Flying car brake parachute system, control method and flying car

Abstract

The invention relates to an aerocar brake parachute system, a control method and an aerocar, the aerocar brake parachute system comprises a car body, a propeller, a brake parachute, an air suspension unit and a control unit, the propeller is arranged at the top of the car body and comprises a containing cavity, and the brake parachute is arranged in the containing cavity; the air suspension unit is used for driving the brake parachute to pop out of the containing cavity and be opened through compressed air under the action of a control signal of the control unit. The brake parachute system of the hovercar drives the brake parachute through compressed air of the air suspension unit of the hovercar, so that the reliability of the brake parachute and the safety of the hovercar can be greatly improved.

Description

Technical Field

[0001] The present application relates to the technical field of transportation vehicles, and in particular to a flying car parachute system, a control method, and a flying car. Background Art

[0002] The current development of flying cars is in full swing. How to ensure their safety during flight is a major challenge facing the industry. Some solutions use parachutes to achieve deceleration during driving and flight. However, the parachute opening agent is completed by detonating gunpowder, and the parachute opening agent itself is a fuel, which poses a fire hazard to the flammable parachute. The gunpowder also has the risk of failure due to moisture. Therefore, how to design a safe and reliable parachute system has become a pressing issue in the design process of flying cars. Summary of the Invention

[0003] In order to solve the above technical problems or at least partially solve the above technical problems, the present application provides a flying car deceleration parachute system, a control method and a flying car.

[0004] In a first aspect, the present application provides a flying car parachute system, the flying car parachute system comprising: a vehicle body, a propeller, a parachute, an air suspension unit, and a control unit;

[0005] The propeller is arranged on the top of the vehicle body, the propeller includes a receiving cavity, and the deceleration parachute is arranged in the receiving cavity;

[0006] The air suspension unit is used to drive the deceleration parachute to pop out and open from the accommodating cavity through compressed air under the control signal of the control unit.

[0007] Optionally, the propeller comprises blades and a rotating center;

[0008] The bottom of the rotating center is fixed to the top of the vehicle body, the blades are fixed to the side surfaces of the rotating center, and the accommodating cavity is arranged at the top of the rotating center.

[0009] Optionally, the accommodating cavity further includes a cover plate, and the cover plate is arranged at the opening of the accommodating cavity.

[0010] Optionally, the air suspension unit includes an air compressor, an air storage tank and an air distribution valve;

[0011] The air path distribution valve is connected to the air compressor, the air storage tank and the accommodating chamber through air paths respectively;

[0012] The air compressor is used to generate compressed air and store the compressed air in the air storage tank;

[0013] The air path distribution valve is used to transmit the compressed air in the air storage tank to the accommodating chamber through the air path under the control signal of the control unit, so as to eject the deceleration parachute from the accommodating chamber.

[0014] Optionally, the air suspension unit further comprises a pressure sensor, the pressure sensor being used to detect the air tank pressure of the compressed air in the air tank;

[0015] The control unit is further configured to control the air compressor to start working when the air tank pressure is less than a first pressure threshold, and to control the air compressor to stop working when the air tank pressure is greater than or equal to a second pressure threshold; the second pressure threshold is greater than the first pressure threshold.

[0016] Optionally, the deceleration parachute includes a parachute body and a towing rope;

[0017] The traction ropes are respectively connected to the parachute body and the accommodating cavity.

[0018] Optionally, the accommodating cavity is detachably connected to the rotation center portion.

[0019] Optionally, the flying car parachute system further includes: a brake controller, an inertial measurement unit, a vehicle controller and an intelligent driving controller;

[0020] The brake controller is used to collect the speed of the flying car;

[0021] The inertial measurement unit is used to collect the vertical acceleration and longitudinal acceleration of the flying car;

[0022] The vehicle controller is used to obtain the driving mode of the flying car and the active parachute opening signal; wherein the driving mode includes a flight mode and a land mode;

[0023] The intelligent driving controller is used to collect obstacle information;

[0024] The control unit is used to output a control signal when the parachute opening condition is met, so as to drive the deceleration parachute to pop out of the accommodating cavity and open through compressed air;

[0025] The parachute opening condition includes at least one of the following conditions:

[0026] Acquiring the active parachute opening signal;

[0027] In the flight mode, the vertical acceleration is greater than a preset acceleration threshold and the flight system fails;

[0028] In the land mode, it is determined that there is a collision risk based on the vehicle speed, the longitudinal acceleration, and the obstacle information.

[0029] In a second aspect, the present application provides a flying car parachute control method, which is applied to the flying car parachute system according to any one of the first aspects, and the method includes:

[0030] The control unit outputs a control signal when the parachute opening conditions are met;

[0031] Under the action of the control signal, the air suspension unit drives the deceleration parachute to pop out from the accommodating cavity through compressed air.

[0032] In a third aspect, the present application provides a flying car, comprising the flying car deceleration parachute system as described in any one of the first aspects.

[0033] In a fourth aspect, the present application provides an electronic device, comprising a processor, a communication interface, a memory, and a communication bus, wherein the processor, the communication interface, and the memory communicate with each other via the communication bus;

[0034] Memory for storing computer programs;

[0035] The processor is configured to implement the steps of the flying car parachute control method described in the second aspect of the embodiment when executing the program stored in the memory.

[0036] In a fifth aspect, the present application provides a computer-readable storage medium having a computer program stored thereon, which, when executed by a processor, implements the steps of the flying car deceleration parachute control method as described in the embodiment of the second aspect.

[0037] Beneficial effects of this application:

[0038] The flying car parachute system provided in an embodiment of the present application includes a vehicle body, a propeller, a parachute, an air suspension unit, and a control unit. The propeller is mounted on top of the vehicle body and includes a chamber containing a parachute. The air suspension unit is configured to deploy the parachute from the chamber using compressed air in response to a control signal from the control unit. Because the parachute is powered by compressed air from the vehicle's own air suspension unit, the system significantly improves the parachute's reliability and the vehicle's safety. BRIEF DESCRIPTION OF THE DRAWINGS

[0039] The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the present application and, together with the description, serve to explain the principles of the present application.

[0040] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments or the description of the prior art. Obviously, for ordinary technicians in this field, other drawings can be obtained based on these drawings without any creative work.

[0041] Figure 1 A structural diagram of a flying car parachute system provided in one embodiment of the present application;

[0042] Figure 2 A schematic structural diagram of a flying car parachute system provided in one embodiment of the present application;

[0043] Figure 3 A schematic diagram of a flying car parachute control method provided in one embodiment of the present application;

[0044] Figure 4 A schematic diagram of opening a parachute in flight mode provided by one embodiment of the present application;

[0045] Figure 5 A schematic diagram of parachute deployment in land mode provided in one embodiment of the present application;

[0046] Figure 6 A schematic structural diagram of an electronic device provided in one embodiment of the present application. DETAILED DESCRIPTION

[0047] The following will describe the embodiments of the present application with reference to the accompanying drawings and preferred embodiments. Those skilled in the art can easily understand the other advantages and effects of the present application from the contents disclosed in this specification. The present application can also be implemented or applied through other different specific embodiments, and the details in this specification can also be modified or changed in various ways based on different viewpoints and applications without departing from the spirit of the present application. It should be understood that the preferred embodiments are only for the purpose of illustrating the present application and are not intended to limit the scope of protection of the present application.

[0048] The first embodiment of the present application provides a flying car parachute system, such as Figure 1 The flying car parachute system includes: a vehicle body 100, a propeller 101, a parachute 102, an air suspension unit 103 and a control unit 104.

[0049] The propeller 101 is arranged on the top of the vehicle body 100. The propeller 101 includes a receiving cavity, and the deceleration parachute 102 is arranged in the receiving cavity. The air suspension unit 103 is used to drive the deceleration parachute 102 to pop out of the receiving cavity through compressed air under the control signal of the control unit 104.

[0050] The vehicle body 100 refers to the main body of the flying car. The number of propellers 101 is not limited and can be one or more. For example, the number can be determined based on the propeller power and the vehicle weight. It should be understood that each propeller 101 corresponds to a parachute 102. When there are multiple propellers 101, each propeller 101 includes a cavity for accommodating the parachute 102. The air suspension unit 103 can be the flying car's own air suspension system, thereby fully utilizing existing vehicle components and reducing costs. The parachute is powered by compressed air, eliminating concerns about fuel moisture or damage to the parachute due to fuel combustion. Because the flying car parachute system uses compressed air from the flying car's own air suspension unit to power the parachute, it greatly improves the reliability of the parachute and the safety of the flying car.

[0051] In a specific embodiment, the structural diagram of the flying car parachute system is as follows: Figure 2 , wherein the propeller 101 includes blades 203 and a rotating center portion 202. The bottom of the rotating center portion 202 is fixed to the top of the vehicle body 100, the blades 203 are fixed to the side of the rotating center portion 202, and the accommodating cavity 201 is arranged at the top of the rotating center portion 202. The rotating center portion 202 can be a cylindrical structure, and the accommodating cavity 201 is a concave structure at the top center of the rotating center portion 202, or the accommodating cavity 201 can also be a cylindrical structure arranged at the concave structure at the top of the rotating center portion 202, without limitation. The number of blades 203 can be set as needed, and the embodiment of the present application does not limit the number of blades 203.

[0052] In one embodiment, the accommodating chamber 201 further includes a cover plate, which is disposed at the opening of the accommodating chamber 201. The cover plate may be a flip-top structure, and the connection between the cover plate and the accommodating chamber opening may be a rotatable connection. For example, when the control unit 104 outputs a control signal, the cover plate is first controlled to open, and then the parachute is driven by compressed air to eject from the accommodating chamber.

[0053] In one embodiment, the air suspension unit 103 includes an air compressor 204 , an air tank 205 , and an air distribution valve 206 .

[0054] The air path distribution valve 206 is connected to the air compressor 204, the air tank 205 and the accommodating chamber 201 through air paths respectively. The air compressor 204 is used to generate compressed air and store the compressed air in the air tank 205. The air path distribution valve 206 is used to transmit the compressed air in the air tank 205 to the accommodating chamber 201 through the air path under the control signal of the control unit, so as to eject the deceleration parachute 102 from the accommodating chamber 201.

[0055] In this embodiment, the air compressor 204, air tank 205, and air distribution valve 206 can be components of the flying car's built-in air suspension system, thereby fully utilizing existing vehicle components and significantly reducing costs. The air compressor 204, air tank 205, and accommodating chamber 201 are each connected to the air distribution valve 206 via air circuits. The flow of compressed air is controlled by opening and closing various valves in the air distribution valve 206.

[0056] In one embodiment, the air suspension unit 103 further includes a pressure sensor for detecting the tank pressure of the compressed air in the air tank 205 .

[0057] The control unit 104 is also used to control the air compressor 204 to start working when the air tank pressure is less than a first pressure threshold, and to control the air compressor 204 to stop working when the air tank pressure is greater than or equal to a second pressure threshold; the second pressure threshold is greater than the first pressure threshold.

[0058] In this embodiment, in order to ensure that the pressure of the compressed air in the air tank is sufficient to support the normal function of the air suspension unit and the pressure requirement when the parachute needs to be deployed, the air tank pressure of the compressed air in the air tank can be detected in real time by a pressure sensor. When the air tank pressure is less than a first pressure threshold, the air compressor 204 is controlled to start working, and when the air tank pressure is greater than or equal to a second pressure threshold, the air compressor 204 is controlled to stop working. Since the second pressure threshold is greater than the first pressure threshold, frequent starting of the air compressor is avoided, thereby improving the life of the air compressor.

[0059] In one embodiment, the deceleration parachute 102 includes a parachute body and a towing rope, wherein the towing rope is connected to the parachute body and the receiving cavity respectively.

[0060] In this embodiment, the deceleration parachute is fixed to the accommodating cavity by a traction rope. The number of traction ropes is not limited, for example, there can be 4, 6, 8 or more traction ropes. One end of the traction rope is connected to the parachute body, and the other end is connected to the accommodating cavity.

[0061] In one embodiment, the accommodating cavity is detachably connected to the rotation center portion.

[0062] After the parachute is deployed in an emergency, restoring the parachute is time-consuming and requires specialized skills. Therefore, a removable connection between the housing chamber and the rotating center can be provided. For example, the connection can be rotationally connected via a threaded structure, with a male threaded head provided at the outer bottom of the housing chamber and a matching female threaded head provided at the rotating center, allowing the housing chamber and the rotating center to be connected and removable via the threaded structure. Alternatively, a female threaded head can be provided at the outer bottom of the housing chamber and a matching male threaded head can be provided at the rotating center, without limitation. Alternatively, the housing chamber and the rotating center can be provided with other removable connections, such as a snap-on connection, without limitation. After the parachute is used once, the driver can remove the used housing chamber and replace it with a spare one, ensuring the vehicle's stability and safety. Since the parachute is located within the housing chamber, only the compressed air path connecting the housing chamber to the compressed air path needs to be replaced. The air path can be integrated into the removable connection structure, and the air path is connected after the housing chamber is replaced and secured, thereby improving the recovery speed of the parachute after use.

[0063] In one embodiment, the flying car parachute system further includes: a brake controller, an inertial measurement unit, a vehicle controller, and an intelligent driving controller.

[0064] The brake controller is used to measure the flying car's speed; the inertial measurement unit is used to collect the flying car's vertical and longitudinal accelerations; the vehicle controller is used to obtain the flying car's driving mode and active parachute deployment signals (driving modes include flight mode and land mode); and the intelligent driving controller is used to collect obstacle information. Vertical acceleration refers to the flying car's acceleration perpendicular to the ground, and longitudinal acceleration refers to the flying car's acceleration in the horizontal forward direction.

[0065] The control unit is used to output a control signal when the parachute opening conditions are met, so as to drive the deceleration parachute to pop out of the accommodation chamber and open through compressed air.

[0066] Among them, the parachute opening conditions include at least one of the following conditions:

[0067] Obtain active parachute opening signal;

[0068] In flight mode, the vertical acceleration exceeds the preset acceleration threshold and the flight system fails;

[0069] In land mode, the risk of collision is determined based on vehicle speed, longitudinal acceleration and obstacle information.

[0070] In this embodiment, the control unit interacts with the brake controller, inertial measurement unit, vehicle controller, and intelligent driving controller via an onboard bus. The brake controller can detect the current speed of the flying car, the inertial measurement unit (IMU) can detect the vertical and longitudinal accelerations of the flying car, the vehicle controller can obtain the flying car's driving mode and the driver's input for active parachute deployment, and the intelligent driving controller can collect information about obstacles ahead, such as obstacle size, type, and distance. The type of onboard bus is not limited and can be, for example, a CAN bus, Ethernet, or other bus. When an active parachute deployment signal is received, indicating that the driver wishes to deploy the parachute, the control unit directly outputs a control signal to eject the parachute from the containment chamber using compressed air. In flight mode, if the vertical acceleration exceeds a preset acceleration threshold and the flight system malfunctions, indicating that the flying car is in a critical state, the control unit outputs a control signal to eject the parachute from the containment chamber using compressed air to ensure a smooth landing of the flying car. In land mode, if it is determined based on vehicle speed, longitudinal acceleration, and obstacle information that the current braking system cannot avoid the risk of collision even at full power, the braking performance needs to be further improved. At this time, the parachute can be deployed to stop the flying car as quickly as possible to avoid a collision.

[0071] Figure 3 A schematic diagram of a flying car parachute control method provided in one embodiment of the present application includes:

[0072] Step S101, parachute opening intention judgment: The control unit receives the driver's parachute opening intention judgment signal sent by the vehicle controller. If the driver has the intention, the process jumps to step S105, otherwise it goes to step S102.

[0073] Step S102: Driving mode determination. The control unit receives the driving mode signal sent by the vehicle controller and determines the type of driving mode. If it is flight mode, the process proceeds to step S103; if it is land mode, the process proceeds to step S104.

[0074] In step S103, the longitudinal acceleration is greater than the threshold and the flight system is faulty. The control unit continuously detects and determines the longitudinal acceleration provided by the inertial measurement unit (IMU) and the flight system fault. If the longitudinal acceleration is greater than the threshold and the flight system is faulty, the control unit proceeds to step S105. Otherwise, the control unit remains in step S103 and repeats the determination.

[0075] Step S104: Collision risk assessment. The control unit performs a real-time, cyclic assessment of the longitudinal acceleration provided by the IMU, the obstacle distance provided by the intelligent driving controller, and the vehicle speed provided by the brake controller. If a collision risk exists, the process proceeds to step S105; otherwise, the process remains at step S104. The specific method for risk assessment is as follows:

[0076] ① Call the Autonomous Emergency Braking (AEB) control algorithm to confirm whether the vehicle has a potential collision risk based on the vehicle's speed, acceleration, and distance to the vehicle in front in real time.

[0077] ② In the event of a potential collision risk, AEB determines whether the collision can be avoided based on the maximum braking capacity of the hydraulic brake.

[0078] ③ If it cannot be avoided, it is considered that there is a collision risk; otherwise, there is no collision risk.

[0079] Step S105, system operation, mainly refers to the control unit opening the air distribution valve connecting the air compressor, the air tank and the parachute, and driving the air compressor to work.

[0080] Step S106: Open the parachute. After the system starts working, high-pressure gas immediately enters the parachute installation area, and the parachute is compressed by the high-pressure gas and opens quickly. Figure 4 , is a schematic diagram of parachute opening in flight mode, such as Figure 5 , which is a schematic diagram of parachute opening in land mode.

[0081] In this embodiment, the flying car parachute system utilizes the vehicle's existing air suspension unit components, such as an air tank, an air compressor, and a distribution valve, which can reduce costs. The parachute is deployed using high-pressure compressed air, which is more reliable than existing technologies. For example, there is no need to worry about the fuel getting wet or damaging the parachute when the fuel burns. Furthermore, it can provide both protection during flight and deceleration on land, and can actively deploy the parachute according to the pilot's wishes. Compared with existing technologies, it has a wider range of applications. Furthermore, the control logic used in the parachute deployment process is rigorous, which can avoid false triggering and improve reliability.

[0082] Based on the same technical concept, the second embodiment of the present application provides a flying car parachute control method, which is applied to the flying car parachute system described in any one of the first embodiments. The method includes:

[0083] The control unit outputs a control signal when the parachute opening conditions are met;

[0084] Under the action of the control signal, the air suspension unit drives the deceleration parachute to pop out from the accommodation cavity through compressed air.

[0085] In this method, since the flying car deceleration parachute system drives the deceleration parachute through the compressed air of the air suspension unit of the flying car itself, the reliability of the deceleration parachute and the safety of the flying car can be greatly improved.

[0086] Based on the same technical concept, the second embodiment of the present application provides a flying car, which includes the flying car deceleration parachute system described in any one of the first embodiments of the present application.

[0087] like Figure 6 As shown, the third embodiment of the present application provides an electronic device, including a processor 111, a communication interface 112, a memory 113 and a communication bus 114, wherein the processor 111, the communication interface 112, and the memory 113 communicate with each other through the communication bus 114.

[0088] Memory 113, for storing computer programs;

[0089] In one embodiment, the processor 111 is configured to implement the flying car parachute control method provided by the aforementioned method embodiment when executing the program stored in the memory 113 .

[0090] The memory and processor in the electronic device communicate via a communication bus and a communication interface. The communication bus can be a Peripheral Component Interconnect (PCI) bus or an Extended Industry Standard Architecture (EISA) bus. The communication bus can be divided into an address bus, a data bus, a control bus, and the like.

[0091] The memory may include random access memory (RAM) or non-volatile memory, such as at least one disk storage. Alternatively, the memory may be at least one storage device located away from the processor.

[0092] The above-mentioned processor can be a general-purpose processor, including a central processing unit (CPU), a network processor (NP), etc.; it can also be a digital signal processor (DSP), an application-specific integrated circuit (ASIC), a field-programmable gate array (FPGA) or other programmable logic devices, discrete gate or transistor logic devices, and discrete hardware components.

[0093] A fourth embodiment of the present application provides a computer-readable medium having non-volatile program code executable by a processor.

[0094] Optionally, in an embodiment of the present application, a computer-readable medium is configured to store program code for a processor to execute the above method.

[0095] Optionally, the specific examples in this embodiment may refer to the examples described in the above embodiments, and this embodiment will not be described in detail here.

[0096] When implementing the embodiments of the present application, reference may be made to the above embodiments, which have corresponding technical effects.

[0097] It is understood that the embodiments described herein may be implemented using hardware, software, firmware, middleware, microcode, or a combination thereof. For hardware implementation, the processing unit may be implemented in one or more application-specific integrated circuits (ASICs), digital signal processors (DSPs), digital signal processing devices (DSPDs), programmable logic devices (PLDs), field-programmable gate arrays (FPGAs), general-purpose processors, controllers, microcontrollers, microprocessors, other electronic units for performing the functions of the present application, or a combination thereof.

[0098] For software implementation, the technology herein can be implemented by a unit that performs the functions herein. The software code can be stored in a memory and executed by a processor. The memory can be implemented in the processor or external to the processor.

[0099] Those skilled in the art will appreciate that the units and algorithm steps of each example described in conjunction with the embodiments disclosed herein can be implemented in electronic hardware, or a combination of computer software and electronic hardware. Whether these functions are performed in hardware or software depends on the specific application and design constraints of the technical solution. Professional and technical personnel can use different methods to implement the described functions for each specific application, but such implementation should not be considered beyond the scope of this application.

[0100] Those skilled in the art will clearly understand that, for the convenience and brevity of description, the specific working processes of the systems, devices and units described above can refer to the corresponding processes in the aforementioned method embodiments and will not be repeated here.

[0101] In the embodiments provided in this application, it should be understood that the disclosed devices and methods can be implemented in other ways. For example, the device embodiments described above are merely schematic. For example, the division of modules is only a logical function division. In actual implementation, there may be other division methods, such as multiple modules or components can be combined or integrated into another system, or some features can be ignored or not executed. Another point is that the mutual coupling or direct coupling or communication connection shown or discussed can be an indirect coupling or communication connection through some interface, device or unit, which can be electrical, mechanical or other forms.

[0102] Units described as separate components may or may not be physically separate, and components shown as units may or may not be physical units, that is, they may be located in one place or distributed across multiple network units. Some or all of these units may be selected to achieve the purpose of this embodiment according to actual needs.

[0103] In addition, each functional unit in each embodiment of the present application may be integrated into one processing unit, or each unit may exist physically separately, or two or more units may be integrated into one unit.

[0104] If the function is implemented in the form of a software functional unit and sold or used as an independent product, it can be stored in a computer-readable storage medium. Based on this understanding, the technical solution of the embodiment of the present application, or the part that contributes to the prior art, or the part of the technical solution, can be embodied in the form of a software product. The computer software product is stored in a storage medium and includes several instructions for enabling a computer device (which can be a personal computer, server, or network device, etc.) to execute all or part of the steps of the various embodiments of the present application. The aforementioned storage medium includes various media that can store program codes, such as a USB flash drive, a mobile hard disk, a ROM, a RAM, a magnetic disk, or an optical disk.

[0105] It should be noted that, in this document, relational terms such as "first" and "second" are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply any actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variations thereof are intended to cover non-exclusive inclusion, so that a process, method, article, or device that includes a series of elements includes not only those elements, but also other elements not explicitly listed, or elements inherent to such process, method, article, or device. In the absence of further limitations, an element defined by the phrase "comprising a ..." does not exclude the presence of other identical elements in the process, method, article, or device that includes the element.

[0106] The above embodiments are only preferred embodiments for fully illustrating the present application, and the protection scope of the present application is not limited thereto. Any equivalent substitutions or modifications made by those skilled in the art based on the present application are within the protection scope of the present application.

Claims

1. A flying car parachute system, characterized in that: The flying car parachute system includes: a vehicle body, a propeller, a parachute, an air suspension unit and a control unit; The propeller is arranged on the top of the vehicle body, the propeller includes a receiving cavity, and the deceleration parachute is arranged in the receiving cavity; The air suspension unit is used to drive the deceleration parachute to pop out and open from the accommodating cavity through compressed air under the control signal of the control unit.

2. The flying car parachute system according to claim 1, characterized in that: The propeller includes blades and a rotating center; The bottom of the rotating center is fixed to the top of the vehicle body, the blades are fixed to the side surfaces of the rotating center, and the accommodating cavity is arranged at the top of the rotating center.

3. The flying car parachute system according to claim 2, characterized in that: The accommodating cavity further includes a cover plate, which is arranged at the opening of the accommodating cavity.

4. The flying car parachute system according to claim 1, characterized in that: The air suspension unit includes an air compressor, an air storage tank and an air distribution valve; The air path distribution valve is connected to the air compressor, the air storage tank and the accommodating chamber through air paths respectively; The air compressor is used to generate compressed air and store the compressed air in the air storage tank; The air path distribution valve is used to transmit the compressed air in the air storage tank to the accommodating chamber through the air path under the control signal of the control unit, so as to eject the deceleration parachute from the accommodating chamber.

5. The flying car parachute system according to claim 4, characterized in that: The air suspension unit further includes a pressure sensor for detecting the air tank pressure of the compressed air in the air tank; The control unit is further configured to control the air compressor to start working when the air tank pressure is less than a first pressure threshold, and to control the air compressor to stop working when the air tank pressure is greater than or equal to a second pressure threshold; the second pressure threshold is greater than the first pressure threshold.

6. The flying car parachute system according to claim 1, characterized in that: The deceleration parachute includes a parachute body and a towing rope; The traction ropes are respectively connected to the parachute body and the accommodating cavity.

7. The flying car parachute system according to claim 2, characterized in that: The accommodating cavity is detachably connected to the rotation center portion.

8. The flying car parachute system according to claim 1, characterized in that: The flying car parachute system also includes: a brake controller, an inertial measurement unit, a vehicle controller and an intelligent driving controller; The brake controller is used to collect the speed of the flying car; The inertial measurement unit is used to collect the vertical acceleration and longitudinal acceleration of the flying car; The vehicle controller is used to obtain the driving mode of the flying car and the active parachute opening signal; wherein the driving mode includes a flight mode and a land mode; The intelligent driving controller is used to collect obstacle information; The control unit is used to output a control signal when the parachute opening condition is met, so as to drive the deceleration parachute to pop out of the accommodating cavity and open through compressed air; The parachute opening condition includes at least one of the following conditions: Acquiring the active parachute opening signal; In the flight mode, the vertical acceleration is greater than a preset acceleration threshold and the flight system fails; In the land mode, it is determined that there is a collision risk based on the vehicle speed, the longitudinal acceleration, and the obstacle information.

9. A flying car parachute control method, characterized in that: The flying car parachute system according to any one of claims 1 to 8 is applied to the method comprising: The control unit outputs a control signal when the parachute opening conditions are met; Under the action of the control signal, the air suspension unit drives the deceleration parachute to pop out from the accommodating cavity through compressed air.

10. A flying car, characterized in that: The flying car includes the flying car deceleration parachute system according to any one of claims 1 to 8.

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