CN201887309U - Aviation plug cable solder stand - Google Patents
Aviation plug cable solder stand Download PDFInfo
- Publication number
- CN201887309U CN201887309U CN2010206598213U CN201020659821U CN201887309U CN 201887309 U CN201887309 U CN 201887309U CN 2010206598213 U CN2010206598213 U CN 2010206598213U CN 201020659821 U CN201020659821 U CN 201020659821U CN 201887309 U CN201887309 U CN 201887309U
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- CN
- China
- Prior art keywords
- plug
- template
- cable
- stand
- nylon
- 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
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- Connections Effected By Soldering, Adhesion, Or Permanent Deformation (AREA)
Abstract
The utility model discloses an aviation plug cable solder stand, which comprises a stand and a nylon template, wherein the nylon template is fixed on the stand, and is provided with 12 through holes matched with the contact pins of an encoder connector assembly. When the stand is in use, 12 pins in the encoder connector assembly are taken out and then are respectively placed in the 12 through holes in the panel of the nylon template, and one end requiring soldering is exposed outside the nylon template. The insulating layer of one corresponding end of a twelve-core cable is stripped according to the actual size of the plug, the cable is respectively soldered on the pins according to the requirement of the soldering position of the 12 pins on the drawing, then the pins are taken out from the template, and then are installed on the corresponding position of the plug, the protection is performed, the plug shell is arranged, now an encoder plug is made. The aviation plug cable solder stand is applied to the soldering of the encoder plug cable in a wind generating set, and is simple and practical, the production efficiency can be improved and the soldering quality of the cable is ensured.
Description
Technical field
The utility model relates to a kind of aviation plug bonding wire support.
Background technology
At present, very inconvenient when the cable of real work welding encoder plug, though because encoder plug size not quite has 12 stitch, and the distance between each stitch is very little.Weld if directly stitch is placed in the plastic seat of plug, be easy to plastic seat is scorched, also cause the short circuit between stitch easily, efficient is also lower.And if contact pin taking-up welding separately, contact pin is too tiny, be difficult for fixing the definite of every wire position and length that also be not easy to.
Summary of the invention
At above-mentioned prior art, the utility model provides a kind of aviation plug bonding wire support, and the utility model is simple in structure, make easily, support can be fixed on the work top solid and reliable, and the contact pin template can be rotated, be convenient to adjust the orientation, make the operator more comfortable.
The utility model is achieved through the following technical solutions:
A kind of aviation plug bonding wire support comprises support, nylon template, and wherein, the nylon template is fixed on the support, and the nylon template is provided with 12 through holes that match with the contact pin of encoder connector assembly.
Described nylon template both sides are provided with double-screw bolt, and the nylon template is fixedlyed connected with support by the connected mode of double-screw bolt-ingot bolt.
During use, 12 stitch in the encoder connector assembly are taken out 12 holes putting into the nylon stencil plane respectively, an end that needs bonding wire is exposed at the outside of nylon template.Because the needle body section diameter of contact pin exposes bonding wire diameter partly less than needs, so can not drop out the nylon template.Cable one end of corresponding 12 cores, actual size according to plug is peelled off insulating barrier to cable, requirement according to drawing on the welding position of 12 contact pins is welded on the contact pin respectively, again contact pin is taken out from template and be installed in respectively in the plug on the corresponding position, properly protect, what a encoder plug first-class plug body has just made.
The utlity model has following advantage:
1) similar with the actual plug position, the length of cable and layout type can be done relatively accurately.
2) owing to the distance that has strengthened between stitch, brazing process is convenient to construction, guarantees welding quality easily.
3) it is fastening that the nylon stencil plane adopts wing nut, and setting angle can rotate easily and be fixing, and the operator can be transferred to the position welding of being convenient to operate, and enhances productivity.
The utility model is applied to the welding job of the encoder plug cable in the wind turbine generator.It is simple and practical, can enhance productivity, and guarantees the welding quality of cable.The utility model not only can be used for wind-driven generator, can be applicable to the cable welding of encoder plug in the control system of other field simultaneously, and prospect is boundless.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 needs the fixedly core print seat and the contact pin schematic diagram of bonding wire for aviation plug;
He 3 is a user mode reference diagram of the present utility model.
Wherein, 1, nylon template; 2, double-screw bolt; 3, wing nut; 4, support; 5, contact pin; 6, encoder connector assembly.
Embodiment
Below in conjunction with accompanying drawing the utility model is further described.
A kind of aviation plug bonding wire support comprises support 4, nylon template 1, and as shown in Figure 1, wherein, nylon template 1 is fixed on the support 4, and nylon template 1 is provided with 12 through holes that match with the contact pin 5 of encoder connector assembly 6.
Described nylon template 1 both sides are provided with double-screw bolt 2, and nylon template 1 is fixedlyed connected with support 4 by 3 connected modes of double-screw bolt 2-ingot bolt.
During use, 12 stitch (as shown in Figure 2) in the encoder connector assembly 6 are taken out 12 holes putting into nylon template 1 plane respectively, an end that needs bonding wire is exposed at the outside of nylon template 1, as shown in Figure 3.Because the needle body section diameter of contact pin 5 exposes bonding wire diameter partly less than needs, so can not drop out nylon template 1.Cable one end of corresponding 12 cores, actual size according to plug is peelled off insulating barrier to cable, requirement according to drawing on the welding position of 12 contact pins 5 is welded on respectively on the contact pin 5, again contact pin 5 is taken out from nylon template 1 and be installed in respectively in the plug on the corresponding position, properly protect, what a encoder plug first-class plug body has just made.
Claims (2)
1. aviation plug bonding wire support, it is characterized in that: comprise support, nylon template, wherein, the nylon template is fixed on the support, and the nylon template is provided with 12 through holes that match with the contact pin of encoder connector assembly.
2. aviation plug bonding wire support according to claim 1 is characterized in that: described nylon template both sides are provided with double-screw bolt, and the nylon template is fixedlyed connected with support by the connected mode of double-screw bolt-ingot bolt.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206598213U CN201887309U (en) | 2010-12-15 | 2010-12-15 | Aviation plug cable solder stand |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2010206598213U CN201887309U (en) | 2010-12-15 | 2010-12-15 | Aviation plug cable solder stand |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201887309U true CN201887309U (en) | 2011-06-29 |
Family
ID=44184856
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2010206598213U Expired - Fee Related CN201887309U (en) | 2010-12-15 | 2010-12-15 | Aviation plug cable solder stand |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201887309U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102983477A (en) * | 2012-11-23 | 2013-03-20 | 西安开容电子技术有限责任公司 | Welding mechanism of connector pin |
| CN108581316A (en) * | 2018-04-16 | 2018-09-28 | 西安飞机工业（集团）有限责任公司 | A kind of cable single hole bolt welding assistor |
| CN109950770A (en) * | 2017-12-20 | 2019-06-28 | 中航光电科技股份有限公司 | Contact pin welds auxiliary tool and contact pin component |
| CN110052765A (en) * | 2019-04-19 | 2019-07-26 | 中电科芜湖钻石飞机制造有限公司 | General-purpose aircraft earphone socket welding tooling and its welding method |
-
2010
- 2010-12-15 CN CN2010206598213U patent/CN201887309U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102983477A (en) * | 2012-11-23 | 2013-03-20 | 西安开容电子技术有限责任公司 | Welding mechanism of connector pin |
| CN109950770A (en) * | 2017-12-20 | 2019-06-28 | 中航光电科技股份有限公司 | Contact pin welds auxiliary tool and contact pin component |
| CN109950770B (en) * | 2017-12-20 | 2020-12-04 | 中航光电科技股份有限公司 | Contact pin welding auxiliary tool and contact pin assembly |
| CN108581316A (en) * | 2018-04-16 | 2018-09-28 | 西安飞机工业（集团）有限责任公司 | A kind of cable single hole bolt welding assistor |
| CN110052765A (en) * | 2019-04-19 | 2019-07-26 | 中电科芜湖钻石飞机制造有限公司 | General-purpose aircraft earphone socket welding tooling and its welding method |
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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: 20110629 Termination date: 20161215 |