Flying platform for low-altitude flying car

Abstract

The utility model discloses a flying platform for a low-altitude aerocar, and relates to the technical field of flying platforms for low-altitude aerocars, the flying platform comprises a platform assembly, a clamping assembly, a damping assembly and a balancing assembly, the platform assembly comprises a take-off and landing platform and an indicating lamp, the indicating lamp is fixedly installed on the top of the take-off and landing platform, the clamping assembly comprises a clamping motor, and the damping assembly is fixedly installed on the platform. The damping assembly comprises a pressing block and a connecting rod, the connecting rod is fixedly installed at one end of the pressing block, and the balance assembly comprises a horizontal detector. Under the combined action of the damping spring, the pressing block and the connecting table, when the low-altitude aerocar lands on the take-off and landing platform, the connecting table is pressed downwards through the take-off and landing platform, so that the connecting table is displaced, and due to the fact that the connecting table is in the shape of a circular truncated cone, the pressing block is pushed outwards when the connecting table moves downwards, the damping spring is compressed by the connecting rod, and the damping effect is achieved. The vibration is absorbed, and the influence of the vibration on the low-altitude flying car is reduced.

Description

Technical Field

[0001] This utility model relates to the technical field of low-altitude flying car flight platforms, specifically to a flight platform for low-altitude flying cars. Background Technology

[0002] Urban public transportation systems are currently a hot research topic in China. Due to limited urban land resources, coupled with the continuous growth of population and motor vehicle numbers, ground traffic congestion occurs frequently, severely impacting travel efficiency and posing a serious challenge to the development of ground transportation systems. With technological advancements and social development, people are wasting more and more time in traffic jams. To make travel more convenient and faster, people have come up with the idea of ​​developing low-altitude flying cars. Low-altitude flying cars can travel on roads like cars and also fly in the air, avoiding traffic jams and allowing people to reach their destination quickly and conveniently.

[0003] However, the landing of low-altitude flying cars on the take-off and landing platform is prone to vibration, which can affect the low-altitude flying cars and damage their internal parts, making it difficult for them to take off and land. Furthermore, if there is severe weather while the low-altitude flying cars are parked on the take-off and landing platform, they may tip over and be damaged, which makes it difficult to promote their use.

[0004] To address this problem, this application provides a low-altitude flying vehicle flight platform. Utility Model Content

[0005] The purpose of this invention is to provide a flight platform for low-altitude flying cars, in order to solve the problems mentioned in the background art, such as the vibration that is easily caused when the low-altitude flying car lands on the take-off and landing platform, and the possibility that the low-altitude flying car may tip over in bad weather, which is not conducive to the take-off and landing of the low-altitude flying car and may damage the low-altitude flying car, resulting in poor performance.

[0006] To solve the above-mentioned technical problems, the technical solution adopted by this utility model is as follows:

[0007] A flight platform for a low-altitude flying car includes a platform assembly, a clamping assembly, a shock absorption assembly, and a balancing assembly. The platform assembly includes a landing platform and indicator lights, with the indicator lights fixedly mounted on the top of the landing platform. The clamping assembly is disposed inside the landing platform and includes a clamping motor, which is fixedly mounted inside the landing platform. The shock absorption assembly is disposed inside the platform assembly and includes a pressure block and a connecting rod, with the connecting rod fixedly mounted on one end of the pressure block. The balancing assembly is disposed at the bottom of the platform assembly and includes a level sensor, which is disposed at the bottom of the landing platform.

[0008] A further improvement of the present invention is that: a base is provided at the bottom of the lifting platform, a threaded rod is fixedly installed at one end of the clamping motor, and a connecting platform is fixedly installed at the bottom of the lifting platform.

[0009] A further improvement of this utility model is that: a clamping block is installed on the external thread of the threaded rod, and rotating bearings are fixedly installed at both ends of the threaded rod.

[0010] A further improvement of the present invention is that: the top of the base is provided with an installation groove, the pressure block is slidably installed inside the installation groove, and a shock-absorbing sleeve is fixedly installed at the other end of the installation groove.

[0011] A further improvement of this utility model is that a shock-absorbing spring is fixedly installed inside the shock-absorbing sleeve, and the other end of the connecting rod is slidably installed inside the shock-absorbing sleeve.

[0012] A further improvement of this utility model is that a balancing hydraulic cylinder is fixedly installed inside the base, and the top of the balancing hydraulic cylinder is movably connected to the bottom of the lifting platform.

[0013] A further improvement of this utility model is that: a limiting sleeve is fixedly installed inside the base, the bottom of the connecting platform is movably connected to the inside of the limiting sleeve, and a limiting spring is fixedly installed inside the limiting sleeve.

[0014] Due to the adoption of the above technical solution, the technological progress achieved by this utility model compared to the prior art is as follows:

[0015] 1. This utility model provides a flight platform for a low-altitude flying car. Under the combined action of the shock-absorbing spring, the pressure block, and the connecting platform, when the low-altitude flying car lands on the landing platform, the landing platform will press the connecting platform downward, causing the connecting platform to displace. Since the connecting platform is frustum-shaped and the contact surface with the pressure block is an arc surface, when the connecting platform moves downward, it will push the pressure block outward, causing the connecting rod to compress the shock-absorbing spring, absorbing the vibration and reducing the impact of vibration on the low-altitude flying car.

[0016] 2. This utility model provides a flight platform for low-altitude flying cars. Through the combined action of a clamping motor, a threaded rod, and a clamping block, when the low-altitude flying car is parked on the landing platform and severe weather occurs, the clamping motor drives the threaded rod to rotate, and then the threaded rod drives the clamping block to slide. The internal threads of two adjacent clamping blocks are reversed, thus clamping the low-altitude flying car parked on the landing platform and reducing the impact of severe weather on the low-altitude flying car. Attached Figure Description

[0017] Figure 1This is a schematic diagram of the structure of the low-altitude flying car flight platform of this utility model;

[0018] Figure 2 This is a schematic diagram of the clamping assembly of this utility model;

[0019] Figure 3 This is a schematic diagram of the structure of the shock absorption component of this utility model;

[0020] Figure 4 This is a schematic diagram of the internal structure of the shock absorption component of this utility model;

[0021] Figure 5 This is a schematic diagram of the internal structure of this utility model.

[0022] In the diagram: 1. Platform assembly; 2. Clamping assembly; 3. Shock absorption assembly; 4. Balancing assembly; 10. Lifting platform; 11. Indicator light; 12. Base; 20. Clamping motor; 21. Threaded rod; 22. Clamping block; 23. Rotary bearing; 30. Mounting slot; 31. Shock absorption sleeve; 32. Connecting rod; 33. Pressure block; 34. Connecting platform; 35. Shock absorption spring; 40. Leveling instrument; 41. Balancing hydraulic cylinder; 42. Limiting sleeve; 43. Limiting spring. Detailed Implementation

[0023] The present invention will be further described in detail below with reference to embodiments:

[0024] like Figure 1-5 As shown, this utility model provides a flight platform for low-altitude flying cars, including a platform component 1, a clamping component 2, a shock absorption component 3 and a balancing component 4. The platform component 1 includes a landing platform 10 and an indicator light 11. The indicator light 11 is fixedly installed on the top of the landing platform 10, and a base 12 is provided at the bottom of the landing platform 10.

[0025] like Figure 2 As shown, the clamping assembly 2 is located inside the landing platform 10. The clamping assembly 2 includes a clamping motor 20, which is fixedly installed inside the landing platform 10. A threaded rod 21 is fixedly installed at one end of the clamping motor 20. A clamping block 22 is installed on the external thread of the threaded rod 21. Rotary bearings 23 are fixedly installed at both ends of the threaded rod 21. When the low-altitude flying car is parked on the landing platform 10 and there is severe weather, the clamping motor 20 drives the threaded rod 21 to rotate, and then the threaded rod 21 drives the clamping block 22 to slide. The internal threads of two adjacent clamping blocks 22 are reversed, which clamps the low-altitude flying car parked on the landing platform 10, reducing the impact of severe weather on the low-altitude flying car.

[0026] like Figure 3 and Figure 4As shown, the shock absorption assembly 3 is located inside the platform assembly 1. The shock absorption assembly 3 includes a pressure block 33 and a connecting rod 32. The connecting rod 32 is fixedly installed at one end of the pressure block 33. The top of the base 12 has an installation groove 30. The bottom of the landing platform 10 is fixedly installed with a connecting platform 34. The pressure block 33 is slidably installed inside the installation groove 30. The other end of the installation groove 30 is fixedly installed with a shock absorption sleeve 31. The shock absorption spring 35 is fixedly installed inside the shock absorption sleeve 31. The other end of the connecting rod 32 is slidably installed inside the shock absorption sleeve 31. When landing, the landing platform 10 will first bear the impact of the low-altitude flying car. The impact force will press the landing platform 10 and the connecting platform 34 downward, causing the connecting platform 34 to displace. Since the connecting platform 34 is frustum-shaped and the contact surface with the pressure block 33 is an arc surface, when the connecting platform 34 moves downward, it will push the pressure block 33 outward, causing the connecting rod 32 to compress the shock absorption spring 35, absorbing the vibration and reducing the impact of the vibration on the low-altitude flying car.

[0027] like Figure 2-4 As shown, the balancing component 4 is located at the bottom of the platform component 1. The balancing component 4 includes a level detector 40, which is located at the bottom of the landing platform 10. A balancing hydraulic cylinder 41 is fixedly installed inside the base 12. The top of the balancing hydraulic cylinder 41 is movably connected to the bottom of the landing platform 10. A limiting sleeve 42 is fixedly installed inside the base 12. The bottom of the connecting platform 34 is movably connected to the inside of the limiting sleeve 42. A limiting spring 43 is fixedly installed inside the limiting sleeve 42. The displacement distance of the connecting platform 34 is limited by the limiting sleeve 42 and the limiting spring 43 to prevent the excessive displacement distance of the connecting platform 34 from damaging the equipment. During landing, the level detector 40 will detect the horizontal angle of the landing platform 10. When the landing platform 10 tilts, it will be adjusted by the balancing hydraulic cylinder 41 inside the base 12 to keep the landing platform 10 in a horizontal state, so as to prevent the landing platform 10 from tilting and causing a low-altitude flying car landing accident.

[0028] The working principle of this low-altitude flying car platform will be explained in detail below.

[0029] like Figure 1-5As shown, when the low-altitude flying car lands on the flight platform, indicator light 11 guides the landing. During landing, the landing platform 10 will first bear the impact of the low-altitude flying car. The impact force will press the landing platform 10 and the connecting platform 34 downward, causing the connecting platform 34 to shift. Since the connecting platform 34 is frustum-shaped and the contact surface with the pressure block 33 is an arc surface, when the connecting platform 34 moves downward, it will push the pressure block 33 outward, causing the connecting rod 32 to compress the shock-absorbing spring 35, absorbing the vibration and reducing the impact of the vibration on the low-altitude flying car. Furthermore, during landing, the level detector 4... The system detects the horizontal angle of the landing platform 10. When the landing platform 10 tilts, it adjusts the platform through the balance hydraulic cylinder 41 inside the base 12 to keep the landing platform 10 level. This prevents the landing platform 10 from tilting and causing a landing accident for the low-altitude flying car. When the low-altitude flying car is parked on the landing platform 10 and there is bad weather, the clamping motor 20 drives the threaded rod 21 to rotate, and then the threaded rod 21 drives the clamping block 22 to slide. The internal threads of the two adjacent clamping blocks 22 are reversed, which clamps the low-altitude flying car parked on the landing platform 10 and reduces the impact of bad weather on the low-altitude flying car.

[0030] The present invention has been described in detail above. However, modifications or improvements can be made to it, which will be obvious to those skilled in the art. Therefore, any modifications or improvements that do not depart from the spirit of the present invention are within the protection scope of the present invention.

Claims

1. A flight platform for a low-altitude flying car, comprising a platform assembly (1), a clamping assembly (2), a shock absorption assembly (3), and a balancing assembly (4), characterized in that: The platform component (1) includes a lifting platform (10) and an indicator light (11). The indicator light (11) is fixedly installed on the top of the lifting platform (10). The clamping component (2) is located inside the lifting platform (10). The clamping component (2) includes a clamping motor (20). The clamping motor (20) is fixedly installed inside the lifting platform (10). The shock absorption component (3) is located inside the platform component (1). The shock absorption component (3) includes a pressure block (33) and a connecting rod (32). The connecting rod (32) is fixedly installed at one end of the pressure block (33). The balancing component (4) is located at the bottom of the platform component (1). The balancing component (4) includes a level detector (40). The level detector (40) is located at the bottom of the lifting platform (10).

2. The low-altitude flying vehicle flight platform according to claim 1, characterized in that: The bottom of the lifting platform (10) is provided with a base (12), one end of the clamping motor (20) is fixedly installed with a threaded rod (21), and the bottom of the lifting platform (10) is fixedly installed with a connecting platform (34).

3. The low-altitude flying vehicle flight platform according to claim 2, characterized in that: The threaded rod (21) has a clamping block (22) installed on its external thread, and both ends of the threaded rod (21) are fixedly installed with rotating bearings (23).

4. The low-altitude flying vehicle flight platform according to claim 2, characterized in that: The base (12) has an installation groove (30) on its top. The pressure block (33) is slidably installed inside the installation groove (30). A shock-absorbing sleeve (31) is fixedly installed at the other end of the installation groove (30).

5. The low-altitude flying vehicle flight platform according to claim 4, characterized in that: The shock-absorbing sleeve (31) is fixedly installed with a shock-absorbing spring (35), and the other end of the connecting rod (32) is slidably installed inside the shock-absorbing sleeve (31).

6. The low-altitude flying vehicle flight platform according to claim 2, characterized in that: A balancing hydraulic cylinder (41) is fixedly installed inside the base (12), and the top of the balancing hydraulic cylinder (41) is movably connected to the bottom of the lifting platform (10).

7. A low-altitude flying vehicle flight platform according to claim 2, characterized in that: A limiting sleeve (42) is fixedly installed inside the base (12), and the bottom of the connecting platform (34) is movably connected to the inside of the limiting sleeve (42). A limiting spring (43) is fixedly installed inside the limiting sleeve (42).

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