CN205207916U - Subassembly is fixed to pencil - Google Patents
Subassembly is fixed to pencil Download PDFInfo
- Publication number
- CN205207916U CN205207916U CN201521014836.3U CN201521014836U CN205207916U CN 205207916 U CN205207916 U CN 205207916U CN 201521014836 U CN201521014836 U CN 201521014836U CN 205207916 U CN205207916 U CN 205207916U
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- Prior art keywords
- wire harness
- fixed unit
- junction surface
- fixed
- assembly
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Abstract
The utility model discloses a subassembly is fixed to pencil. Subassembly is fixed to pencil includes: nylon frenulum (1), polycell fixing device, be provided with a plurality of fixed unit (2) on the polycell fixing device, every fixed unit (2) are with one nylon frenulum (1) cooperation, each fixed unit (2) interconnect to forming one and connecting face (21), this connection face (21) are used for being connected with organism structure (3) of aircraft, connect face (21) be used for placing pencil (4) on the right face, wherein, nylon frenulum (1) is used for passing fixed unit (2), thus bind pencil (4). The utility model discloses a subassembly is fixed to pencil have with structure roof beam, support, the laminating du genggao of cable satisfies the clearance requirement that the aircraft laid, improves airborne system's reliability. In addition, this subassembly is fixed to pencil light in weight replaces the metal clamp in a large number and uses, can greatly reduce the weight of laying of cable.
Description
Technical field
The utility model relates to technical field of aerospace, particularly relates to a kind of wire harness fixing-assembly.
Background technique
At present, in cables manufacturing or laid processes, nylon frenulum is adopted to fix wire harness in a large number.In cables manufacturing, nylon frenulum plays tightens wire harness effect; In laying, nylon frenulum usually by cable tie to structure stand, Liang Shang.But be usually limited to structural type, cause colligation not tight, fit bad with structure.In three-dimensional cables manufacturing, wire harness will be fitted with close structure especially.
Therefore, wish a kind of technological scheme to overcome or at least alleviate at least one above-mentioned defect of prior art.
Model utility content
The purpose of this utility model is at least one the above-mentioned defect providing a kind of wire harness fixing-assembly to overcome or at least alleviate in prior art.
For achieving the above object, the utility model provides a kind of wire harness fixing-assembly, and for the wire harness of fastening aircraft internal body, described wire harness fixing-assembly comprises: nylon frenulum; Multiple-unit fixing device, described multiple-unit fixing device is provided with multiple fixed unit, each fixed unit coordinates with a described nylon frenulum, each fixed unit is interconnected, thus form a junction surface, this junction surface is used for being connected with the housing construction of aircraft, for placing wire harness on the face that described junction surface is right; Wherein, described nylon frenulum is used for through described fixed unit, thus bundlees described wire harness.
Preferably, described in each, fixed unit is one-body molded.
Preferably, fixed unit described in each adopts pouring type one-body molded.
Preferably, described fixed unit is made with nylon polyamide material.
Preferably, between the face that the junction surface of described fixed unit is relative with this junction surface, there is space, be connected by all sidewalls between the face that described junction surface is relative with this junction surface, any two relative walls of described all sidewalls are provided with relative hole, position, and described nylon frenulum can penetrate from the described hole of one of them wall and hole on another wall relative with this wall passes.
Preferably, the fixed unit quantity in described multiple-unit fixing device is two or three.
Wire harness fixing-assembly of the present utility model has and structural beams, support, and the laminating Du Genggao of cable, meets the clearance requirement that aircraft lays, and improves the reliability of mobile system.In addition, this wire harness fixing-assembly is lightweight, and a large amount of alternative metals clip uses, and that greatly can reduce cable lays weight.
Accompanying drawing explanation
Fig. 1 is the structural representation of the wire harness fixing-assembly according to the utility model one embodiment.
Reference character:
| 1 | Nylon frenulum | 4 | Wire harness |
| 2 | Fixed unit | 5 | All sidewalls |
| 21 | Junction surface | 51 | Hole |
| 3 | Housing construction |
Embodiment
The object implemented for making the utility model, technological scheme and advantage clearly, below in conjunction with the accompanying drawing in the utility model embodiment, are further described in more detail the technological scheme in the utility model embodiment.In the accompanying drawings, same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Described embodiment is the utility model part embodiment, instead of whole embodiments.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the utility model, and can not be interpreted as restriction of the present utility model.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.Below in conjunction with accompanying drawing, embodiment of the present utility model is described in detail.
In description of the present utility model, it will be appreciated that, term " " center ", " longitudinal direction ", " transverse direction ", " front ", " afterwards ", " left side ", " right side ", " vertically ", " level ", " top ", " end " " interior ", orientation or the position relationship of the instruction such as " outward " are based on orientation shown in the drawings or position relationship, only the utility model and simplified characterization for convenience of description, instead of indicate or imply that the device of indication or element must have specific orientation, with specific azimuth configuration and operation, therefore the restriction to the utility model protection domain can not be interpreted as.
Fig. 1 is the structural representation of the wire harness fixing-assembly according to the utility model one embodiment.
Wire harness fixing-assembly as shown in Figure 1, for the wire harness of fastening aircraft internal body, described wire harness fixing-assembly comprises nylon frenulum 1 and multiple-unit fixing device, multiple-unit fixing device is provided with multiple fixed unit 2, each fixed unit 2 coordinates with a nylon frenulum 1, and each fixed unit 2 is interconnected, thus forms a junction surface 21, this junction surface 21 for being connected with the housing construction 3 of aircraft, for placing wire harness 4 on the face that junction surface 21 is right; Wherein, nylon frenulum 1 is for passing fixed unit (2), thus binding wire harness 4.
In the present embodiment, each fixed unit 2 is one-body molded.Be understandable that, each fixed unit also can be made split, detachable.Thus need according to diverse location difference and assemble.
In the present embodiment, each fixed unit 2 adopts pouring type one-body molded.
Advantageously, in the present embodiment, fixed unit 2 is made with nylon polyamide material.Adopt this material, there is the advantage of high strength, low weight.
In the present embodiment, between the face that the junction surface 21 of fixed unit 2 is relative with this junction surface, there is space, be connected by all sidewalls 5 between the face that junction surface is relative with this junction surface, week sidewall 5 any two relative walls on be provided with relative hole, position 51, nylon frenulum 1 can penetrate from the hole 51 of one of them wall and hole 51 on another wall relative with this wall passes.
In the present embodiment, fixed unit 2 quantity in multiple-unit fixing device is two or three.
Be understandable that, the quantity of fixed unit can also sets itself as required.Such as, 4,5 or more.
Wire harness fixing-assembly of the present utility model has and structural beams, support, and the laminating Du Genggao of cable, meets the clearance requirement that aircraft lays, and improves the reliability of mobile system.In addition, this wire harness fixing-assembly is lightweight, and a large amount of alternative metals clip uses, and that greatly can reduce cable lays weight.
Finally it is to be noted: above embodiment only in order to the technical solution of the utility model to be described, is not intended to limit.Although be described in detail the utility model with reference to previous embodiment, those of ordinary skill in the art is to be understood that: it still can be modified to the technological scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of each embodiment's technological scheme of the utility model.
Claims (6)
1. a wire harness fixing-assembly, for the wire harness of fastening aircraft internal body, is characterized in that, described wire harness fixing-assembly comprises:
Nylon frenulum (1);
Multiple-unit fixing device, described multiple-unit fixing device is provided with multiple fixed unit (2), each fixed unit (2) coordinates with a described nylon frenulum (1), each fixed unit (2) is interconnected, thus form a junction surface (21), this junction surface (21) for being connected with the housing construction (3) of aircraft, for placing wire harness (4) on the face that described junction surface (21) is right; Wherein,
Described nylon frenulum (1) for passing described fixed unit (2), thus bundlees described wire harness (4).
2. wire harness fixing-assembly as claimed in claim 1, it is characterized in that, fixed unit described in each (2) is one-body molded.
3. wire harness fixing-assembly as claimed in claim 2, is characterized in that, fixed unit described in each (2) adopts pouring type one-body molded.
4. wire harness fixing-assembly as claimed in claim 3, it is characterized in that, described fixed unit (2) is made with nylon polyamide material.
5. as the wire harness fixing-assembly in Claims 1-4 as described in any one, it is characterized in that, between the face that the junction surface (21) of described fixed unit (2) is relative with this junction surface, there is space, be connected by all sidewalls (5) between the face that described junction surface is relative with this junction surface, any two relative walls of described all sidewalls (5) are provided with relative hole, position (51), and described nylon frenulum (1) can penetrate from the described hole (51) of one of them wall and hole (51) on another wall relative with this wall passes.
6. wire harness fixing-assembly as claimed in claim 1, it is characterized in that, fixed unit (2) quantity in described multiple-unit fixing device is two or three.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521014836.3U CN205207916U (en) | 2015-12-09 | 2015-12-09 | Subassembly is fixed to pencil |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521014836.3U CN205207916U (en) | 2015-12-09 | 2015-12-09 | Subassembly is fixed to pencil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205207916U true CN205207916U (en) | 2016-05-04 |
Family
ID=55845633
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521014836.3U Active CN205207916U (en) | 2015-12-09 | 2015-12-09 | Subassembly is fixed to pencil |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205207916U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108754850A (en) * | 2018-05-24 | 2018-11-06 | 芜湖品度电子科技有限公司 | Harness reorganizer for working out machine |
| CN108754849A (en) * | 2018-05-24 | 2018-11-06 | 芜湖品度电子科技有限公司 | The harness collator of establishment machine |
| CN108750811A (en) * | 2018-05-24 | 2018-11-06 | 芜湖品度电子科技有限公司 | Harness collating unit for working out machine |
| CN108823786A (en) * | 2018-05-24 | 2018-11-16 | 芜湖品度电子科技有限公司 | Harness for working out machine arranges accessory |
-
2015
- 2015-12-09 CN CN201521014836.3U patent/CN205207916U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108754850A (en) * | 2018-05-24 | 2018-11-06 | 芜湖品度电子科技有限公司 | Harness reorganizer for working out machine |
| CN108754849A (en) * | 2018-05-24 | 2018-11-06 | 芜湖品度电子科技有限公司 | The harness collator of establishment machine |
| CN108750811A (en) * | 2018-05-24 | 2018-11-06 | 芜湖品度电子科技有限公司 | Harness collating unit for working out machine |
| CN108823786A (en) * | 2018-05-24 | 2018-11-16 | 芜湖品度电子科技有限公司 | Harness for working out machine arranges accessory |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |