advantages of low manufacturing cost and light dead weight, and solves the weight reduction problem of the traditional aerocar design.
Drawings
FIG. 1 is a front view of a manned flying vehicle with form intelligence of the present invention;
FIG. 2 is a schematic view of the internal structure of the passenger flying vehicle of the present invention.
Reference numerals
1. Fan-shaped expandable protection culvert inner ring 2 and fan-shaped expandable protection culvert outer ring
3. Battery box 4, screw
5. Vehicle door 6 and driving seat
7. Steering 8, chassis
9. Left rear upper window 10 and door upper window
11. Roof window 12, left front upper window
13. Right front rotor 14, left front rotor
15. Right rear rotor wing 16, left rear rotor wing
17. Left lower window 18 and carbon fiber tube
19. Aviation aluminum alloy connecting piece 20 and bolt
21. Triangular reinforcing rib carbon fiber pipe
Detailed Description
The invention mainly adopts the conventional layout of multiple rotors, adopts a four-shaft eight-propeller aircraft structure as a main flight structure, and runs on the ground in a chassis type topological fusion structure in the forms of Ackermann steering and Macpherson suspension damping. In order to facilitate the observation and safe driving of a driver to the surrounding environment during ground driving, the flying motor power source layout adopts a non-square parallel different-plane central symmetry structure. The fan-shaped expandable protective duct is adopted around the propeller; when the vehicle runs on the ground, the transverse size is shortened by adopting a fixed-position propeller-stopping method.
The technical solution of the present invention is described in detail below with reference to the accompanying drawings and examples.
Examples
As shown in fig. 1, the embodiment of the present invention provides a manned flying car with form intelligence. The invention mainly explains a fan-shaped expandable protection duct, fixed propeller and topology fusion frame structure with intelligent form, and solves 2 technical problems in an intelligent form.
1. Intelligent-fan-shaped expandable protection duct
The intelligent detection sensor is applied to the flying vehicle, so that manual operation and control can be reduced, the automation control degree is increased, and the convenience in the aspect of operation and control is improved. The intelligent control system is based on the laser displacement sensor, and judges the distance from the front propeller to the ground according to the action characteristics of the front propeller close to and far from the ground so as to realize the corresponding intelligent control of the fan-shaped expandable protection duct on the propeller. When the aerocar driven on the ground is jammed and rises for 2 meters after the flight mode is implemented, the fan-shaped expandable protection duct rotates out of the inner channel to form a closed loop with the inner channel, thereby protecting the propeller and simultaneously improving the pneumatic performance. After the flight operation of the flying automobile is finished, the descending operation is carried out, and when the distance between the fan-shaped expandable protective duct and the ground is 2 meters, the fan-shaped expandable protective duct can rotate to enter the inner duct so as to avoid friction with other vehicles on the road.
The circumference of the propeller 4 adopts a fan-shaped expandable protection duct design; the fan-shaped expandable protection culvert inner ring 1 is connected with the fan-shaped expandable protection culvert outer ring 2 through a slide rail, and the fan-shaped expandable protection culvert inner ring 1 is positioned on the inner side of the fan-shaped expandable protection culvert outer ring 2.
The shape intelligence of protection duct:
when the vehicle is driven on the ground, the fan-shaped expandable protective culvert inner ring 1 rotates to enter the fan-shaped expandable protective culvert outer ring 2, so that the ground trafficability is improved, the transverse size is shortened, the vehicle can be ensured to run in a single lane of a normal pavement road surface when the vehicle runs on the ground, the running of other vehicles is not hindered, the transportation difficulty is reduced after the vehicle is rotatably stored, the transportation cost is obviously reduced, the size of a die opening is reduced, and the processing difficulty is reduced; when the aircraft drives in the air, after the fan-shaped expandable protection duct inner ring 1 rotates out of the fan-shaped expandable protection duct outer ring 2, the propeller is protected from being influenced by other objects, the propeller can generate larger lift force, and the pneumatic performance is improved.
2. Form intelligence-fixed position oar stopping
When the vehicle runs on the ground, the fan-shaped expandable protection duct inner ring 1 rotates to enter the fan-shaped expandable protection duct outer ring 2, and then the propeller 4 performs fixed-position propeller stopping operation, so that the ground trafficability is improved, the transverse size is shortened, and the vehicle can run in a single lane of a normally paved road surface when running on the ground.
3. Morphological intelligence-topology fusion frame structure
FIG. 2 is a schematic view of the internal structure of the passenger flying vehicle of the present invention.
Because large aircraft have higher requirements on structural strength and rigidity and are extremely sensitive to weight, the chassis of the conventional vehicle is usually designed to have higher weight for ensuring driving comfort and reliability. The topology fusion frame structure adopts the scheme that a main carbon fiber tube is connected with aviation aluminum alloy and local aluminum alloy or alloy steel is welded, and an original chassis functional component, a covering piece and the like are directly arranged on a frame. The upper part of the front rotor wing can shield the sight of the driver for land driving and air operation, so the lower part is arranged; the rear rotor wing is arranged downwards, influences the observation visual field of a rearview mirror of a driver when driving on the ground, and is arranged upwards. Thus a design with front rotor below and rear rotor above results. Along with the improvement of the national requirements on energy conservation and emission reduction, how to apply an advanced structural design technology to carry out structural design on the frame is to realize the weight reduction and the light weight of the frame, so that the increasingly strict national regulation requirements and the lifting force are met, and the method becomes a key factor for the survival of future automobile factories.
In order to better realize the weight reduction task in the lightweight design, the invention abandons the traditional automobile chassis and flight frame in the overall design and designs a new flight driving fusion frame structure. The novel fusion vehicle frame adopts an integrated topological structure, the conventional layout of multiple rotors is mainly adopted, a four-shaft eight-propeller aircraft structure is used as a main flight structure, the Ackerman steering 7 and the McPherson suspension damping type chassis 8 are mainly used for ground running, a scheme that a main carbon fiber pipe is connected with aviation aluminum alloy and local aluminum alloy or alloy steel is welded is adopted, and the vehicle frame is connected through the aviation aluminum alloy by using the carbon fiber pipe as a frame. The original chassis functional assembly, the covering part and the like are directly arranged on the frame. In addition, in order to facilitate the observation and safe driving of the surrounding environment by a driver during ground driving, the flying motor power source layout adopts a non-square parallel different-plane central symmetry structure.
The utility model provides a topology fuses frame structure, includes sub vehicle frame body, frame structure hangs 17 (can increase and decrease according to actual need) carbon fiber tubes 18 and aviation aluminum alloy 19 and is connected with the mode of bolt 20 locking with the pin location on the chassis 8 of shock attenuation form by McPherson. The frame is characterized by further comprising a stable triangular reinforcing rib carbon fiber tube 21 structure formed by connecting partial link points on the body, wherein the crossed reinforcing rib structure is arranged at the front lower part of the frame body. The motor of the frame body is supported by the motor support and is connected with the carbon fiber tube through bolts. The frame considers the view safety when the vehicle drives and flies on the ground, and the propellers of the four-shaft eight-propeller aerocar are not arranged on the same plane, but are designed in such a way that the front propeller is arranged from the bottom to the top along with the rear propeller. The front propeller position is positioned under the front glass of the vehicle body in consideration of the reason that the view of the driver is limited. The rear part is positioned at the upper part of the vehicle body in consideration of the problem that the vehicle body collides with a coming vehicle behind.
Because the flying automobile considers the flying requirement, the roof adopts a transparent acrylic plate roof window 11; because the windows on the side of the vehicle body are not limited to the left rear upper window 9 and the left front upper window 12 on the upper part in flight requirements, the lower parts of the windows are also designed into the left lower window 17 and the right lower window (which are not marked in the figure due to the view angle) of the acrylic plate made of transparent materials, and the driving experience is better and the safety is higher.
The invention mainly adopts the conventional layout of multiple rotors, adopts a four-shaft eight-propeller aircraft structure as a main flight structure, and runs on the ground in a chassis type topological fusion structure in the forms of Ackermann steering and Macpherson suspension damping. The flying motor power source layout adopts a non-square parallel non-planar central symmetrical structure, and fan-shaped expandable protection ducts and fixed propellers are arranged around the propellers.
Aiming at the fan-shaped expandable protection duct, the protection duct can be realized by folding the outer propeller cover to the upper part or the lower part of the inner propeller cover along the propeller core, but the stability is poor.
The fixed paddle and the frame part have no alternative scheme temporarily.
The key points of the invention are as follows:
a hovercar with a fixed stop position, which combines a fan-shaped expandable protection duct and a topological fusion frame. In order to reduce the weight of the flying automobile, the key points and points to be protected for the safe and comfortable driving vision and feeling of a driver are as follows:
1. form intelligence-fan-shaped expandable protection duct:
the circumference of the propeller 4 adopts a fan-shaped expandable protection duct design; when the vehicle is driven on the ground, the fan-shaped expandable protective culvert inner ring 1 rotates to enter the fan-shaped expandable protective culvert outer ring 2, so that the ground trafficability is improved, the transverse size is shortened, the vehicle can be ensured to run in a single lane of a normal pavement road surface when the vehicle runs on the ground, the running of other vehicles is not hindered, the transportation difficulty is reduced after the vehicle is rotatably stored, the transportation cost is obviously reduced, the size of a die opening is reduced, and the processing difficulty is reduced; when the aircraft drives in the air, after the fan-shaped expandable protection duct inner ring 1 rotates out of the fan-shaped expandable protection duct outer ring 2, the propeller is protected from being influenced by other objects, the propeller can generate larger lift force, and the pneumatic performance is improved.
2. Morphology intelligence-fixed position feathering:
when the vehicle runs on the ground, the fan-shaped expandable protection duct inner ring 1 rotates to enter the fan-shaped expandable protection duct outer ring 2, and then the propeller 4 performs fixed-position propeller stopping operation, so that the ground trafficability is improved, the transverse size is shortened, and the vehicle can run in a single lane of a normally paved road surface when running on the ground.
3. Morphology intelligence-topology integration frame structure:
topology fuses frame structure, because large aircraft to structural strength and rigidity requirement higher, and extremely sensitive to the weight, traditional vehicle chassis often chooses the design of higher weight for the travelling comfort of assurance and reliability. In order to better realize the weight reduction task in the lightweight design, the invention abandons the traditional automobile chassis and flight frame in the overall design and designs a new flight driving fusion frame structure. The novel fusion frame adopts an integrated topological structure, the invention mainly adopts the conventional layout of multiple rotors, adopts a four-shaft eight-propeller aircraft structure as a main flight structure, mainly adopts Ackerman steering 7 and a Macpherson suspension damping type chassis 8 for ground running, adopts the scheme that a main carbon fiber pipe is connected with aviation aluminum alloy and local aluminum alloy or alloy steel is welded, and directly arranges an original chassis functional component, a covering piece and the like on the frame. In addition, in order to facilitate the observation and safe driving of the surrounding environment by a driver during ground driving, the flying motor power source layout adopts a non-square parallel different-plane central symmetry structure.
Finally, it should be noted that the above embodiments are only used for illustrating the technical solutions of the present invention and are not limited. Although the present invention has been described in detail with reference to the embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted without departing from the spirit and scope of the invention as defined in the appended claims.
Claims (9)
1. The manned flying automobile with the intelligent form is characterized in that the flying automobile adopts a flying and driving fusion frame design with an integrated topological structure, a main flying structure adopts an aircraft structure with multi-rotor type layout and four-shaft eight-propeller, and a ground driving structure adopts a chassis structure with Ackerman steering and Macpherson suspension damping forms; judging based on signals acquired by a laser displacement sensor deployed on the flying automobile, and starting flying operation of the flying automobile when the ground runs and is congested; and after the flight operation is finished, the aerocar performs landing operation, and after the landing operation is finished, the aerocar starts ground driving operation.
2. The manned aerocar with configuration intelligence according to claim 1, wherein the propeller is surrounded by a fan-shaped expandable protection duct, the design comprises a fan-shaped expandable protection duct inner ring (1) and a fan-shaped expandable protection duct outer ring (2) which are connected by a slide rail, and the fan-shaped expandable protection duct inner ring (1) is positioned at the inner side of the fan-shaped expandable protection duct outer ring (2).
3. The manned flying vehicle with configuration intelligence of claim 2,
when the hovercar starts flying operation and rises to a set height, the fan-shaped expandable protective duct inner ring (1) rotates out of the fan-shaped expandable protective duct outer ring (2) to protect the propeller (4) from being influenced by other objects and improve the pneumatic performance of the propeller (4);
when the hovercar starts the descending operation and descends to the set height, the fan-shaped expandable protection duct inner ring (1) rotates to enter the fan-shaped expandable protection duct outer ring (2), and the propeller (4) executes the fixed position propeller stopping operation, so that the transverse size of the hovercar is shortened, and the hovercar is favorable for running in a single lane.
4. The manned flying automobile with configuration intelligence of claim 1, wherein the flying and driving fusion frame uses carbon fiber tubes as a frame, the carbon fiber tubes are connected through aviation aluminum alloy, and the chassis functional component and the covering piece are directly arranged on the frame.
5. The manned flying vehicle with form intelligence of claim 4, wherein the flying drive fusion frame comprises a subframe body, and the subframe body is connected with an aviation aluminum alloy connecting piece (19) through a carbon fiber pipe (18) on a chassis (8) in a Macpherson suspension damping mode in a pin positioning and bolt (20) locking mode.
6. The manned flying vehicle with configuration intelligence of claim 4, wherein the flying-driving fusion frame comprises a frame body, and a triangular reinforcing rib carbon fiber pipe (21) is adopted at the front lower part of the frame body to connect with a linking point.
7. The manned flying vehicle with configuration intelligence of claim 1, wherein the eight propellers are not disposed on the same plane, the front propeller is located under the front glass of the vehicle body, and the rear propeller is located on the vehicle body.
8. The manned flying vehicle with configuration intelligence of claim 1, wherein the layout of the motor power source of the flying vehicle is a non-square parallel non-coplanar centrosymmetric structure.
9. The manned flying automobile with intelligent configuration according to claim 1, wherein the flying automobile comprises a top window, an upper window and a lower window on the left and right sides, and the windows are made of transparent materials.
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| CN202210678769.3A CN114852331A (en) | 2022-06-15 | 2022-06-15 | Manned flying automobile with form intelligence |
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| CN202210678769.3A CN114852331A (en) | 2022-06-15 | 2022-06-15 | Manned flying automobile with form intelligence |
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Application publication date: 20220805 |