CN204976399U - Clamp for circular circular connector of plug - Google Patents
Clamp for circular circular connector of plug Download PDFInfo
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- CN204976399U CN204976399U CN201520701333.7U CN201520701333U CN204976399U CN 204976399 U CN204976399 U CN 204976399U CN 201520701333 U CN201520701333 U CN 201520701333U CN 204976399 U CN204976399 U CN 204976399U
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- clamp
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- clamping bar
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Abstract
The utility model discloses a clamp for circular circular connector of plug, the clamp includes with a common fulcrum alternately swing joint's the first pincers body and the second pincers body, and is divided into handheld portion and clamping part with the fulcrum, first centre gripping subassembly, second centre gripping subassembly that the clamping part set up including the symmetry, first centre gripping subassembly and the upper and lower jack catch cambered surface of second centre gripping subassembly formation crooked relatively, upper and lower jack catch cambered surface cooperatees with circular circular connector's outer fringe. The rotatory plug to circular circular connector can be realized to this clamp, has compensatied direct holding between the fingers with the hand and has held the hard shortcoming of plug, and made through setting up upper and lower jack catch cambered surface the clamp with form the face contact between the circular circular connector, not only can make the cooperation that the clamp can be better press from both sides tight circular circular connector, can also increase frictional force, avoid the problem of clamp in in -process landing on circular circular connector of plug.
Description
Technical field
The utility model relates to a kind of clamp, is specifically related to a kind of clamp in order to plug circular aviation plug.
Background technology
In ruggedized computer and cabinet kind equipment, use the circular aviation plug such as YMG, Y11 in a large number.This kind of plug by rotating and the mode clamped, with socket grafting.This type of plug and socket are connected firmly, but by plug from socket carry out plug operation require great effort very much.Especially when on socket panel, plug is densely distributed, plug operating space is limited, grips plug and extract very inconvenient from socket rotation by finger.In addition, when socket panel is positioned at cabinet, arm can not stretch in front, and the plug operation of structure to plug of cabinet also can form obstacle.For the cable maintenance of ruggedized computer in indication control board, ruggedized computer need be extracted out by maintenance personal, and squats to operating desk, stretches into arm and pulls the plug out of the socket, operating difficulties from ruggedized computer side.Because ruggedized computer socket panel plug is densely distributed, for extracting the plug of a wherein cable, often needing the plug of surrounding all to extract, adding the labour intensity of operation.
Utility model content
In view of this, be necessary to provide a kind of clamp being convenient to plug the circular aviation plug on socket panel.
The utility model provides a kind of clamp in order to plug circular aviation plug, described clamp comprises with the first caliper of a common fulcrum intersection flexible connection and the second caliper, and be divided into Handheld Division and clamping part with fulcrum, described clamping part comprises symmetrically arranged first clamp assemblies, the second clamp assemblies, described first clamp assemblies and the second clamp assemblies local inclination form upper and lower claw cambered surface, and described upper and lower claw cambered surface matches with the outer rim of circular aviation plug.
Preferably, described first clamp assemblies comprises,
First clamping part;
Be arranged on the first connector of described first clamping part free end, described first connector is provided with jack;
Inside insert in the first clamping bar in jack;
The first jaw members be connected with described first clamping bar, described first jaw members has the bending upper clipping claw cambered surface of relative second clamp assemblies.
Preferably, described second clamp assemblies comprises,
Second clamping part;
Be arranged on the second connector of described second clamping part free end, described second connector is provided with jack;
Inside insert in the second clamping bar in jack;
The second jaw members be connected with described second clamping bar, described second jaw members has the bending lower claw cambered surface of relative first clamp assemblies.
Preferably, described first connector, the second connector all at least comprise one group of jack.
Preferably, described first connector, the second connector all comprise one along longitudinal jack and in tong bodies direction perpendicular to the horizontal jack in tong bodies direction.
Preferably, the described tong bodies direction horizontal tilt relative to one end that the first jaw members connects of described first clamping bar extends to form the connecting portion that has inclination angle, and described second clamping bar and one end that the second jaw members connects also extend the connecting portion that has same inclination angle relatively.
Preferably, described upper and lower claw cambered surface is respectively equipped with positioning boss away from grafting port side, for carrying out spacing when clamping to aviation plug.
Preferably, described first clamping bar and the second clamping bar are respectively equipped with relative the first close ladder, the second ladder, make the beeline between described first clamping bar and the second clamping bar be less than beeline between the first connector and the first connector.
Preferably, it is hinged that described first clamping bar and the first jaw members pass through a pivot pin, and the contact surface of described first clamping bar and the first jaw members is cambered surface; It is hinged that described second clamping bar and the second jaw members pass through a pivot pin, and the contact surface of described second clamping bar and the second jaw members is also cambered surface.
Clamp in order to plug circular aviation plug described in the utility model, can realize plugging the rotation of circular aviation plug, compensate for the shortcoming that direct hand grips plug plug effort, and by arranging, lower claw cambered surface makes forming surface between described clamp with described circular aviation plug contact, clamp can not only be enable better to coordinate the circular aviation plug of clamping, can also increasing friction force, avoid the problem of clamp landing on circular aviation plug in the process of plug, simultaneously, jaw members has multiple angle of assembling relative to Handheld Division, Handheld Division is enable to stretch into socket panel with best angle, facilitate people's hand operated.Clamp in order to plug circular aviation plug described in the utility model, structure is simple, easy to operate, is applicable to extensive use.
Accompanying drawing explanation
Fig. 1 is the structural representation of the clamp in order to plug circular aviation plug described in the utility model;
Fig. 2 is the Split type structure schematic diagram of the caliper in order to plug circular aviation plug described in the utility model;
Fig. 3 is the Split type structure schematic diagram of the clamping part in order to plug circular aviation plug described in the utility model;
Fig. 4 is another structural representation of the clamp in order to plug circular aviation plug described in the utility model;
Fig. 5 is the another structural representation of the clamp in order to plug circular aviation plug described in the utility model.
Detailed description of the invention
Clearly understand to make the purpose of this utility model, technical scheme and advantage, below in conjunction with drawings and Examples, the utility model is further elaborated, be to be understood that, specific embodiment described herein only in order to explain the utility model, and is not used in restriction the utility model.
As shown in Figure 1, the utility model provides a kind of clamp in order to plug circular aviation plug, described clamp comprises the caliper 10 be flexibly connected with a common fulcrum intersection, in Fig. 2, described caliper 10 is divided into Handheld Division 20 and clamping part 30 with fulcrum, described clamping part 30 comprises symmetrically arranged first clamp assemblies 31, second clamp assemblies 32, described first clamp assemblies 31 and the second clamp assemblies 32 local inclination form upper and lower claw cambered surface 301,302, and described upper and lower claw cambered surface 301,302 matches with the outer rim of circular aviation plug.
By designing this clamp, make it can realize plugging the rotation of circular aviation plug, compensate for the shortcoming that direct hand grips plug plug effort, and by arranging upper and lower claw cambered surface 301,302, forming surface between described clamp with described circular aviation plug is contacted, clamp can not only be enable better to coordinate the circular aviation plug of clamping, can also increasing friction force, avoid the problem of clamp landing on circular aviation plug in the process of plug.
Concrete, as shown in Figure 3, described first clamp assemblies 31 comprises one first clamping part 311, and be arranged on the first connector 312 of described first clamping part 311 free end, described first connector 312 is provided with jack 303; The first clamping bar 313 in jack 303 is inserted in one; One the first jaw members 314 be connected with described first clamping bar 313, described first jaw members 314 has the bending upper clipping claw cambered surface 301 of relative second clamp assemblies 32.
Described second clamp assemblies 32 comprises one second clamping part 321, and be arranged on the second connector 322 of described second clamping part 321 free end, described second connector 322 is provided with jack 303; The second clamping bar 323 in jack 303 is inserted in one; One the second jaw members 324 be connected with described second clamping bar 323, described second jaw members 324 has the bending lower claw cambered surface 302 of relative first clamp assemblies 31.
By arranging described first clamping bar 313 and the second clamping bar 323, in order to increase the plug degree of depth of clamp, make the less space that the structure of clamp assemblies can adapt between the longer structure of circular aviation plug or circular aviation plug, and circular aviation plug arranges the darker various situations in position, make the application of clamp have popularity, improve the service efficiency of clamp.
Wherein, it is hinged that described first clamping bar 313 and the first jaw members 314 pass through a pivot pin, and the contact surface of described first clamping bar 313 and the first jaw members 314 is cambered surface; Described first jaw members 314 can carry out freely rotating of smaller angle relative to the first clamping bar 313, it is hinged that described second clamping bar 323 and the second jaw members 324 pass through a pivot pin, and the contact surface of described second clamping bar 323 and the second jaw members 324 is also cambered surface, described second jaw members 314 can carry out freely rotating of smaller angle relative to the second clamping bar 323, thus described upper and lower claw cambered surface 301,302 better can fit in the outer rim of circular aviation plug.
Described first connector 312, second connector 322 all at least comprises one group of jack 303.Preferably, as shown in Figure 4, described first connector 312, second connector 322 all comprises one along longitudinal jack 303a and in tong bodies direction perpendicular to the horizontal jack 303b in tong bodies direction.
When the position that circular aviation plug is arranged is on the socket panel in front, can by insert in described first connector 312 in the first clamping bar 313 longitudinal jack 303a in time, described first clamping bar 313 is longitudinally arranged along the body direction of caliper 10, described first jaw members 314 is also arranged on the body bearing of trend of described caliper 10, the second clamping bar 323 simultaneously on described second connector 322 is also equipped with, then first, second jaw members 314,324 described can directly stretch in socket panel, carries out longitudinal plug to circular aviation plug.
When the position that circular aviation plug is arranged is on left and right sides socket panel, and inconvenient longitudinal direction of directly carrying out from left and right side is when plugging, can by insert in described first connector 312 in the first clamping bar 313 horizontal jack 303b in time, described first clamping bar 313 is along the body direction horizontally set of caliper 10, described first jaw members 314 is also arranged perpendicular to the body bearing of trend of described caliper 10, the second clamping bar 323 simultaneously on described second connector 322 is also equipped with, then described first, second jaw members 314, 324 can stretch in socket panel from side, horizontal plug is carried out to circular aviation plug.
Further, as shown in Figure 5, for increasing various applicability of described clamp, the body direction of described first clamping bar 313 described caliper 10 relative to one end that the first jaw members 314 connects tilts to extend to form the first connecting portion 315 that has arbitrary angle, one end that described second clamping bar 323 and the second jaw members 324 connect also extends the second connecting portion 325 that has same inclination angle relatively, itself and the first connecting portion 315 are symmetrical arranged, and do not show in accompanying drawing.Then first, second jaw members 314,324 described can stretch in socket panel with above-mentioned angle, carries out oblique plug to circular aviation plug.
Described circular aviation plug is equipped with the force draw-in groove being convenient to rotate, described upper and lower claw cambered surface 301,302 is equipped with positioning boss 304 away from grafting port side, for carrying out spacing to aviation plug when claw.Concrete, described clamp extends the rotation portion of circular aviation plug, and described positioning boss 304 embeds in the force draw-in groove on circular aviation plug, as spacing, when clamp carries out rotation plug, avoid clamp landing on circular aviation plug in the process of plug.
Further, described first clamping bar 313 and the second clamping bar 323 are respectively equipped with relative the first close ladder 316, second ladder 326, the beeline between described first clamping bar 313 and the second clamping bar 323 is made to be less than beeline between the first connector 312 and the first connector 322, when described clamp clamps circular aviation plug, first clamping bar 313 and the second clamping bar 323 can try one's best parallel press close to plug, avoid interfering with other plugs of surrounding, thus the less space making the structure of clamp assemblies can adapt between the longer structure of circular aviation plug or circular aviation plug, and circular aviation plug arranges the darker various situations in position.
Clamp in order to plug circular aviation plug described in the utility model, by designing this clamp, make it can realize plugging the rotation of circular aviation plug, compensate for the shortcoming that direct hand grips plug plug effort, and by arranging, lower claw cambered surface makes forming surface between described clamp with described circular aviation plug contact, clamp can not only be enable better to coordinate the circular aviation plug of clamping, can also increasing friction force, avoid the problem of clamp landing on circular aviation plug in the process of plug, simultaneously, jaw members has multiple angle of assembling relative to Handheld Division, Handheld Division is enable to stretch into socket panel with best angle, facilitate people's hand operated.Clamp in order to plug circular aviation plug described in the utility model, structure is simple, easy to operate, is applicable to extensive use.
The foregoing is only preferred embodiment of the present utility model, not in order to limit the utility model, all within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (9)
1. one kind in order to plug the clamp of circular aviation plug, it is characterized in that, described clamp comprises the caliper (10) be flexibly connected with a common fulcrum intersection, and be divided into Handheld Division (20) and clamping part (30) with fulcrum, described clamping part (30) comprises symmetrically arranged first clamp assemblies (31), second clamp assemblies (32), described first clamp assemblies (31) and the second clamp assemblies (32) local inclination form upper clipping claw cambered surface (301), lower claw cambered surface (302), described upper clipping claw cambered surface (301), lower claw cambered surface (302) is matched with the outer rim of circular aviation plug.
2. the clamp in order to plug circular aviation plug according to claim 1, is characterized in that, described first clamp assemblies (31) comprises,
First clamping part (311);
Be arranged on first connector (312) of described first clamping part (311) free end, described first connector (312) is provided with jack (303);
Inside insert in the first clamping bar (313) in jack (303);
The first jaw members (314) be connected with described first clamping bar (313), described first jaw members (314) has the bending upper clipping claw cambered surface (301) of relative second clamp assemblies (32).
3. the clamp in order to plug circular aviation plug according to claim 2, is characterized in that, described second clamp assemblies (32) comprises,
Second clamping part (321);
Be arranged on second connector (322) of described second clamping part (321) free end, described second connector (322) is provided with jack (303);
Inside insert in the second clamping bar (323) in jack (303);
The second jaw members (324) be connected with described second clamping bar (323), described second jaw members (324) has the bending lower claw cambered surface (302) of relative first clamp assemblies (31).
4. the clamp in order to plug circular aviation plug according to claim 3, is characterized in that, described first connector (312), the second connector (322) all at least comprise one group of jack (303).
5. the clamp in order to plug circular aviation plug according to claim 4, it is characterized in that, described first connector (312), the second connector (322) all comprise one along longitudinal jack (303a) and in tong bodies direction perpendicular to the horizontal jack (303b) in tong bodies direction.
6. the clamp in order to plug circular aviation plug according to claim 3, it is characterized in that, described first clamping bar (313) described tong bodies direction relative to one end that the first jaw members (314) connects tilts to extend to form the first connecting portion (315) that has inclination angle, and one end that described second clamping bar (323) and the second jaw members (324) connect also extends the second connecting portion (325) that has same inclination angle relatively.
7. the clamp in order to plug circular aviation plug according to claim 1, it is characterized in that, described upper and lower claw cambered surface (301), (302) are equipped with positioning boss (304) away from grafting port side, for carrying out spacing when clamping to circular aviation plug.
8. the clamp in order to plug circular aviation plug according to claim 3, it is characterized in that, described first clamping bar (313) and the second clamping bar (323) are respectively equipped with relative close the first ladder (316), the second ladder (326), make the beeline between described first clamping bar (313) and the second clamping bar (323) be less than beeline between the first connector (312) and the first connector (322).
9. the clamp in order to plug circular aviation plug according to claim 3, it is characterized in that, described first clamping bar (313) is hinged by a pivot pin with the first jaw members (314), and described first clamping bar (313) is cambered surface with the contact surface of the first jaw members (314); Described second clamping bar (323) is hinged by a pivot pin with the second jaw members (324), and described second clamping bar (323) is also cambered surface with the contact surface of the second jaw members (324).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520701333.7U CN204976399U (en) | 2015-09-11 | 2015-09-11 | Clamp for circular circular connector of plug |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520701333.7U CN204976399U (en) | 2015-09-11 | 2015-09-11 | Clamp for circular circular connector of plug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204976399U true CN204976399U (en) | 2016-01-20 |
Family
ID=55110817
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520701333.7U Active CN204976399U (en) | 2015-09-11 | 2015-09-11 | Clamp for circular circular connector of plug |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204976399U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105291036A (en) * | 2015-12-04 | 2016-02-03 | 中国航空工业集团公司洛阳电光设备研究所 | Quick assembling and disassembling device for aviation plug |
| CN107283356A (en) * | 2017-08-01 | 2017-10-24 | 江苏立华食品有限公司 | The light assembler of fowl depilation disk glue stick |
| CN114374131A (en) * | 2022-01-14 | 2022-04-19 | 上海御渡半导体科技有限公司 | Auxiliary disassembling tool for plug-in radio frequency connector |
-
2015
- 2015-09-11 CN CN201520701333.7U patent/CN204976399U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105291036A (en) * | 2015-12-04 | 2016-02-03 | 中国航空工业集团公司洛阳电光设备研究所 | Quick assembling and disassembling device for aviation plug |
| CN105291036B (en) * | 2015-12-04 | 2017-05-10 | 中国航空工业集团公司洛阳电光设备研究所 | Quick assembling and disassembling device for aviation plug |
| CN107283356A (en) * | 2017-08-01 | 2017-10-24 | 江苏立华食品有限公司 | The light assembler of fowl depilation disk glue stick |
| CN114374131A (en) * | 2022-01-14 | 2022-04-19 | 上海御渡半导体科技有限公司 | Auxiliary disassembling tool for plug-in radio frequency connector |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |