CN105510159A - Battery shrapnel fatigue testing device - Google Patents
Battery shrapnel fatigue testing device Download PDFInfo
- Publication number
- CN105510159A CN105510159A CN201510777248.3A CN201510777248A CN105510159A CN 105510159 A CN105510159 A CN 105510159A CN 201510777248 A CN201510777248 A CN 201510777248A CN 105510159 A CN105510159 A CN 105510159A
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- CN
- China
- Prior art keywords
- relay
- electrical panel
- fixedly installed
- time switch
- solenoid valve
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- Granted
Links
- 238000009661 fatigue test Methods 0.000 title claims abstract description 26
- 238000012360 testing method Methods 0.000 claims abstract description 37
- 238000003475 lamination Methods 0.000 claims description 30
- 239000012634 fragment Substances 0.000 claims description 22
- 230000001105 regulatory effect Effects 0.000 abstract 2
- 206010016256 fatigue Diseases 0.000 description 4
- 230000006835 compression Effects 0.000 description 3
- 238000007906 compression Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000001514 detection method Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
Landscapes
- Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)
Abstract
The present invention discloses a battery shrapnel fatigue testing device which includes a stationary frame, a down pushing means, a counting relay, a timing relay, a solenoid valve, an air pressure regulating valve, a shrapnel test stand, a relay controller and a switching power supply, the stationary frame includes a base plate, an electrical panel, a positioning rack and a support column, the electrical panel is fixed on the base plate by the support column, the positioning rack is fixedly disposed on the electrical panel, the down pushing means is fixedly disposed on the positioning rack, the counting relay, the timing relay, the solenoid valve, the air pressure regulating valve and the shrapnel test stand are fixedly disposed on the electrical panel, the shrapnel test stand and the down pushing means are oppositely disposed, the shrapnel test stand is disposed below the down pushing means, the relay controller and the switching power supply are fixedly disposed on the base plate, and the battery shrapnel fatigue testing device is simple in structure and easy to use, and improves test accuracy and test efficiency.
Description
Technical field
The present invention relates to detection technique field, particularly relate to a kind of battery spring lamination fatigue test device.
Background technology
Existing to battery spring lamination testing fatigue mainly through manually pressing battery spring lamination, to assess elasticity and the rigidity of battery spring lamination, but there is following problem: manual operation test dynamics and the bad control of decrement; Manual operation fatiguability and efficiency is low, the metering system of the artificial testing fatigue of battery spring lamination is wasted time and energy and precision is not high.
Summary of the invention
In view of current battery shell fragment testing fatigue above shortcomings, the invention provides a kind of battery spring lamination fatigue test device, its structure is simple, easy to use, improves measuring accuracy and testing efficiency.
For achieving the above object, embodiments of the invention adopt following technical scheme:
A kind of battery spring lamination fatigue test device, described battery spring lamination fatigue test device comprises fixed frame, hold-down devices, counting relay, time switch, solenoid valve, air pressure regulator, shell fragment testing table, relay-operated controller, Switching Power Supply, described fixed frame comprises base plate, electrical panel, locating rack, support column, described electrical panel is fixed on base plate by support column, and described locating rack is fixedly installed in electrical panel, and described hold-down devices is fixedly installed on locating rack, described counting relay, time switch, solenoid valve, air pressure regulator, shell fragment testing table is fixedly installed in electrical panel, and described shell fragment testing table and hold-down devices are oppositely arranged, and described shell fragment testing table is arranged on below hold-down devices, described relay-operated controller, Switching Power Supply is fixedly installed on base plate, described counting relay, time switch is connected with relay-operated controller respectively, described relay-operated controller, counting relay, time switch is connected with solenoid valve respectively, and described air pressure regulator is connected with solenoid valve, and described solenoid valve is connected with hold-down devices, described counting relay, time switch, solenoid valve, relay-operated controller is connected with Switching Power Supply respectively.
According to one aspect of the present invention, described locating rack comprises back up pad, backing plate, corner bracket plate, described back up pad is vertically fixed in electrical panel, described backing plate, corner bracket plate are fixedly installed on the biside plate face of back up pad respectively, described hold-down devices is fixedly installed on backing plate, and described corner bracket plate and back up pad form a groove.
According to one aspect of the present invention, described hold-down devices comprises cylinder and pressing plate, and described pressing plate is arranged in the push strut of cylinder lower end.
According to one aspect of the present invention, described battery spring lamination fatigue test device also comprises time switch switch and counting relay switch, described time switch switch and counting relay switch are fixedly installed in electrical panel, described time switch is connected with time switch, and described counting relay switch is connected with counting relay.
According to one aspect of the present invention, described counting relay, time switch, solenoid valve, air pressure regulator are fixedly installed on electrical panel lower position respectively, and described shell fragment testing table is fixedly installed on electrical panel top position.
Advantage of the invention process: fix cylinder by fixed frame, counting relay, time switch, relay-operated controller, solenoid valve, Switching Power Supply, shell fragment testing table, the compression angle of tested battery spring lamination is guaranteed in the installation site calculating cylinder and shell fragment testing table, the aerodynamic force of compressor is passed to cylinder, by the dynamics that presses down and the pressing time that regulate counting relay and time switch to carry out control cylinder, reach the test objective of expection, the battery spring lamination fatigue test device of said structure, its structure is simple, easy to use, improve measuring accuracy and testing efficiency.
Accompanying drawing explanation
In order to be illustrated more clearly in the technical scheme in the embodiment of the present invention, be briefly described to the accompanying drawing used required in embodiment below, apparently, accompanying drawing in the following describes is only some embodiments of the present invention, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation of a kind of battery spring lamination fatigue test device of the present invention;
Fig. 2 is the locating rack structural representation of the fixed frame of a kind of battery spring lamination fatigue test device of the present invention;
Fig. 3 is the electrical panel structural representation of the fixed frame of a kind of battery spring lamination fatigue test device of the present invention;
Fig. 4 is the base arrangement schematic diagram of the fixed frame of a kind of battery spring lamination fatigue test device of the present invention;
Fig. 5 is the electrical connection schematic diagram of a kind of battery spring lamination fatigue test device of the present invention.
Embodiment
Below in conjunction with the accompanying drawing in the embodiment of the present invention, be clearly and completely described the technical scheme in the embodiment of the present invention, obviously, described embodiment is only the present invention's part embodiment, instead of whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.
As Fig. 1, Fig. 2, Fig. 3, shown in Fig. 4 and Fig. 5, a kind of battery spring lamination fatigue test device, described battery spring lamination fatigue test device comprises fixed frame 1, hold-down devices 2, counting relay 3, time switch 4, solenoid valve 5, air pressure regulator 6, shell fragment testing table 7, relay-operated controller 8, Switching Power Supply 9, described fixed frame 1 comprises base plate 11, electrical panel 12, locating rack 13, support column 14, described electrical panel 12 is fixed on base plate 11 by support column 14, and described locating rack 13 is fixedly installed in electrical panel 12, and described hold-down devices 2 is fixedly installed on locating rack 13, described counting relay 3, time switch 4, solenoid valve 5, air pressure regulator 6, shell fragment testing table 7 is fixedly installed in electrical panel 12, and described shell fragment testing table 7 is oppositely arranged with hold-down devices 2, and described shell fragment testing table 7 is arranged on below hold-down devices 2, described relay-operated controller 8, Switching Power Supply 9 is fixedly installed on base plate 11, described counting relay 3, time switch 4 is connected with relay-operated controller 8 respectively, described relay-operated controller 8, counting relay 3, time switch 4 is connected with solenoid valve 5 respectively, and described air pressure regulator 6 is connected with solenoid valve 5, and described solenoid valve 5 is connected with hold-down devices 2, described counting relay 3, time switch 4, solenoid valve 5, relay-operated controller 8 is connected with Switching Power Supply 9 respectively.In the present embodiment, locating rack 13 comprises back up pad 131, backing plate 132, corner bracket plate 133, described back up pad 131 is vertically fixed in electrical panel 12, described backing plate 132, corner bracket plate 133 are fixedly installed on the biside plate face of back up pad 131 respectively, described hold-down devices 2 is fixedly installed on backing plate 132, and described corner bracket plate 133 forms a groove with back up pad 131.
In the present embodiment, hold-down devices 2 comprises cylinder 21 and pressing plate 22, and described pressing plate 22 is arranged in the push strut of cylinder 21 lower end.
In the present embodiment, battery spring lamination fatigue test device also comprises time switch switch 15 and counting relay switch 16, described time switch switch 15 is fixedly installed in electrical panel with counting relay switch 16, described time switch switch 15 is connected with time switch 4, and described counting relay switch 16 is connected with counting relay 3.
In the present embodiment, counting relay 3, time switch 4, solenoid valve 5, air pressure regulator 6 are fixedly installed on electrical panel 12 lower position respectively, and described shell fragment testing table 7 is fixedly installed on electrical panel 12 top position.
Fixed frame fixes cylinder, counting relay, time switch, relay-operated controller, solenoid valve, Switching Power Supply, shell fragment testing table, the compression angle of tested battery spring lamination is guaranteed in the installation site calculating cylinder and shell fragment testing table, the aerodynamic force of compressor is passed to cylinder, by the dynamics that presses down and the pressing time that regulate counting relay and time switch to carry out control cylinder, reach the test objective of expection.
Advantage of the invention process: fix cylinder by fixed frame, counting relay, time switch, relay-operated controller, solenoid valve, Switching Power Supply, shell fragment testing table, the compression angle of tested battery spring lamination is guaranteed in the installation site calculating cylinder and shell fragment testing table, the aerodynamic force of compressor is passed to cylinder, by the dynamics that presses down and the pressing time that regulate counting relay and time switch to carry out control cylinder, reach the test objective of expection, the battery spring lamination fatigue test device of said structure, its structure is simple, easy to use, improve measuring accuracy and testing efficiency.
The above; be only the specific embodiment of the present invention, but protection scope of the present invention is not limited thereto, the technician of any skilled is in technical scope disclosed by the invention; the change that can expect easily or replacement, all should be encompassed within protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain of described claim.
Claims (5)
1. a battery spring lamination fatigue test device, is characterized in that, described battery spring lamination fatigue test device comprises fixed frame, hold-down devices, counting relay, time switch, solenoid valve, air pressure regulator, shell fragment testing table, relay-operated controller, Switching Power Supply, described fixed frame comprises base plate, electrical panel, locating rack, support column, described electrical panel is fixed on base plate by support column, and described locating rack is fixedly installed in electrical panel, and described hold-down devices is fixedly installed on locating rack, described counting relay, time switch, solenoid valve, air pressure regulator, shell fragment testing table is fixedly installed in electrical panel, and described shell fragment testing table and hold-down devices are oppositely arranged, and described shell fragment testing table is arranged on below hold-down devices, described relay-operated controller, Switching Power Supply is fixedly installed on base plate, described counting relay, time switch is connected with relay-operated controller respectively, described relay-operated controller, counting relay, time switch is connected with solenoid valve respectively, and described air pressure regulator is connected with solenoid valve, and described solenoid valve is connected with hold-down devices, described counting relay, time switch, solenoid valve, relay-operated controller is connected with Switching Power Supply respectively.
2. battery spring lamination fatigue test device according to claim 1, it is characterized in that, described locating rack comprises back up pad, backing plate, corner bracket plate, described back up pad is vertically fixed in electrical panel, described backing plate, corner bracket plate are fixedly installed on the biside plate face of back up pad respectively, described hold-down devices is fixedly installed on backing plate, and described corner bracket plate and back up pad form a groove.
3. battery spring lamination fatigue test device according to claim 2, is characterized in that, described hold-down devices comprises cylinder and pressing plate, and described pressing plate is arranged in the push strut of cylinder lower end.
4. battery spring lamination fatigue test device according to claim 3, it is characterized in that, described battery spring lamination fatigue test device also comprises time switch switch and counting relay switch, described time switch switch and counting relay switch are fixedly installed in electrical panel, described time switch is connected with time switch, and described counting relay switch is connected with counting relay.
5. battery spring lamination fatigue test device according to claim 4, it is characterized in that, described counting relay, time switch, solenoid valve, air pressure regulator are fixedly installed on electrical panel lower position respectively, and described shell fragment testing table is fixedly installed on electrical panel top position.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510777248.3A CN105510159B (en) | 2015-11-13 | 2015-11-13 | A kind of battery spring lamination fatigue test device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510777248.3A CN105510159B (en) | 2015-11-13 | 2015-11-13 | A kind of battery spring lamination fatigue test device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105510159A true CN105510159A (en) | 2016-04-20 |
| CN105510159B CN105510159B (en) | 2018-04-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510777248.3A Active CN105510159B (en) | 2015-11-13 | 2015-11-13 | A kind of battery spring lamination fatigue test device |
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| CN (1) | CN105510159B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107101895A (en) * | 2017-04-24 | 2017-08-29 | 安徽江淮汽车集团股份有限公司 | Shell fragment fatigue durability test device |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1017099A (en) * | 1963-04-04 | 1966-01-12 | Electronique Appliquee | Improvements in and relating to fatigue testing devices |
| US3937071A (en) * | 1975-07-11 | 1976-02-10 | The United States Of America As Represented By The Secretary Of The Army | Fatigue test apparatus |
| JPH08219964A (en) * | 1995-02-13 | 1996-08-30 | Mitsubishi Heavy Ind Ltd | Fretting fatigue test equipment |
| CN201653834U (en) * | 2010-01-25 | 2010-11-24 | 广州市驷雄五金有限公司 | Full-automatic anti-fatigue tester based on metal dome |
| CN102053206A (en) * | 2009-11-05 | 2011-05-11 | 富葵精密组件(深圳)有限公司 | Circuit board testing device and method |
-
2015
- 2015-11-13 CN CN201510777248.3A patent/CN105510159B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1017099A (en) * | 1963-04-04 | 1966-01-12 | Electronique Appliquee | Improvements in and relating to fatigue testing devices |
| US3937071A (en) * | 1975-07-11 | 1976-02-10 | The United States Of America As Represented By The Secretary Of The Army | Fatigue test apparatus |
| JPH08219964A (en) * | 1995-02-13 | 1996-08-30 | Mitsubishi Heavy Ind Ltd | Fretting fatigue test equipment |
| CN102053206A (en) * | 2009-11-05 | 2011-05-11 | 富葵精密组件(深圳)有限公司 | Circuit board testing device and method |
| CN201653834U (en) * | 2010-01-25 | 2010-11-24 | 广州市驷雄五金有限公司 | Full-automatic anti-fatigue tester based on metal dome |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107101895A (en) * | 2017-04-24 | 2017-08-29 | 安徽江淮汽车集团股份有限公司 | Shell fragment fatigue durability test device |
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| Publication number | Publication date |
|---|---|
| CN105510159B (en) | 2018-04-13 |
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Effective date of registration: 20211207 Address after: 102209 room 510, 5 / F, building C, State Grid Park, future science city, Changping District, Beijing Patentee after: STATE GRID SIJI SHENWANG POSITION SERVICE (BEIJING) Co.,Ltd. Address before: 201702 floor 2, block C, No. 599, Gaojing Road, Xujing Town, Qingpu District, Shanghai Patentee before: SHANGHAI HUACE NAVIGATION TECHNOLOGY Ltd. |
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Address after: 102209 room 510, 5 / F, building C, State Grid Park, future science city, Changping District, Beijing Patentee after: State Grid Siji Location Service Co.,Ltd. Address before: 102209 room 510, 5 / F, building C, State Grid Park, future science city, Changping District, Beijing Patentee before: STATE GRID SIJI SHENWANG POSITION SERVICE (BEIJING) Co.,Ltd. |
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| EE01 | Entry into force of recordation of patent licensing contract | ||
| EE01 | Entry into force of recordation of patent licensing contract |
Application publication date: 20160420 Assignee: SHANGHAI HUACE NAVIGATION TECHNOLOGY Ltd. Assignor: State Grid Siji Location Service Co.,Ltd. Contract record no.: X2023980053661 Denomination of invention: A fatigue testing device for battery shrapnel Granted publication date: 20180413 License type: Common License Record date: 20231222 |