CN202471370U - Production test stand for clutch thruster air passage control system assembly - Google Patents
Production test stand for clutch thruster air passage control system assembly Download PDFInfo
- Publication number
- CN202471370U CN202471370U CN2011205716486U CN201120571648U CN202471370U CN 202471370 U CN202471370 U CN 202471370U CN 2011205716486 U CN2011205716486 U CN 2011205716486U CN 201120571648 U CN201120571648 U CN 201120571648U CN 202471370 U CN202471370 U CN 202471370U
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- air
- control system
- pressure
- system assembly
- thruster
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Abstract
The utility model discloses a production test stand for a clutch thruster air passage control system assembly, comprising a compressor, an air passage control test stand, an air passage control assembly and a simulation clutch thruster, wherein the air discharging pipe of the compressor is connected with the air intake pipe of the air passage control test stand, the air discharging pipe of the air control test stand is connected with the air intake pipe of the air passage control system assembly, the air discharging pipe of the air passage control system assembly is connected with the air intake pipe of the simulation clutch thruster, and the air passage control test stand comprises a low pressure pressure-regulating valve, a high pressure pressure-regulating valve, a high and low pressure electromagnetic reversing valve, an air pressure presence and absence electromagnetic reversing valve, a pressure gage and a power supply. The production test stand for a clutch thruster air passage control system assembly can detect whether the clutch thruster can effectively drive a clutch to separate or close through the air passage control system assembly or not and whether the air passage control system assembly is accurate in control or not. The air passage control test stand is simple in operation, and convenient in batch test of air passage control system assemblies, and increases product ex factory qualified rate.
Description
Technical field
The utility model relates to the air-path control system of vehicular clutch thruster, relates in particular to vehicular clutch thruster air-path control system assembly production testing platform.
Background technology
At present; The separation of vehicle master clutch (particularly PHEV) be by the vehicular clutch thruster promptly (cylinder) control; So the air-path control system assembly of vehicular clutch thruster must be set; And then the equipment that needs a cover to carry out production testing to vehicular clutch thruster air-path control system assembly; Thereby whether the vehicular clutch thruster of judge producing can effectively accomplish the separation and the combination of clutch coupling in various situation when higher (when source of the gas air pressure is low or source of the gas air pressure), and perhaps when source of the gas did not have air pressure, whether auxiliary inflating pump can drive separation and the combination that the vehicular clutch thruster is effectively accomplished clutch coupling; Whether the air-path control system assembly assembling that also need detect the vehicular clutch thruster simultaneously exists the problem that gas leaks etc.Do not carry out the equipment that this vehicular clutch thruster air-path control system assembly carries out production testing specially but have on the market at present, so, effort extremely time-consuming to the various detections of vehicular clutch thruster air-path control system assembly.
Summary of the invention
In order to overcome the deficiency of prior art, it is a kind of to the air-path control system assembly of vehicular clutch thruster clutch coupling thruster air-path control system assembly production testing platform easy to detect that the purpose of the utility model is to provide.
The utility model clutch coupling thruster air-path control system assembly production testing platform; It comprises air compressor machine, gas circuit control test platform, air-path control system assembly and simulated clutch thruster; The escape pipe of said air compressor machine connects the draft tube of gas circuit control test platform; The escape pipe of gas circuit control test platform connects the draft tube of air-path control system assembly; The escape pipe of air-path control system assembly connects the draft tube of simulated clutch thruster; Gas circuit control test platform comprises low pressure regulating pressure valve, high-pressure pressure regulating valve, high-low pressure solenoid directional control valve, has or not air pressure solenoid directional control valve, tensimeter and power supply; The draft tube of gas circuit control test platform divides two-way to be connected with the high-pressure pressure regulating valve draft tube with low pressure regulating pressure valve respectively, and the escape pipe of low pressure regulating pressure valve and high-pressure pressure regulating valve is connected with the draft tube of high-low pressure solenoid directional control valve respectively, and the escape pipe of high-low pressure solenoid directional control valve is connected with having or not air pressure solenoid directional control valve draft tube; Have or not the escape pipe of air pressure solenoid directional control valve to be connected with tensimeter, manometric escape pipe is connected with the draft tube of air-path control system assembly.
When needs gas circuit control test platform output high pressure gas, convert the high-low pressure solenoid directional control valve into high pressure output, have or not the air pressure solenoid directional control valve to convert air pressure output into, at this moment the air-path control system assembly is input as high pressure gas; When needs gas circuit control test platform output low pressure gas, convert the high-low pressure solenoid directional control valve into low pressure output, have or not the air pressure solenoid directional control valve to convert air pressure output into, at this moment the air-path control system assembly is input as low pressure gas; When needs gas circuit control test platform does not have air pressure output, have or not the air pressure solenoid directional control valve to convert no air pressure output into, at this moment the air-path control system assembly is input as zero air pressure; Gas circuit control test platform output pressure situation is observed through tensimeter.
Also be provided with solenoid valve button, auxiliary inflating pump button, high-low pressure source of the gas switch and source of the gas on the said gas circuit control test platform and cut off switch.
Said high-low pressure source of the gas switch control high-low pressure solenoid directional control valve.
Said source of the gas cuts off switch control and has or not the air pressure solenoid directional control valve.
In the utility model; The method of inspection of described clutch coupling thruster air-path control system assembly production testing platform is: when source of the gas air pressure is low; Air compressor machine output pressure gas, and send into the air intake opening of gas circuit control test platform along gas circuit, high-low pressure source of the gas switch is transformed on hypobaric gas circuit; And source of the gas break-make switch has been transformed on the air pressure gas circuit; Then low pressure gas successively through low pressure regulating pressure valve, high-low pressure solenoid directional control valve, have or not air pressure solenoid directional control valve, tensimeter, air-path control system assembly, get into the simulated clutch thruster, this moment, low pressure gas promoted the work of simulated clutch separation simulation clutch coupling thruster;
When source of the gas air pressure is higher; Air compressor machine output pressure gas; And send into the air intake opening of gas circuit control test platform along gas circuit; High-low pressure source of the gas switch is transformed on the anticyclonic gas circuit, and source of the gas break-make switch has been transformed on the air pressure gas circuit, then high pressure gas successively through high-pressure pressure regulating valve, high-low pressure solenoid directional control valve, have or not air pressure solenoid directional control valve, tensimeter, air-path control system assembly; Get into the simulated clutch thruster, this moment, high pressure gas promoted the work of simulated clutch separation simulation clutch coupling thruster;
When source of the gas does not have air pressure; Source of the gas break-make switch is transformed on the 0 air pressure gas circuit; The air-path control system assembly does not have from outside air pressure, connects solenoid valve and auxiliary inflating pump button simultaneously, and auxiliary inflating pump output pressure promotes the work of simulated clutch separation simulation clutch coupling thruster.
Said low pressure gas is 0.15MPa.
Said high pressure gas is 0.7MPa.
The clutch coupling thruster air-path control system production testing platform of the utility model; Special in the setting of vehicular clutch thruster air-path control system; Can fast and effeciently detect clutch coupling thruster air-path control system assembly and whether leak gas, can also detect the clutch coupling thruster simultaneously and under various situation, can be defined as dynamic clutch separation and combination.This production testing platform is simple to operate, is convenient to batch detection clutch coupling thruster and air-path control system assembly thereof, improves air-path control system assembly ex factory pass rate.
Description of drawings
Below in conjunction with accompanying drawing and embodiment the utility model is done further detailed explanation:
Fig. 1 is the structural representation of the utility model clutch coupling thruster air-path control system assembly production testing platform.
Embodiment
As shown in Figure 1; The utility model comprises air compressor machine 1, gas circuit control test platform 2, air-path control system assembly 3 and simulated clutch thruster 4; The escape pipe of said air compressor machine 1 connects the draft tube of gas circuit control test platform 2; The escape pipe of gas circuit control test platform 2 connects the draft tube of air-path control system assembly 3; The escape pipe of air-path control system assembly 3 connects the draft tube of simulated clutch thruster 4; Gas circuit control test platform 2 comprises low pressure regulating pressure valve 21, high-pressure pressure regulating valve 22, high-low pressure solenoid directional control valve 23, has or not air pressure solenoid directional control valve 24, tensimeter 25 and power supply 26; The draft tube of gas circuit control test platform 2 divides two-way to be connected with high-pressure pressure regulating valve 22 draft tube with low pressure regulating pressure valve 21 respectively, and the escape pipe of low pressure regulating pressure valve 21 and high-pressure pressure regulating valve 22 is connected with the draft tube of high-low pressure solenoid directional control valve 23 respectively, and the escape pipe of high-low pressure solenoid directional control valve 23 is connected with having or not air pressure solenoid directional control valve 24 draft tube; Have or not the escape pipe of air pressure solenoid directional control valve 24 to be connected with tensimeter 25, the escape pipe of tensimeter 25 is connected with the draft tube of air-path control system assembly 3.
When needs gas circuit control test platform 2 output high pressure gas, convert high-low pressure solenoid directional control valve 23 into high pressure output, have or not air pressure solenoid directional control valve 24 to convert air pressure output into, at this moment air-path control system assembly 3 is input as high pressure gas; When needs gas circuit control test platform 2 output low pressure gas, convert high-low pressure solenoid directional control valve 23 into low pressure output, have or not air pressure solenoid directional control valve 24 to convert air pressure output into, at this moment air-path control system assembly 3 is input as low pressure gas; When needs gas circuit control test platform 2 no air pressure are exported, have or not air pressure solenoid directional control valve 24 to convert no air pressure output into, at this moment air-path control system assembly 3 is input as zero air pressure; Gas circuit control test platform 2 output pressure situation are observed through tensimeter 25.
Also be provided with solenoid valve button 5, auxiliary inflating pump button 6, high-low pressure source of the gas switch 7 and source of the gas on the said gas circuit control test platform 2 and cut off switch 8.
Said high-low pressure source of the gas switch 7 control high-low pressure solenoid directional control valves 23.
Said source of the gas cuts off switch 8 controls and has or not air pressure solenoid directional control valve 24.
In the utility model; The method of inspection of described clutch coupling thruster air-path control system assembly production testing platform is: when source of the gas air pressure is low; Air compressor machine 1 output pressure gas, and send into the air intake opening of gas circuit control test platform 2 along gas circuit, high-low pressure source of the gas switch 7 is transformed on hypobaric gas circuit; And source of the gas break-make switch 8 has been transformed on the air pressure gas circuit; Then low pressure gas successively through low pressure regulating pressure valve 21, high-low pressure solenoid directional control valve 23, have or not air pressure solenoid directional control valve 24, tensimeter 25, air-path control system assembly 3, get into simulated clutch thruster 4, this moment, low pressure gas promoted 4 work of simulated clutch separation simulation clutch coupling thruster;
When detecting more than 5 times repeatedly,, explain that then barometric minimum can effectively accomplish clutch separation and combination, 3 precise controls of air-path control system assembly if low pressure gas all can promote 4 work of simulated clutch separation simulation clutch coupling thruster at every turn through above; Otherwise air-path control system assembly 3 is defective.
When source of the gas air pressure is higher; Air compressor machine 1 output pressure gas; And send into the air intake opening of gas circuit control test platform 2 along gas circuit; High-low pressure source of the gas switch 7 is transformed on the anticyclonic gas circuit, and source of the gas break-make switch 8 has been transformed on the air pressure gas circuit, then high pressure gas successively through high-pressure pressure regulating valve 22, high-low pressure solenoid directional control valve 23, have or not air pressure solenoid directional control valve 24, tensimeter 25, air-path control system assembly 3; Get into simulated clutch thruster 4, this moment, high pressure gas promoted 4 work of simulated clutch separation simulation clutch coupling thruster;
When detecting more than 5 times repeatedly,, explain that then hyperbar can effectively accomplish clutch separation and combination, 3 precise controls of air-path control system assembly if high pressure gas all can promote 4 work of simulated clutch separation simulation clutch coupling thruster at every turn through above; Otherwise air-path control system assembly 3 is defective.Simultaneously, behind the clutch separation EO, air-path control system assembly 3 remains under the hyperbar state, also need carry out air-path control system assembly 3 each pipe adapters assembling Leak Detection.
When source of the gas does not have air pressure; Source of the gas break-make switch 8 is transformed on the 0 air pressure gas circuit; Air-path control system assembly 3 no from outside air pressure are connected solenoid valve button 5 and auxiliary inflating pump button 6 simultaneously, and auxiliary inflating pump 31 output pressures promote 4 work of simulated clutch separation simulation clutch coupling thruster.Detect more than 5 times repeatedly through this; If the air pressure of each auxiliary inflating pump 31 outputs all can promote 4 work of simulated clutch separation simulation clutch coupling thruster; Then auxiliary inflating pump 31 can effectively be accomplished clutch separation and combination, 3 precise controls of air-path control system assembly; Otherwise air-path control system assembly 3 is defective.
Said low pressure gas is 0.15MPa.
Said high pressure gas is 0.7MPa.
Claims (4)
1. clutch coupling thruster air-path control system assembly production testing platform; It is characterized in that: it comprises air compressor machine, gas circuit control test platform, air-path control system assembly and simulated clutch thruster; The escape pipe of said air compressor machine connects the draft tube of gas circuit control test platform; The escape pipe of gas circuit control test platform connects the draft tube of air-path control system assembly; The escape pipe of air-path control system assembly connects the draft tube of simulated clutch thruster; Gas circuit control test platform comprises low pressure regulating pressure valve, high-pressure pressure regulating valve, high-low pressure solenoid directional control valve, has or not air pressure solenoid directional control valve, tensimeter and power supply; The draft tube of gas circuit control test platform divides two-way to be connected with the high-pressure pressure regulating valve draft tube with low pressure regulating pressure valve respectively, and the escape pipe of low pressure regulating pressure valve and high-pressure pressure regulating valve is connected with the draft tube of high-low pressure solenoid directional control valve respectively, and the escape pipe of high-low pressure solenoid directional control valve is connected with having or not air pressure solenoid directional control valve draft tube; Have or not the escape pipe of air pressure solenoid directional control valve to be connected with tensimeter, manometric escape pipe is connected with the draft tube of air-path control system assembly.
2. clutch coupling thruster air-path control system assembly production testing platform according to claim 1 is characterized in that: also be provided with solenoid valve button, auxiliary inflating pump button, high-low pressure source of the gas switch and source of the gas on the said gas circuit control test platform and cut off switch.
3. clutch coupling thruster air-path control system assembly production testing platform according to claim 2 is characterized in that: said high-low pressure source of the gas switch control high-low pressure solenoid directional control valve.
4. clutch coupling thruster air-path control system assembly production testing platform according to claim 2 is characterized in that: said source of the gas cuts off switch control and has or not the air pressure solenoid directional control valve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205716486U CN202471370U (en) | 2011-12-31 | 2011-12-31 | Production test stand for clutch thruster air passage control system assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011205716486U CN202471370U (en) | 2011-12-31 | 2011-12-31 | Production test stand for clutch thruster air passage control system assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202471370U true CN202471370U (en) | 2012-10-03 |
Family
ID=46919522
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011205716486U Withdrawn - After Issue CN202471370U (en) | 2011-12-31 | 2011-12-31 | Production test stand for clutch thruster air passage control system assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202471370U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102519688A (en) * | 2011-12-31 | 2012-06-27 | 福建省福工动力技术股份公司 | Production inspection table and inspection method for air passage control system assembly of clutch thruster |
| CN106762873A (en) * | 2016-12-28 | 2017-05-31 | 中国北方车辆研究所 | For the experiment station of endless-track vehicle hydraulic retarder experiment |
-
2011
- 2011-12-31 CN CN2011205716486U patent/CN202471370U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102519688A (en) * | 2011-12-31 | 2012-06-27 | 福建省福工动力技术股份公司 | Production inspection table and inspection method for air passage control system assembly of clutch thruster |
| CN102519688B (en) * | 2011-12-31 | 2015-06-17 | 福建省福工动力技术有限公司 | Production inspection table and inspection method for air passage control system assembly of clutch thruster |
| CN106762873A (en) * | 2016-12-28 | 2017-05-31 | 中国北方车辆研究所 | For the experiment station of endless-track vehicle hydraulic retarder experiment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: FUJIAN FUGONG POWER TECHNOLOGY CO., LTD. Free format text: FORMER NAME: FUJIAN FUGONG HEV TECHNOLOGIES DEVELOPMENT CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder |
Address after: 350000, Gulou District, Fujian Province, 89 software Avenue, Fuzhou Software Park industrial base two, building 9, No. 1, Fuzhou Patentee after: FUJIAN FUGONG POWER TECHNOLOGY CO., LTD. Address before: 350000, Gulou District, Fujian Province, 89 software Avenue, Fuzhou Software Park industrial base two, building 9, No. 1, Fuzhou Patentee before: Fujian Fugong HEV Technology Co., Ltd. |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20121003 Effective date of abandoning: 20150617 |
|
| RGAV | Abandon patent right to avoid regrant |