CN203932801U - Penetrating cable clamp torque nut disintegrating machine - Google Patents
Penetrating cable clamp torque nut disintegrating machine Download PDFInfo
- Publication number
- CN203932801U CN203932801U CN201420389191.0U CN201420389191U CN203932801U CN 203932801 U CN203932801 U CN 203932801U CN 201420389191 U CN201420389191 U CN 201420389191U CN 203932801 U CN203932801 U CN 203932801U
- Authority
- CN
- China
- Prior art keywords
- head
- fuselage
- cable clamp
- fuselage body
- penetrating cable
- 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 - Fee Related
Links
- 230000000149 penetrating effect Effects 0.000 title claims abstract description 28
- 210000004907 gland Anatomy 0.000 claims abstract description 19
- 230000013011 mating Effects 0.000 claims abstract description 4
- 239000000758 substrate Substances 0.000 claims description 12
- 241000557624 Nucifraga Species 0.000 abstract description 4
- 238000013467 fragmentation Methods 0.000 description 6
- 238000006062 fragmentation reaction Methods 0.000 description 6
- 239000004020 conductor Substances 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
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- Earth Drilling (AREA)
Abstract
The utility model discloses a kind of penetrating cable clamp torque nut disintegrating machine, comprise fuselage, the head that fuselage comprises fuselage body and is integrally formed at the U-shaped structure of fuselage body head, the front side of head is provided with changeable type gland, the rear side of head is provided with cutter head, the setting corresponding to cutter head of changeable type gland and line are between the two vertical with the opening direction of head, changeable type gland is provided with the groove mating with penetrating cable clamp torque nut cap sleeve, fuselage body is axial hollow structure, fuselage body inner chamber is provided with a drive rod vertically, the tail end of the head end butt cutter head of drive rod, the tail end of drive rod passes fuselage body and is connected with power set, these power set drive described drive rod in axial direction flexible at fuselage body inner chamber.The utility model is a kind of small-sized nut cracker, simple to operation, and its broken dynamics can meet the requirement of broken penetrating cable clamp cap sleeve completely.
Description
Technical field
The utility model relates to penetrating cable clamp torque nut disintegrating machine.
Background technology
The insulated wire puncture wire clamp using is at present owing to should guaranteeing to keep close contact not damage to insulated conductor internal core again with insulated conductor core after puncture.Therefore the nut using adopts torque nut, but can rupture when moment reaches certain numerical value back nut, cause puncture excessively to cause insulated conductor internal core is damaged.
Penetrating cable clamp torque nut is enclosed within on a nut, after torque nut fracture, can leave a cap sleeve, and cap sleeve adopts and is closely connected with nut, and cap sleeve is to be a band little central portion of rising as high as the banks, and is difficult to remove with spanner.So, in to the process of its replacing, can only take to destroy cap sleeve and remove, yet the nut cracker using being at present too large, between penetrating cable clamp two nuts, spacing is very little, and present nut cracker can not use.
Utility model content
Technical problem to be solved in the utility model is just to provide a kind of mini penetrating cable clamp torque nut disintegrating machine, simple in structure, easy to use.
For solving the problems of the technologies described above, the utility model adopts following technical scheme: penetrating cable clamp torque nut disintegrating machine, comprise fuselage, the head that described fuselage comprises fuselage body and is integrally formed at the U-shaped structure of fuselage body head, the opening direction of described head is axial vertical with fuselage body, the front side of described head is provided with changeable type gland, the rear side of described head is provided with cutter head, the setting corresponding to cutter head of described changeable type gland and line are between the two vertical with the opening direction of head, described changeable type gland is provided with the groove mating with penetrating cable clamp torque nut cap sleeve, described fuselage body is axial hollow structure, fuselage body inner chamber is provided with a drive rod vertically, the tail end of the head end butt cutter head of described drive rod, the tail end of described drive rod passes fuselage body and is connected with power set, these power set drive described drive rod in axial direction flexible at fuselage body inner chamber.
Preferably, the tail end of described fuselage body is provided with screw shell, and described drive rod is threaded with screw shell.
Preferably, the tail end of described drive rod is provided with turret head, and described power set are spanner.
Preferably, described changeable type gland is fixed by bolt arrangement and head front side.
Preferably, described fuselage is fixed in fuselage fixture, and described fuselage fixture comprises substrate, and the front side of described substrate is provided with boss, described boss is provided with the holddown groove snapping in for fuselage body, and described substrate is provided with fuselage hold-down mechanism the fuselage that snaps in holddown groove is compressed above boss.
Preferably, described fuselage hold-down mechanism comprises U-shaped crane span structure, one side of crane span structure oral area is articulated with one end of boss, crane span structure inside is provided with a compact heap, and compact heap both sides are provided with guiding groove, and the inner both sides of crane span structure are provided with raised line and coordinate with guiding groove, described compact heap bottom is provided with the pressing groove that compresses fuselage body, the bridge floor of the described crane span structure screw rod that has been threaded, described screw tip connects a lever, and described screw rod bottom and compact heap are fixed.
Preferably, the two ends of described boss protrude from substrate both sides, the hinged latch hook of opposite side of described crane span structure oral area, and described latch hook is hooked in boss end.
The utility model is a kind of small-sized nut cracker, and the changeable type gland on head is fixed the cap sleeve of penetrating cable clamp torque nut, and cutter head applies active force to the cap sleeve of penetrating cable clamp torque nut, carries out fragmentation.Its drive unit does not adopt hydraulic way, and adopts conventional mechanical system, and spanner drives drive rod to rotate, and due to the effect between drive rod and screw shell, drive rod is to lateral movement before fuselage body and be with dynamic cutter head extruding nut, and nut is broken.It makes simple to operation, and its broken dynamics can meet the requirement of broken penetrating cable clamp cap sleeve completely.
Therefore the beneficial effects of the utility model are:
1, mini structure, is convenient for carrying, lightweight, simple in structure, changeable type gland fluted with cap sleeve close contact.
2, mechanism adopts mechanical manpower to drive, and type of drive is simple, easy to operate.
3, can use at any time electric wrench as driving manpower to drive when broken dynamics deficiency or personnel's operation fatigue, reduce operator tired.
Accompanying drawing explanation
Below in conjunction with the drawings and specific embodiments, the utility model is further described:
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structural representation of fuselage fixture.
Embodiment
As shown in Figure 1, penetrating cable clamp torque nut disintegrating machine, comprise fuselage 1, the head 10 that described fuselage 1 comprises fuselage body 11 and is integrally formed at the U-shaped structure of fuselage body head, the opening direction of described head 10 is axial vertical with fuselage body 11, the front side of described head 10 is provided with changeable type gland 101, the rear side of described head 10 is provided with cutter head 102, the setting corresponding to cutter head 102 of described changeable type gland 101 and line are between the two vertical with the opening direction of head 10, described changeable type gland 101 is provided with the groove mating with penetrating cable clamp torque nut cap sleeve, described fuselage body is axial hollow structure, fuselage body inner chamber is provided with a drive rod 12 vertically, the tail end of the head end butt cutter head 102 of described drive rod 12, the tail end of described drive rod 12 passes fuselage body 11 and is connected with power set, these power set drive described drive rod in axial direction flexible at fuselage body inner chamber.Changeable type gland on head is fixed the cap sleeve of penetrating cable clamp torque nut, and cutter head applies active force to the cap sleeve of penetrating cable clamp torque nut, carries out fragmentation, and cutter head is driven by drive rod, and drive rod is driven by power set.
The tail end of described fuselage body is provided with screw shell 111, and described drive rod 12 is threaded with screw shell.The tail end of described drive rod is provided with turret head 121, and described power set are spanner.Spanner can be manual, can be also electronic, and spanner drives drive rod 12 to rotate, and due to the effect between drive rod and screw shell, drive rod is to lateral movement before fuselage body and be with dynamic cutter head extruding nut, and nut is broken.Its type of drive is simple, easy to operate, and its broken dynamics can meet the requirement of broken penetrating cable clamp cap sleeve completely.
Described changeable type gland 101 is fixed by bolt arrangement and head front side.Be convenient to the dismounting of changeable type gland and change.
For the ease of carrying out nut fragmentation procedure, a fuselage fixture 2 can also be set, above-mentioned fuselage 1 is fixed in fuselage fixture 2.As shown in Figure 2, described fuselage fixture 2 comprises substrate 20, the front side of described substrate is provided with boss 21, and described boss 21 is provided with the holddown groove 211 snapping in for fuselage body, and described substrate is provided with fuselage hold-down mechanism the fuselage that snaps in holddown groove is compressed above boss.
Described fuselage hold-down mechanism comprises U-shaped crane span structure 22, one side of crane span structure oral area is articulated with one end of boss, crane span structure inside is provided with a compact heap 24, compact heap both sides are provided with guiding groove, the inner both sides of crane span structure are provided with raised line and coordinate with guiding groove, are provided with the pressing groove 241 of compression fuselage body bottom described compact heap, the bridge floor of the described crane span structure screw rod 25 that has been threaded, described screw tip connects a lever 26, and described screw rod bottom and compact heap are fixed.The two ends of described boss protrude from substrate both sides, the hinged latch hook 23 of opposite side of described crane span structure oral area, and described latch hook is hooked in boss end.The cross-sectional profiles of fuselage body can be square or regular hexagon, and the also corresponding setting of shape of holddown groove and pressing groove, is convenient to fuselage to be fixed.
Before carrying out the fragmentation of penetrating cable clamp torque nut, by crane span structure 22 to turning up, fuselage body 11 snaps in fixes 211, then crane span structure 22 closes, latch hook 23 is hooked in boss end, drives screw rod 25 to rotate, due to the cooperation of guiding groove and raised line by lever 26, compact heap 24 moves downward, until pressing groove 241 coordinates fuselage is compressed with holddown groove 211.Like this, operating personnel can carry out fragmentation to nut easily, thereby have improved quality and the efficiency of nut fragmentation.
Claims (7)
1. penetrating cable clamp torque nut disintegrating machine, comprise fuselage (1), it is characterized in that: the head (10) that described fuselage (1) comprises fuselage body (11) and is integrally formed at the U-shaped structure of fuselage body head, the opening direction of described head is axial vertical with fuselage body, the front side of described head is provided with changeable type gland (101), the rear side of described head is provided with cutter head (102), described changeable type gland (101) setting corresponding to cutter head (102) and line are between the two vertical with the opening direction of head, described changeable type gland (101) is provided with the groove mating with penetrating cable clamp torque nut cap sleeve, described fuselage body is axial hollow structure, fuselage body inner chamber is provided with a drive rod (12) vertically, the tail end of the head end butt cutter head of described drive rod, the tail end of described drive rod passes fuselage body and is connected with power set, these power set drive described drive rod in axial direction flexible at fuselage body inner chamber.
2. penetrating cable clamp torque nut disintegrating machine according to claim 1, is characterized in that: the tail end of described fuselage body is provided with screw shell (111), and described drive rod is threaded with screw shell.
3. penetrating cable clamp torque nut disintegrating machine according to claim 2, is characterized in that: the tail end of described drive rod is provided with turret head (121), and described power set are spanner.
4. penetrating cable clamp torque nut disintegrating machine according to claim 1, is characterized in that: described changeable type gland is fixed by bolt arrangement and head front side.
5. according to the penetrating cable clamp torque nut disintegrating machine described in claim 1 to 4 any one, it is characterized in that: described fuselage (1) is fixed in fuselage fixture (2), described fuselage fixture comprises substrate (20), the front side of described substrate is provided with boss (21), described boss is provided with the holddown groove (211) snapping in for fuselage body, and described substrate is provided with fuselage hold-down mechanism the fuselage that snaps in holddown groove is compressed above boss.
6. penetrating cable clamp torque nut disintegrating machine according to claim 5, it is characterized in that: described fuselage hold-down mechanism comprises U-shaped crane span structure (22), one side of crane span structure oral area is articulated with one end of boss, crane span structure inside is provided with a compact heap (24), compact heap both sides are provided with guiding groove, the inner both sides of crane span structure are provided with raised line and coordinate with guiding groove, described compact heap bottom is provided with the pressing groove (241) that compresses fuselage body, the bridge floor of the described crane span structure screw rod (25) that has been threaded, described screw tip connects a lever (26), and described screw rod bottom and compact heap are fixed.
7. penetrating cable clamp torque nut disintegrating machine according to claim 6, is characterized in that: the two ends of described boss protrude from substrate both sides, the hinged latch hook of opposite side (23) of described crane span structure oral area, and described latch hook is hooked in boss end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389191.0U CN203932801U (en) | 2014-07-15 | 2014-07-15 | Penetrating cable clamp torque nut disintegrating machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389191.0U CN203932801U (en) | 2014-07-15 | 2014-07-15 | Penetrating cable clamp torque nut disintegrating machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203932801U true CN203932801U (en) | 2014-11-05 |
Family
ID=51828557
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420389191.0U Expired - Fee Related CN203932801U (en) | 2014-07-15 | 2014-07-15 | Penetrating cable clamp torque nut disintegrating machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203932801U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104167684A (en) * | 2014-07-15 | 2014-11-26 | 国家电网公司 | Torsion nut crusher of puncturing wire clamp |
| CN105680365A (en) * | 2014-07-15 | 2016-06-15 | 国网浙江省电力公司金华供电公司 | Miniature puncture clamp torque nut crusher |
-
2014
- 2014-07-15 CN CN201420389191.0U patent/CN203932801U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104167684A (en) * | 2014-07-15 | 2014-11-26 | 国家电网公司 | Torsion nut crusher of puncturing wire clamp |
| CN105680365A (en) * | 2014-07-15 | 2016-06-15 | 国网浙江省电力公司金华供电公司 | Miniature puncture clamp torque nut crusher |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141105 |