CN210209222U - A clamping tool for military standard aviation plug bonding wire - Google Patents
A clamping tool for military standard aviation plug bonding wire Download PDFInfo
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- CN210209222U CN210209222U CN201921009537.9U CN201921009537U CN210209222U CN 210209222 U CN210209222 U CN 210209222U CN 201921009537 U CN201921009537 U CN 201921009537U CN 210209222 U CN210209222 U CN 210209222U
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Abstract
The utility model belongs to the technical field of the clamping tool technique and specifically relates to a clamping tool for military standard aviation plug bonding wire, including tool bottom plate, tool fixing base, first straight line handle, anchor clamps, the straight line handle of second and nut, install an at least set of tool fixing base on the tool bottom plate, anchor clamps are installed on the tool fixing base through first straight line handle, anchor clamps upper portion cylinder has the opening, the straight line handle of second transversely runs through behind the cylinder through the nut fastening. The utility model discloses a many places of clamping tool are adjustable, and different people can adjust according to self operation custom, but short time adaptation tool improves bonding wire efficiency.
Description
Technical Field
The utility model relates to a clamping tool technical field specifically is a clamping tool for military standard aviation plug bonding wire.
Background
At present, the aviation plug and the electric wire are generally welded manually by an operator, and because the aviation plug is generally cylindrical, the caliber of a jig needs to be made into a whole cylinder to clamp an aviation plug wiring terminal, the clamping force of the whole cylinder cannot be adjusted, the whole cylinder is too loose or too tight, and the wire welding operation is very inconvenient; the clamping opening and the supporting column are integrated or are welded, and the inclination angle of the welding wire jig cannot be adjusted. The efficiency of such complex welds of the aircraft plug is therefore very low.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a clamping tool for military standard aviation plug bonding wire to solve the problem that proposes in the above-mentioned background art. This a clamping tool for military rule aviation plug bonding wire can adjust in many places, and different people can adjust according to self operation custom, but short time adaptation tool improves bonding wire efficiency.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a clamping tool for military standard aviation plug bonding wire, includes tool bottom plate, tool fixing base, first straight line handle, anchor clamps, the straight line handle of second and nut, install at least a set of tool fixing base on the tool bottom plate, anchor clamps are installed on the tool fixing base through first straight line handle, anchor clamps upper portion cylinder has the opening, the straight line handle of second transversely runs through behind the cylinder and fastens through the nut.
Further, the tool fixing seats are two groups, threaded holes are formed in the bottoms of the tool fixing seats and the tool bottom plate, and the inner hexagonal screw pads are in threaded connection with the threaded holes after the inner hexagonal screw pads are elastically cushioned.
Further, the first straight-line handle adopts an M5 straight-line handle, the second straight-line handle adopts an M4 straight-line handle, and the nut adopts an M4 nut.
Further, the clamp jaw is provided with a smooth layer surface sprayed with Teflon.
Further, still include the balancing weight, this balancing weight ties the up end at the tool bottom plate through the nut, tool bottom plate, balancing weight all adopt the steel sheet to make.
Compared with the prior art, the beneficial effects of the utility model are that:
the utility model has two parts of the clamp and the fixture fixing seat which are connected by the first straight-line handle, and aims to realize the adjustment of the inclination angle of the clamp mouth of the clamp until the angle of the welding line is most convenient; the opening of the upper cylinder of the clamp is designed, and the clamp is connected and tensioned by a second straight-line handle, so that the clamping force of the clamp for clamping the welding wire column of the aviation plug of the military standard is adjusted, the clamping is stable, and the quality of the welding wire is greatly improved; two clamps are arranged on one jig base plate, so that the continuous wire welding operation without waiting can be realized, and the wire welding efficiency is greatly improved; the fixture fixing seat is fixed by an inner hexagonal screw, and the fixture fixing seat can horizontally rotate to adjust the orientation of the fixture opening.
The utility model discloses, tool bottom plate material is steel, and steel weight can guarantee that bonding wire process clamping tool is difficult for removing, and the tool fixing base adopts a M6 16 interior hexagonal screw to come fixed connection, the ascending orientation of rotatable adjustment anchor clamps horizontal direction. Anchor clamps and tool fixing base are connected with M5 straight line handle, unscrew the ascending inclination of adjustable anchor clamps vertical direction of handle. The anchor clamps material is the teflon, and paint on colored terminal surface can not be scraped to this kind of material, and anchor clamps upper portion is the opening design, and is taut with M4 straight line handle, and the accessible is unscrewed or is screwed up and adjust the dynamics of anchor clamps centre gripping military standard aviation plug welding wire post, realizes that the anchor clamps bore is adjustable. The whole clamping jig is adjustable in multiple positions, different people can adjust the clamping jig according to self operation habits, the clamping jig can be adapted to the jig in a short time, and the wire welding efficiency is improved.
Drawings
Fig. 1 is a schematic view of the vertical structure of the present invention.
Fig. 2 is a schematic top view of the present invention.
Fig. 3 is a schematic cross-sectional view of the cross-section Y-Y of fig. 2 according to the present invention.
Fig. 4 is a schematic side view of the present invention.
In the figure: 1-a jig base plate, 2-an inner hexagonal screw, 3-a spring pad, 4-a jig fixing seat, 5-a first straight-line handle, 6-a clamp, 7-a second straight-line handle, 8-a nut, 9-a cylinder, 10-an opening, 11-a balancing weight and 12-a military aviation plug welding wire column.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
In the description of the present invention, it should be noted that the terms "upper/lower end", "inner", "outer", "front end", "rear end", "both ends", "one end", "the other end" and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for convenience of description and simplification of description, but do not indicate or imply that the device or element referred to must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
In the description of the present invention, it should be noted that, unless explicitly stated or limited otherwise, the terms "mounted," "disposed/sleeved," "connected," and the like are to be construed broadly, e.g., "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.
Referring to fig. 1-4, the present invention provides a technical solution:
the utility model provides a clamping tool for military standard aviation plug bonding wire, includes tool bottom plate 1, tool fixing base 4, first straight line handle 5, anchor clamps 6, second straight line handle 7 and nut 8, install at least a set of tool fixing base 4 on the tool bottom plate 1, anchor clamps 6 are installed on tool fixing base 4 through first straight line handle 5, 6 upper portion cylinders 9 of anchor clamps have opening 10, second straight line handle 7 transversely runs through behind the cylinder 9 and fastens through nut 8, 6 double-layered mouths of anchor clamps have the smooth aspect of teflon spraying.
In this embodiment, the jig fixing seats 4 are two sets, and the bottom of the jig fixing seat 4 and the jig base plate 1 are both provided with threaded holes, and the inner hexagonal screws 2 are stacked up and connected with the threaded holes after the elastic pads 3.
The first straight-line handle 5 adopts an M5 straight-line handle, the second straight-line handle 7 adopts an M4 straight-line handle, and the nut 8 adopts an M4 nut.
In this embodiment, the upper portion cylinder 9 of anchor clamps 6 has opening 10, and through second straight line handle 7, M4 straight line handle and nut 8's cooperation can press from both sides the adjustable elasticity degree of aperture to (dress) of anchor clamps 6 promptly, can adjust the elasticity of centre gripping dynamics, and good anchor clamps can improve the bonding wire quality of terminal.
In this embodiment, two clamps 6 can be installed on one jig base plate 1 at the same time, and the next clamp can be welded immediately after one clamp is welded, so that waiting is not needed, and the wire welding efficiency can be greatly improved.
In this embodiment, the clamping opening of the fixture 6 is separated from the fixture fixing seat 4, and is connected by the first straight handle 5, i.e. the M5 straight handle, and the inclination angle of the clamping opening can be adjusted at will.
In this embodiment, the clamping opening of the clamp 6 is made of teflon, and the surface is smooth, so that paint on the surface of the binding post cannot be scratched.
In the embodiment, the clamp 6 is simple in structure, low in cost and convenient and fast to use.
In this embodiment, still include balancing weight 11, this balancing weight 11 is bolted through the nut and is connect the up end at tool bottom plate 1, balancing weight 11 all adopt the steel sheet to make, and steel weight has especially added balancing weight 11 and can guarantee that this clamping tool is difficult for removing in the bonding wire process.
In the utility model, the clamp 6 and the fixture fixing seat 4 are connected by the first straight-line handle, so as to adjust the inclination angle of the clamping opening of the clamp 6 until the angle is most convenient for welding the wire; the opening of the cylinder 9 at the upper part of the clamp 6 is designed, and the clamp is connected and tensioned by a second straight-grain handle, so that the clamping force of the clamp 6 for clamping the military aviation plug welding wire column 12 is adjusted, the clamping is stable, and the welding wire quality is greatly improved; two clamps 6 are arranged on one jig base plate 1, so that the continuous wire welding operation without waiting can be realized, and the wire welding efficiency is greatly improved; the fixture fixing seat is fixed by an inner hexagonal screw, and the fixture fixing seat can horizontally rotate to adjust the orientation of the fixture opening.
The utility model discloses, 1 material of tool bottom plate is steel, and weld wire process clamping tool is difficult for removing can be guaranteed to steel weight, and tool fixing base 4 adopts a M6 16 allen key screw to come fixed connection, the ascending orientation of rotatable adjustment anchor clamps horizontal direction. Anchor clamps 6 and tool fixing base 4 are connected with M5 straight line handle, unscrew the ascending inclination of adjustable anchor clamps 6 vertical direction of handle. Anchor clamps 6 material is the teflon, and paint on colored terminal surface can not be scraped to this kind of material, and 6 upper portions of anchor clamps are the opening design, and is taut with M4 straight line handle, and the accessible is unscrewed or is screwed up and adjust the dynamics of 6 centre gripping military standard aviation plug weld wire posts 12 of anchor clamps, realizes that 6 bores of anchor clamps are adjustable. The whole clamping jig is adjustable in multiple positions, different people can adjust the clamping jig according to self operation habits, the clamping jig can be adapted to the jig in a short time, and the wire welding efficiency is improved.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (5)
1. The utility model provides a clamping tool for military standard aviation plug bonding wire which characterized in that: including tool bottom plate (1), tool fixing base (4), first straight line handle (5), anchor clamps (6), second straight line handle (7) and nut (8), install at least a set of tool fixing base (4) on tool bottom plate (1), install on tool fixing base (4) anchor clamps (6) through first straight line handle (5), anchor clamps (6) upper portion cylinder (9) have opening (10), second straight line handle (7) transversely run through behind cylinder (9) through nut (8) fastening.
2. The clamping jig for the military aviation plug wire welding of claim 1, wherein: the jig fixing seats (4) are two groups, threaded holes are formed in the bottoms of the jig fixing seats (4) and the jig base plate (1), and the inner hexagonal screws (2) are stacked up and connected with the elastic pads (3) in a threaded mode.
3. The clamping jig for the military aviation plug wire welding of claim 1, wherein: the first straight-line handle (5) adopts an M5 straight-line handle, the second straight-line handle (7) adopts an M4 straight-line handle, and the nut (8) adopts an M4 nut.
4. The clamping jig for the military aviation plug wire welding of claim 1, wherein: the clamping opening of the clamp (6) is provided with a smooth layer surface sprayed by Teflon.
5. The clamping jig for the military aviation plug wire welding of any one of claims 1 to 4, wherein the clamping jig comprises: still include balancing weight (11), this balancing weight (11) are tied through the nut and are connect the up end at tool bottom plate (1), balancing weight (11) all adopt the steel sheet to make.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921009537.9U CN210209222U (en) | 2019-07-01 | 2019-07-01 | A clamping tool for military standard aviation plug bonding wire |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921009537.9U CN210209222U (en) | 2019-07-01 | 2019-07-01 | A clamping tool for military standard aviation plug bonding wire |
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| Publication Number | Publication Date |
|---|---|
| CN210209222U true CN210209222U (en) | 2020-03-31 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921009537.9U Active CN210209222U (en) | 2019-07-01 | 2019-07-01 | A clamping tool for military standard aviation plug bonding wire |
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| CN (1) | CN210209222U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111521554A (en) * | 2020-05-09 | 2020-08-11 | 中国人民解放军海军航空大学岸防兵学院 | Portable electric connector appearance quality detection system |
-
2019
- 2019-07-01 CN CN201921009537.9U patent/CN210209222U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111521554A (en) * | 2020-05-09 | 2020-08-11 | 中国人民解放军海军航空大学岸防兵学院 | Portable electric connector appearance quality detection system |
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Address after: 523000 Guangdong city of Dongguan province Dalang Zhen Sha Bu Cun Sha Fu Road No. 83 Patentee after: Bronte robotics, Inc Address before: 523000 Guangdong city of Dongguan province Dalang Zhen Sha Bu Cun Sha Fu Road No. 83 Patentee before: GUANGDONG BOLANGTE INTELLIGENT EQUIPMENT Co.,Ltd. |