CN210967627U - Aviation plug pad frock - Google Patents
Aviation plug pad frock Download PDFInfo
- Publication number
- CN210967627U CN210967627U CN201921707956.XU CN201921707956U CN210967627U CN 210967627 U CN210967627 U CN 210967627U CN 201921707956 U CN201921707956 U CN 201921707956U CN 210967627 U CN210967627 U CN 210967627U
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- bearing
- pad
- base
- aviation
- fixed
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Abstract
The utility model discloses an aviation plug pad frock belongs to welding technical field, including the pad base, pad base centre bore below is fixed with baffle under the bearing, and pad base top is fixed with the bearing overhead gage, and the pad support column is installed to the below of pad base, is provided with the bearing under bearing overhead gage and the bearing between the baffle, and the upper portion of bearing overhead gage is provided with aviation unable adjustment base. The utility model discloses can insert fixed base and adapt to various types of aviation plugs according to aviation plug kind replacement aviation, the design of bottom bearing can rotate the position when the welding, and convenient welding can effectively reduce welding time, raises the efficiency, reduction in production cost.
Description
Technical Field
The utility model relates to a pad frock especially relates to an aviation plug pad frock, belongs to the welding technology field.
Background
At present direct current brushless motor uses more and more extensively, and more customers need insert easy to assemble in lead-out wire one end with the aviation, simultaneously, can satisfy protection requirements such as waterproof, dustproof again, and the welding of aviation plug inner line is comparatively troublesome usually, and the operation is wasted time and energy, in order to solve above-mentioned problem, the utility model provides a can fix aviation plug, make things convenient for welded pad frock to this improves production efficiency.
SUMMERY OF THE UTILITY MODEL
The utility model mainly aims at providing an aviation plug pad frock can insert fixed base and adapt to various types of aviation plugs according to aviation plug kind replacement, and the design of bottom bearing can rotate the position when the welding, and convenient welding can effectively reduce welding time, raises the efficiency, reduction in production cost.
The purpose of the utility model can be achieved by adopting the following technical scheme:
the utility model provides an aviation plug pad frock, includes the pad base, pad base centre bore below is fixed with baffle under the bearing, pad base top is fixed with the bearing overhead gage, the pad support column is installed to the below of pad base, the bearing overhead gage with be provided with the bearing under the bearing between the baffle, the upper portion of bearing overhead gage is provided with aviation unable adjustment base.
Preferably, the four corners of the pad base are provided with threaded holes, the upper end of the pad support column is connected with a threaded rod, and the threaded rod and the threaded holes are matched with each other.
Preferably, the aviation fixing base is provided with an opening groove.
Preferably, the bearing upper baffle and the bearing lower baffle are fixed on the pad base through screws.
Preferably, the aviation fixing base is connected through the bearing.
Preferably, the pad base is fixed to the bearing.
The utility model has the advantages of:
the utility model provides a pair of circular connector pad frock, this kind of circular connector pad frock can be inserted fixed base and adapt to various types of circular connector according to circular connector type replacement aviation, and the position can be rotated when the welding in the design of bottom bearing, and convenient welding can effectively reduce welding time, raises the efficiency, reduction in production cost.
Drawings
Fig. 1 is a schematic structural diagram of a preferred embodiment of an aviation plug pad tool according to the present invention;
fig. 2 is a cross-sectional view of a preferred embodiment of an aircraft plug pad tooling in accordance with the present invention.
In the figure: the structure comprises a bonding pad base 1, a bearing upper baffle 2, an aviation plug fixing base 3, a bearing 4, a bearing lower baffle 5 and a bonding pad support column 6.
Detailed Description
In order to make the technical solutions of the present invention clearer and clearer for those skilled in the art, the present invention will be described in further detail with reference to the following embodiments and the accompanying drawings, but the embodiments of the present invention are not limited thereto.
As shown in fig. 1-2, the aviation plug pad tool provided by this embodiment includes a pad base 1, a lower bearing baffle 5 is fixed below a central hole of the pad base 1, an upper bearing baffle 2 is fixed above the pad base 1, a pad support column 6 is installed below the pad base 1, a bearing 4 is arranged between the upper bearing baffle 2 and the lower bearing baffle 5, and an aviation fixing base 3 is arranged on the upper portion of the upper bearing baffle 2.
Can insert unable adjustment base 3 according to aviation plug kind replacement aviation and adapt to various types of aviation plugs, the design of bottom bearing 4 can rotate the position when the welding, and convenient welding can effectively reduce the welding time, raises the efficiency, reduction in production cost.
In this embodiment: the four corners department of pad base 1 is provided with the screw hole, and the upper end of pad support column 6 is connected with the threaded rod, and threaded rod and screw hole mutually support, through screw thread screw in pad base.
In this embodiment: be provided with a mouthful groove on the aviation unable adjustment base 3, settle the lead-out wire when conveniently welding.
In this embodiment: bearing overhead gage 2 and bearing lower baffle 5 all fix on pad base 1 through the screw rod, conveniently dismantle the change.
In this embodiment: aviation unable adjustment base 3 passes through bearing 4 and connects, can rotate the base along with actual operating conditions.
In this embodiment: the pad base 1 is fixed on the bearing 4, and an outgoing line is arranged conveniently during welding.
As shown in fig. 1-2, the operation process of the aviation plug pad tool provided by this embodiment is as follows: when welding the aviation plug, insert unable adjustment base 3 and adapt to various types of aviation plug according to aviation plug kind replacement aviation, the position can be rotated when the welding in the design of bottom bearing 4, and convenient welding can effectively reduce the welding time, raises the efficiency, reduction in production cost.
The above description is only a further embodiment of the present invention, but the scope of protection of the present invention is not limited thereto, and any person skilled in the art can replace or change the technical solution and the concept of the present invention within the scope of the present invention.
Claims (6)
1. The utility model provides an aviation plug pad frock which characterized in that: including pad base (1), pad base (1) centre bore below is fixed with baffle (5) under the bearing, pad base (1) top is fixed with bearing overhead gage (2), pad support column (6) are installed to the below of pad base (1), bearing overhead gage (2) with be provided with bearing (4) under the bearing between baffle (5), the upper portion of bearing overhead gage (2) is provided with aviation unable adjustment base (3).
2. The aircraft plug pad tool of claim 1, wherein: the four corners department of pad base (1) is provided with the screw hole, and the upper end of pad support column (6) is connected with the threaded rod, and threaded rod and screw hole mutually support.
3. The aircraft plug pad tool of claim 1, wherein: and the aviation fixing base (3) is provided with an opening groove.
4. The aircraft plug pad tool of claim 1, wherein: the bearing upper baffle (2) and the bearing lower baffle (5) are fixed on the pad base (1) through screws.
5. The aircraft plug pad tool of claim 1, wherein: the aviation fixing base (3) is connected through the bearing (4).
6. The aircraft plug pad tool of claim 1, wherein: the pad base (1) is fixed on the bearing (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921707956.XU CN210967627U (en) | 2019-10-12 | 2019-10-12 | Aviation plug pad frock |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921707956.XU CN210967627U (en) | 2019-10-12 | 2019-10-12 | Aviation plug pad frock |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210967627U true CN210967627U (en) | 2020-07-10 |
Family
ID=71439623
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921707956.XU Active CN210967627U (en) | 2019-10-12 | 2019-10-12 | Aviation plug pad frock |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN210967627U (en) |
-
2019
- 2019-10-12 CN CN201921707956.XU patent/CN210967627U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP02 | Change in the address of a patent holder | ||
| CP02 | Change in the address of a patent holder |
Address after: 4 / F, building 3, rail transit Industrial Park, 355 Longjin Road, Lucheng street, Changzhou Economic Development Zone, Changzhou City, Jiangsu Province 213100 Patentee after: Changzhou Zhongzhi Electrical Machinery Co.,Ltd. Address before: No. 151, Dongfang East Road, Wujin District, Changzhou City, Jiangsu Province 213100 Patentee before: Changzhou Zhongzhi Electrical Machinery Co.,Ltd. |