CN203981207U - Oil cooler testing table - Google Patents

Oil cooler testing table Download PDF

Info

Publication number
CN203981207U
CN203981207U CN201420275789.7U CN201420275789U CN203981207U CN 203981207 U CN203981207 U CN 203981207U CN 201420275789 U CN201420275789 U CN 201420275789U CN 203981207 U CN203981207 U CN 203981207U
Authority
CN
China
Prior art keywords
reserve tank
liquid reserve
valve
solenoid valve
pipeline
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201420275789.7U
Other languages
Chinese (zh)
Inventor
刘旭东
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BEIJING FUHUA HUIHANG AIRCRAFT ACCESSORIES MAINTENANCE Co Ltd
Original Assignee
BEIJING FUHUA HUIHANG AIRCRAFT ACCESSORIES MAINTENANCE Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BEIJING FUHUA HUIHANG AIRCRAFT ACCESSORIES MAINTENANCE Co Ltd filed Critical BEIJING FUHUA HUIHANG AIRCRAFT ACCESSORIES MAINTENANCE Co Ltd
Priority to CN201420275789.7U priority Critical patent/CN203981207U/en
Application granted granted Critical
Publication of CN203981207U publication Critical patent/CN203981207U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Examining Or Testing Airtightness (AREA)

Abstract

The utility model belongs to oil cooler technical field of measurement and test, particularly a kind of oil cooler testing table.This testing table is divided into oil piping system and Circuits System two parts, and oil piping system comprises the liquid reserve tank, surplus valve, hydraulic pump, sensor, test device, controller, the variable valve that are composed in series loop; 3 pipelines that solenoid valve is set respectively that communicate are set between constant voltage case and liquid reserve tank, and described 3 pipelines that communicate all communicate with the pipeline between surplus valve and liquid reserve tank; Circuits System is: pressure compensation automatic regulator is connected with sensor, control circuit, driving circuit respectively, and driving circuit is also connected with controller, and control circuit is connected with three solenoid valves respectively.This testing table can carry out withstand voltage test, leak test, oil pressure to the heating radiator in airplane auxiliary power system, refrigeratory and fall test, flow test etc., measuring accuracy is high, the every detection to oil cooler can be realized without returning factory, a large amount of testing costs can be saved.

Description

Oil cooler testing table
Technical field
The utility model belongs to oil cooler technical field of measurement and test, particularly a kind of oil cooler testing table.
Background technology
Heating radiator, refrigeratory in airplane auxiliary power system need to regularly overhaul, need the project of test to comprise: test, flow test etc. fall in withstand voltage test, leak test, oil pressure, object be have in order to detect heating radiator or refrigeratory whether ne-leakage, structure complete, whether unobstructed etc. between pipeline.Because oil cooler belongs to more accurate parts, its test request is also quite high, and the common practice in industry is parts to be returned to former factory detect at present, and sense cycle is long, and testing cost is high.
Summary of the invention
The utility model provides a kind of oil cooler testing table, its objective is for aircraft oil cooler is carried out to coherent detection test.
The technical solution adopted in the utility model is:
This testing table is divided into oil piping system and Circuits System two parts;
Described oil piping system is: liquid reserve tank, surplus valve, hydraulic pump, sensor, test device, controller are connected by pipeline successively; Variable valve has 3 mouths, is connected respectively with controller, constant voltage case, liquid reserve tank (18); 3 pipelines that communicate are set between constant voltage case and liquid reserve tank, and described 3 pipelines that communicate all communicate with the pipeline between surplus valve and liquid reserve tank; Pipeline between variable valve and liquid reserve tank is also with the pipeline communication between surplus valve and liquid reserve tank; The two ends of ebullator are connected with liquid reserve tank, constant voltage case respectively;
Described Circuits System is: the first solenoid valve, the second solenoid valve, the 3rd solenoid valve are set respectively on 3 articles of pipelines between constant voltage case and liquid reserve tank; Pressure compensation automatic regulator is connected with sensor, control circuit, driving circuit respectively, and driving circuit is also connected with controller, and control circuit is connected with the first solenoid valve, the second solenoid valve, the 3rd solenoid valve respectively.
The safety valve in parallel with described hydraulic pump is set, and the two ends of safety valve are connected with surplus valve, liquid reserve tank by pipeline respectively.
Between described surplus valve and liquid reserve tank, set up a straight-through pipeline, and on this pipeline, the 4th solenoid valve being connected with control circuit is set.
Described the first solenoid valve, the second solenoid valve, the 3rd solenoid valve, the 4th solenoid valve are guide type electromagnetic high pressure fuel tap.
Described sensor is high-accuracy hydraulic pressure transducer.
The beneficial effects of the utility model are:
Whether this testing table can carry out withstand voltage test, leak test, oil pressure to the heating radiator in airplane auxiliary power system, refrigeratory and fall test, flow test etc., can detect oil cooler and have whether ne-leakage, structure be complete, unobstructed etc. between pipeline.Measuring accuracy is high, can realize the every detection to oil cooler without returning factory, can save a large amount of testing costs.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Number in the figure:
1-test device; 2-pressure compensation automatic regulator; 3-driving circuit; 4-control circuit; 5-controller; 6-sensor; 7-constant voltage case; 8-hydraulic pump; 9-motor; 10-safety valve; 11-surplus valve; 12-the 4th solenoid valve; 13-the first solenoid valve; 14-the second solenoid valve; 15-the 3rd solenoid valve; 16-variable valve; 17-ebullator; 18-liquid reserve tank.
Embodiment
The utility model provides a kind of oil cooler testing table, below in conjunction with the drawings and specific embodiments, the utility model is described further.
The structure of this testing table as shown in Figure 1, is divided into oil piping system and Circuits System two parts.
Described oil piping system is: liquid reserve tank 18, surplus valve 11, hydraulic pump 8, sensor 6, test device 1, controller 5 are connected by pipeline successively; Variable valve 16 has 3 mouths, is connected respectively with controller 5, constant voltage case 7, liquid reserve tank 18; 3 pipelines that communicate are set between constant voltage case 7 and liquid reserve tank 18, and described 3 pipelines that communicate all communicate with the pipeline between surplus valve 11 and liquid reserve tank 18; Pipeline between variable valve 16 and liquid reserve tank 18 is also with the pipeline communication between surplus valve 11 and liquid reserve tank 18; The two ends of ebullator 17 are connected with liquid reserve tank 18, constant voltage case 7 respectively.The safety valve 10 in parallel with described hydraulic pump 8 is set, and the two ends of safety valve 10 are connected with surplus valve 11, liquid reserve tank 18 by pipeline respectively.Between surplus valve and liquid reserve tank 18, set up a straight-through pipeline, and on this pipeline, the 4th solenoid valve 12 being connected with control circuit 4 is set.Motor 9 drives hydraulic pump 8 to work.
Described Circuits System is: the first solenoid valve 13, the second solenoid valve 14, the 3rd solenoid valve 15 are set respectively on 3 articles of pipelines between constant voltage case 7 and liquid reserve tank 18; Pressure compensation automatic regulator is connected with sensor 6, control circuit 4, driving circuit 3 respectively, and driving circuit is also connected with controller 5, and control circuit 4 is connected with the first solenoid valve 13, the second solenoid valve 14, the 3rd solenoid valve 15 respectively.
Wherein, the first solenoid valve 13, the second solenoid valve 14, the 3rd solenoid valve 15, the 4th solenoid valve 12 are guide type electromagnetic high pressure fuel tap.Sensor 6 is high-accuracy hydraulic pressure transducer.
The major parameter of this testing table is: alternating voltage 220V, working pressure 0~10MPa, flow 30L/min.
The principle of work of this testing table is: test device 1 is fixed on testing table, connects pipeline, according to the requirement of test handbook, input corresponding data on pressure compensation automatic regulator 2, hydraulic pump 8 passes through sensor 6 to test device 1 for hydraulic oil.In exerting pressure, the integrality of check test device 1 structure, whether surface has fluid to ooze out, and hydraulic oil returns to liquid reserve tank 18. by controller 5, variable valve 16.The data of pressure compensation automatic regulator 2 detecting sensors 6, as need compensate, output signal to control circuit 4, control the switching of the first solenoid valve 13, the second solenoid valve 14, the 3rd solenoid valve 15, and oil piping system is compensated.Safety valve 10, surplus valve 11, the 4th solenoid valve 12 ensure the pressure stability of oil piping system, and it is constant that ebullator 17 maintains constant voltage case 7 internal pressures.

Claims (5)

1. oil cooler testing table, is divided into oil piping system and Circuits System, it is characterized in that,
Described oil piping system is: liquid reserve tank (18), surplus valve (11), hydraulic pump (8), sensor (6), test device (1), controller (5) are connected by pipeline successively; Variable valve (16) has 3 mouths, is connected respectively with controller (5), constant voltage case (7), liquid reserve tank (18); Between constant voltage case (7) and liquid reserve tank (18), 3 pipelines that communicate are set, and described 3 pipelines that communicate all the pipeline between same surplus valve (11) and liquid reserve tank (18) communicate; Pipeline between variable valve (16) and liquid reserve tank (18) is the pipeline communication between same surplus valve (11) and liquid reserve tank (18) also; The two ends of ebullator (17) are connected with liquid reserve tank (18), constant voltage case (7) respectively;
Described Circuits System is: the first solenoid valve (13), the second solenoid valve (14), the 3rd solenoid valve (15) are set respectively on 3 articles of pipelines between constant voltage case (7) and liquid reserve tank (18); Pressure compensation automatic regulator is connected with sensor (6), control circuit (4), driving circuit (3) respectively, driving circuit is also connected with controller (5), and control circuit (4) is connected with the first solenoid valve (13), the second solenoid valve (14), the 3rd solenoid valve (15) respectively.
2. oil cooler testing table according to claim 1, it is characterized in that, the safety valve (10) in parallel with described hydraulic pump (8) is set, and the two ends of safety valve (10) are connected with surplus valve (11), liquid reserve tank (18) by pipeline respectively.
3. oil cooler testing table according to claim 1, it is characterized in that, between described surplus valve and liquid reserve tank (18), set up a straight-through pipeline, and on this pipeline, the 4th solenoid valve (12) being connected with control circuit (4) is set.
4. oil cooler testing table according to claim 1, it is characterized in that, described the first solenoid valve (13), the second solenoid valve (14), the 3rd solenoid valve (15), the 4th solenoid valve (12) are guide type electromagnetic high pressure fuel tap.
5. oil cooler testing table according to claim 1, is characterized in that, described sensor (6) is high-accuracy hydraulic pressure transducer.
CN201420275789.7U 2014-05-27 2014-05-27 Oil cooler testing table Expired - Fee Related CN203981207U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420275789.7U CN203981207U (en) 2014-05-27 2014-05-27 Oil cooler testing table

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420275789.7U CN203981207U (en) 2014-05-27 2014-05-27 Oil cooler testing table

Publications (1)

Publication Number Publication Date
CN203981207U true CN203981207U (en) 2014-12-03

Family

ID=51978637

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420275789.7U Expired - Fee Related CN203981207U (en) 2014-05-27 2014-05-27 Oil cooler testing table

Country Status (1)

Country Link
CN (1) CN203981207U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107748076A (en) * 2017-12-01 2018-03-02 新乡市豫新航空工业制品有限公司 A kind of radiator combustion oil check conversion pipe-line system

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107748076A (en) * 2017-12-01 2018-03-02 新乡市豫新航空工业制品有限公司 A kind of radiator combustion oil check conversion pipe-line system
CN107748076B (en) * 2017-12-01 2023-09-12 河南新航航空设备科技有限公司 Conversion pipeline system for detecting fuel oil of radiator

Similar Documents

Publication Publication Date Title
CN102865271A (en) Detection method and device of internal leakage of hydraulic valve
CN103644151A (en) Energy-conservation and low-impact hydraulic cylinder test testbed hydraulic control system
CN103234718B (en) Performance testing system for air brake valve of tractor trailer
CN204783953U (en) Energy -conserving test device of synthesis of solenoid valve and pneumatic cylinder reliability
CN105020128A (en) Comprehensive performance test bed of fuel pumps
CN104154017A (en) Water pump detection system
CN108240371B (en) Oil cylinder oil leakage detection method and detection device
CN101349608A (en) Method and apparatus for detecting pressure vessel air tightness
CN210375687U (en) Detection apparatus for simulation deep sea environment reciprocating motion sealing washer sealing performance
CN104895871A (en) Comprehensive and energy-saving testing device and method for reliability of electromagnetic valves and hydraulic cylinders
CN203685769U (en) Oil cylinder test board control system
CN204942157U (en) A kind of can testing pump, oil cylinder multifunctional servo valve detection system
CN104481971A (en) Torque-type hydraulic pump and hydraulic motor power recovery test platform
CN203981207U (en) Oil cooler testing table
CN206206322U (en) A kind of low discharge leakage tester
CN203720025U (en) Multifunctional gas cylinder water pressure testing equipment
CN102297066B (en) System and method for detecting spraying angle of engine oil sprayer
CN104007251A (en) Hydraulic oil stability determinator
CN102288252B (en) System for testing micro leakage of sealed component
CN202177417U (en) Test system for micro-leakage amount of sealing element
CN110617959A (en) Detection apparatus for simulation deep sea environment reciprocating motion sealing washer sealing performance
CN204403051U (en) A kind of torsion type oil hydraulic pump and oil hydraulic motor Power Recovery test platform
CN203083885U (en) Novel outside-measuring-method hydrostatic test device
CN207816531U (en) A kind of thermostat of automobile engine leakage amount detector
CN105275921A (en) Aviation hydraulic test system

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141203

Termination date: 20170527