CN209626836U - Universal clip mounting bracket of picking up the ears - Google Patents
Universal clip mounting bracket of picking up the ears Download PDFInfo
- Publication number
- CN209626836U CN209626836U CN201821862628.2U CN201821862628U CN209626836U CN 209626836 U CN209626836 U CN 209626836U CN 201821862628 U CN201821862628 U CN 201821862628U CN 209626836 U CN209626836 U CN 209626836U
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- CN
- China
- Prior art keywords
- bracket
- hole
- clamping stirrup
- mounting
- ears
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- 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.)
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Abstract
The utility model relates to universal clip mounting brackets of picking up the ears, it is characterized by comprising bracket cornual plates 1 and clamping stirrup 5, the top of bracket cornual plate 1 is set there are two the screw mounting hole 2 with airframe structure connection, and lower part is equipped with circular hole 3 and slotted hole 4 with 5 connection of clamping stirrup；Bracket cornual plate 1 is connect by screw mounting hole 2 with aircraft fuselage structure, and is connect by circular hole 3 and slotted hole 4 with clamping stirrup 5.The universal clip mounting bracket of picking up the ears of the utility model, it can guarantee the suitability of complicated electrical interconnection system bracket cornual plate 1 and the installation connection of clamping stirrup 5 when clip specification is picked up the ears in practical set adjustment, it eliminates and is replacing bracket and carrying out the step of scene is with mounting hole is bored on bracket, improve the versatility of mounting bracket.
Description
Technical field
The utility model belongs to electrical interconnection system wiring mounting design field, is related to a kind of double bolt sides fixing belt pad
Clamping stirrup mounting bracket aperture mode, especially can be as the universal mounting bracket of such clip.
Background technique
Currently, the electrical interconnection system of well known complexity often can not accurately calculate required clip in the wires design stage
Diameter specifications, to allow to adjust the clip for selecting appropriate size according to practical harness size in practical set.But double spiral shells
The mounting hole spacing of the clamping stirrup of bolt side fixing belt pad can change with the variation of clip diameter specifications, when giving practical set
The clamping stirrup for installing double bolt sides fixing belt pads causes difficulty, be easy to cause original mounted clip bracket cornual plate with
It picks up the ears clip the case where clip bracket cornual plate is needed replacing away from inconsistent due to connecting hole.Original double bolt side fixing belt pads
Clamping stirrup installation when, generally according to the diameter of practical clip, scene is carried out on bracket with boring mounting hole, it is this
Mode is more time-consuming, does not have versatility.
Summary of the invention
Goal of the invention is to overcome existing mounting bracket to be easy to appear and double bolt sides after adjustment diameter specifications
For the clamping stirrup connecting hole of fixing belt pad away from unmatched problem, the utility model provides a kind of universal clip installation branch of picking up the ears
Frame, the mounting bracket can not be influenced by the mounting hole spacing variation of the clamping stirrup of double bolt side fixing belt pads, be guaranteed effectively
The different mounting hole spacings of this kind of clip are adapted to, harness assembly efficiency is effectively improved and save Material Cost.
The technical scheme adopted by the utility model to solve the technical problem is as follows:
The top of universal clip mounting bracket of picking up the ears, including bracket cornual plate 1 and clamping stirrup 5, bracket cornual plate 1 is equipped with two
A screw mounting hole 2 with airframe structure connection, lower part are equipped with circular hole 3 and slotted hole 4 with 5 connection of clamping stirrup；Branch
Frame cornual plate 1 is connect by screw mounting hole 2 with aircraft fuselage structure, and is connect by circular hole 3 and slotted hole 4 with clamping stirrup 5.
The distance between center of circle and the 4 bottom center of circle of slotted hole of circular hole 3 are 5 mounting hole spacing minimum value of clamping stirrup, circular hole 3
The center of circle and the distance between the 4 top center of circle of slotted hole be 5 mounting hole spacing maximum value of clamping stirrup.According to selected more on aircraft
The variation range of 5 mounting hole spacing of clamping stirrup of a specification is come the mounting hole spacing minimum value and maximum value that determine.
Clamping stirrup 5 is double bolt sides fixing belt mat structure.
Bracket cornual plate 1 is rectangle sheet metal.
The utility model has the advantages that the utility model has the beneficial effects that complicated electrical interconnection system can be guaranteed in practical set
The suitability for adjusting bracket cornual plate and clip installation connection of picking up the ears when picking up the ears clip specification, eliminates and passively replaces bracket and propping up
The step of scene is with mounting hole is bored is carried out on frame, improves the versatility of mounting bracket.
Detailed description of the invention
The present invention will be further described with reference to the accompanying drawings and examples.
Fig. 1 is the universal clip mounting support structure figure of picking up the ears of the utility model.
Fig. 2 is universal clip mounting bracket and the clamping stirrup connection schematic diagram of picking up the ears.
Specific embodiment
Referring to attached drawing 1, the universal clip mounting bracket of picking up the ears of the utility model, including bracket cornual plate 1 and clamping stirrup
5。
Wherein, bracket cornual plate 1 is rectangle sheet metal, and there are two the spiral shells of bracket cornual plate 1 and airframe structure connection on top
Mounting hole 2 is followed closely, bracket cornual plate 1 and 5 screw connection slotted hole 4 of clamping stirrup, bracket cornual plate are arranged at two 2 lower parts of screw mounting hole
1 connect with 5 screw of clamping stirrup and uses circular hole 3 with having below slotted hole 4 bracket cornual plate 1 to connect with 5 screw of clamping stirrup.
As shown in Fig. 2, counting the folder of multiple specifications selected on aircraft before bracket cornual plate 1 is connect with clamping stirrup 5
The variation range of 5 mounting hole spacing of tight clip determines mounting hole spacing minimum value and maximum value, the center of circle and 4 bottom of slotted hole of circular hole 3
The distance between center of circle is mounting hole spacing minimum value, and the distance between center of circle and the 4 top center of circle of slotted hole of circular hole 3 are mounting hole
Away from maximum value.On bracket cornual plate 1 that circular hole 3 and 4 aperture of slotted hole is good again, when general assembly, bracket cornual plate 1 first leads to airframe structure
It crosses the installation of screw mounting hole 2 that bracket cornual plate 1 connect with airframe structure to fix, when cloth wire routing, according to the reality of clamping stirrup 5
Border mounting hole spacing connects mounting bracket 1 with clamping stirrup 5 by adjusting upper and lower position of the screw in slotted hole 4.
Claims (5)
1. universal clip mounting bracket of picking up the ears, it is characterised in that: including bracket cornual plate (1) and clamping stirrup (5), bracket cornual plate
(1) top is set there are two the screw mounting hole (2) with airframe structure connection, and lower part, which is equipped with, connect use with clamping stirrup (5)
Circular hole (3) and slotted hole (4)；Bracket cornual plate (1) is connect by screw mounting hole (2) with aircraft fuselage structure, and passes through circle
Hole (3) and slotted hole (4) are connect with clamping stirrup (5).
2. mounting bracket as described in claim 1, which is characterized in that the center of circle of circular hole (3) and slotted hole (4) bottom center of circle it
Between distance be clamping stirrup (5) mounting hole spacing minimum value, the center of circle of circular hole (3) and slotted hole (4) top the center of circle between away from
From for clamping stirrup (5) mounting hole spacing maximum value.
3. mounting bracket as claimed in claim 2, which is characterized in that according to the clamping stirrup of multiple specifications selected on aircraft
(5) variation range of mounting hole spacing is come the mounting hole spacing minimum value and maximum value that determine.
4. mounting bracket as described in claim 1, which is characterized in that clamping stirrup (5) is double bolt sides fixing belt pad knot
Structure.
5. mounting bracket as described in claim 1, which is characterized in that bracket cornual plate (1) is rectangle sheet metal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821862628.2U CN209626836U (en) | 2018-11-12 | 2018-11-12 | Universal clip mounting bracket of picking up the ears |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821862628.2U CN209626836U (en) | 2018-11-12 | 2018-11-12 | Universal clip mounting bracket of picking up the ears |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209626836U true CN209626836U (en) | 2019-11-12 |
Family
ID=68443761
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821862628.2U Active CN209626836U (en) | 2018-11-12 | 2018-11-12 | Universal clip mounting bracket of picking up the ears |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209626836U (en) |
-
2018
- 2018-11-12 CN CN201821862628.2U patent/CN209626836U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20201223 Address after: 519040 building 201, 999 Jinhai Middle Road, Jinwan District, Zhuhai City, Guangdong Province Patentee after: SOUTH CHINA AIRCRAFT INDUSTRY CO., LTD. OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. Address before: 519000 AVIC Tongfei industrial base, aviation industrial park, Jinwan District, Zhuhai City, Guangdong Province Patentee before: R&D INSTITUTE OF CHINA AVIATION INDUSTRY GENERAL AIRCRAFT Co.,Ltd. |