CN115091905B - Electric flying car - Google Patents
Electric flying car Download PDFInfo
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- CN115091905B CN115091905B CN202210864688.2A CN202210864688A CN115091905B CN 115091905 B CN115091905 B CN 115091905B CN 202210864688 A CN202210864688 A CN 202210864688A CN 115091905 B CN115091905 B CN 115091905B
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- 238000005265 energy consumption Methods 0.000 claims description 6
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- 229910000838 Al alloy Inorganic materials 0.000 claims description 4
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- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 2
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Classifications
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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
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
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- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
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Abstract
The flying car can run on the ground and fly in the air, and becomes a novel vehicle capable of solving the problem of urban traffic jam and flexibly transporting people or goods. However, the existing flying automobile has high oil consumption or electricity consumption, high risk of medium-high altitude flying and large occupied space of Liu Hangshi wings. Therefore, the invention provides an electric flying automobile, which belongs to the technical field of vehicles and aviation, and comprises an automobile body, a battery system, a left automobile wing, a right automobile wing, an automobile wing upper connecting piece, a left propeller, a right propeller, a tail wing mounting bracket, a tail wing, a motor connecting arm, a folding wing rotating motor and the like, wherein the electric flying automobile has two modes of land running and ultra-low altitude flying: when flying, the wings extend, and the automobile is in the ground effect area; the wing is put into the body when the road is on the ground. The invention has the advantages of convenient folding of the wing, small occupied space of Liu Hangshi, energy conservation, high safety and the like, and has very wide application prospect.
Description
Technical Field
The invention relates to an electric aircraft based on foldable wings, in particular to an electric flying automobile, and belongs to the technical field of aviation and automobiles.
Background
With the progress of technology, the variety of vehicles has become a trend. The aerocar can run on the ground and fly in the air, so that the aerocar becomes a novel vehicle capable of solving the problem of urban traffic jam and flexibly transporting people or goods, and various enterprises and institutions at home and abroad are developing the research and development and engineering application work of the aerocar. The flying car is different according to the mode of taking off and landing, can divide into two kinds of vertical take off and landing and running take off and landing. The aerocar of vertical take off and landing is mostly similar with many rotor unmanned aerial vehicle, and take off and landing are nimble, and the accuse is easy to be controlled in the flight, but the flight speed is slow, and the flight energy consumption of cruising is high, and many rotors are difficult to lay when the car is on land moreover, influence ground function of traveling, make it be difficult to have with ordinary car the same ground stability and the operability of traveling. The landing-and-taking-off flying automobile can take off only by running on a road with a certain length, and has low energy consumption in cruising flight, but the space occupied by the folded wings is large. In addition, the existing aerocar is basically a medium-high altitude aerocar, flies at a height of hundreds of meters or kilometers, and can cause disastrous results once the aerocar breaks down, so that the requirements on the driving skills and psychological diathesis of a user are very high, and in addition, people generally worry about high altitude flight, so that the aerocar is difficult to popularize and apply. Moreover, the higher the flying height of the flying car, the greater the fuel consumption or electricity consumption, and the worse the economy.
The ground effect is a wonderful aerodynamic phenomenon, namely when a moving object is very close to the ground (or the water surface), the pressure difference between the upper surface and the lower surface of the object is increased, and the lifting force of the object is increased suddenly, so that the ground or sea flying can be realized. The electric ground effect flying automobile can travel on a ground road and realize ultra-low altitude flying below ten meters, and has the advantages of high safety, good economy, flexible and convenient use and very wide application prospect.
Disclosure of Invention
1. The invention aims to:
the invention aims to provide an electric flying car which can fly on land and can fly at ultra-low altitude based on the ground effect, and the wings can be folded so as to solve the problems of high risk, high energy consumption, poor economy, large occupied space of wings and the like of the existing flying car.
2. The technical scheme is as follows:
The invention relates to an electric flying car which is characterized by comprising the following parts: the automobile comprises an automobile body, a front automobile window, a battery system, a front wheel, a chassis system, a left automobile wing front section, a left automobile wing rear section, an automobile wing upper connecting piece, an automobile tail, a left propeller, an automobile tail mounting bracket, an automobile tail, a right propeller, a rear wheel, a right automobile wing, a roof, an automobile wing supporting rod connecting piece, a right automobile wing supporting rod, a hinging piece, a front swing arm, a transverse rotating shaft, a lower swing arm, a rear swing arm, a motor connecting arm, a folding wing rotating motor, a left automobile wing supporting rod, a right automobile wing front section and a right automobile wing rear section; the relationship between them is: the vehicle body is a main body bearing structure of the flying vehicle, and the battery system is positioned at the middle position of the bottom of the vehicle body; the left wing and the right wing are symmetrically arranged on two sides of the vehicle body, so that the left wing and the right wing are distinguished from each other in view of a driver; the left wing consists of a left wing front section, a left wing rear section, a wing upper connecting piece and a wing lower locking mechanism; the right wing consists of a right wing front section, a right wing rear section, a wing upper connecting piece and a wing lower locking mechanism; the tail wing is arranged on the tail of the car body through a tail wing mounting bracket; the left propeller and the right propeller are arranged at the tail of the vehicle; the wing strut connecting piece, the right wing strut, the hinge piece, the front swing arm, the transverse rotating shaft, the lower swing arm, the rear swing arm, the motor connecting arm, the folding wing rotating motor and the left wing strut are positioned in the vehicle body, and form a folding wing system of the aerocar together with the wing;
The electric flying automobile has two modes of land running and ultra-low altitude ground effect flying, and has the functions of automatic take-off and landing: when flying, the automobile is in a ground effect action area, the left wing and the right wing are in an extending state, lift force is provided for flying, and the flying automobile is pushed to advance in the air through rotation of the left propeller and the right propeller; when the vehicle runs on land, the rear part of the vehicle roof and the two sides of the rear part of the vehicle body shrink, the left wing and the right wing are folded around the upper connecting pieces of the respective wings along the central lines of the length directions of the wings, then the left wing stay bar and the right wing stay bar drive the left wing and the right wing to be folded and then put into the vehicle body, and meanwhile, the attack angle of the tail wing becomes negative, so that the air lift force of the vehicle is reduced, the downward pressure is increased, and the running stability is improved;
The body is a bearing type body, the body-in-white part is made of aluminum alloy materials, after being subjected to split-region die casting, the body-in-white part is assembled by punching and riveting, and the key bearing region is reinforced by using an internal adhesive fiber reinforced composite material layer so as to obtain a light high-strength body structure; the bottom of the automobile body is covered with a bottom guard plate made of engineering plastics, the outer surface of the bottom guard plate is used for protecting the impact of broken stones and the like on the ground, the inner surface of the bottom guard plate is provided with an air bag interlayer, and when the flying automobile falls off the ground in a runaway manner, the air bag at the bottom of the automobile body pops out of the interlayer and is used for buffering the impact force of the ground so as to protect the safety of members;
the front window is made of polymethyl methacrylate resin organic glass, and the middle and rear areas have a sliding opening function and are used for passengers to get on or off the vehicle;
The battery system comprises a battery module, a battery box, a heat dissipation system, a sensor, a relay, a wire harness and a battery management system; the upper cover and the lower box body of the battery box are of bearing structures and are integrated with the vehicle body and the chassis system so as to reduce parts of the flying vehicle; the vehicle wing is arranged on the upper cover of the battery box through a vehicle wing stay bar connecting piece;
The front wheel and the rear wheel are driven by the hub motor, the power of the hub motor is provided by the battery system, when the automobile runs on land, the running driving force is provided, when the automobile leaves the ground and enters a cruising flight state, the front wheel and the rear wheel are retracted and covered by the wheel covers, air turbulence and excitation are prevented from being generated near the wheels in the flight process, and air flow field disorders on two sides of the automobile body are prevented;
The left wing mainly plays roles in improving lift force and ensuring stable flying of an automobile, is of a combined structure, and is connected by a front section of the left wing and a rear section of the left wing through a connecting piece at the upper part of the wing; the front section of the left wing and the rear section of the left wing are made of carbon fiber or basalt fiber reinforced composite materials; the automobile is unfolded in a flight state, the front section of the left automobile wing and the rear section of the left automobile wing are fixed together through the locking mechanism at the lower part of the automobile wing, and the attack angle is 4 degrees during cruising flight, so that good energy consumption economy is obtained; when the vehicle runs on the ground, the locking mechanism at the lower part of the vehicle wing is opened, and the vehicle wing is folded;
the left propeller and the right propeller provide propulsion for the flight of the automobile and are made of carbon fiber reinforced composite materials so as to reduce the weight and improve the fatigue life;
The tail wing is made of carbon fiber reinforced composite materials so as to reduce weight and improve fatigue life; the tail wing mounting bracket is arranged at the tail part of the vehicle body, the upper part of the tail wing mounting bracket is of a V-shaped lifting structure, and the lower part of the tail wing mounting bracket is of an inner X-shaped rib matched with an outer concave frame structure so as to firmly support the tail wing; the tail wing has an automatic rotation function, the attack angle of the flight state is a positive value, enough lift force is obtained, and the economy of flight is improved; the attack angle of the tail wing in the land state is a negative value, so that enough downward pressure is obtained, and the stability of the land is improved;
The vehicle roof is made of fiber reinforced composite materials, and the rear part of the vehicle roof has a folding function, so that the space for folding the vehicle wings is increased;
One end of the right wing stay bar is connected with the front section of the right wing through a wing stay bar connecting piece, and the other end of the right wing stay bar is connected with the hinge piece; the folding wing rotating motor rotates, the driving motor connecting arm rotates to drive the lower swing arm, the front swing arm rotates around the transverse rotating shaft, and then the right wing supporting rod and the left wing supporting rod are driven to move, so that the folding or unfolding of the left wing and the right wing is realized.
3. Compared with the prior art, the electric flying car has the following advantages:
(1) The two-stage folding design is adopted for the wings at the two sides, so that the wings can be folded and then put into the vehicle body, the occupied space and parking space of the road are saved, and the running stability of the ground road can be improved;
(2) The ultra-low-altitude flight close to the ground or sea surface is realized by utilizing the ground effect, the flight height is low, the safety is better, the user cannot generate fear of falling in high altitude, the economy is good, and the energy consumed by climbing hundreds of meters or even thousands of meters of an airplane automobile is saved;
(3) The automobile body adopts aluminum alloy die casting to form, and structures such as a wing, a tail wing and the like adopt composite materials, so that the weight of the whole automobile is greatly reduced, the oil consumption or the electricity consumption is reduced, and the endurance mileage is increased.
In a word, the invention is an energy-saving and safe electric flying vehicle, can fly quickly in ultra-low altitude and also can run at high speed on a ground road, is a novel vehicle, and has wide application prospect.
Drawings
FIG. 1 is a three-dimensional perspective view of the present invention in flight;
FIG. 2 is a three-dimensional box plot of the flight status of the present invention;
FIG. 3 is a view showing a wing deployment state of the present invention;
Fig. 4 is a three-dimensional frame diagram of the ground running state of the present invention;
the symbols in the drawings are as follows:
1-vehicle body, 2-front window, 3-battery system, 4-front wheel, 5-chassis system, 6-left wing, 7-left wing front section, 8-left wing rear section, 9-upper wing connector, 10-rear, 11-left propeller, 12-rear mounting bracket, 13-rear wing, 14-right propeller, 15-rear wheel, 16-right wing, 17-roof, 18-wing strut connector, 19-right wing strut, 20-hinge, 21-front swing arm, 22-transverse shaft, 23-lower swing arm, 24-rear swing arm, 25-motor connector arm, 26-folding wing rotary motor, 27-left wing strut, 28-right wing front section, 29-right wing rear section.
Detailed Description
Embodiments of the invention are described in further detail below with reference to the attached drawing figures:
as shown in the accompanying drawings, the electric flying car of the invention comprises the following parts: a vehicle body 1, a front window 2, a battery system 3, a front wheel 4, a chassis system 5, a left wing 6, a left wing front section 7, a left wing rear section 8, a wing upper connector 9, a rear 10, a left propeller 11, a rear mounting bracket 12, a rear 13, a right propeller 14, a rear wheel 15, a right wing 16, a roof 17, a wing stay connector 18, a right wing stay 19, a hinge 20, a front swing arm 21, a lateral rotation shaft 22, a lower swing arm 23, a rear swing arm 24, a motor connecting arm 25, a folding wing rotating motor 26, a left wing stay 27, a right wing front section 28, a right wing rear section 29; the relationship between them is: the vehicle body 1 is a main body bearing structure of the flying vehicle, and the battery system 3 is positioned at the middle position of the bottom of the vehicle body 1; the left wing 6 and the right wing 16 are symmetrically arranged at both sides of the vehicle body 1 to distinguish left and right from each other in view of a driver; the left wing 6 consists of a left wing front section 7, a left wing rear section 8, a wing upper connecting piece 9 and a wing lower locking mechanism; the right wing 16 is composed of a right wing front section 28, a right wing rear section 29, a wing upper connecting piece 9 and a wing lower locking mechanism; the tail wing 13 is arranged on the tail 10 of the vehicle body 1 through a tail wing mounting bracket 12; the left propeller 11 and the right propeller 14 are mounted on the vehicle tail 10; the wing strut connector 18, the right wing strut 19, the hinge 20, the front swing arm 21, the transverse rotating shaft 22, the lower swing arm 23, the rear swing arm 24, the motor connecting arm 25, the folding wing rotating motor 26 and the left wing strut 27 are positioned in the vehicle body 1, and form a folding wing system of the aerocar together with the wing;
The automobile body 1 is a bearing type automobile body, the white automobile body part is made of aluminum alloy materials, is assembled by punching and riveting after being subjected to regional die casting, and is reinforced by using an internal adhesive fiber reinforced composite material layer in a key bearing region so as to obtain a light high-strength automobile body structure; the bottom of the automobile body is covered with a bottom guard plate made of engineering plastics, the outer surface of the bottom guard plate is used for protecting the impact of broken stones and the like on the ground, the inner surface of the bottom guard plate is provided with an air bag interlayer, and when the flying automobile falls off the ground in a runaway manner, the air bag at the bottom of the automobile body pops out of the interlayer and is used for buffering the impact force of the ground so as to protect the safety of members;
the front window 2 is made of polymethyl methacrylate resin organic glass, and the middle and rear areas have a sliding opening function and are used for passengers to get on or off the vehicle;
The battery system 3 comprises a battery module, a battery box, a heat dissipation system, a sensor, a relay, a wire harness and a battery management system; the upper cover and the lower box body of the battery box are of bearing structures and are integrated with the vehicle body 1 and the chassis system 5 so as to reduce parts of the flying vehicle; the wing is mounted on the upper cover of the battery box through a wing stay bar connecting piece 18;
The front wheel 4 and the rear wheel 15 are driven by a hub motor, the power of the hub motor is provided by the battery system 3, when the automobile runs on land, the running driving force is provided, when the automobile leaves the ground and enters a cruising flight state, the front wheel and the rear wheel are retracted and covered by a wheel cover, air turbulence and excitation are avoided being generated near the wheels in the flight process, and air flow field disorders on two sides of the automobile body are prevented;
the left wing 6 mainly plays a role in improving lifting force and ensuring stable flying of an automobile, has a combined structure and is connected with the left wing front section 7 and the left wing rear section 8 through a wing upper connecting piece 9; the left wing front section 7 and the left wing rear section 8 are made of carbon fiber or basalt fiber reinforced composite materials; the automobile is unfolded in a flight state, the front section 7 of the left automobile wing and the rear section 8 of the left automobile wing are fixed together through a locking mechanism at the lower part of the automobile wing, and the attack angle is 4 degrees during cruising flight, so that good energy consumption economy is obtained; when the vehicle runs on the ground, the locking mechanism at the lower part of the vehicle wing is opened, and the vehicle wing is folded;
the left propeller 11 and the right propeller 14 are used for providing propulsion for the flight of the automobile and are made of carbon fiber reinforced composite materials so as to reduce the weight and improve the fatigue life;
The tail wing 13 is made of carbon fiber reinforced composite materials, so that the weight is reduced, and the fatigue life is prolonged; the tail wing mounting bracket 12 is arranged at the tail part of the vehicle body 1, the upper part of the tail wing mounting bracket 12 is of a V-shaped lifting structure, and the lower part of the tail wing mounting bracket is of an inner X-shaped rib matched with an outer concave frame structure so as to firmly support the tail wing 13; the tail wing 13 has an automatic rotation function, the attack angle of the flight state is a positive value, enough lift force is obtained, and the economy of flight is improved; the attack angle of the tail 13 in the land state is a negative value, so that enough downward pressure is obtained, and the stability of the land is improved;
the roof 17 is made of fiber reinforced composite material, and the rear part has a folding function, so that the space for folding the wing is increased;
One end of the right wing stay 19 is connected with the right wing front section 28 through the wing stay connecting piece 18, and the other end is connected with the hinge piece 20; the folding wing rotating motor 26 rotates, the driving motor connecting arm 25 rotates to drive the lower swing arm 23 to rotate the front swing arm 21 around the transverse rotating shaft 22, and then the right wing stay 19 and the left wing stay 27 are driven to move, so that the left wing 6 and the right wing 16 are folded or unfolded;
As shown in the attached drawings, the electric flying automobile has two modes of land running and ultra-low altitude ground effect flying, and has the functions of automatic take-off and landing: when flying, the automobile is in a ground effect action area, the left wing 6 and the right wing 16 are in an extending state, lift force is provided for flying, and the flying automobile is pushed to advance in the air through the rotation of the left propeller 11 and the right propeller 14; when the vehicle runs on land, the rear part of the roof 17 and the two sides of the rear part of the vehicle body 1 are contracted, the left wing 6 and the right wing 16 are folded around the upper connecting pieces of the respective wings along the central lines of the length directions of the wings, then the left wing stay bar 27 and the right wing stay bar 19 drive the left wing and the right wing to be folded and then put into the vehicle body, and meanwhile, the attack angle of the tail wing 13 becomes negative, so that the air lift force of the vehicle is reduced, the downward pressure is increased, and the running stability is improved.
The invention has been described in terms of specific embodiments envisaged, but is not limited to the examples described above, all the solutions obtained by adopting similar structures and material substitution methods, which are in line with the idea of the invention, are within the scope of protection of the invention.
Claims (2)
1. An electric flying automobile comprises an automobile body, a front automobile window, a battery system, a front wheel, a chassis system, a left automobile wing, an automobile tail, a left propeller, an empennage mounting bracket, an empennage, a right propeller, a rear wheel, a right automobile wing, a roof, a automobile wing stay bar connecting piece, a right wing stay bar, a hinge piece, a front swing arm, a transverse rotating shaft, a lower swing arm, a rear swing arm, a motor connecting arm, a folding wing rotating motor and a left wing stay bar; the method is characterized in that: the vehicle body is a main body bearing structure of the flying vehicle, and the battery system is positioned at the middle position of the bottom of the vehicle body; the left wing and the right wing are symmetrically arranged on two sides of the vehicle body, so that the left wing and the right wing are distinguished from each other in view of a driver; the left wing consists of a left wing front section, a left wing rear section, a wing upper connecting piece and a wing lower locking mechanism; the right wing consists of a right wing front section, a right wing rear section, a wing upper connecting piece and a wing lower locking mechanism; the tail wing is arranged on the tail of the car body through a tail wing mounting bracket; the left propeller and the right propeller are arranged at the tail of the vehicle; the wing strut connecting piece, the right wing strut, the hinge piece, the front swing arm, the transverse rotating shaft, the lower swing arm, the rear swing arm, the motor connecting arm, the folding wing rotating motor and the left wing strut are positioned in the vehicle body, and form a folding wing system of the aerocar together with the wing;
The electric flying automobile has two modes of land running and ultra-low altitude ground effect flying, and has the functions of automatic take-off and landing: when flying, the automobile is in a ground effect action area, the left wing and the right wing are in an extending state, lift force is provided for flying, and the flying automobile is pushed to advance in the air through rotation of the left propeller and the right propeller; when the vehicle runs on land, the rear part of the vehicle roof and the two sides of the rear part of the vehicle body shrink, the left wing and the right wing are folded around the upper connecting pieces of the respective wings along the central lines of the length directions of the wings, then the left wing stay bar and the right wing stay bar drive the left wing and the right wing to be folded and then put into the vehicle body, and meanwhile, the attack angle of the tail wing becomes negative, so that the air lift force of the vehicle is reduced, the downward pressure is increased, and the running stability is improved;
the body is a bearing type body, the body-in-white part is made of aluminum alloy materials, after being subjected to split-region die casting, the body-in-white part is assembled by punching and riveting, and the key bearing region is reinforced by using an internal adhesive fiber reinforced composite material layer so as to obtain a light high-strength body structure; the bottom of the automobile body is covered with a bottom guard plate made of engineering plastics, the outer surface of the bottom guard plate is used for protecting the impact of broken stone on the ground, the inner surface of the bottom guard plate is provided with an air bag interlayer, and when the flying automobile falls off the ground in a runaway manner, the air bag at the bottom of the automobile body pops out of the interlayer and is used for buffering the impact force of the ground so as to protect the safety of members;
the front window is made of polymethyl methacrylate resin organic glass, and the middle and rear areas have a sliding opening function and are used for passengers to get on or off the vehicle;
The battery system comprises a battery module, a battery box, a heat dissipation system, a sensor, a relay, a wire harness and a battery management system; the upper cover and the lower box body of the battery box are of bearing structures and are integrated with the vehicle body and the chassis system so as to reduce parts of the flying vehicle; the vehicle wing is arranged on the upper cover of the battery box through a vehicle wing stay bar connecting piece;
The front wheel and the rear wheel are driven by the hub motor, the power of the hub motor is provided by the battery system, when the automobile runs on land, the running driving force is provided, when the automobile leaves the ground and enters a cruising flight state, the front wheel and the rear wheel are retracted and covered by the wheel covers, air turbulence and excitation are prevented from being generated near the wheels in the flight process, and air flow field disorders on two sides of the automobile body are prevented;
The left wing mainly plays roles in improving lift force and ensuring stable flying of an automobile, is of a combined structure, and is connected by a front section of the left wing and a rear section of the left wing through a connecting piece at the upper part of the wing; the front section of the left wing and the rear section of the left wing are made of carbon fiber or basalt fiber reinforced composite materials; the automobile is unfolded in a flight state, the front section of the left automobile wing and the rear section of the left automobile wing are fixed together through the locking mechanism at the lower part of the automobile wing, and the attack angle is 4 degrees during cruising flight, so that good energy consumption economy is obtained; when the vehicle runs on the ground, the locking mechanism at the lower part of the vehicle wing is opened, and the vehicle wing is folded;
the left propeller and the right propeller provide propulsion for the flight of the automobile and are made of carbon fiber reinforced composite materials so as to reduce the weight and improve the fatigue life;
The tail wing is made of carbon fiber reinforced composite materials so as to reduce weight and improve fatigue life; the tail wing mounting bracket is arranged at the tail part of the vehicle body, the upper part of the tail wing mounting bracket is of a V-shaped lifting structure, and the lower part of the tail wing mounting bracket is of an inner X-shaped rib matched with an outer concave frame structure so as to firmly support the tail wing; the tail wing has an automatic rotation function, the attack angle of the flight state is a positive value, enough lift force is obtained, and the economy of flight is improved; the attack angle of the tail wing in the land state is a negative value, so that enough downward pressure is obtained, and the stability of the land is improved;
The vehicle roof is made of fiber reinforced composite materials, and the rear part of the vehicle roof has a folding function, so that the space for folding the vehicle wings is increased.
2. An electric flying vehicle according to claim 1, wherein: one end of the right wing stay bar is connected with the front section of the right wing through a wing stay bar connecting piece, and the other end of the right wing stay bar is connected with the hinge piece; the folding wing rotating motor rotates, the driving motor connecting arm rotates to drive the lower swing arm, the front swing arm rotates around the transverse rotating shaft, and then the right wing supporting rod and the left wing supporting rod are driven to move, so that the folding or unfolding of the left wing and the right wing is realized.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210864688.2A CN115091905B (en) | 2022-07-21 | 2022-07-21 | Electric flying car |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202210864688.2A CN115091905B (en) | 2022-07-21 | 2022-07-21 | Electric flying car |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115091905A CN115091905A (en) | 2022-09-23 |
| CN115091905B true CN115091905B (en) | 2024-05-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202210864688.2A Active CN115091905B (en) | 2022-07-21 | 2022-07-21 | Electric flying car |
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| CN (1) | CN115091905B (en) |
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|---|---|---|---|---|
| CN1390743A (en) * | 2002-04-30 | 2003-01-15 | 广州天象地效飞行器股份有限公司 | Effectively power-boosting ground effect aircraft |
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| CN115091905A (en) | 2022-09-23 |
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