A device, method, apparatus, and storage medium for automatically launching a water rocket

Abstract

The application provides a device, method, equipment and storage medium for automatically launching a water rocket, which comprises a power gas pump module, a gas-liquid control unit, a water storage tank, a release assembly and a pressure sensor. The power gas pump module comprises a plurality of gas output sides, the plurality of gas output sides are connected with a first electromagnetic valve and a second electromagnetic valve in the gas-liquid control unit, and the second electromagnetic valve is connected with the release assembly. The water storage tank comprises an input side, an output side and a bidirectional transmission side, the input side is connected with the first electromagnetic valve, the output side is connected with a fourth electromagnetic valve in the gas-liquid control unit, and the bidirectional transmission side is connected with a third electromagnetic valve in the gas-liquid control unit, and the third electromagnetic valve is connected with the release assembly. The pressure sensor is connected with the release assembly. The release assembly comprises a rudder and a release element. Through the device, the effect of fully automatically launching the water rocket can be achieved.

Description

Technical Field

[0001] The present application relates to the field of water rockets, and in particular, to a device, method, equipment and storage medium for automatically launching a water rocket. Background Art

[0002] Water rockets are a very famous case in science and technology education. They cover physical knowledge, have strong hands-on practical skills, and can enrich teaching. Especially in the field of aerospace science and technology education, water rockets can help understand and recognize aerospace knowledge and physical principles.

[0003] At present, water rocket launching devices are basically manual launching devices. After water is poured into the water rocket, it is pressurized and finally released using the bicycle brake line. Some water rockets are launched automatically, but the control methods are very complicated and it is difficult to control the water rocket.

[0004] The above method has great limitations. The launch method is relatively complicated and cannot achieve automatic control of the entire process.

[0005] Therefore, how to simply realize the fully automatic launch of water rockets is a technical problem that needs to be solved. Summary of the Invention

[0006] The purpose of the embodiments of the present application is to provide a method for automatically launching a water rocket. Through the technical solution of the embodiments of the present application, the effect of simply realizing the fully automatic launch of the water rocket can be achieved.

[0007] In the first aspect, an embodiment of the present application provides a device for automatically launching a water rocket, comprising an energy supply air pump module, a gas-liquid control unit, a water tank, a release assembly and a pressure sensor, wherein the energy supply air pump module comprises a plurality of gas output sides, wherein the plurality of gas output sides are connected to the first solenoid valve and the second solenoid valve in the gas-liquid control unit, and the second solenoid valve is connected to the release assembly; the plurality of gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water tank and the release assembly; the water tank comprises an input side, an output side and a bidirectional transmission side, wherein an input side is connected to the first solenoid valve, an output side is connected to the fourth solenoid valve in the gas-liquid control unit, a bidirectional transmission side is connected to the third solenoid valve in the gas-liquid control unit, and the third solenoid valve is connected to the release assembly; an output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release assembly

[0008] force; a bidirectional transmission side is used to: output or input liquid, the liquid is used to provide 5 pressure or release pressure for the release component: the pressure sensor is connected to the release component to measure the liquid pressure in the release component; the release component includes a servo and a release element, and the servo is used to control the release element.

[0009] In the above embodiments of the present application, the automatic launch of the water rocket can be achieved through the connection of the above devices, the operation is relatively simple, and a large amount of resources can be saved.

[0010] In some embodiments, the apparatus further comprises: a controller;

[0011] A controller is connected to the energy supply air pump module, the gas-liquid control unit, the pressure sensor, the servo, and the communication module. The controller is used to control the opening and closing of the energy supply air pump module, the gas-liquid control unit, the pressure sensor, and the servo, and to communicate with the communication module.

[0012] In the above embodiments of the present application, the controller can be used to control each module of the water rocket, thereby achieving the purpose of automatic launch and reducing complex operating steps.

[0013] In some embodiments, the energy supply air pump module includes: an air pump and a protective plate,

[0014] Wherein, the protective plate is connected to the air pump to protect the air pump from overpressure and overheating.

[0015] In the above embodiments of the present application, the protective plate can achieve overpressure and overheating protection, thereby ensuring safety.

[0016] In a second aspect, an embodiment of the present application provides a method for automatically launching a water rocket, comprising:

[0017] By controlling the gas-liquid control unit, the liquid is pressed into the release component; when the water storage volume in the release component reaches the preset water storage volume, the gas is pressed into the release component by controlling the gas-liquid control unit; when the pressure in the release component reaches the preset pressure value, the release component is controlled to release and launch the water rocket.

[0018] In the above embodiment of the present application, the automatic launch of the water rocket can be achieved by releasing the increased pressure of the gas and liquid in the assembly and finally releasing the liquid, which makes the operation simpler.

[0019] In some embodiments, the liquid is pressed into the release assembly by controlling the gas-liquid control unit, including:

[0020] By controlling a solenoid valve in the gas-liquid control unit, the gas in the energy supply air pump is pressed into the water storage tank;

[0021] By controlling a solenoid valve in the gas-liquid control unit, the liquid in the water tank is pressed into the release assembly.

[0022] In the above embodiment of the present application, the solenoid valve can be used to control the gas to enter the water tank and the liquid to enter the release component, thereby achieving a pressurization effect.

[0023] In some embodiments, the gas is pressed into the release assembly by controlling the gas-liquid control unit, including:

[0024] By controlling a solenoid valve in the gas-liquid control unit, the gas in the power supply pump is pressed into the release component.

[0025] In the above embodiment of the present application, the gas can also be directly pressed into the release component through the solenoid valve to increase the pressure inside the release component.

[0026] In some embodiments, releasing and launching a water rocket via a controlled release assembly includes:

[0027] The liquid in the release assembly is pressed into the water storage tank by controlling the release assembly and a solenoid valve in the gas-liquid control module;

[0028] The liquid in the water tank is released by controlling a solenoid valve in the air and liquid control module.

[0029] In the above embodiment of the present application, the liquid can be discharged by opening the solenoid valve, thereby achieving the effect of releasing the pressure and recovering the water rocket midway.

[0030] In some embodiments, after pressing the liquid into the release component, the method further comprises:

[0031] The water storage capacity in the release component is calculated using the differential pressure water injection method based on the value of the pressure sensor.

[0032] In the above embodiment of the present application, the optimal time to release the liquid is determined by the value of the pressure sensor, which can ensure that the water rocket can be accurately launched automatically.

[0033] In a third aspect, an embodiment of the present application provides a device for automatically launching a water rocket, comprising:

[0034] a first control module, configured to press the liquid into the release assembly by controlling the gas-liquid control unit;

[0035] The second control module is used to pressurize gas into the release component by controlling the gas-liquid control unit when the water storage amount in the release component reaches a preset water storage amount;

[0036] The third control module is used to release and launch the water rocket by controlling the release assembly when the pressure in the release assembly reaches a preset pressure value.

[0037] Optionally, the first control module is specifically configured to:

[0038] By controlling a solenoid valve in the gas-liquid control unit, the gas in the energy supply air pump is pressed into the water storage tank;

[0039] The liquid in the water storage tank is pressed into the release assembly by controlling one electromagnetic valve in the gas-liquid control unit.

[0040] Optionally, the second control module is specifically configured to:

[0041] The gas in the energy supply gas pump is pressed into the release assembly by controlling one electromagnetic valve in the gas-liquid control unit.

[0042] Optionally, the third control module is specifically configured to:

[0043] The liquid in the release assembly is pressed into the water storage tank by controlling one electromagnetic valve in the release assembly and the gas-liquid control unit module.

[0044] The liquid in the water storage tank is released by controlling one electromagnetic valve in the gas-liquid control module.

[0045] Optionally, the device further comprises:

[0046] The calculation module is configured to calculate the water storage amount in the release assembly by using the differential pressure water injection method according to the value of the pressure sensor after the first control module presses the liquid into the release assembly.

[0047] In a fourth aspect, an embodiment of the present application provides an electronic device, including a processor and a memory, the memory stores computer readable instructions, when the computer readable instructions are executed by the processor, the steps in the method provided in the second aspect are executed.

[0048] In a fifth aspect, an embodiment of the present application provides a readable storage medium, which stores a computer program, when the computer program is executed by a processor, the steps in the method provided in the second aspect are executed.

[0049] Other features and advantages of the present application will be described in the following description, and some will become apparent from the description, or will be learned through practice of the application. The purpose and other advantages of the present application can be achieved and obtained by the structure specifically pointed out in the written description, claims, and drawings. BRIEF DESCRIPTION OF DRAWINGS

[0050] In order to more clearly illustrate the technical solutions of the embodiments of the present application, the following will briefly introduce the drawings needed to be used in the embodiments of the present application. It should be understood that the following drawings only show some embodiments of the present application, and therefore should not be regarded as limiting the scope, and for those skilled in the art, other related drawings can also be obtained without creative labor on the basis of these drawings.

[0051] Figure 1 A structural schematic diagram of a device for automatically launching water rockets provided by an embodiment of the present application;

[0052] Figure 2 A schematic diagram of a controller for automatically launching a water rocket provided in an embodiment of the present application;

[0053] Figure 3 A flow chart of a method for automatically launching a water rocket provided in an embodiment of the present application;

[0054] Figure 4 A schematic structural diagram of another device for automatically launching a water rocket provided in an embodiment of the present application;

[0055] Figure 5 This is a schematic block diagram of the structure of a device for automatically launching a water rocket provided in an embodiment of the present application.

[0056] Icons: power supply air pump module 110, air-liquid control unit 120, water tank 130, release assembly 140, pressure sensor 150, servo 160, release element 161, first solenoid valve 121, second solenoid valve 122, third solenoid valve 123, fourth solenoid valve 124, controller 180, air pump 192, communication module 190 and protective plate 191. DETAILED DESCRIPTION

[0057] The technical solutions in the embodiments of the present application will be clearly and completely described below in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all of the embodiments. The components of the embodiments of the present application generally described and shown in the drawings here can be arranged and designed in various different configurations. Therefore, the following detailed description of the embodiments of the present application provided in the drawings is not intended to limit the scope of the application for protection, but merely represents the selected embodiments of the present application. Based on the embodiments of the present application, all other embodiments obtained by those skilled in the art without making creative work fall within the scope of protection of the present application.

[0058] It should be noted that similar reference numerals and letters represent similar items in the following drawings. Therefore, once an item is defined in one drawing, it does not need to be further defined or explained in subsequent drawings. At the same time, in the description of this application, the terms "first", "second", etc. are only used to distinguish the description and should not be understood as indicating or implying relative importance.

[0059] This application is applied to the scenario of water rocket launch. The specific scenario is to realize the automatic launch of the water rocket through the cooperation of multiple modules inside the launch device.

[0060] However, currently, most water rocket launchers are manual, requiring water to be poured into the rocket, pressurized, and then released using a bicycle brake line. Some systems also offer automatic launchers, but these systems are extremely complex, making them difficult to control. These methods have significant limitations, including complex launch methods and the inability to achieve full automatic control of the entire process.

[0061] To this end, the present application provides a device for automatically launching a water rocket, comprising an energy supply air pump module, an air-liquid control unit, a water tank, a release assembly, and a pressure sensor. The energy supply air pump module includes multiple gas output sides, wherein the multiple gas output sides are connected to a first solenoid valve and a second solenoid valve in the air-liquid control unit, and the second solenoid valve is connected to the release assembly; the multiple gas output sides are used to output gas, wherein the gas is used to provide pressure for the water tank and the release assembly; the water tank includes an input side, an output side, and a bidirectional transmission side, wherein one input side is connected to the first solenoid valve, one output side is connected to the fourth solenoid valve in the air-liquid control unit, and one bidirectional transmission side is connected to the third solenoid valve in the air-liquid control unit, and the third solenoid valve is connected to the release assembly; one output side is used to output gas and liquid, wherein the gas and liquid are used to release pressure for the release assembly; one bidirectional transmission side is used to output or input liquid, wherein the liquid is used to provide pressure or release pressure for the release assembly; the pressure sensor is connected to the release assembly and is used to measure the pressure of the liquid in the release assembly; the release assembly includes a servo and a release element, and the servo is used to control the release element. With this device, the effect of simply achieving fully automatic launch of a water rocket can be achieved.

[0062] In the embodiment of the present application, the executing entity may be an automatic water rocket launching device in an automatic water rocket launching system. In actual application, the automatic water rocket launching device may be an automatic launching platform, which is not limited here.

[0063] The following combination Figure 1 The device for automatically launching a water rocket in an embodiment of the present application is described in detail.

[0064] Please see Figure 1 , Figure 1 A schematic diagram of the structure of a device for automatically launching a water rocket provided in an embodiment of the present application is shown as follows: Figure 1 The device for automatically launching a water rocket shown comprises:

[0065] The power supply air pump module 110, the gas-liquid control unit 120, the water storage tank 130, the release component 140 and the pressure sensor 150, wherein the power supply air pump module 110 includes multiple gas output sides, wherein the multiple gas output sides are connected to the first solenoid valve 121 and the second solenoid valve 122 in the gas-liquid control unit 120, and the second solenoid valve 122 is connected to the release component 140; the multiple gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water storage module 130 and the release component 140; the water storage tank 130 includes an input side, an output side and a bidirectional transmission side, wherein one input side is connected to the first solenoid valve 121, and one output side is connected to the first solenoid valve 121. It is connected to the fourth solenoid valve 124 in the gas-liquid control unit, a two-way transmission side is connected to the third solenoid valve 123 in the gas-liquid control unit 120, and the third solenoid valve 123 is connected to the release component 140; an output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release component 140; a two-way transmission side is used to: output or input liquid, and the liquid is used to provide pressure or release pressure for the release component 140: a pressure sensor 150 is connected to the release component 140, and is used to measure the liquid pressure in the release component 140; the release component 140 includes the servo 160 and the release element 161, and the servo 160 is used to control the release element 161.

[0066] In the above embodiments of the present application, the automatic launch of the water rocket can be achieved through the connection of the above devices, the operation is relatively simple, and a large amount of resources can be saved.

[0067] Among them, the energy supply air pump module 110 includes an air pump 192 and a protective plate 191, which can output gas, which can be air. The air pump is connected to a control circuit, which can directly realize the energy output and control of the air pump, the control of the gas-liquid control pipeline and the control of the water rocket release component. The control circuit can be powered by three 18650 lithium batteries. The gas-liquid control unit 120 includes multiple solenoid valves, which may include a first solenoid valve 121, a second solenoid valve 122, a third solenoid valve 123, and a fourth solenoid valve 124. The release component 140 includes a release element 161 and a servo 160. The pressure sensor 150 includes a hydraulic sensor. The servo 160 can control the release element to release pressure and launch the water rocket.

[0068] The water rocket launch process is as follows: The first stage is the water filling phase. The power supply air pump module 110 is opened, and the first and third solenoid valves 121 and 123 are opened. The water in the water tank 130 is pressed into the release assembly 140 by the pressure of the power supply air pump module 110, entering the water rocket. The water storage level can be calculated by reading the pressure value from the pressure sensor 150. Once the pressure reaches a preset value, the first and third solenoid valves 121 and 123 are closed, shutting down the power supply air pump module 110. The second stage is the pressurization phase. The second solenoid valve 122 is opened, and the power supply air pump module 110 is turned on. Gas passes through the second solenoid valve 122 and enters the water rocket through the release assembly 140. The pressure value can be calculated by reading the pressure value from the pressure sensor 150. Once the pressure reaches a preset value, the second solenoid valve 122 is closed, shutting down the power supply air pump module 110. The third stage is the release phase. By controlling the servo 160, the release assembly 140 is controlled, completing the launch of the water rocket. The fourth group is for releasing pressure to recover liquid, which is achieved by controlling the third solenoid valve 123 and the fourth solenoid valve 124 to open. That is, the pressure in the release assembly 140 is released to pressurize the water back to the water storage tank 170.

[0069] In some embodiments, the device also includes: a controller 180; a controller 180 is connected to the power supply air pump module 110, the gas-liquid control unit 120, the pressure sensor 150, the servo 160 and the communication module 190, wherein a controller 180 is used to control the opening and closing of the power supply air pump module 110, the gas-liquid control unit 120, the pressure sensor 150 and the servo 160 and to communicate with the communication module 190.

[0070] In the above embodiment of the present application, the controller 180 can be used to control each module of the water rocket, thereby achieving the purpose of automatic launch and reducing complicated operating steps.

[0071] For details, please see Figure 2 , Figure 2 This is a schematic diagram of a controller for automatically launching a water rocket provided by the present application, wherein the controller 180 is respectively connected to the energy supply air pump module 110, the first solenoid valve 121, the second solenoid valve 122, the third solenoid valve 123 and the fourth solenoid valve 124 in the gas-liquid control unit 120, the pressure sensor 150, the steering gear 160 and the communication module 190. The controller 180 is used to control the opening and closing of the energy supply air pump module 110, the gas-liquid control unit 120, the pressure sensor 150 and the steering gear 160, and to communicate with the communication module 190. The communication module 190 is connected to the App (application) host computer, which can be a mobile phone, computer and other devices.

[0072] Furthermore, the launch pad structure can be constructed of acrylic, with mortise and tenon joints and screws securing all supports. The inflation and pressurization system utilizes a differential pressure method to simulate the process of refueling a real rocket with liquid fuel. Water pressure is measured using a pressure measurement method for easy measurement. The controller directly controls the gas-liquid control unit, measures the pressure sensor, and drives the air pump module, reducing the overall system coupling and making the entire area modular. Using a host computer, it can be connected to devices such as mobile phones and computers for control.

[0073] In some embodiments, the power supply air pump module 110 includes: an air pump 192 and a protective plate 191, wherein the protective plate 191 is connected to the air pump 192 to protect the air pump from overpressure and overheating.

[0074] In the above embodiment of the present application, the protective plate 191 can implement overpressure and overheating protection for the air pump 192, thereby ensuring safety.

[0075] In the above Figure 1 In the process shown, the present application provides a device for automatically launching a water rocket, including an energy supply air pump module, an air-liquid control unit, a water tank, a release assembly and a pressure sensor, wherein the energy supply air pump module includes multiple gas output sides, wherein the multiple gas output sides are connected to the first solenoid valve and the second solenoid valve in the air-liquid control unit, and the second solenoid valve is connected to the release assembly; the multiple gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water tank and the release assembly; the water tank includes an input side, an output side and a bidirectional transmission side, wherein an input side is connected to the first solenoid valve, an output side is connected to the fourth solenoid valve in the air-liquid control unit, a bidirectional transmission side is connected to the third solenoid valve in the air-liquid control unit, and the third solenoid valve is connected to the release assembly; an output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release assembly; a bidirectional transmission side is used to: output or input liquid, and the liquid is used to provide pressure or release pressure for the release assembly: the pressure sensor is connected to the release assembly for measuring the liquid pressure in the release assembly; the release assembly includes a servo and a release element, and the servo is used to control the release element. The device can achieve the effect of simply realizing the fully automatic launching of the water rocket.

[0076] Previous article passed Figure 1 and Figure 2 The device for automatically launching water rockets is described below. Figure 3 Describe the method for automatically launching a water rocket.

[0077] The following combination Figure 3 The method for automatically launching a water rocket in an embodiment of the present application is described in detail.

[0078] Please see Figure 3 ,Figure 3 A flow chart of a method for automatically launching a water rocket provided in an embodiment of the present application is shown as follows: Figure 3 The method of automatically launching a water rocket shown includes:

[0079] Step 310: Press the liquid into the release assembly by controlling the gas-liquid control unit.

[0080] In some embodiments, the liquid is pressed into the release component by controlling the gas-liquid control unit, including: pressing the gas in the power air pump into the water tank by controlling a solenoid valve in the gas-liquid control unit; and pressing the liquid in the water tank into the release component by controlling a solenoid valve in the gas-liquid control unit.

[0081] In the above embodiment of the present application, the solenoid valve can be used to control the gas to enter the water tank and the liquid to enter the release component, thereby achieving a pressurization effect.

[0082] In some embodiments, after the liquid is pressed into the release assembly, Figure 2 The method shown also includes: calculating the water storage amount in the release component using the pressure differential water injection method based on the value of the pressure sensor.

[0083] In the above embodiment of the present application, the optimal time to release the liquid is determined by the value of the pressure sensor, which can ensure that the water rocket can be accurately launched automatically.

[0084] Step 320: When the water storage amount in the release component reaches a preset water storage amount, the gas is pressed into the release component by controlling the gas-liquid control unit.

[0085] In some embodiments, the gas is pressed into the release component by controlling the gas-liquid control unit, including: pressing the gas in the power supply air pump into the release component by controlling a solenoid valve in the gas-liquid control unit.

[0086] In the above embodiment of the present application, the gas can also be directly pressed into the release component through the solenoid valve to increase the pressure inside the release component.

[0087] Step 330: When the pressure in the release assembly reaches a preset pressure value, the water rocket is released and launched by controlling the release assembly.

[0088] In some embodiments, a water rocket is released and launched by controlling a release assembly, including: pressing the liquid in the release assembly into a water tank by controlling the release assembly and a solenoid valve in the gas-liquid control module; and releasing the liquid in the water tank by controlling a solenoid valve in the gas-liquid control module.

[0089] In the above embodiment of the present application, the liquid can be discharged by opening the solenoid valve, thereby achieving the effect of releasing the pressure and recovering the water rocket midway.

[0090] Among them, the water rocket is unlocked and connected with the release component through the servo control release component to launch the water rocket.

[0091] Figure 3 In the process shown, by releasing the increased pressure of the gas and liquid in the assembly, the connection between the water rocket and the release assembly is finally unlocked, and the water rocket is launched, which makes the operation simpler.

[0092] Previous article passed Figure 3 Describes the method of automatically launching water rockets. Figures 4-5 Describe a device for automatically launching water rockets.

[0093] Please refer to Figure 4 , is a schematic block diagram of a device 400 for automatically launching a water rocket provided in an embodiment of the present application. The device 400 may be a module, program segment or code on an electronic device. The device 400 is similar to the above-mentioned Figure 2 The method embodiment corresponds to the embodiment that can be executed Figure 2 The various steps involved in the method embodiment and the specific functions of the device 400 can be found in the description below. To avoid repetition, detailed description is appropriately omitted here.

[0094] Optionally, the device 400 includes:

[0095] A first control module 410 is configured to pressurize the liquid into the release assembly by controlling the gas-liquid control unit;

[0096] The second control module 420 is configured to pressurize gas into the release assembly by controlling the gas-liquid control unit when the water storage amount in the release assembly reaches a preset water storage amount;

[0097] The third control module 430 is used to release and launch the water rocket by controlling the release assembly when the pressure in the release assembly reaches a preset pressure value.

[0098] Optionally, the first control module is specifically configured to:

[0099] By controlling a solenoid valve in the gas-liquid control unit, the gas in the energy supply air pump is pressed into the water storage tank; by controlling a solenoid valve in the gas-liquid control unit, the liquid in the water storage tank is pressed into the release component.

[0100] Optionally, the second control module is specifically configured to:

[0101] By controlling a solenoid valve in the gas-liquid control unit, the gas in the power supply pump is pressed into the release component.

[0102] Optionally, the third control module is specifically configured to:

[0103] By controlling the release component and a solenoid valve in the gas-liquid control module, the liquid in the release component is pressed into the water tank; by controlling a solenoid valve in the gas-liquid control module, the liquid in the water tank is released.

[0104] Optionally, the device further includes:

[0105] The calculation module is used for calculating the water storage amount in the release component by using the pressure differential water injection method based on the value of the pressure sensor after the first control module presses the liquid into the release component.

[0106] Please refer to Figure 5 This is a schematic block diagram of the structure of a device for automatically launching a water rocket provided in an embodiment of the present application. The device may include a memory 510 and a processor 520. Optionally, the device may also include: a communication interface 530 and a communication bus 540. The device is similar to the above-mentioned Figure 2 The method embodiment corresponds to the embodiment that can be executed Figure 2 The various steps involved in the method embodiment and the specific functions of the device can be found in the description below.

[0107] Specifically, the memory 510 is used to store computer-readable instructions.

[0108] Processor 520 is used to process the readable instructions stored in the memory and can execute Figure 2 The steps in the method.

[0109] The communication interface 530 is used for signaling or data communication with other node devices, for example, for communication with a server or terminal, or for communication with other device nodes, but the embodiments of the present application are not limited thereto.

[0110] The communication bus 540 is used to realize direct connection and communication among the above components.

[0111] Among them, the communication interface 530 of the device in the embodiment of the present application is used to communicate signaling or data with other node devices. The memory 510 can be a high-speed RAM memory or a non-volatile memory (non-volatile memory), such as at least one disk memory. The memory 510 can also be at least one storage device located away from the aforementioned processor. The memory 510 stores computer-readable instructions. When the computer-readable instructions are executed by the processor 520, the electronic device executes the above-mentioned Figure 2The method process shown. The processor 520 can be used on the device 400 and is used to perform the functions in the present application. Exemplarily, the above-mentioned processor 520 can be a general-purpose processor, a digital signal processor (DSP), an application-specific integrated circuit (ASIC), a field programmable gate array (FPGA) or other programmable logic device, a discrete gate or transistor logic device, or a discrete hardware component, and the embodiments of the present application are not limited thereto.

[0112] The embodiment of the present application further provides a readable storage medium, wherein when the computer program is executed by a processor, Figure 2 The method process in the illustrated method embodiment is performed by the electronic device.

[0113] Those skilled in the art will clearly understand that, for the convenience and brevity of description, the specific working process of the device described above can refer to the corresponding process in the aforementioned method, and will not be described in detail here.

[0114] In summary, the embodiments of the present application provide an apparatus, method, equipment and storage medium for automatically launching a water rocket. The method includes an energy supply air pump module, a gas-liquid control unit, a water tank, a release component and a pressure sensor, wherein the energy supply air pump module includes multiple gas output sides, wherein the multiple gas output sides are connected to the first solenoid valve and the second solenoid valve in the gas-liquid control unit, and the second solenoid valve is connected to the release component; the multiple gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water tank and the release component; the water tank includes an input side, an output side and a bidirectional transmission side, wherein an input side is connected to the first solenoid valve, an output side is connected to the fourth solenoid valve in the gas-liquid control unit, a bidirectional transmission side is connected to the third solenoid valve in the gas-liquid control unit, and the third solenoid valve is connected to the release component; an output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release component; a bidirectional transmission side is used to: output or input liquid, and the liquid is used to provide pressure or release pressure for the release component: the pressure sensor is connected to the release component for measuring the liquid pressure in the release component; the release component includes a servo and a release element, and the servo is used to control the release element.

[0115] In several embodiments provided in the present application, it should be understood that the disclosed apparatus and method can also be implemented by other means. The apparatus embodiments described above are only illustrative, for example, the flowcharts and block diagrams in the drawings show the possible implementation architecture, function and operation of the apparatus, method and computer program product according to the embodiments of the present application. In this regard, each block in the flowchart or block diagram can represent a module, a program segment or a part of code, which contains one or more executable instructions for implementing the specified logic function. It should also be noted that in some alternative implementations, the functions noted in the blocks can occur in different order from that shown in the drawings. For example, two consecutive blocks can actually be executed substantially in parallel, and sometimes they can be executed in reverse order, depending on the functions involved. It should also be noted that each block in the block diagram and / or flowchart, and the combination of blocks in the block diagram and / or flowchart, can be implemented by a dedicated hardware-based system for performing the specified function or action, or can be implemented by a combination of dedicated hardware and computer instructions.

[0116] In addition, the functional modules in the various embodiments of the present application can be integrated together to form an independent part, or each module can exist independently, or two or more modules can be integrated to form an independent part.

[0117] If the functions are implemented in the form of software function modules and sold or used as independent products, they can be stored in a computer readable storage medium. Based on this understanding, the technical solutions of the present application can be embodied in the form of a software product, and the computer software product is stored in a storage medium, including a number of instructions for causing a computer device (which can be a personal computer, a server, or a network device, etc.) to execute all or part of the steps of the methods described in the various embodiments of the present application. The aforementioned storage medium includes: a U disk, a mobile hard disk, a read-only memory (ROM, Read-Only Memory), a random access memory (RAM, Random Access Memory), a magnetic disk or an optical disk, and various program code storage media.

[0118] The foregoing is merely an embodiment of the present application and is not intended to limit the scope of protection of the present application. Various modifications and variations are possible for those skilled in the art. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present application shall be included within the scope of protection of the present application. It should be noted that similar reference numerals and letters represent similar items in the following figures. Therefore, once an item is defined in one figure, it does not need to be further defined or explained in subsequent figures.

[0119] The above description is merely a specific embodiment of the present application, but the scope of protection of the present application is not limited thereto. Any changes or substitutions that can be easily conceived by a person skilled in the art within the technical scope disclosed in the present application should be included in the scope of protection of the present application. Therefore, the scope of protection of the present application should be based on the scope of protection of the claims.

[0120] It should be noted that, in this document, relational terms such as first and second, etc., are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply the existence of any such actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article, or device comprising 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 comprising the element.

Claims

1. A device for automatically launching a water rocket, characterized in that: include: Energy supply air pump module, air-liquid control unit, water storage tank, release assembly and pressure sensor, among which, The energy supply air pump module includes multiple gas output sides, wherein the multiple gas output sides are connected to the first solenoid valve and the second solenoid valve in the gas-liquid control unit, the second solenoid valve is connected to the release component, the energy supply air pump module includes an air pump and a protective plate, the air pump is used to output gas, the air pump is connected to a control circuit, the control circuit is used for energy output and control of the air pump, control of the gas-liquid control pipeline and control of the release component of the water rocket; The plurality of gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water storage tank and the release assembly; The water storage tank includes an input side, an output side, and a bidirectional transmission side, wherein the input side is connected to the first solenoid valve, the output side is connected to the fourth solenoid valve in the gas-liquid control unit, the bidirectional transmission side is connected to the third solenoid valve in the gas-liquid control unit, and the third solenoid valve is connected to the release assembly; The one output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release component; The one bidirectional transmission side is used to output or input liquid, and the liquid is used to provide pressure or release pressure for the release component. The pressure sensor is connected to the release assembly and is used to measure the liquid pressure in the release assembly. The water storage capacity in the release assembly is calculated by using the differential pressure injection method based on the value of the pressure sensor; The release assembly includes a steering gear and a release element, wherein the steering gear is used to control the release element; When launching a water rocket: by controlling the gas-liquid control unit, the liquid is pressed into the release component; when the water storage volume in the release component reaches a preset water storage volume, by controlling the gas-liquid control unit, the gas is pressed into the release component; when the pressure in the release component reaches a preset pressure value, the water rocket is released and launched by controlling the release component.

2. The device according to claim 1, characterized in that The device further includes: a controller; The one controller is connected to the power supply air pump module, the gas-liquid control unit, the pressure sensor, the servo and the communication module, wherein the one controller is used to control the opening and closing of the power supply air pump module, the gas-liquid control unit, the pressure sensor and the servo and to communicate with the communication module.

3. The device according to claim 1 or 2, characterized in that The energy supply air pump module includes: an air pump and a protective plate, wherein the protective plate is connected to the air pump and is used to protect the air pump from overpressure and overheating.

4. A method for automatically launching a water rocket, characterized in that: include: By controlling the gas-liquid control unit, the liquid is pressed into the release component; When the water storage amount in the release component reaches a preset water storage amount, the gas is pressed into the release component by controlling the gas-liquid control unit; When the pressure in the release assembly reaches a preset pressure value, the release assembly is controlled to release and launch the water rocket; After the liquid is pressed into the release assembly, the method further comprises: calculating the amount of water stored in the release assembly using a differential pressure injection method based on the value of the pressure sensor; The automatic launch of the water rocket is achieved by a device for automatically launching the water rocket, which includes: an energy supply air pump module, an air-liquid control unit, a water storage tank, a release component and a pressure sensor, wherein: The energy supply air pump module includes multiple gas output sides, wherein the multiple gas output sides are connected to the first solenoid valve and the second solenoid valve in the gas-liquid control unit, the second solenoid valve is connected to the release component, the energy supply air pump module includes an air pump and a protective plate, the air pump is used to output gas, the air pump is connected to a control circuit, the control circuit is used for energy output and control of the air pump, control of the gas-liquid control pipeline and control of the release component of the water rocket; The plurality of gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water storage tank and the release assembly; The water storage tank includes an input side, an output side, and a bidirectional transmission side, wherein the input side is connected to the first solenoid valve, the output side is connected to the fourth solenoid valve in the gas-liquid control unit, the bidirectional transmission side is connected to the third solenoid valve in the gas-liquid control unit, and the third solenoid valve is connected to the release assembly; The one output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release component; The one bidirectional transmission side is used to output or input liquid, and the liquid is used to provide pressure or release pressure for the release component. The pressure sensor is connected to the release assembly and is used to measure the pressure of the liquid in the release assembly; The release assembly includes a steering gear and a release element, and the steering gear is used to control the release element.

5. The method according to claim 4, characterized in that The method of pressing the liquid into the release component by controlling the gas-liquid control unit includes: By controlling a solenoid valve in the gas-liquid control unit, the gas in the energy supply air pump is pressed into the water storage tank; By controlling a solenoid valve in the gas-liquid control unit, the liquid in the water tank is pressed into the release assembly.

6. The method according to claim 4 or 5, characterized in that The method of controlling the gas-liquid control unit to pressurize the gas into the release assembly comprises: By controlling a solenoid valve in the gas-liquid control unit, the gas in the energy supply air pump is pressed into the release component.

7. The method according to claim 4 or 5, characterized in that The method of releasing and launching the water rocket by controlling the release assembly includes: By controlling the release component and a solenoid valve in the gas-liquid control module, the liquid in the release component is pressed into the water storage tank; The liquid in the water tank is released by controlling a solenoid valve in the gas-liquid control module.

8. A device for automatically launching a water rocket, characterized in that: include: a first control module, configured to press the liquid into the release assembly by controlling the gas-liquid control unit; a second control module, configured to pressurize gas into the release assembly by controlling the gas-liquid control unit when the water storage amount in the release assembly reaches a preset water storage amount; a third control module, configured to release and launch the water rocket by controlling the release assembly when the pressure in the release assembly reaches a preset pressure value; After the first control module presses the liquid into the release component, it is also used to: calculate the water storage amount in the release component by using the pressure differential water injection method based on the value of the pressure sensor; The automatic launch of the water rocket is achieved by a device for automatically launching the water rocket, which includes: an energy supply air pump module, an air-liquid control unit, a water storage tank, a release assembly and a pressure sensor, wherein: The energy supply air pump module includes multiple gas output sides, wherein the multiple gas output sides are connected to the first solenoid valve and the second solenoid valve in the gas-liquid control unit, the second solenoid valve is connected to the release component, the energy supply air pump module includes an air pump and a protective plate, the air pump is used to output gas, the air pump is connected to a control circuit, the control circuit is used for energy output and control of the air pump, control of the gas-liquid control pipeline and control of the release component of the water rocket; The plurality of gas output sides are used to: output gas, wherein the gas is used to provide pressure for the water storage tank and the release assembly; The water storage tank includes an input side, an output side, and a bidirectional transmission side, wherein the input side is connected to the first solenoid valve, the output side is connected to the fourth solenoid valve in the gas-liquid control unit, the bidirectional transmission side is connected to the third solenoid valve in the gas-liquid control unit, and the third solenoid valve is connected to the release assembly; The one output side is used to: output gas and liquid, and the gas and liquid are used to release pressure for the release component; The one bidirectional transmission side is used to output or input liquid, and the liquid is used to provide pressure or release pressure for the release component. The pressure sensor is connected to the release assembly and is used to measure the pressure of the liquid in the release assembly; The release assembly includes a steering gear and a release element, and the steering gear is used to control the release element.

9. An electronic device, characterized in that: include: A memory and a processor, wherein the memory stores computer-readable instructions, and when the computer-readable instructions are executed by the processor, the steps of the method according to any one of claims 4 to 7 are executed.

10. A computer-readable storage medium, characterized in that include: A computer program, when running on a computer, causes the computer to perform the method according to any one of claims 4 to 7.

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