Flying car

Abstract

The utility model belongs to the field of vehicles, and discloses a flying car. Comprising a bearing platform, a cockpit body and a rotor wing structure, the cockpit body is arranged on the upper end face of the bearing platform, and a cockpit is formed in the cockpit body; the rotor structure is movably mounted on the cockpit body, the rotor structure has a working position and a storage position, the rotor structure generates lift force to drive the cockpit body to fly when in the working position, and the rotor structure is stored on the bearing platform when in the storage position. According to the hovercar, when the hovercar needs to fly, the rotor wing structure is installed on the cockpit body, then the cockpit body is driven to take off, the whole hovercar does not need to be taken up, the cockpit part in the hovercar is taken up, the bearing weight is small, a smaller rotor wing structure can be conveniently formed, and meanwhile the hovercar is convenient to use. The rotor wings are designed in a split mode, the rotor wing structure can be folded when the hovercar does not need to fly, and the situation that the surrounding space is excessively occupied is avoided.

Description

TECHNICAL FIELD

[0001] The utility model relates to traffic tool technical field especially relates to a flying car. BACKGROUND

[0002] With the rapid development of science and technology and the increasing application requirements, people's daily travel and professional department's customized requirements are more and more, and efficient travel and door-to-door convenience have become a new mode in urgent need, therefore, low-altitude traffic tool gradually attracts more attention. In some special application scenarios and time environment, a single car may not be able to directly arrive at the scheduled destination on time, and small aircraft such as helicopters have certain limitations and are difficult to promote on a large scale.

[0003] In the prior art, more and more enterprises pay attention to flying cars, and the existing flying cars adopt the technology of assembling wings or propellers on both sides of the vehicle body, which has great limitations in limited ordinary roads. In summary, the existing flying car is difficult to realize the take-off and landing of road space. UTILITARY MODEL CONTENT

[0004] The main purpose of the utility model is to provide a flying car, which aims to solve the problem that the existing flying car is difficult to realize the take-off and landing of road space.

[0005] To achieve the above purpose, the utility model provides a flying car, which comprises:

[0006] A bearing platform;

[0007] A cockpit body arranged on the upper end surface of the bearing platform, wherein a cockpit is formed in the cockpit body; and

[0008] A rotor structure movably installed on the cockpit body, wherein the rotor structure has a working position and a storage position, the rotor structure generates lift to drive the cockpit body to fly when the rotor structure is in the working position, and the rotor structure is used to be stored on the bearing platform when the rotor structure is in the storage position.

[0009] In an embodiment, the rotor structure comprises:

[0010] A rotor holder rotatably installed on one end of the cockpit body and movably installed on the other end between the working position and the storage position; and

[0011] A propeller rotatably installed on the other end of the rotor holder around an up-down extending rotation shaft to generate lift by rotation.

[0012] In an embodiment, the rotor holder and the propeller jointly form a lift group, a plurality of lift groups are arranged along the circumference of the cockpit body.

[0013] In an embodiment, a lower end surface of the cockpit body is provided with a take-off and landing support, which is used to carry the cockpit body.

[0014] In an embodiment, a hidden groove is formed in the lower end surface of the cockpit body, one end of the take-off and landing support is rotatably installed in the hidden groove, and the other end has a hidden position that is moved into the hidden groove and a support position that is moved out of the hidden groove.

[0015] In an embodiment, an alignment structure is further formed between the carrying platform and the cockpit body, which is used to align the cockpit body on the carrying platform.

[0016] In an embodiment, the alignment structure includes alignment protrusions and alignment grooves that are arranged in cooperation with each other, the alignment protrusions are movably installed in the alignment grooves, and one of the alignment protrusions and the alignment grooves is arranged on the upper end surface of the carrying platform, and the other is arranged on the lower end surface of the cockpit body.

[0017] In an embodiment, a charging structure is further formed between the carrying platform and the cockpit body, the charging structure includes a charging coil arranged in the carrying platform and a receiving coil arranged in the cockpit body, and the charging coil is used to generate an electric current in the receiving coil by being electrified.

[0018] In an embodiment, the flying car further includes a car body, the car body includes a car frame and a wheel system arranged on the car frame, the wheel system is used to drive the car frame to move, and the carrying platform includes the car frame.

[0019] In an embodiment, a plurality of car bodies are provided, and the cockpit body is selectively arranged on the car frame of one of the car bodies to realize switching between the car bodies at different positions.

[0020] The flying car includes a carrying platform and a cockpit body arranged on the carrying platform, and a rotor structure is arranged on the cockpit body. When the flying car needs to fly, the rotor structure is moved to a working position, the rotor structure is controlled to work to generate lift, and then the cockpit body is lifted off, without lifting the entire flying car. Instead, only the cockpit body is lifted, the carrying weight is small, and a smaller rotor structure is formed. Meanwhile, the rotor structure can be moved to a storage position, the rotor structure can be stowed when the flying car does not need to fly, the surrounding space is not excessively occupied, and the flying car can be used as a car on general roads. BRIEF DESCRIPTION OF DRAWINGS

[0021] Figure 1 The utility model provides a three-dimensional structure schematic diagram of flying car.

[0022] Figure 2 The utility model discloses a three-dimensional structure schematic diagram of flying car. Figure 1 The utility model discloses a three-dimensional structure schematic diagram of flying car.

[0023] Figure 3 The utility model discloses a three-dimensional structure schematic diagram of flying car. Figure 1 The utility model discloses a three-dimensional structure schematic diagram of flying car.

[0024] Figure 4 The utility model discloses a three-dimensional structure schematic diagram of flying car. Figure 1 The utility model discloses a three-dimensional structure schematic diagram of flying car.

[0025] Figure 5 The utility model discloses a three-dimensional structure schematic diagram of flying car. Figure 1 The utility model discloses a three-dimensional structure schematic diagram of flying car.

[0026] Figure 6 The utility model discloses a three-dimensional structure schematic diagram of flying car. Figure 1 The utility model discloses a three-dimensional structure schematic diagram of flying car.

[0027] 100, flying car;1, bearing platform;11, car frame;12, wheel system;2, cockpit body;2a, limiting section;2b, cockpit section;21, rotor holder;22, propeller;41, limiting cover plate;41a, engine cover;41b, trunk lid.

[0028] The utility model discloses a three-dimensional structure schematic diagram of flying car. Specific embodiments

[0029] The utility model discloses a three-dimensional structure schematic diagram of flying car.

[0030] It should be noted that if the embodiments of the utility model have directionality indication (such as up, down, left, right, front, back, etc.), the directionality indication is only used to explain the relative position relationship, movement condition, etc. between components in a certain specific posture (as shown in the drawings), if the specific posture changes, the directionality indication also changes accordingly.

[0031] In addition, if the embodiments of the utility model have descriptions such as "first", "second", etc., the descriptions of "first", "second", etc. are only for description purposes and cannot be understood as indicating or implying the relative importance or implicitly indicating the number of the indicated technical features. Therefore, the features limited by "first" and "second" can explicitly or implicitly include at least one of the features. In addition, the meaning of "and / or" appearing throughout the text includes three parallel schemes, for example, "A and / or B" includes A scheme, or B scheme, or A and B simultaneously satisfy the scheme. In addition, the technical solutions of each embodiment can be combined with each other, but it must be based on the realization of ordinary technical personnel in the art, when the combination of technical solutions appears contradictory or unachievable, it should be considered that the combination of technical solutions does not exist, nor is it within the protection scope required by the utility model.

[0032] With the rapid development of science and technology and the increasing demand for scene-based applications, whether it is people's daily travel or the customization needs of professional departments, efficient travel and door-to-door convenience have become an urgent new mode, therefore, low-altitude transportation tools have gradually attracted more attention. In some special application scenarios and time environments, a single car may not be able to directly arrive at the scheduled destination on time; and small aircraft such as helicopters have certain limitations and are difficult to promote on a large scale.

[0033] In the prior art, more and more enterprises pay attention to flying cars, and the technology used in the existing flying cars is mostly equipped with wings or propellers on both sides of the vehicle body, which has great limitations in limited ordinary roads. In summary, the existing flying car is difficult to realize the take-off and landing of the road space.

[0034] Please refer to Figure 1 The utility model provides a kind of flying car 100, including bearing platform 1, cockpit body 2 and rotor structure;The cockpit body 2 is placed in the upper end surface of the bearing platform 1, and the cockpit is formed in the cockpit body 2;The rotor structure is movably installed to the cockpit body, the rotor structure has working position and storage position, the rotor structure generates lift when being in the working position to drive the cockpit body to fly, and the rotor structure is in the storage position to be stored on the bearing platform.

[0035] In the embodiment, the flying car 100 comprises a bearing platform 1 and a cockpit body 2 arranged on the bearing platform 1, and a rotor structure arranged on the cockpit body 2. When the flying car needs to fly, the rotor structure is moved to a working position, the rotor structure is controlled to work to generate lift, and then the cockpit body is lifted off, without lifting the whole flying car, but only the cockpit body, so that the bearing weight is small, the rotor structure is small, and the rotor structure can be moved to a storage position when the flying car does not need to fly, so that the rotor structure does not occupy too much space, and the flying car can be used as a car on a general road.

[0036] Further, referring to Figure 2 , the rotor structure comprises a rotor support 21 and a propeller 22. One end of the rotor support 21 is rotatably arranged on the cockpit body, and the other end is movable between the working position and the storage position. The propeller 22 is rotatably arranged on the other end of the rotor support around an up-down extending rotating shaft, and is used to rotate to generate lift. In the embodiment, the rotor support 21 is arranged on the cockpit body by rotating, and is switched between the working position and the storage position by rotating, so that the movement is simple and reliable, and the working and storage are facilitated.

[0037] Further, the rotor support 21 and the propeller 22 jointly form a lift group, and a plurality of lift groups are arranged along the circumference of the cockpit body. In the embodiment, by arranging a plurality of lift groups, the size of each lift group can be effectively reduced, the space occupied can be reduced, the cockpit body 2 can be uniformly stressed, and the cockpit body 2 can be lifted and landed.

[0038] In the embodiment, the lift groups are arranged in a central symmetry, so that the flying car 100 is controlled.

[0039] In addition, the propeller 22 is electrically connected to the cockpit, so that the cockpit body 2 supplies power to the propeller 22 to rotate, and the cockpit controls the propeller 22.

[0040] On the other hand, the lower end surface of the cockpit body 2 is provided with a landing support for bearing the cockpit body 2. In the embodiment, the landing support is arranged on the lower end surface of the cockpit body 2, so that the cockpit body 2 can land after taking off, and the cockpit body 2 can not directly fall on the bottom surface to scratch the bottom surface.

[0041] Further, the lower end surface of the cockpit body 2 is formed with a hidden groove, one end of the take-off and landing support is rotatably installed in the hidden groove, and the other end has a hidden position that is moved to the hidden groove and a support position that is moved to outside the hidden groove. In this embodiment, the take-off and landing support can be hidden through the hidden groove, and when the cockpit body 2 is placed on the upper end surface of the bearing platform, it can be attached to the upper end surface of the bearing platform 1, thereby saving the space occupied by the flying car.

[0042] On the other hand, an alignment structure is further formed between the bearing platform 1 and the cockpit body 2, so as to align the cockpit body 2 on the bearing platform 1. In this embodiment, since the cockpit body 2 needs to be parked on the bearing platform and needs to interact with the electronic elements on the bearing platform, it is necessary to ensure that the cockpit body 2 remains at the same position after take-off and landing. In this embodiment, an alignment structure is provided between the bearing platform 1 and the cockpit body 2 to ensure that the cockpit body 2 can be correctly parked on the bearing platform 1.

[0043] Specifically, the alignment structure includes an alignment protrusion and an alignment groove that are arranged in cooperation with each other, the alignment protrusion is movably installed in the alignment groove, and one of the alignment protrusion and the alignment groove is arranged on the upper end surface of the bearing platform, and the other is arranged on the lower end surface of the cockpit body. In this embodiment, the alignment protrusion and the alignment groove are arranged on the upper end surface of the bearing platform 1 and the lower end surface of the cockpit body 2 respectively. Through the cooperation of the alignment protrusion and the alignment groove, the cockpit body 2 can be correctly parked on the bearing platform 1 after falling.

[0044] It should be noted that in this embodiment, the flying car further includes a detection camera, which is arranged on the cockpit body 2 to video monitor the cooperation state of the alignment protrusion and the alignment groove.

[0045] It should be noted that in this embodiment, a battery system is arranged in the cockpit body 2 to supply power to the rotor structure.

[0046] On the other hand, a charging structure is further formed between the bearing platform 1 and the cockpit body 2, the charging structure includes a charging coil arranged in the bearing platform and a receiving coil arranged in the cockpit body, and the charging coil is used to generate current in the receiving coil by electrification. In this embodiment, the cockpit body 2 is charged through the charging structure, so as to facilitate the cockpit body 2 to start charging after being parked on the bearing platform 1.

[0047] On the other hand, please refer to Figure 3In the embodiment, the flying car 100 further comprises a car body, which comprises a car frame 11 and a wheel system 12 arranged on the car frame 11 and used to drive the car frame 11 to move, and the carrying platform 1 comprises the car frame 11. In the embodiment, the carrying platform is the car frame 11, so that the flying car can realize normal driving on the road, and when flight is needed, the cockpit body 2 is separated from the car frame 11, and only the cockpit part needs to be taken away.

[0048] It should be noted that the wheel system comprises two front wheels and two rear wheels, and the specific mounting mode of the wheel system is the prior art, which will not be described in detail here.

[0049] Further, the car body is provided with a plurality of car bodies, and the cockpit body 2 is arranged on the car frame 11 of one of the car bodies to realize switching between the car bodies at different positions. In the embodiment, one cockpit body 2 is provided with a plurality of car bodies, so as to facilitate switching between different car bodies, and take off at one place and land at another place. In the process of commercial operation, since the low-altitude route needs to be kept fixed, the car frame 11 can be first driven on the road to the corresponding position, and then the cockpit body 2 is flown, and landed on the car frame 11 of another car body at another position, and then driven on the road again to realize the combination of ground traffic and low-altitude traffic, and ensure the use of the flying car 100.

[0050] On the other hand, the flying car further comprises a limiting structure arranged on the car body and used to limit the cockpit body 2 on the car frame 11. In the embodiment, the limiting structure is arranged between the cockpit body 2 and the car frame 11 to ensure that the cockpit body 2 can be fixed on the car frame 11 and avoid shaking.

[0051] Specifically, in the embodiment, please refer to Figure 3The cockpit body 2 comprises two opposite limiting sections 2a and a cockpit section 2b between the two limiting sections 2a. The limiting structure comprises a limiting cover plate 41, one end of which is rotatably installed on the automobile frame 11, and the other end is rotatably installed on the limiting section 2a or avoids the limiting section 2a. In this embodiment, when the cockpit body 2 is placed on the upper end surface of the automobile frame, the limiting cover plate 41 is rotated so that the other end of the limiting cover plate 41 is pressed on the limiting section 2a, and the cockpit body 2 is pressed and fixed on the automobile frame 11, which is simple and reliable. When the cockpit body 2 needs to take off, the limiting cover plate 41 is rotated so that the other end of the limiting cover plate 41 avoids the limiting section 2a, which is convenient for the cockpit body 2 to fly upward and downward.

[0052] Further, the limiting cover plate 41 is provided with two limiting cover plates 41 corresponding to the two limiting sections 2a, and the two limiting cover plates 41 are respectively arranged at the two ends of the automobile frame 11 to limit the two ends of the cockpit body 2. In this embodiment, the two ends of the cockpit body 2 are clamped by the two limiting cover plates 41 at the same time, which ensures the safety of the position of the cockpit body 2.

[0053] In this embodiment, the two limiting cover plates 41 are respectively arranged at the front end and the rear end of the flying automobile, and the two limiting cover plates 41 can be additional structures arranged on the automobile (fuel car or new energy car), or can be structures of the automobile itself.

[0054] In some embodiments, the limiting cover plate 41 on the front side can be arranged as the front part of the automobile, specifically as at least part of the engine cover 41a. The limiting cover plate 41 on the rear side can be arranged as the rear part of the automobile, specifically as at least part of the trunk cover 41b.

[0055] In this embodiment, the limiting structure further comprises a driving device for driving the limiting cover plate 41 to move, so as to facilitate the automatic operation of the flying automobile 100.

[0056] Specifically, the driving device comprises a driving hydraulic cylinder, one of the fixed end and the driving end of which is arranged on the automobile frame 11, and the other is arranged on the limiting cover plate 41. In this embodiment, the limiting cover plate 41 is controlled to rotate by the driving hydraulic cylinder, which is simple and convenient for the position of the limiting cover plate 41 to be kept.

[0057] On the other hand, referring to Figures 3 to 6In the embodiment, the rotor structure forms the limiting section when the rotor structure is in the storage position, the limiting cover plate is turned to the limiting position to cover the rotor structure, and the limiting cover plate is turned to the avoiding position to allow the rotor structure to be turned to the working position. In the embodiment, when the rotor structure is moved to the storage position, the rotor structure forms the limiting section to facilitate the placement of the rotor structure to be removed, the limiting cover plate is pressed on the rotor structure, and the flying frame is fixed on the automobile body.

[0058] The above are only preferred embodiments of the present application, and do not limit the patent scope of the present application, and any equivalent structure or equivalent process transformation, or direct or indirect application in other related technical fields, which are made by using the content of the present application specification and drawings, are also included in the patent protection scope of the present application.

Claims

1. A flying car, characterized by, The flying car comprises: a bearing platform; a cockpit body arranged on the upper end surface of the bearing platform, a cockpit being formed in the cockpit body; a rotor structure movably mounted to the cockpit body, the rotor structure having a working position outside the bearing platform and a storage position inside the bearing platform in the movement range thereof, the rotor structure generating lift to drive the cockpit body to fly in the working position, and the rotor structure being stored on the bearing platform in the storage position; the rotor structure comprises: a rotor holder rotatably mounted to one end of the cockpit body and movably arranged between the working position and the storage position; and a propeller rotatably mounted to the other end of the rotor holder around a rotation shaft extending upward and downward to generate lift by rotation. The rotor holder and the propeller jointly form a lift group, and a plurality of lift groups are arranged along the circumference of the cockpit body. The lower end surface of the cockpit body is provided with a take-off and landing support for bearing the cockpit body.

2. The flying car of claim 1, wherein, The lower end surface of the cockpit body is provided with a hidden groove, one end of the take-off and landing support is rotatably mounted in the hidden groove, and the other end has a hidden position movably arranged in the hidden groove and a support position movably arranged outside the hidden groove.

3. The flying car of claim 1, wherein, The bearing platform and the cockpit body are further provided with an alignment structure for aligning the cockpit body on the bearing platform.

4. The flying car of claim 3, wherein, The alignment structure comprises an alignment protrusion and an alignment groove arranged in cooperation, the alignment protrusion is movably arranged in the alignment groove, and one of the alignment protrusion and the alignment groove is arranged on the upper end surface of the bearing platform, and the other is arranged on the lower end surface of the cockpit body.

5. The flying car of claim 1, wherein, The bearing platform and the cockpit body are further provided with a charging structure, the charging structure comprises a charging coil arranged in the bearing platform and a receiving coil arranged in the cockpit body, the charging coil is used to generate current in the receiving coil by electrification.

6. The flying car of claim 5, wherein, The flying car further comprises a car body, the car body comprises a car frame and a wheel system arranged on the car frame, the wheel system is used to drive the car frame to move, and the bearing platform comprises the car frame.

7. The flying car of claim 1, wherein, The car body is provided with a plurality of car frames, and the cockpit body is arranged on one of the car frames of the car body to realize switching between the car bodies at different positions.

8. The flying car of claim 1, wherein, ​ 9. The flying car of claim 8, wherein, ​

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