CN202768364U - Performance testing system for compressors - Google Patents
Performance testing system for compressors Download PDFInfo
- Publication number
- CN202768364U CN202768364U CN 201220350949 CN201220350949U CN202768364U CN 202768364 U CN202768364 U CN 202768364U CN 201220350949 CN201220350949 CN 201220350949 CN 201220350949 U CN201220350949 U CN 201220350949U CN 202768364 U CN202768364 U CN 202768364U
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- compressor
- microprocessor
- tested
- pressure gauge
- suction port
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Abstract
The utility model discloses a performance testing system for compressors. The performance testing system for the compressors comprises a gas storage cylinder group (1), a vibration detector (14) and a microprocessor (16), a compressor inlet and a compressor outlet are arranged on a to-be-tested compressor (6), an input pipeline between the gas storage cylinder group (1) and the compressor inlet is sequentially provided with a first ball valve (3) and a turbine flow meter (5), an output pipeline between the compressor outlet and the gas storage cylinder group (1) is sequentially provided with a filter (8), a second one-way valve (12) and a third ball valve (13), and a circulation connection pipeline which is arranged between the compressor outlet and the compressor inlet is sequentially connected with the filter (8), the second ball valve (9), a pressure regulating valve (10), a first one-way valve (11) and the turbine flow meter (5). According to the performance testing system for the compressors, nitrogen gas is utilized to simulate rated operating conditions of the to-be-tested compressor (6), the reliable performance of the to-be-tested compressor (6) is tested under the rated operating conditions, and therefore the conformance of the to-be-tested compressor (6) to the design can be judged, and the effect that the compressors which are manufactured and then leave a factory are reliable and risk free is guaranteed.
Description
Technical field
The utility model relates to a kind of compressor performance pilot system.
Background technique
At present, mostly produce the producer of compressor after the production and assembly compressor is finished, owing to be subjected to the restriction of plant produced condition, the factory that produces compressor often can not be detected the performance of compressor, or only limiting to operation test to its mechanical property, this is just so that there is certain risk in compressor on the reliable performance in actual applications.
Summary of the invention
For the deficiencies in the prior art, but the purpose of this utility model is to provide a kind of analog compression machine declared working condition and under its declared working condition it is carried out the compressor performance pilot system that reliable performance test detects.
For achieving the above object, the utility model provides a kind of compressor performance pilot system, comprise air cylinder group 1, vibrating detector 14, microprocessor 16, compressor 6 to be tested is provided with suction port of compressor and compressor outlet, is provided with successively the first ball valve 3, turbine flowmeter 5 on the input pipeline between air cylinder group 1 and the suction port of compressor; Be provided with successively filter 8, the second one-way valve 12, the 3rd ball valve 13 on the output pipeline between compressor outlet and the air cylinder group 1; Also be connected with the circulation connecting tube between compressor outlet and the suction port of compressor, be connected with successively filter 8, the second ball valve 9, pressure regulator valve 10, the first one-way valve 11, turbine flowmeter 5 on the described circulation connecting tube; Described microprocessor 16 is connected with the Automatically controlled control cabinet 15 that compressor 6 to be tested carries; Described vibrating detector 14 is installed on the compressor 6 to be tested and with microprocessor 16 and is connected, and is used for testing the Vibration Condition of compressor 6 processs of the test to be tested and sending the result to microprocessor 16; On described air cylinder group 1, suction port of compressor and the compressor outlet respectively correspondence be equiped with the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7, described the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7 and turbine flowmeter 5 all are connected with microprocessor 16.
The beneficial effects of the utility model are: adopt above-mentioned pilot system, the user can be first with in the compressor 6 access pilot systems to be tested, inject a certain amount of nitrogen toward 1 li of air cylinder group again, and the operation of the Automatically controlled control cabinet 15 controls compressor 6 to be tested that carries with compressor 6 to be tested, after compressor 6 starts to be tested, open first the first ball valve 3, the nitrogen of 1 li of air cylinder group is entered in the suction port of compressor of compressor 6 to be tested, and keep the inlet pressure of suction port of compressor identical with the specified inlet pressure of compressor 6 to be tested, open simultaneously again the second ball valve 9 and pressure regulator valve 10, and make the outlet pressure of compressor outlet reach the specified outlet pressure of compressor 6 to be tested by the adjusting of pressure regulator valve 10, close the first ball valve 3 this moment, nitrogen is circulated in compressor 6 to be tested to be tested, microprocessor 16 gathers the inlet pressure that shows on the second pressure gauge 4 in the process of the test, the outlet pressure that shows on the 3rd pressure gauge 7, the flow that shows on the turbine flowmeter 5, and the Vibration Condition of the compressor to be tested 6 that detects of vibrating detector 14, and by converting, draw the ride quality test data of compressor 6 to be tested, judge itself and the accordance of design, guarantee to manufacture all reliable devoids of risk of the compressor that dispatches from the factory.During off-test, can close the second ball valve 9, open the 3rd ball valve 13, the nitrogen in the pilot system be returned 1 li of air cylinder group again, in order to reuse.
The utility model can further be set to also include a display device 17, described display device 17 is connected with microprocessor 16, for the data that receive on the instant playback microprocessor 16, also be provided with autostore module and printout module on the described microprocessor 16.
Adopt said structure, the user can understand the data that receive on the microprocessor 16 by display device 17 immediate observations, and the autostore module can in time store related data information, and the printout module can print related data information according to user's needs.
The utility model also can further be set to described input pipeline and be provided with the suction port of compressor adpting flange 18 that is connected with the suction port of compressor, and described output pipeline is provided with the compressor outlet adpting flange 19 that is connected with compressor outlet.
Adopt said structure, described suction port of compressor adpting flange 18, compressor outlet adpting flange 19 can greatly make things convenient for being connected and loading and unloading of compressor 6 to be tested and pilot system pipeline.
The utility model also can further be set to described the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7 and all be connected with microprocessor 16 by pressure transducer 20.
Adopt said structure, pressure transducer 20 can make the pressure information on the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7 in time be passed on the microprocessor 16.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
Provided as shown in Figure 1 a kind of compressor performance pilot system, comprise air cylinder group 1, vibrating detector 14, microprocessor 16, display device 17, compressor 6 to be tested is provided with suction port of compressor and compressor outlet, be provided with successively the first ball valve 3, turbine flowmeter 5 on the input pipeline between air cylinder group 1 and the suction port of compressor, also be provided with the suction port of compressor adpting flange 18 that is connected with the suction port of compressor on the described input pipeline; Be provided with successively filter 8, the second one-way valve 12, the 3rd ball valve 13 on the output pipeline between compressor outlet and the air cylinder group 1, also be provided with the compressor outlet adpting flange 19 that is connected with compressor outlet on the described output pipeline; Also be connected with the circulation connecting tube between compressor outlet and the suction port of compressor, be connected with successively filter 8, the second ball valve 9, pressure regulator valve 10, the first one-way valve 11, turbine flowmeter 5 on the described circulation connecting tube; Described microprocessor 16 is connected with the Automatically controlled control cabinet 15 that compressor 6 to be tested carries; Described vibrating detector 14 is installed on the compressor 6 to be tested and with microprocessor 16 and is connected, and is used for testing the Vibration Condition of compressor 6 processs of the test to be tested and sending the result to microprocessor 16; On described air cylinder group 1, suction port of compressor and the compressor outlet respectively correspondence be equiped with the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7, described the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7 and turbine flowmeter 5 all are connected with microprocessor 16, and described the first pressure gauge 2, the second pressure gauge 4, the 3rd pressure gauge 7 all are connected with microprocessor 16 by pressure transducer 20; Described display device 17 is connected with microprocessor 16, for the data that receive on the instant playback microprocessor 16, also is provided with autostore module and printout module on the described microprocessor 16.
Adopt above-mentioned pilot system, the user can be first with in the compressor 6 access pilot systems to be tested, inject a certain amount of nitrogen toward 1 li of air cylinder group again, and the operation of the Automatically controlled control cabinet 15 controls compressor 6 to be tested that carries with compressor 6 to be tested, after compressor 6 starts to be tested, open first the first ball valve 3, the nitrogen of 1 li of air cylinder group is entered in the suction port of compressor of compressor 6 to be tested, and keep the inlet pressure of suction port of compressor identical with the specified inlet pressure of compressor 6 to be tested, open simultaneously again the second ball valve 9 and pressure regulator valve 10, and make the outlet pressure of compressor outlet reach the specified outlet pressure of compressor 6 to be tested by the adjusting of pressure regulator valve 10, close the first ball valve 3 this moment, nitrogen is circulated in compressor 6 to be tested to be tested, microprocessor 16 gathers the inlet pressure that shows on the second pressure gauge 4 in the process of the test, the outlet pressure that shows on the 3rd pressure gauge 7, the flow that shows on the turbine flowmeter 5, and the Vibration Condition of the compressor to be tested 6 that detects of vibrating detector 14, and by converting, draw the ride quality test data of compressor 6 to be tested, judge itself and the accordance of design, guarantee to manufacture all reliable devoids of risk of the compressor that dispatches from the factory.During off-test, can close the second ball valve 9, open the 3rd ball valve 13, the nitrogen in the pilot system be returned 1 li of air cylinder group again, in order to reuse.
Claims (4)
1. compressor performance pilot system, it is characterized in that: comprise air cylinder group (1), vibrating detector (14), microprocessor (16), compressor to be tested (6) is provided with suction port of compressor and compressor outlet, is provided with successively the first ball valve (3), turbine flowmeter (5) on the input pipeline between air cylinder group (1) and the suction port of compressor; Be provided with successively filter (8), the second one-way valve (12), the 3rd ball valve (13) on the output pipeline between compressor outlet and the air cylinder group (1); Also be connected with the circulation connecting tube between compressor outlet and the suction port of compressor, be connected with successively filter (8), the second ball valve (9), pressure regulator valve (10), the first one-way valve (11), turbine flowmeter (5) on the described circulation connecting tube; Described microprocessor (16) is connected with the Automatically controlled control cabinet (15) that compressor to be tested (6) carries; Described vibrating detector (14) is installed in compressor to be tested (6) and upward and with microprocessor (16) is connected, and is used for testing the Vibration Condition of compressor to be tested (6) process of the test and sending the result to microprocessor (16); On described air cylinder group (1), suction port of compressor and the compressor outlet respectively correspondence be equiped with the first pressure gauge (2), the second pressure gauge (4), the 3rd pressure gauge (7), described the first pressure gauge (2), the second pressure gauge (4), the 3rd pressure gauge (7) and turbine flowmeter (5) all are connected with microprocessor (16).
2. compressor performance pilot system according to claim 1, it is characterized in that: also include a display device (17), described display device (17) is connected with microprocessor (16), for the data that receive on the instant playback microprocessor (16), also be provided with autostore module and printout module on the described microprocessor (16).
3. compressor performance pilot system according to claim 1, it is characterized in that: described input pipeline is provided with the suction port of compressor adpting flange (18) that is connected with the suction port of compressor, and described output pipeline is provided with the compressor outlet adpting flange (19) that is connected with compressor outlet.
4. compressor performance pilot system according to claim 1, it is characterized in that: described the first pressure gauge (2), the second pressure gauge (4), the 3rd pressure gauge (7) all are connected with microprocessor (16) by pressure transducer (20).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220350949 CN202768364U (en) | 2012-07-19 | 2012-07-19 | Performance testing system for compressors |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220350949 CN202768364U (en) | 2012-07-19 | 2012-07-19 | Performance testing system for compressors |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202768364U true CN202768364U (en) | 2013-03-06 |
Family
ID=47774945
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220350949 Withdrawn - After Issue CN202768364U (en) | 2012-07-19 | 2012-07-19 | Performance testing system for compressors |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202768364U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102734149A (en) * | 2012-07-19 | 2012-10-17 | 浙江强盛压缩机制造有限公司 | Compressor performance testing system |
-
2012
- 2012-07-19 CN CN 201220350949 patent/CN202768364U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102734149A (en) * | 2012-07-19 | 2012-10-17 | 浙江强盛压缩机制造有限公司 | Compressor performance testing system |
| CN102734149B (en) * | 2012-07-19 | 2015-01-28 | 浙江强盛压缩机制造有限公司 | Compressor performance testing system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20130306 Effective date of abandoning: 20150128 |
|
| RGAV | Abandon patent right to avoid regrant |