Method, system, device and medium for acquiring automobile model tail wing test data
The aerodynamic data of different tail angles is obtained by adjusting the mechanism to drive the upper cover plate to rotate, which solves the problem that the tail structure changes need to be remade, and efficient aerodynamic performance evaluation and automotive design optimization are achieved.
Patent Information
- Application Number
- CN202210809323.X
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2022-07-11
- Publication Date
- 2025-08-19
- Estimated Expiration
- 2042-07-11
AI Technical Summary
In the prior art, the rear wing structure needs to be changed, which wastes time and increases costs, and cannot be replaced separately for testing, which affects the efficiency of aerodynamic performance evaluation.
The adjustment mechanism is adopted, including the motor, the rotation shaft, the bottom plate and the upper cover plate. The motor drives the upper cover plate to rotate about the rotation shaft to change the angle, obtain the aerodynamic data at different tail angles, and judge the coefficient range based on the design standard value and feedback the stress diagram.
It improves the convenience of aerodynamic data acquisition, reduces design costs, promptly feedback on stress conditions, and improves automotive design production efficiency.
Smart Images

Figure CN115200825B_ABST
Abstract
Description
Technical Field
[0001] The present application relates to the field of production and manufacturing technology, and in particular to a method, system, device and medium for acquiring test data of a car model tail wing. Background Art
[0002] Cars are an important means of transportation today, bringing great convenience to people's lives and work. With the development of automobile technology, people's requirements for cars are getting higher and higher.
[0003] In related technologies, the rear wing is a key component that influences aerodynamic performance. Therefore, during the automotive manufacturing process, especially during the model development phase, the rear wing's structure and design often require repeated changes and redesigns. Furthermore, once the rear wing structure has been finalized, aerodynamic testing is required to obtain test data from a car model's rear wing to determine whether the aerodynamic performance meets the requirements. Specifically, once the design is finalized, a complete car model is constructed using that design for aerodynamic testing, and the model components cannot be modified. When test data for a different rear wing angle is needed, a new car model must be constructed for testing. Changes to the rear wing design cannot be made individually, requiring the re-production of a new car model for testing, which wastes time and increases costs.
[0004] In summary, the problems existing in related technologies need to be solved urgently. Summary of the Invention
[0005] The purpose of this application is to solve one of the technical problems existing in the related art to at least a certain extent.
[0006] To this end, an object of embodiments of the present application is to provide a method, system, device and medium for acquiring automobile model tail wing test data.
[0007] In order to achieve the above technical objectives, the technical solutions adopted in the embodiments of the present application include:
[0008] On the one hand, an embodiment of the present application provides a method for obtaining test data of a car model's rear wing, the method being performed based on an adjustment mechanism; the adjustment mechanism includes a motor, a rotating shaft, a base plate, and an upper cover plate, wherein a variable angle is formed between the base plate and the upper cover plate, the upper cover plate being mounted on the rear portion of the car model's body, and the base plate being mounted on the car model's body; the motor is used to drive the upper cover plate to rotate about the rotating shaft to change the angle between the upper cover plate and the base plate;
[0009] The method comprises:
[0010] Fixing the adjustment mechanism according to the current included angle between the upper cover plate and the bottom plate;
[0011] performing an aerodynamic test on the automobile model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test;
[0012] determining whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values;
[0013] If at least one of the lift coefficient or the drag coefficient is not within the predetermined range, outputting the current angle and a stress diagram of the vehicle model;
[0014] After controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, the process returns to the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate.
[0015] In addition, the method for obtaining automobile model tail wing test data according to the above embodiment of the present application may also have the following additional technical features:
[0016] Furthermore, in one embodiment of the present application, the method further includes:
[0017] If the lift coefficient and the drag coefficient are both within the predetermined range, outputting the current angle, the lift coefficient, the drag coefficient, and a stress diagram of the vehicle model;
[0018] Turn off the power supply of the regulating mechanism to end the aerodynamic test.
[0019] Furthermore, in one embodiment of the present application, turning off the power supply of the regulating mechanism and ending the aerodynamic test includes:
[0020] Query user instructions;
[0021] When it is determined that the user instruction does not include the need to perform aerodynamic tests at other angles, the power supply of the adjustment mechanism is turned off to end the aerodynamic test.
[0022] Furthermore, in one embodiment of the present application, driving the upper cover plate to rotate in a predetermined direction includes:
[0023] The upper cover plate is driven to rotate in a direction in which the included angle increases.
[0024] Furthermore, in one embodiment of the present application, after controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, returning to the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate includes:
[0025] Controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, and detecting a first angle after the rotation;
[0026] Comparing the first angle with a preset angle threshold;
[0027] When the first angle is less than or equal to the preset angle threshold, the process returns to the step of fixing the adjustment mechanism according to the current angle between the upper cover plate and the bottom plate.
[0028] Furthermore, in one embodiment of the present application, the method further includes:
[0029] When the first angle is greater than the preset angle threshold, the aerodynamic test is ended.
[0030] Furthermore, in one embodiment of the present application, judging whether the lift coefficient and the drag coefficient are within a predetermined range based on the design standard value includes:
[0031] Determining a first design range corresponding to a lift index and a second design range corresponding to a drag index based on the design standard value;
[0032] determining, based on the lift coefficient and the first design range, whether the lift coefficient is within a predetermined range;
[0033] According to the drag coefficient and the second design range, it is determined whether the drag coefficient is within a predetermined range.
[0034] On the other hand, an embodiment of the present application provides a system for acquiring test data of a car model's rear wing, the system being executed based on an adjustment mechanism; the adjustment mechanism comprising a motor, a rotating shaft, a base plate, and an upper cover plate, wherein a variable angle is formed between the base plate and the upper cover plate, the upper cover plate being mounted on the rear portion of the car model's body, and the base plate being mounted on the car model's body; the motor being configured to drive the upper cover plate to rotate about the rotating shaft to change the angle between the upper cover plate and the base plate;
[0035] The system comprises:
[0036] A fixing module, used for fixing the adjustment mechanism according to the current included angle between the upper cover plate and the bottom plate;
[0037] a test module, configured to perform an aerodynamic test on the automobile model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test;
[0038] a judgment module, configured to judge whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values;
[0039] an output module, configured to output the current angle and a stress diagram of the vehicle model if at least one of the lift coefficient or the drag coefficient is not within the predetermined range;
[0040] The driving module is used to control the movement of the motor, drive the upper cover to rotate in a predetermined direction by a specified angle, and then return to the fixing module to execute the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate.
[0041] In another aspect, an embodiment of the present application provides a computer device, including:
[0042] at least one processor;
[0043] at least one memory for storing at least one program;
[0044] When the at least one program is executed by the at least one processor, the at least one processor implements the above-mentioned method for acquiring automobile model tail wing test data.
[0045] On the other hand, an embodiment of the present application further provides a computer-readable storage medium storing a program executable by a processor. When the program is executed by the processor, it is used to implement the above-mentioned method for obtaining the test data of the automobile model tail wing.
[0046] The advantages and benefits of this application will be partially given in the following description, and partially become apparent from the following description, or learned through practice of this application:
[0047] The present application discloses a method for obtaining test data for a car model's tail wing. The method is based on an adjustment mechanism. The adjustment mechanism includes a motor, a rotating shaft, a base plate, and an upper cover plate. A variable angle is formed between the base plate and the upper cover plate. The upper cover plate is mounted on the rear of the car model, and the base plate is mounted on the body of the car model. The motor is used to drive the upper cover plate to rotate about the rotating shaft to change the angle between the upper cover plate and the base plate. The method includes: fixing the adjustment mechanism according to a current angle between the upper cover plate and the base plate; performing an aerodynamic test on the car model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test; determining whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values; if at least one of the lift coefficient or the drag coefficient is not within the predetermined range, outputting the current angle and a stress diagram of the car model; controlling the motor to rotate the upper cover plate in a predetermined direction by a specified angle, and then returning to the step of fixing the adjustment mechanism according to the current angle between the upper cover plate and the base plate. This method can use the upper cover plate to act as a rear wing, and its angle is adjustable. Only one upper cover plate model needs to be made to obtain aerodynamic data at different rear wing angles, which can greatly improve the convenience of obtaining aerodynamic data and reduce the design cost of the car. Moreover, during the test process, timely feedback on the stress conditions at various rear wing angles can facilitate designers to adjust the car shape according to the stress data of the car model, which is conducive to improving the design and production efficiency of the car. BRIEF DESCRIPTION OF THE DRAWINGS
[0048] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following introduction is made to the drawings of the embodiments of the present application or the related technical solutions in the prior art. It should be understood that the drawings introduced below are only for the convenience of clearly describing some embodiments of the technical solutions of the present invention. For those skilled in the art, other drawings can be obtained based on these drawings without any creative work.
[0049] Figure 1 A schematic diagram of an implementation environment for a method for acquiring test data of a car model tail wing provided in an embodiment of the present application;
[0050] Figure 2 This is a schematic structural diagram of an adjustment mechanism provided in an embodiment of the present application;
[0051] Figure 3 A schematic flow chart of a method for acquiring test data of a car model tail wing provided in an embodiment of the present application;
[0052] Figure 4 A schematic diagram of the structure of a computer device provided in an embodiment of the present application. DETAILED DESCRIPTION
[0053] The present application is further described below in conjunction with the accompanying drawings and specific embodiments. The described embodiments should not be considered as limiting the present application. All other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of this application.
[0054] In the following description, reference is made to “some embodiments”, which describes a subset of all possible embodiments, but it will be understood that “some embodiments” may be the same subset or different subsets of all possible embodiments and may be combined with each other without conflict.
[0055] Unless otherwise defined, all technical and scientific terms used herein have the same meaning as commonly understood by those skilled in the art to which this application pertains. The terms used herein are for the purpose of describing the embodiments of this application only and are not intended to limit this application.
[0056] Cars are an important means of transportation today, bringing great convenience to people's lives and work. With the development of automobile technology, people's requirements for cars are getting higher and higher.
[0057] In related technologies, the rear wing is a key component that influences aerodynamic performance. Therefore, during the automotive manufacturing process, especially during the model development phase, the rear wing's structure and design often require repeated changes and redesigns. Furthermore, once the rear wing structure has been finalized, aerodynamic testing is required to obtain test data from a car model's rear wing to determine whether the aerodynamic performance meets the requirements. Specifically, once the design is finalized, a complete car model is constructed using that design for aerodynamic testing, and the model components cannot be modified. When test data for a different rear wing angle is needed, a new car model must be constructed for testing. Changes to the rear wing design cannot be made individually, requiring the re-production of a new car model for testing, which wastes time and increases costs.
[0058] In view of this, a method for obtaining test data of a car model's rear wing is provided in an embodiment of the present application. This method can use an upper cover plate to act as a rear wing, and its angle is adjustable. Only one upper cover plate model needs to be made to obtain aerodynamic data at different rear wing angles, which can greatly improve the convenience of obtaining aerodynamic data and reduce the design cost of the car; and during the test process, timely feedback on the stress conditions at various rear wing angles can facilitate designers to adjust the car shape according to the car model stress data, which is conducive to improving the design and production efficiency of the car.
[0059] Figure 1 This is a schematic diagram of the implementation environment of a method for obtaining test data of a car model tail wing provided in an embodiment of the present application. Figure 1The hardware and software components of this implementation environment primarily include a vehicle 101 and a server 102, with vehicle 101 communicating with server 102. The method for acquiring vehicle model tail wing test data can be executed locally on vehicle 101 or based on interaction between vehicle 101 and server 102. The specific method can be appropriately selected based on actual application circumstances and is not specifically limited in this embodiment.
[0060] The server 102 may be an independent physical server, a server cluster or distributed system composed of multiple physical servers, or a cloud server that provides basic cloud computing services such as cloud services, cloud databases, cloud computing, cloud functions, cloud storage, network services, cloud communications, middleware services, domain name services, security services, CDN (Content Delivery Network), and big data and artificial intelligence platforms. A communication connection may be established between the vehicle 101 and the server 102 via a wireless network or a wired network that uses standard communication technologies and / or protocols. The network may be the Internet or any other network, such as, but not limited to, a local area network (LAN), a metropolitan area network (MAN), a wide area network (WAN), a mobile, wired or wireless network, a private network, or any combination of a virtual private network.
[0061] It should be noted that the method for obtaining test data for a car model rear wing in the embodiment of this application is based on the adjustment structure. Therefore, before describing the method for obtaining test data for a car model rear wing provided in this application, the components of the adjustment mechanism in the embodiment of this application will first be introduced.
[0062] Reference Figure 2 In the embodiment of the present application, the adjustment mechanism includes a motor 1, a rotating shaft 2, a base plate 3, and an upper cover plate 4, wherein a variable angle exists between the base plate 3 and the upper cover plate 4. The upper cover plate 4 is mounted on the rear of the car model, and the base plate 3 is mounted on the body of the car model. Here, the upper cover plate 4 can serve as a rear wing or a part of the rear wing structure of the car. The present application does not limit its specific shape. In the embodiment of the present application, the motor 1 in the adjustment mechanism is used to drive the upper cover plate 4 to rotate around the rotating shaft 2, thereby changing the angle between the base plate 3 and the upper cover plate 4.
[0063] It should be noted that, since it is necessary to detect and determine the angle between the bottom plate 3 and the upper cover plate 4 during subsequent testing, in the embodiment of the present application, a relevant angle sensor 5 may be installed at the adjustment mechanism to detect and obtain the angle.
[0064] Please refer to Figure 3 , Figure 3 This is a flow chart of a method for obtaining test data of a car model tail wing provided in an embodiment of the present application, referring to Figure 3 The method for obtaining the test data of the car model tail wing includes but is not limited to:
[0065] Step 110: Fix the adjustment mechanism according to the current included angle between the upper cover plate and the bottom plate;
[0066] During this step, to minimize the impact of upper cover plate deflection on the tail wing during aerodynamic testing, the positional relationship between the upper cover and the base plate must be fixed after each adjustment. In other words, the adjustment mechanism must be fixed according to the current angle between the upper cover and the base plate. Specifically, in some embodiments, the upper cover plate can be fixed in position by means of a device such as an electromagnet. Alternatively, in other embodiments, a fixed fixture or other assembly can be used to secure the upper cover and base plate, although this application does not limit this.
[0067] Step 120: Perform an aerodynamic test on the automobile model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test;
[0068] In this step, after the upper cover and base are installed, the relevant components can be activated to perform aerodynamic testing on the current car model. Generally speaking, aerodynamic testing requires a wind tunnel laboratory, where the relevant test data is calculated by blowing the test object (i.e., the car model in this application) through the wind tunnel. Specifically, in the embodiments of this application, the relevant equipment and parameters used during the aerodynamic testing process can be implemented in accordance with relevant standards, and this application does not impose any restrictions on this.
[0069] In this step, the lift coefficient and drag coefficient can be obtained during the test process. Here, the lift coefficient is generally the ratio of the lift force on an object to the product of the airflow pressure and the reference area; the drag coefficient is the ratio of the drag force on an object to the product of the airflow pressure and the reference area. They are one of the main indicators for evaluating the aerodynamic performance of a car, which will directly affect the operational stability and power of the car. As the speed of the car increases, the requirements for the lift coefficient and drag coefficient of different models may also be different. Therefore, in the embodiment of the present application, it is necessary to obtain the lift coefficient and drag coefficient obtained by the aerodynamic test of the car model, so as to judge whether it meets the design requirements and determine the appropriate vehicle model structure.
[0070] Step 130: Determine whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values.
[0071] In this step, after obtaining the lift and drag coefficients from the aerodynamic test, the aerodynamic test data for the vehicle model in the current upper cover state can be determined based on pre-determined design standard values to determine whether it meets the design requirements. Specifically, the lift and drag coefficients can be compared with the design standard values to determine whether they are within a predetermined range.
[0072] Specifically, for example, based on the design standard values, the lift coefficient should be within a range of values for the lift index, which is recorded as the first design range. Furthermore, for the drag index, the drag coefficient should be within a range of values, which is recorded as the second design range. Then, based on whether the lift coefficient obtained from aerodynamic testing is within the first design range, it can be determined whether the lift coefficient is within the predetermined range. Similarly, based on whether the drag coefficient obtained from aerodynamic testing is within the second design range, it can be determined whether the drag coefficient is within the predetermined range.
[0073] It should be noted that in the embodiments of the present application, the specific size and range of the design standard value can be flexibly set as needed, and the present application does not impose any specific restrictions on this.
[0074] Step 140: If at least one of the lift coefficient or the drag coefficient is not within the predetermined range, output the current angle and the stress diagram of the vehicle model;
[0075] In this step, if at least one of the lift coefficient or the drag coefficient is determined to be outside the predetermined range, the current rear wing structure of the car model does not meet the design requirements and requires further adjustment. At this point, the current angle between the base plate and the upper cover can be output, along with a stress diagram of the car model. In this embodiment of the present application, the simultaneous output of stress data from the car model facilitates adjustments to the car's structure based on stress conditions, improving the shape of the rear wing and ultimately enhancing vehicle quality and production design efficiency.
[0076] Step 150 : Control the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, and then return to the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate.
[0077] In this step, if at least one of the current lift coefficient or drag coefficient is not within the predetermined range, the motor can be controlled to move and control the upper cover to adjust a specified angle in a predetermined direction. Here, the predetermined direction can be either an increasing direction or a decreasing direction, and this application does not impose any restrictions on this. Of course, in order to improve the efficiency of production design, it can be rotated slowly from the smallest angle to the increasing direction. Moreover, in an embodiment of the present application, the angle at which the upper cover is controlled to be "opened" or "closed" each time can be pre-set, for example, it can be 1 degree. In this way, by detecting the angle change during the rotation process, the start and shut down of the motor can be conveniently controlled. After adjusting the position of the upper cover, you can return to the aforementioned step 110 to continue the test, so that you can continue to judge whether the adjusted car model meets the design standards.
[0078] In some embodiments, the method further comprises:
[0079] If the lift coefficient and the drag coefficient are both within the predetermined range, outputting the current angle, the lift coefficient, the drag coefficient, and a stress diagram of the vehicle model;
[0080] Turn off the power supply of the regulating mechanism to end the aerodynamic test.
[0081] In this embodiment of the present application, if both the lift coefficient and the drag coefficient are within the predetermined range, the current vehicle model structure meets the design requirements. The angle between the current floor and upper cover, the lift coefficient, the drag coefficient, and a stress diagram of the vehicle model can then be output. The power to the relevant components of the adjustment mechanism can then be turned off, completing and ending the aerodynamic test.
[0082] In some embodiments, turning off the power supply of the regulating mechanism and ending the aerodynamic test includes:
[0083] Query user instructions;
[0084] When it is determined that the user instruction does not include the need to perform aerodynamic tests at other angles, the power supply of the adjustment mechanism is turned off to end the aerodynamic test.
[0085] In some cases, designers may need to obtain multiple sets of aerodynamic test data for comparison in order to determine the appropriate vehicle structure. Even if the design requirements are met, further testing may still be necessary to facilitate subsequent comparisons. In this case, the user can issue relevant user instructions in advance. By querying the user instructions, it can be determined whether they include requirements for aerodynamic testing at other angles. If not, the power to the adjustment mechanism can be turned off, terminating the aerodynamic test. Otherwise, the test can continue.
[0086] In some embodiments, after controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, returning to the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate includes:
[0087] Controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, and detecting a first angle after the rotation;
[0088] Comparing the first angle with a preset angle threshold;
[0089] When the first angle is less than or equal to the preset angle threshold, the process returns to the step of fixing the adjustment mechanism according to the current angle between the upper cover plate and the bottom plate.
[0090] When the first angle is greater than the preset angle threshold, the aerodynamic test is ended.
[0091] In an embodiment of the present application, when adjusting the angle by adjusting the structure, if the angle is selected from small to large for testing, it should be noted that due to structural limitations, the inclination of the upper cover plate cannot exceed a certain threshold. For this case, an angle threshold can be set in advance, such as 10 degrees. Each time the upper cover plate is driven to rotate a specified angle in a predetermined direction, the angle after rotation is detected and recorded as the first angle. Then, the first angle is compared with the preset angle threshold. If the first angle is less than or equal to the preset angle threshold, return to the step of fixing the adjustment mechanism according to the current angle between the upper cover plate and the bottom plate, and the test can continue; if the first angle is greater than the preset angle threshold, the aerodynamic test is ended.
[0092] It can be understood that the method for obtaining automobile model tail wing test data provided in the embodiment of the present application can use the upper cover plate to act as the tail wing, and its angle is adjustable. Only one upper cover plate model needs to be made to obtain the aerodynamic data at different tail wing angles, which can greatly improve the convenience of obtaining aerodynamic data and reduce the design cost of the automobile; and during the test process, timely feedback on the stress conditions at various tail wing angles can facilitate designers to adjust the automobile shape according to the automobile model stress data, which is conducive to improving the design and production efficiency of the automobile.
[0093] The present application also provides a system for acquiring test data of a car model's tail wing, the system being based on an adjustment mechanism; the adjustment mechanism comprising a motor, a rotating shaft, a base plate, and an upper cover plate; a variable angle being formed between the base plate and the upper cover plate; the upper cover plate being mounted on the rear of the car model, and the base plate being mounted on the body of the car model; the motor being configured to drive the upper cover plate to rotate about the rotating shaft to change the angle between the upper cover plate and the base plate;
[0094] The system comprises:
[0095] A fixing module, used for fixing the adjustment mechanism according to the current included angle between the upper cover plate and the bottom plate;
[0096] a test module, configured to perform an aerodynamic test on the automobile model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test;
[0097] a judgment module, configured to judge whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values;
[0098] an output module, configured to output the current angle and a stress diagram of the vehicle model if at least one of the lift coefficient or the drag coefficient is not within the predetermined range;
[0099] The driving module is used to control the movement of the motor, drive the upper cover to rotate in a predetermined direction by a specified angle, and then return to the fixing module to execute the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate.
[0100] It is understandable that Figure 3 The contents of the embodiment of the method for obtaining the test data of the automobile model tail wing are applicable to the embodiment of the system for obtaining the test data of the automobile model tail wing. The functions specifically implemented by the embodiment of the system for obtaining the test data of the automobile model tail wing are similar to those of the embodiment of the method for obtaining the test data of the automobile model tail wing. Figure 3 The method for obtaining the test data of the automobile model tail wing shown in the embodiment is the same as that of the embodiment shown in the embodiment, and the beneficial effects achieved are the same as those achieved in the embodiment shown in the embodiment. Figure 3 The beneficial effects achieved by the embodiment of the method for obtaining the test data of the automobile model tail wing are also the same.
[0101] Reference Figure 4 , the embodiment of the present application further discloses a computer device, including:
[0102] at least one processor 301;
[0103] At least one memory 302, configured to store at least one program;
[0104] When at least one program is executed by at least one processor 301, the at least one processor 301 implements the following Figure 3 An embodiment of a method for obtaining test data of a car model rear wing is shown.
[0105] It is understandable that if Figure 3 The contents of the method for obtaining the test data of the automobile model tail wing shown in the embodiment are all applicable to the embodiment of the computer device. The functions specifically implemented by the embodiment of the computer device are similar to those in the embodiment of the computer device. Figure 3The method for obtaining the test data of the automobile model tail wing shown in the embodiment is the same as that of the embodiment shown in the embodiment, and the beneficial effects achieved are the same as those of the embodiment shown in the embodiment. Figure 3 The beneficial effects achieved by the embodiment of the method for obtaining the test data of the automobile model tail wing are also the same.
[0106] The present application also discloses a computer-readable storage medium in which a program executable by a processor is stored. When the program is executed by the processor, it is used to implement the following Figure 3 An embodiment of a method for obtaining test data of a car model rear wing is shown.
[0107] It is understandable that if Figure 3 The contents of the embodiment of the method for obtaining the test data of the automobile model tail wing are applicable to the embodiment of the computer-readable storage medium. The functions specifically implemented by the embodiment of the computer-readable storage medium are similar to those in the embodiment of the computer-readable storage medium. Figure 3 The method for obtaining the test data of the automobile model tail wing shown in the embodiment is the same as that of the embodiment shown in the embodiment, and the beneficial effects achieved are the same as those of the embodiment shown in the embodiment. Figure 3 The beneficial effects achieved by the embodiment of the method for obtaining the test data of the automobile model tail wing are also the same.
[0108] In some optional embodiments, the functions / operations mentioned in the block diagram may not occur in the order mentioned in the operation diagram. For example, depending on the functions / operations involved, the two boxes shown in succession may actually be executed substantially simultaneously or the boxes can sometimes be executed in reverse order. In addition, the embodiments presented and described in the flow chart of the present application are provided in an exemplary manner for the purpose of providing a more comprehensive understanding of the technology. The disclosed method is not limited to the operations and logic flows presented herein. Optional embodiments are contemplated in which the order of the various operations is changed and the sub-operations described as a part of a larger operation are performed independently.
[0109] In addition, although the present application is described in the context of functional modules, it should be understood that, unless otherwise stated, one or more of the functions and / or features can be integrated into a single physical system and / or software module, or one or more functions and / or features can be implemented in separate physical systems or software modules. It is also understood that a detailed discussion of the actual implementation of each module is not necessary for understanding the present application. More specifically, given the properties, functions, and internal relationships of the various functional modules in the system disclosed herein, the actual implementation of the module will be understood within the conventional skills of an engineer. Therefore, those skilled in the art can implement the present application as set forth in the claims using ordinary techniques without undue experimentation. It is also understood that the specific concepts disclosed are merely illustrative and are not intended to limit the scope of the present application, which is determined by the full scope of the appended claims and their equivalents.
[0110] 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 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 read-only memory (ROM), a random access memory (RAM), a magnetic disk or an optical disk.
[0111] The logic and / or steps represented in the flowcharts or otherwise described herein, for example, can be considered as an ordered list of executable instructions for implementing the logical functions, and can be embodied in any computer-readable medium for use by, or in conjunction with, an instruction execution system, system, or device (e.g., a computer-based system, a system including a processor, or other system that can fetch instructions from and execute instructions on an instruction execution system, system, or device). For purposes of this specification, a "computer-readable medium" can be any system that can contain, store, communicate, propagate, or transport a program for use by, or in conjunction with, an instruction execution system, system, or device.
[0112] More specific examples (a non-exhaustive list) of computer-readable media include the following: an electrical connection with one or more wires (electronic systems), a portable computer disk cartridge (magnetic systems), a random access memory (RAM), a read-only memory (ROM), an erasable and programmable read-only memory (EPROM or flash memory), a fiber optic system, and a portable compact disk read-only memory (CDROM). In addition, the computer-readable medium may even be paper or other suitable medium on which the program is printed, since the program may be obtained electronically, for example, by optically scanning the paper or other medium, followed by editing, deciphering, or processing in another suitable manner as necessary, and then stored in a computer memory.
[0113] It should be understood that various parts of the present application can be implemented using hardware, software, firmware, or a combination thereof. In the above embodiments, multiple steps or methods can be implemented using software or firmware stored in a memory and executed by a suitable instruction execution system. For example, if implemented using hardware, as in another embodiment, any one of the following technologies known in the art or a combination thereof can be used to implement: a discrete logic circuit having a logic gate circuit for implementing a logic function on a data signal, an application-specific integrated circuit having a suitable combination of logic gate circuits, a programmable gate array (PGA), a field programmable gate array (FPGA), etc.
[0114] In the above description of this specification, reference to the terms "one embodiment / example," "another embodiment / example," or "certain embodiments / examples" means that the specific features, structures, materials, or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present application. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described can be combined in any appropriate manner in any one or more embodiments or examples.
[0115] Although the embodiments of the present application have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions, and variations may be made to the embodiments without departing from the principles and intent of the present application, and that the scope of the present application is defined by the claims and their equivalents.
[0116] The above is a detailed description of the preferred implementation of the present application, but the present application is not limited to the embodiments. Those skilled in the art can make various equivalent modifications or substitutions without violating the spirit of the present application. These equivalent modifications or substitutions are all included in the scope defined by the claims of the present application.
[0117] In the description of this specification, reference to the terms "one embodiment," "another embodiment," or "certain embodiments" means that the specific features, structures, materials, or characteristics described in conjunction with the embodiment or example are included in at least one embodiment or example of the present application. In this specification, the schematic representation of the above terms does not necessarily refer to the same embodiment or example. Moreover, the specific features, structures, materials, or characteristics described can be combined in any appropriate manner in any one or more embodiments or examples.
[0118] Although the embodiments of the present application have been shown and described, those skilled in the art will appreciate that various changes, modifications, substitutions, and variations may be made to the embodiments without departing from the principles and intent of the present application, and that the scope of the present application is defined by the claims and their equivalents.
Claims
1. A method for obtaining test data of a car model tail wing, characterized in that: The method is performed based on an adjustment mechanism; the adjustment mechanism includes a motor, a rotating shaft, a bottom plate and an upper cover plate, a variable angle is formed between the bottom plate and the upper cover plate, the upper cover plate is mounted on the rear of the car model, and the bottom plate is mounted on the body of the car model; The motor is used to drive the upper cover plate to rotate around the rotation axis to change the angle between the upper cover plate and the bottom plate; The method comprises: Fixing the adjustment mechanism according to the current included angle between the upper cover plate and the bottom plate; performing an aerodynamic test on the automobile model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test; determining whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values; If at least one of the lift coefficient or the drag coefficient is not within the predetermined range, outputting the current angle and a stress diagram of the vehicle model; the stress diagram is used for designers to adjust the structure of the vehicle model according to the stress situation; Controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, and then returning to the step of fixing the adjustment mechanism according to the current angle between the upper cover and the bottom plate; The determining, based on the design standard values, whether the lift coefficient and the drag coefficient are within a predetermined range includes: Determining a first design range corresponding to a lift index and a second design range corresponding to a drag index based on the design standard value; determining, based on the lift coefficient and the first design range, whether the lift coefficient is within a predetermined range; It is determined whether the drag coefficient is within a predetermined range based on the drag coefficient and the second design range.
2. The method for obtaining test data of a car model tail wing according to claim 1, characterized in that: The method further comprises: If the lift coefficient and the drag coefficient are both within the predetermined range, outputting the current angle, the lift coefficient, the drag coefficient, and a stress diagram of the vehicle model; Turn off the power supply of the regulating mechanism to end the aerodynamic test.
3. The method for obtaining test data of a car model tail wing according to claim 2, characterized in that: The power supply of the regulating mechanism is turned off to end the aerodynamic test, including: Query user instructions; When it is determined that the user instruction does not include the need to perform aerodynamic tests at other angles, the power supply of the adjustment mechanism is turned off to end the aerodynamic test.
4. The method for obtaining test data of a car model tail wing according to claim 1, characterized in that: The driving of the upper cover plate to rotate in a predetermined direction comprises: The upper cover plate is driven to rotate in a direction in which the included angle increases.
5. The method for obtaining test data of a car model tail wing according to claim 4, characterized in that: After controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, returning to the step of fixing the adjustment mechanism according to the current included angle between the upper cover and the bottom plate includes: Controlling the motor to drive the upper cover to rotate in a predetermined direction by a specified angle, and detecting a first angle after the rotation; Comparing the first angle with a preset angle threshold; When the first angle is less than or equal to the preset angle threshold, the process returns to the step of fixing the adjustment mechanism according to the current angle between the upper cover plate and the bottom plate.
6. The method for obtaining test data of a car model tail wing according to claim 5, characterized in that: The method further comprises: When the first angle is greater than the preset angle threshold, the aerodynamic test is ended.
7. A system for acquiring test data of a car model tail wing, characterized in that: The system is executed based on an adjustment mechanism; the adjustment mechanism includes a motor, a rotating shaft, a base plate and an upper cover plate, wherein a variable angle is formed between the base plate and the upper cover plate, the upper cover plate is mounted on the rear of the car model, and the base plate is mounted on the body of the car model; The motor is used to drive the upper cover plate to rotate around the rotation axis to change the angle between the upper cover plate and the bottom plate; The system comprises: A fixing module, used for fixing the adjustment mechanism according to the current included angle between the upper cover plate and the bottom plate; a test module, configured to perform an aerodynamic test on the automobile model to obtain a lift coefficient and a drag coefficient obtained from the aerodynamic test; a judgment module, configured to judge whether the lift coefficient and the drag coefficient are within a predetermined range based on design standard values; an output module, configured to output the current angle and a stress diagram of the vehicle model if at least one of the lift coefficient or the drag coefficient is not within the predetermined range; the stress diagram is used by a designer to adjust the structure of the vehicle model according to the stress condition; a driving module configured to control the motor to rotate the upper cover plate in a predetermined direction and at a specified angle, and then return to the fixing module to execute the step of fixing the adjustment mechanism according to the current angle between the upper cover plate and the bottom plate; The judgment module is specifically used for: Determining a first design range corresponding to a lift index and a second design range corresponding to a drag index based on the design standard value; determining, based on the lift coefficient and the first design range, whether the lift coefficient is within a predetermined range; It is determined whether the drag coefficient is within a predetermined range based on the drag coefficient and the second design range.
8. A computer device, characterized in that: include: at least one processor; at least one memory for storing at least one program; When the at least one program is executed by the at least one processor, the at least one processor implements the method for acquiring automobile model tail wing test data according to any one of claims 1 to 6.
9. A computer-readable storage medium storing a program executable by a processor, characterized in that: The processor-executable program is used to implement the method for acquiring automobile model tail wing test data as described in any one of claims 1 to 6 when executed by the processor.
Citation Information
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