CN201765303U - Flying probe testing machine - Google Patents
Flying probe testing machine Download PDFInfo
- Publication number
- CN201765303U CN201765303U CN201020248443XU CN201020248443U CN201765303U CN 201765303 U CN201765303 U CN 201765303U CN 201020248443X U CN201020248443X U CN 201020248443XU CN 201020248443 U CN201020248443 U CN 201020248443U CN 201765303 U CN201765303 U CN 201765303U
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- duplex
- wheel
- flying probe
- testing machine
- ring shaped
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Abstract
The utility model belongs to the technical field of detecting machines, and discloses a flying probe testing machine. The main technical characteristics of the flying probe testing machine are that the flying probe testing machine comprises a base seat, wherein, an upper guide rail, a lower guide rail and a stepping motor are arranged on the base seat; a detecting column provided with a manipulator and a detecting needle is arranged between the upper and the lower guide rails; a duplex driving synchronous wheel is arranged on the stepping motor; the inner side of the duplex driving synchronous wheel is connected with the inner side of a duplex driven wheel, a first simplex driven wheel and a second simplex driven wheel through a large ring shaped synchronous belt; the outer side of the duplex driving synchronous wheel is connected with the outer side of the duplex driven wheel through a small ring shaped synchronous belt; and the large ring shaped synchronous belt and the small ring shaped synchronous belt are respectively fixed with the detecting column. The flying probe testing machine provided by the utility model has the advantages that a transmission shaft is eliminated, rigid transmission is changed into soft transmission, errors caused by the machine structure are avoided, the problem of detecting needle swinging is avoided, the testing precision is greatly improved, the transmission torsion is reduced, and the testing speed is increased.
Description
Technical field
The utility model belongs to the detection field of mechanical technique, relates in particular to a kind of flying probe tester.
Background technology
To miniaturization, high integrated, high performance trend development, the volume of electronic devices and components is more and more littler day by day for modern electronic product, and density is more and more higher.As the printed panel of the interconnected carrier of electronic devices and components, the density of its density and chip is closely bound up, and its number of plies is more and more, and wiring density is more and more higher.Continuous increase along with wiring density, distance between the test point is microcosmicization day by day also,---0.127mm 0.05mm pitch number of test points per square inch is 500---2500,0.05mm---0.025mm ultra fine pitch number of test points per square inch is 2500---5000.Along with the requirement to detection means improves day by day, current printed board producer wire wound and the needle-bar formula testing apparatuss that adopt more, obviously lag behind the needs that reach high-density test flexibly fast, flying probe equipment is applied in the production by increasing printed board producer.Presently used flying probe tester, base is provided with lower guideway and stepper motor, be provided with the test column that has mechanical arm and chaining pin between last lower guideway, each test column is driven by the stepper motor corresponding with it respectively, stepper motor is connected with transmission shaft, the transmission shaft two ends are provided with up and down active synchronization wheel, up and down the active synchronization wheel by up and down synchronously band be connected with passive and synchronous wheel the up and down, be with synchronously up and down to be connected with test column.This flying probe tester has finer pitch, is not subjected to mesh restraint, tests characteristics such as flexible, that speed is fast, rate of false alarm is low.But in the rigid transmission of transmission shaft, because transmission shaft is elongated, make the wheel of active synchronization up and down at transmission shaft two ends can't guarantee concentricity 0.05mm, transmission shaft radially also can't guarantee 0.05mm in addition, more than two kinds of reasons cause test column under band effect synchronously up and down, top and bottom to occur to swing, produce rotatablely moving of crank type, swinging appears in the test column that causes having mechanical arm and chaining pin, because of physical construction causes error, reduce measuring accuracy.
The utility model content
The technical problems to be solved in the utility model just provide a kind of can be because of physical construction does not cause error, the flying probe tester that measuring accuracy is high.
For solving the problems of the technologies described above, the technical solution adopted in the utility model is: comprise the base that is provided with lower guideway and stepper motor, be provided with the test column that has mechanical arm and chaining pin between last lower guideway, described stepper motor is provided with duplex active synchronization wheel, duplex active synchronization wheel is inboard by big ring-like synchronous band and duplex engaged wheel inboard, the first simply connected engaged wheel, the second simply connected engaged wheel is connected, the duplex active synchronization wheel outside is connected with the duplex engaged wheel outside by little ring-like synchronous band, and big ring-like synchronous band and little ring-like synchronous band fix with test column respectively.
Its additional technical feature is: described test column is four, and two in front, and two in the back.
Flying probe tester provided by the utility model compared with prior art, cancelled transmission shaft, duplex active synchronization wheel has been installed on stepper motor, duplex active synchronization wheel is inboard to be connected with duplex engaged wheel inboard, the first simply connected engaged wheel, the second simply connected engaged wheel by big ring-like synchronous band, the duplex active synchronization wheel outside is connected with the duplex engaged wheel outside by little ring-like synchronous band, and big ring-like synchronous band and little ring-like synchronous band fix with test column respectively.Like this, big ring-like synchronous band connects duplex active synchronization wheel inboard, duplex engaged wheel inboard, the first simply connected engaged wheel and the second simply connected engaged wheel, and between the first simply connected engaged wheel and the second simply connected engaged wheel with test column on/lower end is fixed.Little ring-like synchronous band connects the duplex active synchronization wheel outside and the duplex engaged wheel outside, and fixes with the following/upper end of test column between duplex active synchronization wheel and duplex engaged wheel.When stepper motor rotated, simultaneously to a direction motion, during the stepper motor rotating, test column, mechanical arm and chaining pin back and forth movement were realized test job under big ring-like synchronous band and little ring-like synchronous band acting in conjunction in the top and bottom of test column.Above-mentioned test process changes rigid transmission into flexible transmission, has avoided the error that causes because of physical construction, has solved side pin vibration problems, and measuring accuracy improves greatly, has reduced transmission torsion, has improved test speed.
Description of drawings
Fig. 1 is the structural representation of the utility model flying probe tester;
Fig. 2 is the structural representation of duplex active synchronization wheel.
Embodiment
Be described in further details below in conjunction with the concrete structure and the use principle of accompanying drawing the utility model flying probe tester.
As shown in Figure 1, the utility model flying probe tester comprises base 1, base 1 is provided with upper rail 2, lower guideway 3 and stepper motor 4, upper rail 2,3 of lower guideways are provided with test column 5, test column 5 has mechanical arm 6 and chaining pin 7, stepper motor 4 is provided with duplex active synchronization wheel 8, the duplex active synchronization take turns 8 inboards by big ring-like be with synchronously 9 with duplex engaged wheel 10 inboards, the first simply connected engaged wheel 11, the second simply connected engaged wheel 12 is connected, the duplex active synchronization is taken turns 8 outsides and also ring-likely is with 13 to be connected with duplex engaged wheel 10 outsides synchronously by little, big ring-likely be with 9 and ring-likely be with 13 to fix with test column 5 respectively synchronously for a short time synchronously, test column 5 can be four as figure, two in front, and two in the back.As shown in Figure 2, the inboard 81 of duplex active synchronization wheel 8 ring-likely is with 9 to be connected with big synchronously, and the duplex active synchronization is taken turns 8 the outside 82 and ring-likely is with 13 to be connected synchronously with little.
Flying probe tester provided by the utility model, big ring-likely be with 9 to connect the duplex active synchronization and take turns 8 inboards, duplex engaged wheel 10 inboards, the first simply connected engaged wheel 11 and the second simply connected engaged wheel 12 synchronously, and between the first simply connected engaged wheel 11 and the second simply connected engaged wheel 12 with test column 5 on/lower end is fixed.The little ring-like 13 connection duplex active synchronization of being with are synchronously taken turns 8 outsides and duplex engaged wheel 10 outsides, and fix with the following/upper end of test column 5 between duplex active synchronization wheel 8 and duplex engaged wheel 10.When stepper motor 4 rotations, the top and bottom of test column 5 ring-likely are with 9 and little ring-like being with synchronously under 13 actings in conjunction simultaneously to a direction motion synchronously big, during stepper motor 4 rotatings, test column 5, mechanical arm 6 and chaining pin 7 back and forth movements are realized test job.Test column 5 can be four as figure, and two in front, and two in the back, and two stepper motors 4 are installed in the base 1 at lower guideway 3 two ends respectively.Above-mentioned test process changes rigid transmission into flexible transmission, has avoided the error that causes because of physical construction, has solved side pin vibration problems, and measuring accuracy improves greatly, has reduced transmission torsion, has improved test speed.
Claims (2)
1. flying probe tester, comprise the base that is provided with lower guideway and stepper motor, be provided with the test column that has mechanical arm and chaining pin between last lower guideway, it is characterized in that: described stepper motor is provided with duplex active synchronization wheel, duplex active synchronization wheel is inboard to be connected with duplex engaged wheel inboard, the first simply connected engaged wheel, the second simply connected engaged wheel by big ring-like synchronous band, the duplex active synchronization wheel outside is connected with the duplex engaged wheel outside by little ring-like synchronous band, and big ring-like synchronous band and little ring-like synchronous band fix with test column respectively.
2. flying probe tester according to claim 1 is characterized in that: described test column is four, and two in front, and two in the back.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201020248443XU CN201765303U (en) | 2010-06-30 | 2010-06-30 | Flying probe testing machine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201020248443XU CN201765303U (en) | 2010-06-30 | 2010-06-30 | Flying probe testing machine |
Publications (1)
Publication Number | Publication Date |
---|---|
CN201765303U true CN201765303U (en) | 2011-03-16 |
Family
ID=43717911
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201020248443XU Expired - Fee Related CN201765303U (en) | 2010-06-30 | 2010-06-30 | Flying probe testing machine |
Country Status (1)
Country | Link |
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CN (1) | CN201765303U (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103499785A (en) * | 2013-10-14 | 2014-01-08 | 无锡俊达测试技术服务有限公司 | Flying probe tester |
CN111086882A (en) * | 2019-11-05 | 2020-05-01 | 深圳市迈创力科技有限公司 | Method for shortening transfer cycle time |
CN113866587A (en) * | 2021-08-20 | 2021-12-31 | 苏州恒测电子科技有限公司 | Flying probe test equipment |
-
2010
- 2010-06-30 CN CN201020248443XU patent/CN201765303U/en not_active Expired - Fee Related
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103499785A (en) * | 2013-10-14 | 2014-01-08 | 无锡俊达测试技术服务有限公司 | Flying probe tester |
CN111086882A (en) * | 2019-11-05 | 2020-05-01 | 深圳市迈创力科技有限公司 | Method for shortening transfer cycle time |
CN113866587A (en) * | 2021-08-20 | 2021-12-31 | 苏州恒测电子科技有限公司 | Flying probe test equipment |
CN113866587B (en) * | 2021-08-20 | 2024-05-24 | 苏州国科测试科技有限公司 | Flying probe test equipment |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C17 | Cessation of patent right | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20110316 Termination date: 20130630 |