CN211717483U - Parameter measuring device for aviation sensor - Google Patents
Parameter measuring device for aviation sensor Download PDFInfo
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- CN211717483U CN211717483U CN202020114563.4U CN202020114563U CN211717483U CN 211717483 U CN211717483 U CN 211717483U CN 202020114563 U CN202020114563 U CN 202020114563U CN 211717483 U CN211717483 U CN 211717483U
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Abstract
The utility model provides an aerosensor parameter measurement device, include: at least one measuring device; the multi-channel switching device is connected with at least one sensor to be measured and measuring equipment; the industrial personal computer is respectively connected with the measuring equipment and the multi-channel switching device through a channel expansion interface and/or a serial bus; the output device is connected with the industrial personal computer through an output bus; and the storage device is connected with the industrial personal computer through a network bus, wherein the industrial personal computer sends an instruction to control the on-off of a channel in the multi-channel switching device so as to control the opening of the measuring equipment and measure the sensor to be measured. The industrial personal computer controls the switching among the channels to realize the one-by-one test of multiple parameter technical indexes of the multiple sensors to be tested, thereby obviously improving the detection efficiency; and automatic parameter measurement, automatic output and storage are realized.
Description
Technical Field
The utility model belongs to the technical field of the aeroengine sensor, specifically speaking relates to an aerosensor parameter measurement device.
Background
Electrical accessories in aircraft engines are the basic building blocks of each control system, which are applied to the acquisition of various electrical parameters and the regulation of the related control system. The technical indexes of parameters of the aeroengine sensor are high in requirement, and the technical indexes of the parameters of various sensors including weight, identification, size, resistance, current, voltage, temperature, insulation parameters and polarity parameters need to be measured, recorded and filed accurately.
However, in the prior art, the demand of the sensors in the engine is huge, and various sensors with different models, specifications and appearances are involved, and lots of various products are complicated and the quantity fluctuation is large, so that the sensors with different specifications and appearances are difficult to be tested in a unified manner through a pipeline type automatic test.
In order to solve the technical problems, in consideration of equipment quality and finished product safety, sensors of different specifications, models and shapes can be tested one by one at the present stage only in a manual mode to accurately measure technical indexes of various parameters of the sensors, and then measurement results are recorded and filed in a manual mode. Obviously, although the measuring method and the recording method ensure that the technical parameters of each sensor can meet the set specification standard, the technical problems of long product inspection period, low inspection efficiency and high dependence degree on inspection and measurement personnel exist simultaneously.
In view of the above, the prior art should be improved to solve the technical problems that the aeroengine sensor insulation performance measurement period is long, the inspection efficiency is low, and the dependence degree on inspection and measurement personnel is high in the prior art.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the technical problem that overcome prior art not enough, provide one kind and can replace prior art down through the mode of artifical mode measurement aeroengine in a plurality of parameter technical indicator of a plurality of sensors, realize the automatic measurement of parameter, the aerosensor parameter measurement device of automatic output, storage.
The utility model provides an aviation sensor parameter measurement device, measuring device includes: at least one measuring device; the multi-channel switching device is connected with at least one sensor to be measured and the measuring equipment; the industrial personal computer is respectively connected with the measuring equipment and the multi-channel switching device through a channel expansion interface and/or a serial bus; the output device is connected with the industrial personal computer through an output bus; and the storage device is connected with the industrial personal computer through a network bus, wherein the industrial personal computer sends an instruction to control the on-off of a channel in the multi-channel switching device so as to control the opening of the measuring equipment and measure the sensor to be measured.
Preferably, the multichannel switching device comprises a plurality of groups of relays, wherein the input end of each relay is connected with the output end of the measuring unit, the input end of the measuring unit is connected with the output node of the industrial personal computer, and the output end of each relay is connected with the sensor to be measured.
Further preferably, the multi-channel switching device further comprises a control unit, the control unit is connected with the industrial personal computer, and the control unit receives an instruction of the industrial personal computer and controls the suction of the relays in the multi-channel switching device so as to realize the on-off of the channels corresponding to the relays.
Due to the adoption of the technical scheme, compared with the prior art, the utility model have the following advantage:
1. the industrial personal computer sends instructions to the control unit, and the instructions are transmitted and decoded through the serial interface to control switching among the channels, so that the channels communicated with the test equipment can be switched in sequence to realize one-by-one test on multiple parameter technical indexes of the multiple sensors to be tested, thereby replacing the mode of one-by-one test through a manual method in the prior art and obviously improving the detection efficiency;
2. when the measuring unit executes measurement, the preset parameters are read, a counter for calculating the measuring times and a timer for calculating the measuring time are configured, then various parameter technical indexes of the sensor are continuously acquired for many times according to the set acquisition frequency, the acquired data are compared with the standard value in the preset parameters, the counter is increased or decreased once the data are acquired until the counter reaches the set times, meanwhile, the timer times the whole acquisition process, and when the measuring time exceeds the set time, the polarity parameter acquired is judged to have large fluctuation, and an abnormal result is output, so that the rapid measurement of the parameter polarity is realized through the synchronous measurement of the counter and the timer, the measuring efficiency is further improved, and the measuring precision is improved;
3. the method comprises the steps that various parameters measured in a single measurement period, various parameters in the single measurement period, measurement times and upper and lower limits of measurement time are set in preset parameters, return data which do not accord with the preset parameters are abandoned through the range of the various parameters, and the return data which accord with the preset parameters are weighted and averaged to be output as sampling results, so that the accuracy and the reliability of output data are improved;
4. the multi-channel switching module is switched to corresponding channels, and is used for sequentially measuring the technical indexes of parameters of various sensors including weight, identification, size, resistance, current, voltage, temperature, insulation parameters and polarity parameters of the sensors to be measured respectively, and outputting the technical indexes through output equipment, so that a sensor parameter measuring method is optimized, and the automatic measurement of sensor parameters is realized;
5. the output device is connected with the industrial personal computer through an output bus, the output device outputs returned data and sampled data in real time, the output can be displayed through a display, or the data can be directly printed and output through a printer, meanwhile, the storage device is arranged, the storage device is in data connection with the industrial personal computer through a network bus, the measured data can be stored, and further, the measured data can be sorted through establishing a data table or a database, so that the aerial equipment production and test efficiency and quality are improved.
Drawings
Fig. 1 is a flow chart illustrating a flow of a measuring method of an aviation sensor parameter measuring device according to a preferred embodiment of the present invention;
FIG. 2 is a flow chart illustrating the steps of configuring a multi-channel measurement module in the preferred embodiment shown in FIG. 1;
FIG. 3 is a flow chart illustrating the flow of actions performed by the configuration measurement unit in the preferred embodiment shown in FIG. 1;
fig. 4 is a frame diagram showing the frame structure of the aviation sensor parameter measuring device according to the preferred embodiment of the present invention;
wherein: 10. a measuring device; 20. a sensor to be tested; 30. a multi-channel switching device; 31. A relay; 32. a control unit; 40. an industrial personal computer; 50. a serial bus; 60. an output bus; 61. an output device; 70. a network bus; 71. and a storage device.
Detailed Description
An embodiment of the invention for an aviation sensor parameter measurement device will be described below with reference to the accompanying drawings. Those of ordinary skill in the art will recognize that the described embodiments can be modified in various different ways without departing from the spirit and scope of the present invention. Accordingly, the drawings and description are illustrative in nature and not intended to limit the scope of the claims. Furthermore, in the present description, the drawings are not to scale and like reference numerals refer to like parts.
Fig. 1 is a flow chart showing a flow of a measurement method of an aviation sensor parameter measurement device according to a preferred embodiment of the present invention. Referring to fig. 1, the measurement method of the device for measuring parameters of an aviation sensor according to the preferred embodiment of the present invention includes: a step S1 of configuring a multi-channel measuring module connected to the sensor to be measured and the plurality of measuring units; a step S2 of configuring and controlling a control unit for controlling the on-off of the channel in the multi-channel measuring module; step S3 of configuring a serial bus connecting the industrial personal computer and the multi-channel measuring module and configuring a universal expansion interface connecting the industrial personal computer and the plurality of measuring units; step S4 of configuring at least one gear of the measuring unit according to the instruction of the industrial personal computer, and returning data after the measuring unit executes the measuring step; and step S5, outputting the comparison result of the returned data and the preset parameters.
The utility model discloses in, the passageway correspond by a plurality of relays and connect a plurality of sensors that await measuring and a plurality of measuring unit in order to constitute the passageway, it is a plurality of through control the break-make of passageway, also the actuation of the relay that each passageway of control corresponds to break-make through control channel is with the switching that realizes the passageway, then realize measuring one by one in order of a plurality of relays that await measuring. FIG. 2 is a flow chart showing the steps of configuring a multi-channel measurement module in the preferred embodiment shown in FIG. 1. Referring to fig. 2, specifically, a channel switching circuit is configured for each relay, that is, each channel, to correspondingly connect input nodes of the plurality of relays to output nodes of the plurality of measurement units, and to connect the input nodes of the plurality of measurement units to the output node of the industrial personal computer. The single chip microcomputer is used as a control unit of the multi-channel measurement module to send upper computer instructions to the channels, so that the upper computer instructions are correspondingly connected with the switching circuits of the channels. In this embodiment, the industrial personal computer and the control unit are connected through a serial bus, and the control unit is respectively communicated with a plurality of channels through the serial bus, such as an RS232 serial bus, or a universal expansion interface, such as a usb hub, and at the same time, a serial interface communicated with each channel or each relay switching circuit is configured. The industrial personal computer sends an instruction and transmits the instruction to the control unit through the serial bus, and after receiving the instruction, the serial interface of the control unit decodes and transmits the instruction sent by the control unit, controls the on-off and switching of the channel and finally controls the measuring unit to execute corresponding actions.
The multiple measuring units respectively complete different measuring items, for example, the multiple measuring units may be an insulation resistance tester to measure the insulation performance of the sensor, or an electronic scale to measure the mass parameter of the sensor, a vernier caliper to measure the size of the sensor, a scanning gun to measure the initialization parameter of the sensor, and the like, the measuring units may include one or more of the above measuring devices, and, as described above, the channel switching circuit may control the opening of the channel corresponding to a certain relay according to an instruction, thereby achieving single-purpose measurement, or may control the multiple relays to sequentially pass through the channels according to a sequence, thereby achieving the measurement of the technical indexes of the multiple parameters of the sensor one by one, and of course, may also enable some of the channels in the multiple channels to achieve the synchronous measurement of several parameters.
The process that the industrial personal computer sends the instruction to set the measuring unit to the measuring unit is to send an upper instruction through the industrial personal computer according to a transmission protocol and then send the upper instruction to the corresponding at least one measuring unit through the serial bus. FIG. 3 is a flow chart illustrating the flow of actions performed by the configuration measurement unit in the preferred embodiment shown in FIG. 1. Referring to fig. 3, in the preferred embodiment, each measurement unit is respectively configured with a counter for counting the number of times of measurement sampling and a timer for counting the time of measurement sampling, and preset parameters are set for each parameter specification. The preset parameters include various parameters measured in a single measurement period, and an upper limit reference value and a lower limit reference value of each parameter, the number of measurements and the measurement time. After the measurement acquisition is executed, the measurement unit reads the preset parameters, acquires the corresponding parameter values of the current sensor for multiple times continuously according to the set acquisition frequency, compares the measurement results with the reference values in the preset parameters, and after each comparison, if the current parameter values are larger than the reference values, the counter correspondingly executes the step of adding one, and if the current parameter values are smaller than the reference values, the counter correspondingly executes the step of subtracting one. The counter counts until an upper limit reference value or a lower limit reference value of the number of measurements in the preset parameter is reached. Meanwhile, in the process, the timer times the acquisition process, and stops when the timer reaches the upper limit reference value of the measurement time in the preset parameters. Taking the example of measuring the resistance or voltage value at the temperature corresponding to the sensor to be measured, reading normal temperature data (resistance or voltage) in preset parameters in advance, aligning a hot air gun to the sensor to be measured for heating, controlling the channel where the resistance tester or the digital meter is located to be communicated by an industrial personal computer at the moment, setting the resistance tester or the digital meter as a resistance or voltage measuring gear, timing the measuring process by a timer in the continuous measuring process, comparing the measured return data with the normal temperature data in the preset parameters, if the measured return data is greater than the normal temperature parameters, executing the step of adding one by the counter, if the measured return data is less than the normal temperature parameters, executing the step of subtracting one by the counter, stopping the measurement until the upper limit reference value of the measurement times in the preset parameters is reached, or stopping the measurement until the upper limit reference value of the measurement time in.
The process of comparing the measurement result with the reference value in the preset parameter is to compare the multiple groups of return data sampled for many times rapidly with the upper limit reference value and the lower limit reference value of the parameter in the preset parameter one by one, discard the return data which is larger than the upper limit reference value or smaller than the lower limit reference value, respectively carry out weighting and averaging on the multiple groups of return data which are collected for many times and represent different measurement parameters, and take the obtained average value as the final result of sampling.
Fig. 4 is a frame diagram showing the frame structure of the aviation sensor parameter measurement device in this preferred embodiment of the present invention, referring to fig. 4, in this preferred embodiment of the present invention, the aviation sensor parameter measurement device includes a plurality of measurement devices 10, a plurality of sensors 20 to be measured, a multi-channel switching device 30 connecting the measurement devices 10 and the sensors to be measured, and an industrial control connected to the measurement devices 10 and the multi-channel switching device 30 through a channel expansion interface and/or a serial bus. The industrial personal computer 40 sends an instruction to control the on-off of the channels in the multi-channel switching device 30, so as to control the plurality of measuring devices 10 to be started and measure the sensor 20 to be measured.
The multiple channels in the multi-channel switching device 30 are composed of multiple sets of relays 31, the input end of each relay 31 is connected with the output end of the measuring device 10, the input end of the measuring device 10 is connected with the output node of the industrial personal computer 40, and the output end of each relay 31 is connected with the sensor 20 to be measured. The control unit 32 using the single chip as the multi-channel switching device 30 sends the upper computer instructions to the multiple channels, so that the upper computer instructions are correspondingly connected with the switching circuits of the channels. In this embodiment, the industrial personal computer 40 is connected to the control unit 32 via a serial bus 50, and the control unit is connected to a plurality of channels via a serial bus, such as RS232 serial bus, or a universal expansion interface, such as usb hub, and at the same time, a serial interface is configured to be connected to each channel or each relay switching circuit. The industrial personal computer 40 sends an instruction and transmits the instruction to the control unit through the serial bus 50, and after receiving the instruction, the serial interface of the control unit 32 decodes and transmits the instruction sent by the control unit, controls the on-off and switching of the channel, and finally controls the measurement unit to execute corresponding actions.
The multiple measuring devices respectively complete different measuring items, for example, the multiple measuring devices may be an insulation resistance tester to measure the insulation performance of the sensor, or an electronic scale to measure the mass parameter of the sensor, a vernier caliper to measure the size of the sensor, a scanning gun to measure the initialization parameter of the sensor, and the like, the measuring unit may include one or more of the above measuring devices, and, as described above, the channel switching circuit may control the opening of the channel corresponding to a certain relay according to an instruction, thereby achieving single-purpose measurement, or may control the multiple relay devices to sequentially pass through the channels according to a sequence, thereby achieving the measurement of multiple parameter technical indexes of the sensor one by one, and of course, may also enable some of the channels to achieve the synchronous measurement of several parameters.
In this embodiment, the system further comprises an output device 61 connected with the industrial personal computer 40 through an output bus 60, and a storage device 71 connected with the industrial personal computer 40 through a network bus 70, wherein the output mode of the output device 61 can be display on a display device, or can be immediately printed and output through a printing device, so that hidden dangers can be found in time, and more convincing and accurate data can be provided for troubleshooting and improvement. The storage device 71 stores the measurement data, and further, the measurement data can be collated by establishing a data table or a database so as to be convenient for calling and inquiring, and the efficiency and the quality of production and test of the aviation equipment are improved.
Due to the adoption of the technical scheme, the utility model discloses compare in prior art and have following beneficial technological effect:
1. the industrial personal computer sends instructions to the control unit, and the instructions are transmitted and decoded through the serial interface to control switching among the channels, so that the channels communicated with the test equipment can be switched in sequence to realize one-by-one test on multiple parameter technical indexes of the multiple sensors to be tested, thereby replacing the mode of one-by-one test through a manual method in the prior art and obviously improving the detection efficiency;
2. when the measuring unit executes measurement, the preset parameters are read, a counter for calculating the measuring times and a timer for calculating the measuring time are configured, then various parameter technical indexes of the sensor are continuously acquired for many times according to the set acquisition frequency, the acquired data are compared with the standard value in the preset parameters, the counter is increased or decreased once the data are acquired until the counter reaches the set times, meanwhile, the timer times the whole acquisition process, and when the measuring time exceeds the set time, the polarity parameter acquired is judged to have large fluctuation, and an abnormal result is output, so that the rapid measurement of the parameter polarity is realized through the synchronous measurement of the counter and the timer, the measuring efficiency is further improved, and the measuring precision is improved;
3. the method comprises the steps that various parameters measured in a single measurement period, various parameters in the single measurement period, measurement times and upper and lower limits of measurement time are set in preset parameters, return data which do not accord with the preset parameters are abandoned through the range of the various parameters, and the return data which accord with the preset parameters are weighted and averaged to be output as sampling results, so that the accuracy and the reliability of output data are improved;
4. the multi-channel switching device is used for respectively and sequentially measuring the parameter technical indexes of various sensors including weight, identification, size, resistance, current, voltage, temperature, insulation parameters and polarity parameters of the sensor to be measured through corresponding channels, and outputting the parameters through output equipment, so that a sensor parameter measuring method is optimized, and the automatic measurement of sensor parameters is realized;
5. the output device is connected with the industrial personal computer through an output bus, the output device outputs returned data and sampled data in real time, the output can be displayed through a display, or the data can be directly printed and output through a printer, meanwhile, the storage device is arranged, the storage device is in data connection with the industrial personal computer through a network bus, the measured data can be stored, and further, the measured data can be sorted through establishing a data table or a database, so that the aerial equipment production and test efficiency and quality are improved.
The above description of the present invention is provided to help understand the method and the core idea of the present invention, and the purpose of the present invention is to allow people familiar with the art to understand the contents of the present invention and to implement the method, and thus the protection scope of the present invention cannot be limited by the above description. All equivalent changes and modifications made according to the spirit of the present invention should be covered by the protection scope of the present invention.
Claims (3)
1. An aircraft sensor parameter measurement device, the measurement device comprising:
at least one measuring device;
the multi-channel switching device is connected with at least one sensor to be measured and the measuring equipment;
the industrial personal computer is respectively connected with the measuring equipment and the multi-channel switching device through a channel expansion interface and/or a serial bus;
the output device is connected with the industrial personal computer through an output bus;
a storage device connected with the industrial personal computer through a network bus, wherein,
and the industrial personal computer sends an instruction to control the on-off of a channel in the multi-channel switching device so as to control the opening of the measuring equipment and measure the sensor to be measured.
2. The device for measuring the parameters of the aviation sensor as claimed in claim 1, wherein the multi-channel switching device comprises a plurality of sets of relays, the input end of each relay is connected with the output end of the measuring equipment, the input end of the measuring equipment is connected with the output node of the industrial personal computer, and the output end of each relay is connected with the sensor to be measured.
3. The device for measuring the parameters of the aviation sensor as claimed in claim 2, wherein the multi-channel switching device further comprises a control unit, the control unit is connected with the industrial personal computer, and the control unit receives an instruction of the industrial personal computer and controls the suction of the relays in the multi-channel switching device so as to realize the on-off of the channels corresponding to the relays.
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| CN202020114563.4U CN211717483U (en) | 2020-01-19 | 2020-01-19 | Parameter measuring device for aviation sensor |
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| CN202020114563.4U CN211717483U (en) | 2020-01-19 | 2020-01-19 | Parameter measuring device for aviation sensor |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111141323A (en) * | 2020-01-19 | 2020-05-12 | 苏州长风航空电子有限公司 | Aviation sensor parameter measuring method and measuring device |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111141323A (en) * | 2020-01-19 | 2020-05-12 | 苏州长风航空电子有限公司 | Aviation sensor parameter measuring method and measuring device |
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