CN213731484U - Aviation plug fast loading and unloading frock - Google Patents
Aviation plug fast loading and unloading frock Download PDFInfo
- Publication number
- CN213731484U CN213731484U CN202022405485.6U CN202022405485U CN213731484U CN 213731484 U CN213731484 U CN 213731484U CN 202022405485 U CN202022405485 U CN 202022405485U CN 213731484 U CN213731484 U CN 213731484U
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- ring
- aviation plug
- main part
- cover main
- ring cover
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Abstract
The utility model discloses an aviation plug fast loading and unloading frock, including ring cover main part (1) and fingerboard (2), the internal face of ring cover main part (1) has a plurality of dogtooths (3) along the circumferencial direction equipartition, the length of dogtooth (3) with the length of ring cover main part (1) is the same, dogtooth (3) be used for with the recess meshing on the aviation plug outer wall, the quantity of fingerboard (2) is two, for the axle center symmetrical arrangement of ring cover main part (1), with the outer wall fixed connection of ring cover main part (1). The utility model discloses can replace the dismantlement spanner fast with the installation with dismantle the aviation plug, effectively solve the problem of the inconvenient dismouting in narrow and small space.
Description
Technical Field
The utility model relates to a dismouting frock, concretely relates to aviation plug fast loading and unloading frock.
Background
Along with the development of automation equipment, the internal structure is more and more compact, and simultaneously a large amount of aviation plugs such as encoders, servo motors, sensors and the like are used. When the aviation plug in a certain narrow space needs to be disassembled during maintenance, the plug is usually disassembled only by leaving enough space after the shielding object is disassembled. This greatly reduces the efficiency of the maintenance.
The existing special dismounting tool for the aviation plug rotates the lower aviation plug in a radial or axial stress application mode, a certain operation space is needed, and the operation within a visual range is needed to facilitate the operation.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing an aviation plug fast loading and unloading frock to solve the technical problem among the prior art, it can replace to dismantle the spanner and will install and dismantle aviation plug fast, effectively solves the problem of the inconvenient dismouting in narrow and small space.
The utility model provides an aviation plug fast loading and unloading frock, including ring cover main part and fingerboard, the internal face of ring cover main part has a plurality of dogtooths along the circumferencial direction equipartition, the length of dogtooth with the length of ring cover main part is the same, the dogtooth is used for meshing with the recess on the aviation plug outer wall, the quantity of fingerboard is two, for the axle center symmetrical arrangement of ring cover main part, with the outer wall fixed connection of ring cover main part.
In the quick aviation plug assembling and disassembling tool, preferably, chamfers are formed at two ends of each of the convex teeth.
In the aviation plug quick assembly and disassembly tool, preferably, the tool further comprises a first inner sleeve toothed ring sleeved in the ring sleeve main body and a second inner sleeve toothed ring sleeved in the first inner sleeve toothed ring.
In the aviation plug quick assembly and disassembly tool, preferably, the second inner sleeve toothed ring has the same structure as the first inner sleeve toothed ring, and is composed of a ring body, outer convex teeth and inner convex teeth, the outer convex teeth are arranged at equal intervals along the outer peripheral wall of the ring body, and the inner convex teeth are arranged at equal intervals along the inner peripheral wall of the ring body.
In the quick assembly and disassembly tool for the aviation plug, preferably, rubber pads are arranged between any two adjacent convex teeth and between any two adjacent inner convex teeth.
Compared with the prior art, the utility model discloses a ring cover main part and fingerboard, the internal face of ring cover main part has a plurality of dogtooths along the circumferencial direction equipartition, and the length of dogtooth is the same with the length of ring cover main part, and the dogtooth is used for meshing with the recess on the aviation plug outer wall, and the quantity of fingerboard is two, for the axle center symmetrical arrangement of ring cover main part, with the outer wall fixed connection of ring cover main part. When dismantling the aviation plug, will the utility model discloses a ring cover main part cup joints on the outer wall of aviation plug, pulls two fingerboards with the hand and can easily install or dismantle the aviation plug, solves the unable problem that uses the spanner in narrow and small space.
Drawings
Fig. 1 is an isometric view of the present invention;
figure 2 is a front view of the collar body.
Description of reference numerals: 1-ring sleeve main body, 2-finger plate, 3-convex tooth, 4-chamfer, 5-first inner sleeve toothed ring, 6-second inner sleeve toothed ring, 7-circular ring body, 8-external convex tooth, 9-internal convex tooth and 10-rubber pad.
Detailed Description
Reference will now be made in detail to embodiments of the present invention, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below by referring to the drawings are exemplary only for explaining the present invention, and should not be construed as limiting the present invention.
The embodiment of the utility model provides a: as shown in fig. 1 and 2, the aviation plug fast loading and unloading tool comprises a ring sleeve main body 1 and finger plates 2, wherein a plurality of convex teeth 3 are uniformly distributed on the inner wall surface of the ring sleeve main body 1 along the circumferential direction, the length of each convex tooth 3 is the same as that of the ring sleeve main body 1, the convex teeth 3 are used for being meshed with grooves in the outer wall of an aviation plug, the number of the finger plates 2 is two, the two finger plates are symmetrically arranged relative to the axis of the ring sleeve main body 1 and fixedly connected with the outer wall of the ring sleeve main body 1.
In order to facilitate the installation, the both ends of dogtooth 3 all are formed with chamfer 4, and the preferred design of the whole shape of dogtooth 3 is frustum body structure, like this when cup jointing the snare main part 1 on the outer wall of aviation plug, can easily peg graft, even if see not in the recess that also can insert the dogtooth 3 on the aviation plug outer wall with eyes under the effect of chamfer 4. Two fingerboards 2 are arranged, so that hands can exert force conveniently, and the aviation plug can be detached easily.
When the installation aviation plug, do not have the one end of pipeline to insert with ring cover main part 1 from the aviation plug, then rotate, can take off and fix ring cover main part 1 on the pipeline after having installed the aviation plug, only need install when needing to dismantle the aviation plug can, ring cover main part 1, fingerboard 2 and protruding tooth 3 are preferred to adopt the integrated into one piece structure, can choose the plastics material for use for reduce cost, through the utility model discloses a dismouting problem of aviation plug in narrow and small space can be solved in the setting to and solve the problem that spanner instrument damaged the aviation plug outer wall tooth's socket easily.
In a preferred embodiment, the ring sleeve further comprises a first inner sleeve toothed ring 5 sleeved in the ring sleeve main body 1 and a second inner sleeve toothed ring 6 sleeved in the first inner sleeve toothed ring 5. The second inner sleeve toothed ring 6 and the first inner sleeve toothed ring 5 are identical in structure, and the difference between the second inner sleeve toothed ring and the first inner sleeve toothed ring lies in the size and consists of a ring body 7, outer convex teeth 8 and inner convex teeth 9, the outer convex teeth 8 are arranged at equal intervals along the outer peripheral wall of the ring body 7, and the inner convex teeth 9 are arranged at equal intervals along the inner peripheral wall of the ring body 7. Rubber pads 10 are arranged between any two adjacent convex teeth 3 and between any two adjacent inner convex teeth 9.
Through the design of first endotheca ring gear 5 and second endotheca ring gear 6, only need add first endotheca ring gear 5 and second endotheca ring gear 6 to the aviation plug of different specifications can, improved the utility model discloses an application scope, in addition, through the setting of rubber pad 10, makes the utility model discloses can firmly cup joint with aviation plug.
The structure, features and effects of the present invention have been described in detail above according to the embodiment shown in the drawings, and the above description is only the preferred embodiment of the present invention, but the present invention is not limited to the implementation scope shown in the drawings, and all changes made according to the idea of the present invention or equivalent embodiments modified to the same changes should be considered within the protection scope of the present invention when not exceeding the spirit covered by the description and drawings.
Claims (5)
1. The utility model provides an aviation plug fast loading and unloading frock which characterized in that: including ring cover main part (1) and fingerboard (2), the internal face of ring cover main part (1) has a plurality of dogtooths (3) along the circumferencial direction equipartition, the length of dogtooth (3) with the length of ring cover main part (1) is the same, dogtooth (3) are used for meshing with the recess on the aviation plug outer wall, the quantity of fingerboard (2) is two, for the axle center symmetrical arrangement of ring cover main part (1), with the outer wall fixed connection of ring cover main part (1).
2. The quick aviation plug assembling and disassembling tool of claim 1, wherein: chamfers (4) are formed at two ends of each convex tooth (3).
3. The quick aviation plug assembling and disassembling tool of claim 2, wherein: the ring sleeve is characterized by further comprising a first inner sleeve toothed ring (5) sleeved in the ring sleeve main body (1) and a second inner sleeve toothed ring (6) sleeved in the first inner sleeve toothed ring (5).
4. The quick aviation plug assembling and disassembling tool of claim 3, wherein: the second inner sleeve toothed ring (6) and the first inner sleeve toothed ring (5) are identical in structure and composed of a ring body (7), outer convex teeth (8) and inner convex teeth (9), the outer convex teeth (8) are arranged at equal intervals along the outer peripheral wall of the ring body (7), and the inner convex teeth (9) are arranged at equal intervals along the inner peripheral wall of the ring body (7).
5. The quick aviation plug assembling and disassembling tool of claim 4, wherein: rubber pads (10) are arranged between any two adjacent convex teeth (3) and between any two adjacent inner convex teeth (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022405485.6U CN213731484U (en) | 2020-10-26 | 2020-10-26 | Aviation plug fast loading and unloading frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022405485.6U CN213731484U (en) | 2020-10-26 | 2020-10-26 | Aviation plug fast loading and unloading frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213731484U true CN213731484U (en) | 2021-07-20 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022405485.6U Active CN213731484U (en) | 2020-10-26 | 2020-10-26 | Aviation plug fast loading and unloading frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213731484U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113904198A (en) * | 2021-09-29 | 2022-01-07 | 中船黄埔文冲船舶有限公司 | Plug loading and unloading tool for marine watertight socket |
-
2020
- 2020-10-26 CN CN202022405485.6U patent/CN213731484U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113904198A (en) * | 2021-09-29 | 2022-01-07 | 中船黄埔文冲船舶有限公司 | Plug loading and unloading tool for marine watertight socket |
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