CN209700979U - Airline carriers of passengers main cabin hydroelectric facility combined test stand - Google Patents
Airline carriers of passengers main cabin hydroelectric facility combined test stand Download PDFInfo
- Publication number
- CN209700979U CN209700979U CN201822252653.5U CN201822252653U CN209700979U CN 209700979 U CN209700979 U CN 209700979U CN 201822252653 U CN201822252653 U CN 201822252653U CN 209700979 U CN209700979 U CN 209700979U
- Authority
- CN
- China
- Prior art keywords
- test
- water
- water tank
- main cabin
- solenoid valve
- 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
Links
Abstract
The utility model discloses a kind of airline carriers of passengers main cabin hydroelectric facility combined test stands, including water route test macro and circuit test system: the water route test macro includes test water tank, the test water tank respectively connected air inlet, water inlet, exhaust outlet and water outlet, pressure regulator valve is disposed between the air inlet and test water tank, boost gauge and intake solenoid valve, water supply solenoid valve is disposed between the water inlet and test water tank, inlet gage and check valve, exhaust solenoid valve is provided between the exhaust outlet and test water tank, flowmeter and discharge pressure table are disposed between the water outlet and test water tank, water level sensor is provided in the test water tank.Water power test is integrated on a testboard by the utility model, and all realizes automation and visualization by the index and operation of observation required when will test, and is improved the accuracy of operation, is avoided and maloperation and leakage operation occur.
Description
Technical field
The utility model is specifically related to a kind of airline carriers of passengers main cabin hydroelectric facility combined test stand.
Background technique
The existing hydroelectric facility performance for airline carriers of passengers main cabin carries out test and multiple devices is needed to be tested respectively,
Not only test process is cumbersome, takes a long time, and entire test automation and visualization are poor, be easy to appear maloperation and
Leakage operation, the precision of last test are also not highly desirable.
Summary of the invention
Goal of the invention: in order to overcome the deficiencies in the prior art, water power performance test can be integrated by providing one kind
Together and have automation and visualized operation well, the high airline carriers of passengers main cabin hydroelectric facility of measurement accuracy is comprehensive to be surveyed
Test stand.
Technical solution: to achieve the above object, the utility model provides a kind of airline carriers of passengers main cabin hydroelectric facility comprehensive survey
Test stand, including water route test macro and circuit test system: the water route test macro includes test water tank, the test water tank
It respectively connected air inlet, water inlet, exhaust outlet and water outlet, be disposed with pressure regulation between the air inlet and test water tank
Valve, boost gauge and intake solenoid valve are disposed with water supply solenoid valve, influent pressure between the water inlet and test water tank
Power table and check valve are provided with exhaust solenoid valve between the exhaust outlet and test water tank, the water outlet and test water tank it
Between be disposed with flowmeter and discharge pressure table, water level sensor, the circuit test system are provided in the test water tank
System includes A phase current table, B phase current table and C phase current table, and the A phase current table, B phase current table and C phase current table are all connected with
Trigger, the trigger be connected to timer.
Further, first filter is provided between the water inlet and water supply solenoid valve.
Further, the second filter is provided between the discharge pressure table and test water tank.
Further, muffler is provided between the exhaust outlet and exhaust solenoid valve.
Further, water tank cleaning mouth is provided on the test water tank.
Further, the A phase current table, B phase current table and C phase current table are respectively arranged with A phase indicator light, B phase refers to
Show lamp and C phase indicator light.
Further, pressurization indicator light is provided on the intake solenoid valve.
Further, the pressurization switch for controlling intake solenoid valve switch is provided in the water route test macro.
Further, moisturizing indicator light is provided in the water supply solenoid valve.
Further, the water route test macro and circuit test system are all connected with A.C. voltmeter.
The utility model has the advantages that the utility model compared with prior art, has following advantage:
1, water power test is integrated on a testboard, and complete by the index and operation of observation required when will test
Portion realizes automation and visualization, improves the accuracy of operation, avoids and maloperation and leakage operation occurs, realizes testboard
High universalizable, high reliability and ease for operation；
2, by the way of entire pressurisation, the stability and adjustability when pressure test is realized, the essence of measurement is improved
Degree；
3, the starting of clocking capability and cut-off direct monitoring operating current are more accurate compared to manual time-keeping.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of water route test macro；
Fig. 2 is the circuit connection diagram of the utility model.
Specific embodiment
In the following with reference to the drawings and specific embodiments, the utility model is furtherd elucidate, it should be understood that these embodiments are only used for
Illustrate the utility model rather than limitation the scope of the utility model, after having read the utility model, art technology
Personnel fall within the application range as defined in the appended claims to the modification of the various equivalent forms of the utility model.
As depicted in figs. 1 and 2, the utility model provides a kind of airline carriers of passengers main cabin hydroelectric facility combined test stand, including
Water route test macro and circuit test system:
The water route test macro includes test water tank 5, and the test water tank 5 respectively connected air inlet 1, water inlet
10, exhaust outlet 13 and water outlet 17 are disposed with pressure regulator valve 2, boost gauge 3 between the air inlet 1 and test water tank 5
With intake solenoid valve 4, the water inlet 10 and test water tank 5 between be disposed with water supply solenoid valve 8, inlet gage 7 and
Check valve 6 is provided with exhaust solenoid valve 11, the water outlet 17 and test water tank 5 between the exhaust outlet 13 and test water tank 5
Between be disposed with flowmeter 16 and discharge pressure table 15, be provided with water level sensor 18 in the test water tank 5.
The circuit test system includes A phase current table 20, B phase current table 21 and C phase current table 22, the A phase current
Table 20, B phase current table 21 and C phase current table 22 are all connected with trigger 23, and the trigger 23 is connected to timer 24.
First filter 9, the discharge pressure table 15 and test are provided between the water inlet 10 and water supply solenoid valve 8
It is provided with the second filter 14 between water tank 5, muffler 12 is provided between the exhaust outlet 13 and exhaust solenoid valve 11, it is described
It is provided with water tank cleaning mouth 51 on test water tank 5, the A phase current table 20, B phase current table 21 and C phase current table 22 are set respectively
It is equipped with A phase indicator light 25, B phase indicator light 26 and C phase indicator light 27, pressurization indicator light 41 is provided on the intake solenoid valve 4,
The pressurization switch 42 for controlling the switch of intake solenoid valve 4 is provided in the water route test macro, in the water supply solenoid valve 8
It is provided with moisturizing indicator light 81, the water route test macro and circuit test system are all connected with A.C. voltmeter 28, the water
Path test system and circuit test system are provided with equipment master switch 29.
The water level sensor 18 controls water supply solenoid valve 8, when water level is lower than water level sensor 18, moisturizing indicator light 81
It lights, the control of water level sensor 18 opens water supply solenoid valve 8 and connects water source moisturizing into test water tank 5, when water level did not had water level
When sensor 18, moisturizing indicator light 81 extinguishes, and water supply solenoid valve 8 is closed, to realize the automatic benefit for testing water tank 5
Water.
Intake solenoid valve 4 is in close state under normal condition, and exhaust solenoid valve 11 is in the open state, when needing to be pressurized
When, pressurization switch 42 is pressed, intake solenoid valve 4 is opened at this time, and exhaust solenoid valve 11 is in close state, plenum is carried out,
When needing to release stress, then pressurization switch 42 is pressed again, intake solenoid valve 4 is in close state at this time, exhaust solenoid valve
11 is in the open state.
Claims (10)
1. airline carriers of passengers main cabin hydroelectric facility combined test stand, it is characterised in that: including water route test macro and circuit test system
System:
The water route test macro includes test water tank (5), and the test water tank (5) respectively connected air inlet (1), water inlet
(10), exhaust outlet (13) and water outlet (17) are disposed with pressure regulator valve between the air inlet (1) and test water tank (5)
(2), boost gauge (3) and intake solenoid valve (4) are disposed with benefit between the water inlet (10) and test water tank (5)
Water solenoid valve (8), inlet gage (7) and check valve (6), the row of being provided between the exhaust outlet (13) and test water tank (5)
Pneumoelectric magnet valve (11) is disposed with flowmeter (16) and discharge pressure table between the water outlet (17) and test water tank (5)
(15), water level sensor (18) are provided in the test water tank (5)；
The circuit test system includes A phase current table (20), B phase current table (21) and C phase current table (22), the A phase electricity
Flow table (20), B phase current table (21) and C phase current table (22) are all connected with trigger (23), and the trigger (23) is connected to
Timer (24).
2. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the water inlet
(10) it is provided between water supply solenoid valve (8) first filter (9).
3. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the water outlet pressure
The second filter (14) are provided between power table (15) and test water tank (5).
4. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the exhaust outlet
(13) it is provided between exhaust solenoid valve (11) muffler (12).
5. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the test water
Water tank cleaning mouth (51) are provided on case (5).
6. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the A phase electricity
Flow table (20), B phase current table (21) and C phase current table (22) are respectively arranged with A phase indicator light (25), B phase indicator light (26) and C
Phase indicator light (27).
7. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the air inlet electricity
Pressurization indicator light (41) is provided on magnet valve (4).
8. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the water route is surveyed
The pressurization switch (42) for controlling intake solenoid valve (4) switch is provided on test system.
9. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the moisturizing electricity
Moisturizing indicator light (81) are provided on magnet valve (8).
10. airline carriers of passengers main cabin hydroelectric facility combined test stand according to claim 1, it is characterised in that: the water route
Test macro and circuit test system are all connected with A.C. voltmeter (28).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822252653.5U CN209700979U (en) | 2018-12-29 | 2018-12-29 | Airline carriers of passengers main cabin hydroelectric facility combined test stand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822252653.5U CN209700979U (en) | 2018-12-29 | 2018-12-29 | Airline carriers of passengers main cabin hydroelectric facility combined test stand |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209700979U true CN209700979U (en) | 2019-11-29 |
Family
ID=68638872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822252653.5U Expired - Fee Related CN209700979U (en) | 2018-12-29 | 2018-12-29 | Airline carriers of passengers main cabin hydroelectric facility combined test stand |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209700979U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625321A (en) * | 2018-12-29 | 2019-04-16 | 南京王行航空附件维修工程有限公司 | Water power integrated test system |
-
2018
- 2018-12-29 CN CN201822252653.5U patent/CN209700979U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625321A (en) * | 2018-12-29 | 2019-04-16 | 南京王行航空附件维修工程有限公司 | Water power integrated test system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20191129 Termination date: 20211229 |