阅读说明：本技术 一种浮空器囊体气密性检测设备及方法 (Aerostat airbag air tightness detection device and method ) 是由 张强辉 李家隆 李蕊 赵春阳 付强 于 2021-02-01 设计创作，主要内容包括：本发明提供一种浮空器囊体气密性检测设备及方法。其中,该设备包括：传感器阵列单元、数据管理单元、数据存储单元及人机交互单元；所述传感器阵列单元用于采集检测过程中的传感器数据；所述数据管理单元用于获取所述传感器阵列单元和电源管理单元中的目标数据,对所述目标数据进行校验和滤波后,得出测试结果并确定浮空器囊体的气密状态；所述目标数据包含所述传感器数据和电源数据；所述数据存储单元用于存储检测过程中检测设备及所述传感器阵列单元输出的测试数据,并实现所述测试数据的导出操作；所述人机交互单元用于图形化显示测试数据。采用本发明公开的浮空器囊体气密性检测设备,提高了囊体气密性的检测效率,及数据的有效率和可读性。(The invention provides aerostat capsule air tightness detection equipment and method. Wherein, this equipment includes: the system comprises a sensor array unit, a data management unit, a data storage unit and a human-computer interaction unit; the sensor array unit is used for acquiring sensor data in the detection process; the data management unit is used for acquiring target data in the sensor array unit and the power management unit, checking and filtering the target data to obtain a test result and determine the airtight state of the aerostat capsule; the target data includes the sensor data and power supply data; the data storage unit is used for storing test data output by the detection equipment and the sensor array unit in the detection process and realizing the export operation of the test data; the human-computer interaction unit is used for displaying the test data in a graphical mode. By adopting the aerostat air tightness detection equipment disclosed by the invention, the detection efficiency of air tightness of the aerostat and the efficiency and readability of data are improved.)

1. The utility model provides an aerostatics utricule gas tightness check out test set which characterized in that includes: the system comprises a sensor array unit, a data management unit, a data storage unit and a human-computer interaction unit;

the sensor array unit is used for acquiring sensor data in the detection process;

the data management unit is used for acquiring target data in the sensor array unit and the power management unit, checking and filtering the target data to obtain a test result and determine the airtight state of the aerostat capsule; the target data includes the sensor data and power supply data;

the data storage unit is used for storing test data output by the detection equipment and the sensor array unit in the detection process, and is connected with external computer equipment through a preset interface to realize the export operation of the test data;

and the human-computer interaction unit is used for displaying the test data based on a graphical mode and realizing interactive operation of parameter setting.

2. The aerostat balloon airtightness detection apparatus according to claim 1, wherein said power supply management unit is connected to said sensor array unit, said data management unit, said human-computer interaction unit and said data storage unit, respectively, and is configured to supply electric energy of different specifications to said sensor array unit, said data management unit, said human-computer interaction unit and said data storage unit.

3. The aerostat capsule airtightness detection apparatus according to claim 1, further comprising: a chassis; the case is used for fixing and installing the power management unit, the sensor array unit, the data management unit, the data storage unit and the human-computer interaction unit.

4. The aerostat capsule airtightness detection apparatus according to claim 3, further comprising: an interface unit; the interface unit is arranged in the case and used for realizing signal transmission and power supply of devices in the case.

5. The aerostat capsule airtightness detection apparatus according to claim 4, wherein said interface unit comprises a sensor interface and a power supply interface;

the power supply interface is connected with the power supply management unit; the power supply interface is used for connecting 220V alternating current outside the case to the power supply management unit;

the sensor interface is connected with the sensor array unit; the sensor interface is used for connecting a sensor signal outside the case to the sensor array unit.

6. The aerostat balloon airtightness detection apparatus according to claim 1, wherein said sensor array unit comprises a voltage sensor module, a differential pressure sensor module, an atmospheric pressure sensor module, a temperature sensor module, a humidity sensor module and corresponding drive circuits;

the voltage sensor module is used for detecting the working voltage of the equipment board level and acquiring the working state of the detection equipment; the pressure difference sensor module is used for measuring the difference value of the gas in the capsule body of the aerostat relative to the atmospheric pressure; the atmospheric pressure sensor module is used for measuring an atmospheric pressure value; the temperature sensor module is used for measuring the atmospheric temperature, the gas temperature inside the aerostat airbag body and the surface temperature of the aerostat airbag body; the humidity sensor module is used for measuring atmospheric humidity.

7. The aerostat capsule air tightness detection device according to claim 1, wherein the sensor array unit is connected with the data management unit and is used for outputting collected sensor data to the data management unit for processing to obtain test data;

the data management unit is connected with the human-computer interaction unit and used for transmitting the test data to the human-computer interaction unit, displaying the test data based on a graphical mode and receiving a control instruction sent by the human-computer interaction unit; the human-computer interaction unit comprises a touch liquid crystal display screen and a driving circuit;

the data management unit is connected with the data storage unit and used for sending the sensor data acquired by the sensor array unit and the airtight state data of the aerostat capsule to the data storage unit for storage.

8. The aerostat capsule airtightness detection apparatus according to claim 1, wherein the power supply management unit is configured to convert externally input 220V alternating current into 24V, 12V, 5V and 3.3V direct current, and to supply electric energy to the sensor array unit, the data management unit, the human-computer interaction unit and the data storage unit, respectively.

9. A method for detecting the air tightness of an aerostat capsule body is characterized by comprising the following steps:

acquiring first temperature data inside an aerostat capsule to be detected based on a first temperature sensor arranged inside the aerostat capsule to be detected; acquiring second temperature data of the surface of the aerostat capsule to be detected based on a second temperature sensor arranged on the surface of the aerostat capsule to be detected; acquiring environmental humidity data around the aerostat capsule to be detected based on a humidity sensor arranged at a preset position in the atmospheric environment around the aerostat capsule to be detected; acquiring atmospheric pressure data around a detection capsule body based on an atmospheric pressure sensor arranged at a preset position in the atmospheric environment around the capsule body of the aerostat to be detected;

the method comprises the steps of triggering detection equipment to be started, circularly acquiring various types of test data acquired by a first temperature sensor, a second temperature sensor, a humidity sensor and an atmospheric pressure sensor according to a preset time period, recording the test data, and displaying the test data and a corresponding dynamic detection result on a preset human-computer interaction unit interface.

10. The aerostat bladder airtightness detection method according to claim 9, wherein said test data comprises at least one of said first temperature data, said second temperature data, said ambient humidity data and said atmospheric pressure data.

Technical Field

The invention relates to the technical field of equipment air tightness detection, in particular to aerostat capsule air tightness detection equipment. In addition, the method also relates to a method for detecting the air tightness of the aerostat capsule.

Background

The aerostat is an aircraft which is provided with helium gas filled into a capsule body and realizes flying by utilizing self buoyancy. The skin material of the aerostat is mostly made of organic materials, and the skin material can be kneaded and aged to different degrees in the processes of processing, storing, transferring and the like, so that the performance of the material is reduced, and the air tightness is poor. The airtightness of the skin of the aerostat is deteriorated, the helium leakage rate inside the aerostat is too high, and the net buoyancy loss in the flight process is too much, so that the flight safety of the aerostat is influenced, and even the flight termination or failure is directly caused in severe conditions. Therefore, before the aerostat executes a flight task, the air tightness of the capsule of the aerostat is detected as a precondition for ensuring the aerostat to fly stably.

At present, in the traditional detection method, a tester measures required parameters in a manual mode, records results and performs post-processing analysis, and the method has the following problems: the air tightness detection period of the bag body is generally longer, the manual test mode is used, the human resources are excessively consumed, and the tester is fatigued after working for a long time, so that the measurement error is easily caused, and the measurement result is influenced; the manual measurement mode is adopted, a serial mode is adopted in the process, the measurement values of different sensors can not be guaranteed to be sampled at the same time, and the analysis of the air tightness detection result is adversely affected; the manual measurement mode is used for determining that the data acquisition frequency is very low, the efficiency is low, enough data volume cannot be acquired for certain tests, and the analysis and judgment of the air tightness result are influenced; the manual measurement mode is used, a plurality of types of sensors are needed, different power supply requirements and communication interfaces are related, the test preparation process is long, and the early-stage preparation time of the flight test is greatly prolonged. In order to solve the problems scientifically and rigorously, how to design an automatic detection device for the air tightness of the aerostat envelope becomes a problem to be solved urgently.

Disclosure of Invention

Therefore, the invention provides aerostat airbag air tightness detection equipment and method, and aims to solve the problems that detection personnel are easy to fatigue, low in efficiency, asynchronous in data, long in preparation period and the like in existing aerostat air tightness detection, and actual use requirements cannot be met.

The invention provides aerostat capsule air tightness detection equipment, which comprises: the system comprises a sensor array unit, a data management unit, a data storage unit and a human-computer interaction unit;

the sensor array unit is used for acquiring sensor data in the detection process;

the data management unit is used for acquiring target data in the sensor array unit and the power management unit, checking and filtering the target data to obtain a test result and determine the airtight state of the aerostat capsule; the target data includes the sensor data and power supply data;

the data storage unit is used for storing test data output by the detection equipment and the sensor array unit in the detection process, and is connected with external computer equipment through a preset interface to realize the export operation of the test data;

and the human-computer interaction unit is used for displaying the test data based on a graphical mode and realizing interactive operation of parameter setting.

Furthermore, the power management unit is respectively connected with the sensor array unit, the data management unit, the human-computer interaction unit and the data storage unit and is used for providing electric energy with different specifications for the sensor array unit, the data management unit, the human-computer interaction unit and the data storage unit.

Further, aerostatics utricule gas tightness check out test set, still include: a chassis; the case is used for fixing and installing the power management unit, the sensor array unit, the data management unit, the data storage unit and the human-computer interaction unit.

Further, aerostatics utricule gas tightness check out test set, still include: an interface unit; the interface unit is arranged in the case and used for realizing signal transmission and power supply of devices in the case.

Further, the interface unit comprises a sensor interface and a power supply interface;

the power supply interface is connected with the power supply management unit; the power supply interface is used for connecting 220V alternating current outside the case to the power supply management unit;

the sensor interface is connected with the sensor array unit; the sensor interface is used for connecting a sensor signal outside the case to the sensor array unit.

Further, the sensor array unit comprises a voltage sensor module, a differential pressure sensor module, an atmospheric pressure sensor module, a temperature sensor module, a humidity sensor module and a corresponding driving circuit;

the voltage sensor module is used for detecting the working voltage of the equipment board level and acquiring the working state of the detection equipment; the pressure difference sensor module is used for measuring the difference value of the gas in the capsule body of the aerostat relative to the atmospheric pressure; the atmospheric pressure sensor module is used for measuring an atmospheric pressure value; the temperature sensor module is used for measuring the atmospheric temperature, the gas temperature inside the aerostat airbag body and the surface temperature of the aerostat airbag body; the humidity sensor module is used for measuring atmospheric humidity.

Further, the sensor array unit is connected with the data management unit and used for outputting the acquired sensor data to the data management unit for processing to obtain test data;

the data management unit is connected with the human-computer interaction unit and used for transmitting the test data to the human-computer interaction unit, displaying the test data based on a graphical mode and receiving a control instruction sent by the human-computer interaction unit; the human-computer interaction unit comprises a touch liquid crystal display screen and a driving circuit;

the data management unit is connected with the data storage unit and used for sending the sensor data acquired by the sensor array unit and the airtight state data of the aerostat capsule to the data storage unit for storage.

Further, the power management unit is configured to convert an externally input 220V alternating current into 24V, 12V, 5V and 3.3V direct current, and respectively provide electric energy to the sensor array unit, the data management unit, the human-computer interaction unit and the data storage unit.

Correspondingly, the invention also provides an aerostat capsule air tightness detection method, which comprises the following steps:

acquiring first temperature data inside an aerostat capsule to be detected based on a first temperature sensor arranged inside the aerostat capsule to be detected; acquiring second temperature data of the surface of the aerostat capsule to be detected based on a second temperature sensor arranged on the surface of the aerostat capsule to be detected; acquiring environmental humidity data around the aerostat capsule to be detected based on a humidity sensor arranged at a preset position in the atmospheric environment around the aerostat capsule to be detected; acquiring atmospheric pressure data around a detection capsule body based on an atmospheric pressure sensor arranged at a preset position in the atmospheric environment around the capsule body of the aerostat to be detected;

the method comprises the steps of triggering detection equipment to be started, circularly acquiring various types of test data acquired by a first temperature sensor, a second temperature sensor, a humidity sensor and an atmospheric pressure sensor according to a preset time period, recording the test data, and displaying the test data and a corresponding dynamic detection result on a preset human-computer interaction unit interface.

Further, the first temperature sensor is not in direct contact with the aerostat capsule surface material; the second temperature sensor is in contact with the surface material of the aerostat capsule body through heat-conducting silica gel; the positive pressure end of the differential pressure sensor is connected to the inside of the aerostat balloon through a pressure guiding hose, and the negative pressure end of the differential pressure sensor is arranged in the atmospheric environment outside the aerostat balloon; the humidity sensor is fixed in the atmospheric environment close to the aerostat capsule to be detected; the atmospheric pressure sensor is fixed in the atmospheric environment close to the aerostat envelope to be detected;

the first temperature sensor, the second temperature sensor, the humidity sensor and the atmospheric pressure sensor are connected with the detection device.

Further, the test data includes at least one of the first temperature data, the second temperature data, the ambient humidity data, and the atmospheric pressure data.

By adopting the aerostat airbag air tightness detection equipment, automatic data acquisition and storage are realized, excessive manual participation is not needed in the detection process, the operation is convenient, the detection result is displayed in a graphical mode in real time, the data readability is improved, the air tightness of the aerostat airbag can be quickly and accurately detected, the efficiency of airbag air tightness detection and the data efficiency are greatly improved, and the aerostat airbag air tightness detection equipment has guiding significance for planning the aerostat flight task.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly introduced below, and it is obvious that the drawings in the following description are some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.

Fig. 1 is a schematic structural diagram illustrating a component structure of an aerostat capsule air-tightness detection apparatus according to an embodiment of the present invention;

FIG. 2 is a schematic structural diagram of a sensor array unit according to an embodiment of the present invention;

FIG. 3 is a schematic diagram of a data management unit according to an embodiment of the present invention;

FIG. 4 is a schematic diagram of a data storage unit according to an embodiment of the present invention;

fig. 5 is a schematic diagram of an interface unit structure according to an embodiment of the present invention;

FIG. 6 is a schematic diagram of a power management unit according to an embodiment of the present invention;

FIG. 7 is a complete schematic diagram of a device test site provided by an embodiment of the present invention;

fig. 8 is a schematic flow chart of a method for detecting air tightness of an aerostat capsule according to an embodiment of the present invention;

fig. 9 is a schematic physical structure diagram of an electronic device according to an embodiment of the present invention.

Detailed Description

In order to make the objects, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are some, but not all, embodiments of the present invention. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

The following describes an embodiment of the aerostat balloon airtightness detection apparatus (i.e., aerostat balloon airtightness detection apparatus system) in detail based on the present invention. As shown in fig. 1, which is a schematic view of a composition structure of an aerostat capsule airtightness detection apparatus provided in an embodiment of the present invention, a specific implementation process at least includes the following steps: a case 107, a power management unit 106, an interface unit 105, a sensor array unit 101, a data management unit 102, a data storage unit 104, and a human-computer interaction unit 103.

The sensor array unit 101 is used for acquiring sensor data in a detection process; the data management unit 102 is configured to acquire target data in the sensor array unit 101 and the power management unit 106, check and filter the target data, obtain a test result, and determine an airtight state of the aerostat capsule; the target data includes the sensor data and power supply data; the data storage unit 104 is configured to store test data output by the detection device and the sensor array unit 101 during the detection process, and is connected to an external computer device through a preset interface to implement an operation of exporting the test data; the human-computer interaction unit 103 is configured to display the test data based on a graphical manner, and implement interactive operation of parameter setting. The test data at least includes sensor data acquired by the sensor array unit 101 during the detection process and data detected by the detection device during the detection process.

Specifically, as shown in fig. 2, the sensor array unit 101 includes a voltage sensor module 1011, a differential pressure sensor module 1012, an atmospheric pressure sensor module 1013, a temperature sensor module 1014 (including a first temperature sensor and a second temperature sensor), a humidity sensor module 1015, and a corresponding driving circuit. The voltage sensor module 1011 is used for detecting the board-level working voltage of the equipment, and acquiring the working state of the detection equipment; the differential pressure sensor module 1012 is used for measuring the difference value of the gas inside the capsule of the aerostat relative to the atmospheric pressure; the atmospheric pressure sensor module 1013 is configured to measure an atmospheric pressure value; the temperature sensor module 1014 is used for measuring the atmospheric temperature, the gas temperature inside the aerostat balloon and the temperature of the aerostat balloon surface; the humidity sensor module 1014 is used to measure atmospheric humidity.

As shown in fig. 3, the sensor array unit 101 is connected to the data management unit 102, and is configured to output the acquired sensor data to the data management unit 102 for processing, so as to obtain test data. The data management unit 102 is connected to the human-computer interaction unit 103, and is configured to transmit the test data to the human-computer interaction unit 103, display the test data based on a graphical manner, and receive a control instruction sent by the human-computer interaction unit 103, so as to implement human-computer interaction control. Specifically, the human-computer interaction unit 103 includes a touch liquid crystal display and a driving circuit. The data management unit 102 includes a sampling circuit module 1021, a main control circuit module 1022, a communication circuit module 1024, and a human-computer interaction control circuit module 1023. The sampling circuit module 1021 is configured to obtain data of the sensor array unit, and send the data to the main control circuit module 1022, and the main control circuit module 1022 performs checksum filtering on the data according to a predetermined algorithm, and calculates a dynamic test result; the main control circuit module 1022 is connected to the human-computer interaction control circuit module 1023 through the communication circuit module 1024, and is used for controlling the human-computer interaction unit 103 and realizing interactive operation of test data display and parameter setting.

In addition, the data management unit 102 is further connected to the data storage unit 104, and is configured to send the sensor data acquired by the sensor array unit 101 and the airtight state data of the aerostat capsule to the data storage unit 104 for storage. As shown in fig. 4, the data storage unit 104 includes a storage controller module 105 and a corresponding SD card storage module 106, a USB controller module 107 and a corresponding USB interface module 108. The SD card memory module 106 is used to store the device status and the sensor array data during the test, and the USB interface module 108 is used to connect with an external PC to realize the data export operation.

As shown in fig. 5, the interface unit 105 includes an electrical connector 1051 and a signal conditioning circuit module 1054, and is functionally divided into two types, i.e., a sensor interface (i.e., a signal interface 1053) and a power supply interface (i.e., a power interface 1052), for supplying power and transmitting signals to each unit of the device, and the signal conditioning circuit module 1054 conditions the acquired sensor signal. In a specific implementation process, the power supply interface may be connected to the power management unit 106, and the power supply interface is used for connecting 220V ac power outside the chassis to the power management unit 106; the sensor interface is connected to the sensor array unit 101, and the sensor interface is used for connecting a sensor signal outside the chassis to the sensor array unit 101.

The power management unit 106 is respectively connected to the sensor array unit 101, the data management unit 102, the human-computer interaction unit 103, and the data storage unit 104, and can provide electric energy of different specifications to the sensor array unit 101, the data management unit 102, the human-computer interaction unit 103, and the data storage unit 104. For example, as shown in fig. 6, in a specific implementation process, the power management unit 106 includes AC/DC converter modules with different specifications, and 220V AC power input from outside can be converted into 24V, 12V, 5V and 3.3V DC power through the AC/DC converter modules with different specifications, so as to respectively provide electric power to the sensor array unit 101, the data management unit 102, the human-computer interaction unit 103 and the data storage unit 104.

In the aerostat capsule airtightness detection apparatus of the present invention, the case may be an integrated case 107, which may be used to fix and mount the power management unit 102, the interface unit 105, the sensor array unit 101, the data management unit 102, the data storage unit 104, and the human-computer interaction unit 103.

As shown in fig. 7, in a specific implementation, the first temperature sensor 1016 may be fixed inside the aerostat capsule to be detected, the first temperature sensor 1016 is not in direct contact with the material of the aerostat capsule, and the first temperature sensor 1016 is connected to a detection device through a signal line; fixing a second temperature sensor 1017 on the surface of the aerostat capsule to be detected, wherein the second temperature sensor 1017 is in close contact with aerostat capsule materials through heat-conducting silica gel, and the second temperature sensor 1017 is connected to detection equipment through a signal line; fixing a differential pressure sensor module 1012 on the surface of an aerostat envelope to be detected, connecting a positive pressure end of the differential pressure sensor module 1012 into the aerostat envelope through a pressure guiding hose, exposing a negative pressure end of the differential pressure sensor module 1012 to the external atmospheric environment of the aerostat envelope, and connecting the differential pressure sensor module 1012 to detection equipment through a signal line; fixing the humidity sensor module 1015 in the atmospheric environment near the aerostat envelope to be detected, approaching the aerostat envelope as much as possible, but not contacting the aerostat envelope, and connecting the humidity sensor module 1015 to a detection device through a signal line; the atmospheric pressure sensor module 1013 is fixed in the atmosphere near the aerostat bladder to be detected, and is as close to the aerostat bladder as possible, and the atmospheric pressure sensor module 1013 is connected to the detection device through a signal line. The detection equipment is powered by alternating current mains supply, and after the detection equipment is powered on, the detection equipment automatically acquires sensor data of various types by triggering a start icon on a man-machine interaction screen and displays the sensor data in two modes, namely a data mode and a curve mode. And setting the time length of the test by triggering a time setting icon on a man-machine interaction screen. The detection equipment dynamically calculates the air tightness parameter of the capsule in a test time period and displays the air tightness parameter on a human-computer interaction screen in a percentage mode; after the test is finished, the computer equipment can be connected through the USB interface, and the data of the test is exported to the computer equipment.

By adopting the aerostat capsule air tightness detection equipment provided by the embodiment of the invention, automatic data synchronous acquisition and storage are realized, excessive manual participation is not needed in the detection process, the operation is convenient, the detection result is displayed in a graphical mode in real time, the readability of data is improved, the air tightness of the aerostat capsule can be quickly and accurately detected, the efficiency of capsule air tightness detection and the effective rate of data are greatly improved, and the aerostat capsule air tightness detection equipment has guiding significance for planning of aerostat flight tasks.

Corresponding to the aerostat airbag air tightness detection device, the invention also provides an aerostat airbag air tightness detection method. Since the embodiment of the method is similar to the above-mentioned embodiment of the apparatus, the description is simple, and for the relevant points, reference may be made to the description of the above-mentioned embodiment of the apparatus, and the embodiment of the aerostat bladder airtightness detection method described below is only illustrative. Fig. 8 is a schematic flow chart of a method for detecting air tightness of an aerostat capsule according to an embodiment of the present invention.

The invention relates to an aerostat capsule air tightness detection method which specifically comprises the following steps:

step 801: acquiring first temperature data inside an aerostat capsule to be detected based on a first temperature sensor arranged inside the aerostat capsule to be detected; acquiring second temperature data of the surface of the aerostat capsule to be detected based on a second temperature sensor arranged on the surface of the aerostat capsule to be detected; acquiring environmental humidity data around the aerostat capsule to be detected based on a humidity sensor arranged at a preset position in the atmospheric environment around the aerostat capsule to be detected; the atmospheric pressure data around the detection capsule are obtained based on an atmospheric pressure sensor arranged at a preset position in the atmospheric environment around the capsule of the aerostat to be detected.

Wherein the first temperature sensor is not in direct contact with aerostat balloon surface material; the second temperature sensor is in contact with the surface material of the aerostat capsule body through heat-conducting silica gel; the positive pressure end of the differential pressure sensor is connected to the inside of the aerostat balloon through a pressure guiding hose, and the negative pressure end of the differential pressure sensor is arranged in the atmospheric environment outside the aerostat balloon; the humidity sensor is fixed in the atmospheric environment close to the aerostat capsule to be detected; the atmospheric pressure sensor is fixed in the atmospheric environment close to the aerostat capsule to be detected. The first temperature sensor, the second temperature sensor, the humidity sensor and the atmospheric pressure sensor are connected with the detection device.

Step 802: the method comprises the steps of triggering detection equipment to be started, circularly acquiring various types of test data acquired by a first temperature sensor, a second temperature sensor, a humidity sensor and an atmospheric pressure sensor according to a preset time period, recording the test data, and displaying the test data and a corresponding dynamic detection result on a preset human-computer interaction unit interface.

After the data preparation work is completed in step 801, in this step, the detection device can be triggered to be turned on, various types of test data acquired by the first temperature sensor, the second temperature sensor, the humidity sensor and the atmospheric pressure sensor are cyclically acquired according to a preset time period, the test data are recorded, analysis processing is performed to obtain a corresponding dynamic detection result, and the test data and the dynamic detection result are displayed on a preset human-computer interaction unit interface. Wherein the test data comprises at least one of first temperature data, second temperature data, ambient humidity data, and atmospheric pressure data.

By adopting the aerostat capsule air tightness detection method provided by the embodiment of the invention, automatic data acquisition and storage are realized, excessive manual participation is not required in the detection process, the operation is convenient, the detection result is displayed in a graphical mode in real time, the readability of data is improved, the air tightness of the aerostat capsule can be quickly and accurately detected, the air tightness detection efficiency of the capsule and the data efficiency are greatly improved, and the aerostat capsule air tightness detection method has guiding significance for planning the aerostat flight task.

Corresponding to the aerostat capsule air tightness detection method, the invention also provides electronic equipment. Since the embodiment of the electronic device is similar to the above method embodiment, the description is simple, and please refer to the description of the above method embodiment, and the electronic device described below is only schematic. Fig. 9 is a schematic physical structure diagram of an electronic device according to an embodiment of the present invention. The electronic device may include: a processor (processor) 901, a memory (memory) 902 and a communication bus 903, wherein the processor 901 and the memory 902 communicate with each other through the communication bus 903. The processor 901 may invoke logic instructions in the memory 902 to execute an aerostat bladder airtightness detection apparatus, the method comprising: acquiring first temperature data inside an aerostat capsule to be detected based on a first temperature sensor arranged inside the aerostat capsule to be detected; acquiring second temperature data of the surface of the aerostat capsule to be detected based on a second temperature sensor arranged on the surface of the aerostat capsule to be detected; acquiring environmental humidity data around the aerostat capsule to be detected based on a humidity sensor arranged at a preset position in the atmospheric environment around the aerostat capsule to be detected; acquiring atmospheric pressure data around a detection capsule body based on an atmospheric pressure sensor arranged at a preset position in the atmospheric environment around the capsule body of the aerostat to be detected; the method comprises the steps of triggering detection equipment to be started, circularly acquiring various types of test data acquired by a first temperature sensor, a second temperature sensor, a humidity sensor and an atmospheric pressure sensor according to a preset time period, recording the test data, and displaying the test data and a corresponding dynamic detection result on a preset human-computer interaction unit interface.

Furthermore, the logic instructions in the memory 902 may be implemented in software functional units and stored in a computer readable storage medium when sold or used as a stand-alone product. Based on such understanding, the technical solution of the present invention may be embodied in the form of a software product, which is stored in a storage medium and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device) to execute all or part of the steps of the method according to the embodiments of the present invention. And the aforementioned storage medium includes: a U-disk, a removable hard disk, a Read-Only Memory (ROM), a Random Access Memory (RAM), a magnetic disk or an optical disk, and other various media capable of storing program codes.

In another aspect, an embodiment of the present invention further provides a computer program product, where the computer program product includes a computer program stored on a non-transitory computer-readable storage medium, where the computer program includes program instructions, and when the program instructions are executed by a computer, the computer is capable of executing the aerostat capsule airtightness detection method provided in the above-mentioned method embodiments, where the method includes: acquiring first temperature data inside an aerostat capsule to be detected based on a first temperature sensor arranged inside the aerostat capsule to be detected; acquiring second temperature data of the surface of the aerostat capsule to be detected based on a second temperature sensor arranged on the surface of the aerostat capsule to be detected; acquiring environmental humidity data around the aerostat capsule to be detected based on a humidity sensor arranged at a preset position in the atmospheric environment around the aerostat capsule to be detected; acquiring atmospheric pressure data around a detection capsule body based on an atmospheric pressure sensor arranged at a preset position in the atmospheric environment around the capsule body of the aerostat to be detected; the method comprises the steps of triggering detection equipment to be started, circularly acquiring various types of test data acquired by a first temperature sensor, a second temperature sensor, a humidity sensor and an atmospheric pressure sensor according to a preset time period, recording the test data, and displaying the test data and a corresponding dynamic detection result on a preset human-computer interaction unit interface.

In yet another aspect, an embodiment of the present invention further provides a non-transitory computer-readable storage medium, on which a computer program is stored, where the computer program is implemented by a processor to perform the aerostat balloon airtightness detection method provided in the foregoing embodiments, where the method includes: acquiring first temperature data inside an aerostat capsule to be detected based on a first temperature sensor arranged inside the aerostat capsule to be detected; acquiring second temperature data of the surface of the aerostat capsule to be detected based on a second temperature sensor arranged on the surface of the aerostat capsule to be detected; acquiring environmental humidity data around the aerostat capsule to be detected based on a humidity sensor arranged at a preset position in the atmospheric environment around the aerostat capsule to be detected; acquiring atmospheric pressure data around a detection capsule body based on an atmospheric pressure sensor arranged at a preset position in the atmospheric environment around the capsule body of the aerostat to be detected; the method comprises the steps of triggering detection equipment to be started, circularly acquiring various types of test data acquired by a first temperature sensor, a second temperature sensor, a humidity sensor and an atmospheric pressure sensor according to a preset time period, recording the test data, and displaying the test data and a corresponding dynamic detection result on a preset human-computer interaction unit interface.

The above-described embodiments are merely illustrative, and the units described as separate parts may or may not be physically separate, and parts displayed as units may or may not be physical units, may be located in one place, or may be distributed on a plurality of network units. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of the present embodiment. One of ordinary skill in the art can understand and implement it without inventive effort.

Through the above description of the embodiments, those skilled in the art will clearly understand that each embodiment can be implemented by software plus a necessary general hardware platform, and certainly can also be implemented by hardware. With this understanding in mind, the above-described technical solutions may be embodied in the form of a software product, which can be stored in a computer-readable storage medium such as ROM/RAM, magnetic disk, optical disk, etc., and includes instructions for causing a computer device (which may be a personal computer, a server, or a network device, etc.) to execute the methods described in the embodiments or some parts of the embodiments.

Finally, it should be noted that: the above examples are only intended to illustrate the technical solution of the present invention, but not to limit it; although the present invention has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical solutions described in the foregoing embodiments may still be modified, or some technical features may be equivalently replaced; and such modifications or substitutions do not depart from the spirit and scope of the corresponding technical solutions of the embodiments of the present invention.