CN204966169U - Concentric stranded wire machine and drum after -combustion device thereof - Google Patents
Concentric stranded wire machine and drum after -combustion device thereof Download PDFInfo
- Publication number
- CN204966169U CN204966169U CN201520789083.7U CN201520789083U CN204966169U CN 204966169 U CN204966169 U CN 204966169U CN 201520789083 U CN201520789083 U CN 201520789083U CN 204966169 U CN204966169 U CN 204966169U
- Authority
- CN
- China
- Prior art keywords
- drum
- latch body
- wing aircraft
- aircraft system
- rewinder
- 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.)
- Withdrawn - After Issue
Links
Landscapes
- Storing, Repeated Paying-Out, And Re-Storing Of Elongated Articles (AREA)
Abstract
The utility model discloses a concentric stranded wire machine and drum after -combustion device thereof, this drum after -combustion device include the drum, the drum with the coaxial setting of all -wing aircraft system of concentric stranded wire machine, just the drum with the adjacent setting of all -wing aircraft system, just the drum is equipped with the slot, but the all -wing aircraft system be equipped with plug ground with slot matched with bolt device. According to the configuration, the utility model provides a drum after -combustion device of concentric stranded wire machine, its simple structure, with low costs and rate of equipment utilization is higher.
Description
Technical field
The utility model relates to cable processing technique field, more particularly, relates to a kind of concentric lay conductor machine and drum rewinder thereof.
Background technology
The drum of concentric lay conductor machine comprises after-combustion drum and draw drum, after-combustion drum is for being wrapped in after-combustion drum by wire, after-combustion drum needs drive unit to drive, and usually needs frictional disk to carry out after-combustion drum and rotates, or driven separately by motor in prior art.And draw drum only drives draw drum to rotate by the tension force of the wire of releasing.
So, after-combustion drum of the prior art needs to arrange drive unit and drives, and after-combustion drum and draw drum are arranged separately, and this kind of complicated structure, cost is high and cause the lower problem of utilization rate of equipment and installations.
Utility model content
In view of this, the utility model provides a kind of drum rewinder of concentric lay conductor machine, and its structure is simple, cost is low and utilization rate of equipment and installations is higher.The utility model additionally provides a kind of concentric lay conductor machine comprising above-mentioned drum rewinder.
The drum rewinder of a kind of concentric lay conductor machine that the utility model provides, comprise drum, the all-wing aircraft system coaxial of described drum and described concentric lay conductor machine is arranged, and described drum is disposed adjacent with described all-wing aircraft system, and described drum is provided with slot, described all-wing aircraft system is provided with the bolt device matched with described slot pluggablely.
Preferably, described bolt device comprises latch body and is arranged at the mounting groove of described all-wing aircraft system, and described latch body is telescopic to be arranged in described mounting groove; And described bolt device also comprises the positioner that described latch body can be positioned the state of stretching out and retracted state.
Preferably, described positioner comprises and is arranged at stretching out a location notch and regaining position location notch, be arranged at described mounting groove and stretch out the alignment pin of a location notch and described withdrawal position location notch described in can being inserted into of described latch body.
Preferably, described bolt device also comprises elastic component, the two ends of described elastic component offset with described mounting groove and described latch body respectively, when latch body be in stretch out time, the elastic force that described elastic component puts on described latch body is directed to the direction, withdrawal position of described latch body.
The utility model additionally provides a kind of concentric lay conductor machine, comprises drum rewinder and all-wing aircraft system, and described drum rewinder is the drum rewinder as above described in any one.
The drum rewinder of a kind of concentric lay conductor machine that the utility model provides, comprise drum, the all-wing aircraft system coaxial of described drum and described concentric lay conductor machine is arranged, and described drum is disposed adjacent with described all-wing aircraft system, and described drum is provided with slot, described all-wing aircraft system is provided with the bolt device matched with described slot pluggablely.Setting like this, the drum rewinder that the utility model provides, its drum as after-combustion drum, also can be used as draw drum.Because drum and all-wing aircraft system coaxial are arranged, when drum is as after-combustion drum, only need be inserted in the slot of drum by the bolt device of all-wing aircraft system, all-wing aircraft system can drive drum to carry out rotation to carry out coiling.When drum uses as draw drum, only bolt device need be extracted from the slot of drum, drum loses the driving relationship of all-wing aircraft system, and then can use as draw drum.Setting like this, the drum rewinder that the utility model provides, does not need to arrange draw drum and after-combustion drum more respectively, and does not need to arrange drive unit separately for after-combustion drum, and its structure is simple, cost is lower, and improves the utilance of equipment.
The utility model additionally provides a kind of concentric lay conductor machine comprising above-mentioned drum rewinder, so arranges, the concentric lay conductor machine that the utility model provides, and its structure is simple, cost is lower and utilization rate of equipment and installations is higher.
Accompanying drawing explanation
In order to be illustrated more clearly in the utility model embodiment or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment or description of the prior art below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those of ordinary skill in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
The drum rewinder schematic diagram that Fig. 1 provides for the utility model embodiment;
Fig. 2 is A portion enlarged diagram in Fig. 1;
Wherein, all-wing aircraft system-11, drum-12, slot-13, latch body-14, elastic component-15.
Embodiment
This embodiment provides a kind of drum rewinder of concentric lay conductor machine, and its structure is simple, cost is low and utilization rate of equipment and installations is higher.This embodiment additionally provides a kind of concentric lay conductor machine comprising above-mentioned drum rewinder.
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only the utility model part embodiment, instead of whole embodiments.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.
Please refer to Fig. 1 and Fig. 2, the drum rewinder of a kind of concentric lay conductor machine that this embodiment provides, comprises drum 12, and drum 12 is coaxially arranged with the all-wing aircraft system 11 of concentric lay conductor machine, and drum 12 is disposed adjacent with all-wing aircraft system 11.
Those skilled in the art are understandable that, concentric lay conductor machine of the prior art is provided with all-wing aircraft system 11, and during operation, drive unit is by driving axis of rotation and then driving all-wing aircraft system 11 to rotate.
In this embodiment, drum 12 is provided with slot 13, and all-wing aircraft system 11 is provided with the bolt device matched with slot 13 pluggablely.
Setting like this, the drum rewinder that this embodiment provides, its drum 12 as after-combustion drum, also can be used as draw drum.Because drum 12 and all-wing aircraft system 11 are coaxially arranged, when drum 12 is as the after-combustion drum used time, only need be inserted in the slot 13 of drum 12 by the bolt device of all-wing aircraft system 11, all-wing aircraft system 11 can drive drum 12 to carry out rotation to carry out coiling.When drum 12 uses as draw drum, only bolt device need be extracted from the slot 13 of drum 12, drum 12 loses the driving relationship of all-wing aircraft system 11, and then can use as draw drum.Therefore, the drum rewinder that this embodiment provides, does not need to arrange draw drum and after-combustion drum more respectively, and does not need to arrange drive unit separately for after-combustion drum, and its structure is simple, cost is lower, and improves the utilance of equipment.
In this embodiment, bolt device specific as followsly can state setting, and bolt device can comprise latch body 14 and be arranged at the mounting groove of all-wing aircraft system 11, and latch body 14 is telescopic to be arranged in mounting groove; And bolt device also comprises the positioner that latch body 14 can be positioned the state of stretching out and retracted state.
Setting like this, by arranging mounting groove in all-wing aircraft system 11, latch body 14 telescopically is arranged on the installation that can realize latch body 14 in this mounting groove, in addition, in order to prevent latch body 14 when the state of stretching out or retracted state, flip-flop stretches out or the problem of retracted state, can be provided with the positioner for latch body 14 being positioned in the state of stretching out or retracted state.
This positioner can comprise and is arranged at stretching out a location notch and regaining position location notch, be arranged at mounting groove and can be inserted into the alignment pin stretching out a location notch and regain position location notch of latch body 14.
Setting like this, when latch body 14 is positioned at the state of stretching out or retracted state, only need be inserted into alignment pin and stretches out a location notch or regain position location notch and can position latch body 14, prevent latch body 14 play.
Further, bolt device can also comprise elastic component 15, and the two ends of elastic component 15 offset with mounting groove and latch body 14 respectively.And, when latch body 14 be in stretch out time, the elastic force that described elastic component 15 puts on latch body 14 is directed to the direction, withdrawal position of latch body 14.Setting like this, when latch body 14 be in stretch out state time, only need pull out alignment pin, latch body 14 gets final product automatic drawing back, and then removes the locking to drum 12.
This embodiment additionally provides a kind of concentric lay conductor machine, comprises drum rewinder and all-wing aircraft system, and described drum rewinder is the drum rewinder as above described in any one.Setting like this, the concentric lay conductor machine that this embodiment provides, its structure is simple, cost is lower and utilization rate of equipment and installations is higher, and the derivation of the beneficial effect that the derivation of this beneficial effect and above-mentioned drum rewinder bring is substantially similar, therefore repeats no more herein.
In this specification, each embodiment adopts the mode of going forward one by one to describe, and what each embodiment stressed is the difference with other embodiments, between each embodiment identical similar portion mutually see.
To the above-mentioned explanation of the disclosed embodiments, professional and technical personnel in the field are realized or uses the utility model.To be apparent for those skilled in the art to the multiple amendment of these embodiments, General Principle as defined herein when not departing from spirit or scope of the present utility model, can realize in other embodiments.Therefore, the utility model can not be restricted to these embodiments shown in this article, but will meet the widest scope consistent with principle disclosed herein and features of novelty.
Claims (5)
1. the drum rewinder of a concentric lay conductor machine, comprise drum, it is characterized in that, the all-wing aircraft system coaxial of described drum and described concentric lay conductor machine is arranged, and described drum is disposed adjacent with described all-wing aircraft system, and described drum is provided with slot, described all-wing aircraft system is provided with the bolt device matched with described slot pluggablely.
2. drum rewinder as claimed in claim 1, is characterized in that, described bolt device comprises latch body and is arranged at the mounting groove of described all-wing aircraft system, and described latch body is telescopic to be arranged in described mounting groove; And described bolt device also comprises the positioner that described latch body can be positioned the state of stretching out and retracted state.
3. drum rewinder as claimed in claim 2, it is characterized in that, described positioner comprises and is arranged at stretching out a location notch and regaining position location notch, be arranged at described mounting groove and stretch out the alignment pin of a location notch and described withdrawal position location notch described in can being inserted into of described latch body.
4. drum rewinder as claimed in claim 3, it is characterized in that, described bolt device also comprises elastic component, the two ends of described elastic component offset with described mounting groove and described latch body respectively, when latch body be in stretch out time, the elastic force that described elastic component puts on described latch body is directed to the direction, withdrawal position of described latch body.
5. a concentric lay conductor machine, comprises drum rewinder and all-wing aircraft system, it is characterized in that, described drum rewinder is the drum rewinder as described in any one of claim 1-4.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520789083.7U CN204966169U (en) | 2015-10-10 | 2015-10-10 | Concentric stranded wire machine and drum after -combustion device thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520789083.7U CN204966169U (en) | 2015-10-10 | 2015-10-10 | Concentric stranded wire machine and drum after -combustion device thereof |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204966169U true CN204966169U (en) | 2016-01-13 |
Family
ID=55061218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520789083.7U Withdrawn - After Issue CN204966169U (en) | 2015-10-10 | 2015-10-10 | Concentric stranded wire machine and drum after -combustion device thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204966169U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105719775A (en) * | 2016-04-12 | 2016-06-29 | 浙江晨光电缆股份有限公司 | Concentric stranding machine |
| CN106571196A (en) * | 2015-10-10 | 2017-04-19 | 合肥神马科技集团有限公司 | Concentric stranding machine and wire coil compound winding device thereof |
-
2015
- 2015-10-10 CN CN201520789083.7U patent/CN204966169U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106571196A (en) * | 2015-10-10 | 2017-04-19 | 合肥神马科技集团有限公司 | Concentric stranding machine and wire coil compound winding device thereof |
| CN106571196B (en) * | 2015-10-10 | 2019-01-04 | 合肥神马科技集团有限公司 | A kind of concentric lay conductor machine and its drum rewinder |
| CN105719775A (en) * | 2016-04-12 | 2016-06-29 | 浙江晨光电缆股份有限公司 | Concentric stranding machine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN205222311U (en) | Power communication cable pay -off and take -up device | |
| CN205240964U (en) | Hank reeling machine's stranded conductor frame | |
| CN204966169U (en) | Concentric stranded wire machine and drum after -combustion device thereof | |
| CN108249231A (en) | It is tethered at the change torque cable winding apparatus of unmanned plane and its folding and unfolding cable method | |
| CN108249232A (en) | A kind of bus cable device for being used to be tethered at unmanned plane | |
| CN109607304A (en) | A kind of Computer Network Project take-up | |
| CN209823279U (en) | Fast assembly's unwrapping wire coaster | |
| CN204474220U (en) | A kind of electric hoist conductor rope device with position-limited lever | |
| CN106448937B (en) | The planetary wire stranding machine of high speed | |
| CN203232748U (en) | Planar cable forming machine | |
| CN204057441U (en) | Planer-type is paying out machine initiatively | |
| CN106571196A (en) | Concentric stranding machine and wire coil compound winding device thereof | |
| CN108923202A (en) | Combined electrical source manager | |
| CN202687860U (en) | Manual brake releasing device | |
| CN204416770U (en) | Steel wire pay off rack | |
| CN201234112Y (en) | Electric friction type wire-drawing mechanism for aircraft service ground well | |
| CN205069232U (en) | Stranding machine and many lines pull after -combustion device thereof | |
| CN103474174B (en) | A kind of reverse-twisting draft gear of spiral cable reverse-twisting machine | |
| CN203806872U (en) | Plastic rope bundling auxiliary device | |
| CN204680482U (en) | Multiply core automatic winding device | |
| CN106848616B (en) | The locking device of wire screw fastener in a kind of power equipment | |
| CN102910491A (en) | Automatic winding device | |
| CN204151511U (en) | Anti drop-off weaving creel | |
| CN207142722U (en) | It is easily installed the Portable lifting machine of rope | |
| CN205105496U (en) | Cable steel band device and have machine of cable steel band device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20160113 Effective date of abandoning: 20190104 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20160113 Effective date of abandoning: 20190104 |
|
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |