CN204118408U - A kind of aerospace connectors mounting structure - Google Patents
A kind of aerospace connectors mounting structure Download PDFInfo
- Publication number
- CN204118408U CN204118408U CN201420522716.3U CN201420522716U CN204118408U CN 204118408 U CN204118408 U CN 204118408U CN 201420522716 U CN201420522716 U CN 201420522716U CN 204118408 U CN204118408 U CN 204118408U
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- clip
- mounting structure
- aerospace connectors
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Abstract
Utility model provides a kind of aerospace connectors mounting structure, comprise body and cabinet, described body corner is equipped with screwed hole, described body comprises the first clip and second clip of Symmetric Composite setting, the combinatorial surface of the first clip is provided with two alignment pins, and the combinatorial surface of the second clip is provided with two location holes with alignment pin adaptation on the first clip; First clip and the second clip are respectively provided with an installation half slot, the installation half slot combination of the first clip and the second clip forms complete installation circular hole, the mounting structure of a kind of Fast Installation aerospace connectors of the utility model, be used for replacing nut that aerospace connectors is installed, solve nut and the problem wasted time and energy is installed, be particularly suitable for device panel thinner, and narrow space, nut is difficult to install the occasion even cannot installed, and this structure installment is convenient, fast, and operating efficiency is high.
Description
Technical field
The utility model relates to a kind of mounting structure, particularly a kind of aerospace connectors mounting structure.
Background technology
Modern electronic equipment uses various connector in a large number in order to realize Signal transmissions, and comparatively speaking, connector nut is installed has solid and reliable feature; apply very general; during installation generally with screw through device panel, then install nut tension and make it to combine closely, reach fixed effect; this kind of method is installed uncomplicated; but waste time and energy, particularly in narrow space, nut can frequent landing; operation inconvenience and special charges time, condition of contact is restricted.
Utility model content
Utility model object: technical problem to be solved in the utility model is for the deficiencies in the prior art, provides a kind of aerospace connectors mounting structure.
In order to solve the problems of the technologies described above, the utility model discloses a kind of aerospace connectors mounting structure, comprise body and cabinet, described body corner is equipped with screwed hole, described body comprises the first clip and second clip of Symmetric Composite setting, the combinatorial surface of the first clip is provided with two alignment pins, and the combinatorial surface of the second clip is provided with two location holes with alignment pin adaptation on the first clip; First clip and the second clip are respectively provided with an installation half slot, and the installation half slot combination of the first clip and the second clip forms complete installation circular hole.
In the utility model, the projection of the upper/lower terminal symmetry of described body a pair claw for locating.
In the utility model, the projection of the left and right two ends symmetry of described body a pair claw for locating.
In the utility model, the inwall of described cabinet is provided with the draw-in groove with described claw adaptation.
Beneficial effect: the utility model provides a kind of mounting structure of Fast Installation aerospace connectors, be used for replacing nut that aerospace connectors is installed, solve nut and the problem wasted time and energy is installed, be particularly suitable for device panel thinner, and narrow space, nut is difficult to install the occasion even cannot installed, and this mounting structure is easy for installation, quick, and operating efficiency is high.
Accompanying drawing explanation
To do the utility model below in conjunction with the drawings and specific embodiments and further illustrate, above-mentioned or otherwise advantage of the present utility model will become apparent.
Fig. 1 a is structural representation of the present utility model;
Fig. 1 b is left view of the present utility model;
Fig. 1 c is the first clip schematic diagram of aerospace connectors mounting structure;
Fig. 1 d is the second clip schematic diagram of aerospace connectors mounting structure;
Fig. 2 a and 2b is the utility model built-in type mounting structure schematic diagram;
Fig. 3 a and 3b is the utility model fitted outside mounting structure schematic diagram;
Embodiment
Below in conjunction with accompanying drawing, the utility model is elaborated.
Embodiment 1
As Fig. 1 a, Fig. 1 b, Fig. 1 c and Fig. 1 d, the utility model comprises body 1, screwed hole 2, claw 3a and 3b, first clip 4, second clip 5, alignment pin 6 and location hole 7, wherein body 1 comprises the first clip 4 and the second clip 5, first clip 4 and the second clip 5 are respectively provided with one and install half slot, two half slot is installed and is combined into a complete installation circular hole, the cylinder of connector can be made to pass, body 1 four jiaos is provided with screwed hole 2, the symmetrical projection in body about 1 two ends a pair claw 3a, the symmetrical projection in body about 1 two ends a pair claw 3b, claw 3a and claw 3b makes it to rotate in order to fix this structure, first clip 4 combinatorial surface is provided with two alignment pins 6, second clip 5 combinatorial surface is provided with two location holes 7, alignment pin 6 and location hole 7 suitable, in order to fix this structure.
As shown in Figure 2 a and 2 b, the utility model in use, when needing to select connector built-in type according to the mounting means of aerospace connectors, aerospace connectors 8 is put into the installation site of this connector in cabinet, with screw assemblies 10 successively through the hole on the panel of cabinet 9 and aerospace connectors ring flange 11, again body 1 is placed on flange adapter rear end, being combined by the alignment pin 6 on the first clip 4 and the second clip 5 and location hole 7 is fixed on connector 8 by body 1, body 1 is fixed on the ring flange 11 of connector by adjustment jaw position, finally screw assemblies 10 is screwed in successively the panel of cabinet 9, screw in the ring flange 11 of connector and the screwed hole 2 of body 1.
Embodiment 2
As Fig. 3 a and 3b, when selecting connector fitted outside, aerospace connectors 8 is put on the connector installation site of the panel of cabinet 9, then body 1 is placed on the rear wall of cabinet female connector installation site, be enclosed within connector rear end, the first clip 4 and the second clip 5 is made to be fastened on connector 8 by alignment pin 6 and location hole 7, and the draw-in groove 9a making body 1 be stuck on cabinet wall by claw reaches fixing, screw in the screwed hole 2 screwing in body 1 with screw assemblies 10 through the hole on aerospace connectors ring flange 11 and cabinet panel 9, it is thinner that this kind of connector fitted outside mounting means is applicable to cabinet panel, cannot machining screw or panel material hardness inadequate, the unstable situation of screw thread of processing.
The utility model provides a kind of aerospace connectors mounting structure; the method and access of this technical scheme of specific implementation is a lot; the above is only preferred implementation of the present utility model; should be understood that; for those skilled in the art; under the prerequisite not departing from the utility model principle; some improvements and modifications can also be made; these improvements and modifications also should be considered as protection range of the present utility model, and all available prior art of each part not clear and definite in the present embodiment is realized.
Claims (4)
1. an aerospace connectors mounting structure, it is characterized in that, comprise body (1) and cabinet (9), described body (1) corner is equipped with screwed hole (2), described body (1) comprises the first clip (4) and second clip (5) of Symmetric Composite setting, the combinatorial surface of the first clip (4) is provided with two alignment pins (6), and the combinatorial surface of the second clip (5) is provided with two location holes (7) that upper alignment pin (6) is adaptive with the first clip (4); First clip (4) and the second clip (5) are respectively provided with an installation half slot, and the installation half slot combination of the first clip (4) and the second clip (5) forms complete installation circular hole.
2. a kind of aerospace connectors mounting structure according to claim 1, is characterized in that, the projection of the upper/lower terminal symmetry of described body (1) a pair claw (3a) for locating.
3. a kind of aerospace connectors mounting structure according to claim 1 and 2, is characterized in that, the projection of the left and right two ends symmetry of described body (1) a pair claw (3b) for locating.
4. a kind of aerospace connectors mounting structure according to claim 3, is characterized in that, the inwall of described cabinet is provided with the draw-in groove (9a) with described claw adaptation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420522716.3U CN204118408U (en) | 2014-09-11 | 2014-09-11 | A kind of aerospace connectors mounting structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420522716.3U CN204118408U (en) | 2014-09-11 | 2014-09-11 | A kind of aerospace connectors mounting structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204118408U true CN204118408U (en) | 2015-01-21 |
Family
ID=52335689
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420522716.3U Active CN204118408U (en) | 2014-09-11 | 2014-09-11 | A kind of aerospace connectors mounting structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204118408U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109193277A (en) * | 2018-08-17 | 2019-01-11 | 合肥昌燎科技有限公司 | A kind of electric mechanical port fixing device |
-
2014
- 2014-09-11 CN CN201420522716.3U patent/CN204118408U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109193277A (en) * | 2018-08-17 | 2019-01-11 | 合肥昌燎科技有限公司 | A kind of electric mechanical port fixing device |
| CN109193277B (en) * | 2018-08-17 | 2020-05-22 | 瑞安市驰恒传动设备有限公司 | Electronic machinery port fixing device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |