CN210572651U - Test maintenance system - Google Patents
Test maintenance system Download PDFInfo
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- CN210572651U CN210572651U CN201920798578.4U CN201920798578U CN210572651U CN 210572651 U CN210572651 U CN 210572651U CN 201920798578 U CN201920798578 U CN 201920798578U CN 210572651 U CN210572651 U CN 210572651U
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Abstract
The utility model provides a test maintenance system for emergency power supply part to the aircraft tests and maintains, include: the emergency power supply testing device comprises an emergency power supply part testing device, a special testing cable and an RS232 testing terminal; wherein, the emergency power supply component test equipment is in communication connection with the special test cable and the RS232 test terminal. The utility model discloses a computer terminal carries out the communication through RS232 test terminal control and emergency power supply part test equipment, can test emergency power supply through test terminal, parts such as charger and battery to combine emergency power supply part test equipment can realize corresponding emergency power supply monitoring and maintenance, filled this maintenance project at internal technological blank.
Description
Technical Field
The utility model relates to an electronic equipment test maintenance technical field particularly, relates to a test maintenance system for test and maintenance are carried out emergency power supply part on the aircraft.
Background
At present, in order to attract passengers, a large number of emergency power supply components are installed on an airplane by an airline company so as to meet the emergency lighting requirement in an emergency state, but the newly installed emergency power supply components are generally produced abroad, the maintenance is also carried out abroad, and no factory can maintain the components at home, so that the problems of long maintenance period, high maintenance cost, requirement of a large number of spare parts and the like are caused, and the problems cause the delay of the airplane of the airline company and the reduction of the service quality, and directly influence the economic benefit of the airline company.
Therefore, it is an urgent need to develop a system for testing and repairing emergency power components.
SUMMERY OF THE UTILITY MODEL
The present invention aims at least solving one of the technical problems existing in the prior art or the related art.
Therefore, an object of the present invention is to provide a test maintenance system.
In view of this, according to the utility model discloses an aim of the utility model, the utility model provides a test maintenance system for test and maintain the emergency power supply part on the aircraft, include: the system comprises emergency power supply component test equipment, an RS232 test terminal and a special test cable; wherein, emergency power supply part test equipment and special test cable and RS232 test terminal communication connection.
The utility model provides a test maintenance system, including emergency power supply part test equipment, special test cable and RS232 test terminal, wherein, emergency power supply part test equipment for monitoring and maintenance emergency power supply part, special test cable are used for designing according to hardware interface circuit specially, with the continuity test of realization to test maintenance system, RS232 test terminal for emergency power supply part's inside self-checking system's data monitoring, with the generation trouble report. The utility model discloses an emergency power supply test assembly handles and controls emergency power supply's mode of operation and load simulation test, can monitor emergency power supply core module's operating condition through RS232 test terminal, monitors working data to combine emergency power supply part maintenance equipment can realize monitoring and the maintenance that corresponds emergency power supply part, filled this maintenance project at internal technological blank.
In one embodiment, the emergency power component repair apparatus includes: the device comprises a selection module, a load module and a simulation module; the load function module is logically connected with the control function module and the display function module.
In the technical scheme, the emergency power supply component maintenance equipment comprises a selection module, a load module and a simulation module, the test and maintenance system can complete the test and maintenance of the selection module, the load module and the simulation module through the functional modules, and the monitoring and maintenance of the components are realized through the corresponding functional modules of the emergency power supply component maintenance equipment.
In one embodiment, the RS232 test terminal includes: the device comprises a monitoring module, a detection module and a generation module.
In the technical scheme, the RS232 test terminal comprises a monitoring module and a detection module, the working state of the emergency power supply component on the airplane can be monitored through the RS232 test terminal, the acquisition of the working data of the emergency power supply on the airplane can be realized, and the monitoring of the functions can be realized through each functional module provided by the RS232 test terminal.
The monitoring module monitors data according to different emergency power supply components, and specifically, firstly, different monitoring data are selected for testing different emergency power supply components through an RS232 test terminal so as to observe the data type generated by the test terminal; the detection module is used for carrying out decoding operation according to different test data, specifically, according to the hardware connection relation of the tested emergency power supply component, through an RS232 test terminal, and the decoding module is used for sending fault data to the CPU of the emergency power supply component for decoding so as to test whether each function is normal or not; the generation module is used for generating test data, the test data is a fault test result report of the emergency power supply component, the test data further comprises a function test condition and a conduction condition of each electronic component in the emergency power supply component, specifically, the fault test report can be generated through the generation module of the RS232 test terminal, and the report is downloaded so that the emergency power supply component maintenance equipment can maintain the tested emergency power supply component according to the report.
To sum up, the utility model discloses an emergency power supply test assembly handles and controls emergency power supply's mode of operation and load simulation test, can monitor the operating condition of emergency power supply kernel module through RS232 test terminal, monitors working data to combine emergency power supply part maintenance equipment can realize monitoring and the maintenance that corresponds emergency power supply part, filled this maintenance project at internal technological blank.
Additional aspects and advantages of the invention will be set forth in part in the description which follows and, in part, will be obvious from the description, or may be learned by practice of the invention.
Drawings
The above and/or additional aspects and advantages of the present invention will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
FIG. 1 shows a schematic block diagram of a test and repair system of one embodiment of the present invention;
fig. 2 shows a schematic block diagram of an emergency power supply component repair device of an embodiment of the present invention;
fig. 3 shows a schematic control panel diagram of an emergency power component maintenance device according to an embodiment of the present invention;
fig. 4 shows a schematic block diagram of a software test terminal according to an embodiment of the present invention.
Detailed Description
In order to make the aforementioned objects, features and advantages of the present invention more clearly understood, the present invention will be described in further detail with reference to the accompanying drawings and detailed description. It should be noted that the embodiments and features of the embodiments of the present application may be combined with each other without conflict.
In the following description, numerous specific details are set forth in order to provide a thorough understanding of the present invention, however, the present invention may be practiced in other ways than those specifically described herein, and therefore the scope of the present invention is not limited by the specific embodiments disclosed below.
A test and repair system according to some embodiments of the present invention is described below with reference to fig. 1-4.
As shown in fig. 1, the utility model provides a test maintenance system for test and maintenance are carried out to emergency power supply part on the aircraft, include: the emergency power supply component testing device 11, the special testing cable 14 and the RS232 testing terminal 12; wherein, the emergency power supply component test device 11 is in communication connection with the RS232 test terminal 12.
The utility model provides a test maintenance system, including emergency power supply part test equipment 11, special test cable 14 and RS232 test terminal 12, wherein, emergency power supply part test equipment 11 for monitoring and maintenance emergency power supply part, RS232 test terminal 12 for the function of simulation emergency power supply part, in order to generate the fault report. The working state of the components can be monitored through the RS232 test terminal 12, the emergency power supply component test equipment 11 is combined to realize monitoring and maintenance of the emergency power supply components, and the technical blank of the maintenance project in China is filled.
In one embodiment, fig. 2 shows a schematic block diagram of an emergency power component testing apparatus 11 according to an embodiment of the present invention, the emergency power component testing apparatus 11 includes: a power supply module 102, a load function module 104, a control function module 106 and a display function module 108; the power supply module 102 is logically connected to the load function module 104, the control function module 106, and the display function module 108.
In this embodiment, the emergency power component testing apparatus 11 includes a power supply module 102, a load function module 104, a control function module 106, and a display function module 108, and these function modules enable the testing and testing system 11 to perform emergency power testing and maintenance, and monitor and maintain the above components through the corresponding function modules of the emergency power component testing apparatus.
In one embodiment, fig. 3 shows a schematic control panel diagram of the emergency power component testing apparatus 11 according to an embodiment of the present invention, which includes a power supply module 102, a load function module 104, a control function module 106, and a display function module 108.
In an embodiment, fig. 4 shows a schematic block diagram of the RS232 testing terminal 12 according to an embodiment of the present invention, and the RS232 testing terminal 12 includes: a monitoring module 202, a detection module 204, and a generation module 206.
In this embodiment, the RS232 test terminal 12 includes a monitoring module 202, a detecting module 204, and a generating module 206, and the RS232 test terminal 12 can simulate the function of an emergency power supply component on an aircraft, can test the function of the emergency power supply on the aircraft, and can simulate the function through each functional module provided by the RS232 test terminal 12.
The monitoring module 202 monitors data according to different emergency power supply components, and specifically, firstly, selects different monitoring data for testing different emergency power supply components through the RS232 test terminal 12 so as to observe the data type generated by the test terminal; the detection module 204 is configured to perform a decoding operation according to different test data, specifically, according to a hardware connection relationship of the tested emergency power supply component, through the RS232 test terminal, and the decoding module is configured to decode fault data sent by the CPU of the emergency power supply component so as to test whether each function is normal; the generating module 206 is configured to generate test data, where the test data is a fault test result report of the emergency power supply component, and further the test data includes a function test condition and a conduction condition of each electronic component in the emergency power supply component, and specifically, the generating module of the RS232 test terminal 12 can generate a fault test report and download the fault test report, so that the emergency power supply component maintenance equipment can maintain the tested emergency power supply component according to the fault test report.
In one embodiment, dedicated test cables are used to: an interface of the emergency power supply part test apparatus 11 is defined and connected to the RS232 test terminal 12.
In this embodiment, the emergency power component testing device 11 includes a power supply module 102, a load function module 104, a control function module 106, and a display function module 108, wherein the power supply module 102 is capable of operating to supply power to other function modules within the device.
To sum up, the utility model provides a test maintenance system can test emergency power supply part through the adoption through RS232 test terminal 12 to combine emergency power supply part test equipment 11 can realize monitoring and the maintenance that corresponds emergency power supply part, filled this maintenance project at internal technical blank.
In the present application, the term "plurality" means two or more unless expressly defined otherwise. The terms "mounted," "connected," "fixed," and the like are to be construed broadly, and for example, "connected" may be a fixed connection, a removable connection, or an integral connection; "coupled" may be direct or indirect through an intermediary. The specific meaning of the above terms in the present invention can be understood according to specific situations by those skilled in the art.
In the present disclosure, the description of the terms "one embodiment," "some embodiments," "specific embodiments," etc., means that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the disclosure. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention, and various modifications and changes may be made by those skilled in the art. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.
Claims (4)
1. A test and repair system for testing and repairing emergency power supply components on an aircraft, comprising:
the system comprises emergency power supply testing equipment, an RS232 testing terminal and a special testing cable;
and the emergency power supply part maintenance equipment is in communication connection with the RS232 test terminal.
2. The test and repair system of claim 1, wherein the emergency power repair device comprises:
the power supply module, the load function module, the control function module and the display function module;
the load function module is logically connected with the control function module and the display function module.
3. The test repair system of claim 1, wherein the RS232 test terminal comprises:
the device comprises a monitoring module, a detection module and a generation module.
4. The test and repair system of claim 1, wherein the dedicated test cable is to:
and defining an interface of the emergency power supply component testing equipment, and connecting the interface with the RS232 testing terminal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920798578.4U CN210572651U (en) | 2019-05-28 | 2019-05-28 | Test maintenance system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920798578.4U CN210572651U (en) | 2019-05-28 | 2019-05-28 | Test maintenance system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210572651U true CN210572651U (en) | 2020-05-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920798578.4U Active CN210572651U (en) | 2019-05-28 | 2019-05-28 | Test maintenance system |
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| Country | Link |
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| CN (1) | CN210572651U (en) |
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- 2019-05-28 CN CN201920798578.4U patent/CN210572651U/en active Active
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