CN202691301U - Cable lathedog of flying device and special rubber pad thereof - Google Patents
Cable lathedog of flying device and special rubber pad thereof Download PDFInfo
- Publication number
- CN202691301U CN202691301U CN 201220383087 CN201220383087U CN202691301U CN 202691301 U CN202691301 U CN 202691301U CN 201220383087 CN201220383087 CN 201220383087 CN 201220383087 U CN201220383087 U CN 201220383087U CN 202691301 U CN202691301 U CN 202691301U
- Authority
- CN
- China
- Prior art keywords
- rubber pad
- circular arc
- metal frame
- lathedog
- bulge
- Prior art date
- 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.)
- Expired - Lifetime
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Abstract
The utility model discloses a cable lathedog of a flying device and a special rubber pad thereof, wherein the cable lathedog comprises a metal framework and the rubber pad, the whole metal framework is obtained by a bent metal sheet, the metal framework comprises a circular arc-shaped circular arc part for being clamped and connected on a wire harness pipeline and further comprises extension parts which are formed by outward extension from the two open ends of the circular arc part, bolt holes for mounting bolts for fastening the metal framework are arranged on the extension parts, the rubber pad is clamped on the circular arc part of the metal framework, the metal framework is made of aluminum alloy material, and one bulge is arranged on the inner side at one end of the rubber pad. One side of the bulge is flush with the end surface of the end part of the rubber pad, where the bulge is located, and the other side of the bulge forms the smooth circular arc-shaped transition with the rubber pad. According to the cable lathedog disclosed by the utility model, the bulge is increased at one end of the rubber pad, so that the vibration damping effect of the lathedog can be improved to the greatest extent; and simultaneously, the bulge and the rubber pad can be integrally formed, so that the cable lathedog further has the advantages of simple structure and convenience in processing.
Description
Technical field
The utility model relates to a kind of clip, especially a kind of flight equipment client cables clip.
Background technique
All need to arrange a large amount of wire harness and pipeline in the control system of flight equipment such as aircraft, cooling system extension, oil-fired system, air inlet system and exhaust system and the hydraulic system, the fixedly system extension of these wire harness pipelines can be used the clamping stirrup of the outer embedding rubber pad of a kind of metal frame.Its existing structure is for comprising metal frame and rubber pad, described metal frame integral body is obtained by the tinsel of bending, what metal frame had a circular arc is used for being connected to circular arc part on the wire harness pipeline, also has the extension part that stretches out and form from two open ends of circular arc part, be provided with on the extension part for construction bolt and make metal frame be able to fastening bolt hole, described rubber pad clamp are on the circular arc part of metal frame.
The rubber pad of this existing clamping stirrup China and foreign countries' embedding, major function is that damping is shockproof, prevent that metal frame from grinding line or damage pipeline in vibrations, but rubber pad tends to occur space, certain dead angle at the closure place of clip, can not realize 360 ° parcel to cable or tube bank, can not reach 360 ° damping vibration.Therefore damping effect also has much room for improvement.
The model utility content
For above-mentioned deficiency, technical problem to be solved in the utility model is, how a kind of flight equipment wire cable clamp that can improve damping effect is provided, and provides simultaneously to make it reach a kind of flight equipment wire cable clamp special (purpose) rubber pad of this effect.
In order to solve the problems of the technologies described above, adopted following technological scheme in the utility model.
A kind of flight equipment wire cable clamp, comprise metal frame and rubber pad, described metal frame integral body is obtained by the tinsel of bending, what metal frame had a circular arc is used for being connected to circular arc part on the wire harness pipeline, also has the extension part that stretches out and form from two open ends of circular arc part, being provided with on the extension part for construction bolt makes metal frame be able to fastening bolt hole, described rubber pad clamp are on the circular arc part of metal frame, it is characterized in that, described metal frame is aluminum alloy material, and an end inboard of described rubber pad has a projection.
In the utility model, described projection can be used in fill metal frame when chucking circular arc part and the space of extension part jointing place, therefore can increase rubber pad and wire harness pipeline area of contact, can improve the clip damping effect.Described metal frame is aluminum alloy material, can at utmost reduce metal frame weight, guarantees simultaneously metal frame strength performance.
As further optimization, the end face of a side of described projection and rubber pad end, protruding place forms smooth circular arc transition between the opposite side of projection and the rubber pad.After optimizing like this, projection can be farthest filled the circular arc part of metal frame when the chucking completely with the space of extension part jointing place, makes it not stay the space, at utmost improves the clip damping effect.
The utility model also provides a kind of rubber pad that is exclusively used in above-mentioned flight equipment wire cable clamp, comprises the rubber pad body, and an end inboard of rubber pad body has a projection.As optimization, the end face of a side of described projection and protruding place rubber pad body end forms smooth circular arc transition between the opposite side of projection and the rubber pad body.
In sum, in the utility model, in projection of end increase of rubber pad, can farthest improve the damping effect of clip; Projection can obtain with rubber pad is one-body molded simultaneously, therefore also possess advantage simple in structure, easy to process.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
The utility model is described in further detail below in conjunction with the drawings and specific embodiments.
During implementation, as shown in Figure 1, a kind of flight equipment wire cable clamp, comprise metal frame 1 and rubber pad 2, described metal frame 1 integral body is obtained by the tinsel of bending, what metal frame 1 had a circular arc is used for being connected to circular arc part on the wire harness pipeline, also has the extension part that stretches out and form from two open ends of circular arc part, being provided with on the extension part for construction bolt makes metal frame 1 be able to fastening bolt hole, described rubber pad 2 clamp are on the circular arc part of metal frame 1, wherein, described metal frame 1 is aluminum alloy material, and an end inboard of described rubber pad 2 has a projection 5.The end face of a side of described protruding 5 and rubber pad end, protruding place forms smooth circular arc transition between the opposite side of projection 5 and the rubber pad.
Claims (4)
1. flight equipment wire cable clamp, comprise metal frame and rubber pad, described metal frame integral body is obtained by the tinsel of bending, what metal frame had a circular arc is used for being connected to circular arc part on the wire harness pipeline, also has the extension part that stretches out and form from two open ends of circular arc part, being provided with on the extension part for construction bolt makes metal frame be able to fastening bolt hole, described rubber pad clamp are on the circular arc part of metal frame, it is characterized in that, described metal frame is aluminum alloy material, and an end inboard of described rubber pad has a projection.
2. flight equipment wire cable clamp as claimed in claim 1 is characterized in that, the end face of a side of described projection and rubber pad end, protruding place forms smooth circular arc transition between the opposite side of projection and the rubber pad.
3. a flight equipment wire cable clamp special (purpose) rubber pad comprises the rubber pad body, it is characterized in that, an end inboard of rubber pad body has a projection.
4. flight equipment wire cable clamp special (purpose) rubber pad as claimed in claim 3 is characterized in that, the end face of a side of described projection and protruding place rubber pad body end forms smooth circular arc transition between the opposite side of projection and the rubber pad body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220383087 CN202691301U (en) | 2012-08-03 | 2012-08-03 | Cable lathedog of flying device and special rubber pad thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220383087 CN202691301U (en) | 2012-08-03 | 2012-08-03 | Cable lathedog of flying device and special rubber pad thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202691301U true CN202691301U (en) | 2013-01-23 |
Family
ID=47546923
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220383087 Expired - Lifetime CN202691301U (en) | 2012-08-03 | 2012-08-03 | Cable lathedog of flying device and special rubber pad thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202691301U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103104749A (en) * | 2013-02-05 | 2013-05-15 | 侯如升 | Cable fixing device for numerically controlled lathe |
-
2012
- 2012-08-03 CN CN 201220383087 patent/CN202691301U/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103104749A (en) * | 2013-02-05 | 2013-05-15 | 侯如升 | Cable fixing device for numerically controlled lathe |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20130123 |
|
| CX01 | Expiry of patent term |