CN205722993U - A kind of flying-wing device - Google Patents
A kind of flying-wing device Download PDFInfo
- Publication number
- CN205722993U CN205722993U CN201620302407.4U CN201620302407U CN205722993U CN 205722993 U CN205722993 U CN 205722993U CN 201620302407 U CN201620302407 U CN 201620302407U CN 205722993 U CN205722993 U CN 205722993U
- Authority
- CN
- China
- Prior art keywords
- wing aircraft
- wing
- flying
- main shaft
- wire
- 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.)
- Active
Links
Landscapes
- Ropes Or Cables (AREA)
Abstract
The utility model discloses a kind of flying-wing device, including the all-wing aircraft body being sleeved on main shaft, described all-wing aircraft body connects all-wing aircraft swivel head, described all-wing aircraft swivel head is rotationally connected with all-wing aircraft body, being provided with retaining mechanism between described all-wing aircraft swivel head and all-wing aircraft body, described flying-wing device is provided with all-wing aircraft guide wheel assembly.Owing to by the regulation of flying-wing device, storage line capstan winch can realize wire after-combustion and twisted wire, it is to avoid shuts down the appearance of upper and lower drum situation, improves production efficiency.
Description
Technical field
This utility model relates to cable and produces equipment, is specifically related to wire twisting equipment.
Background technology
At present in China, the commonly used wire twisting equipment of wires and cables industry has fork strand, frame strand, pipe strand, cage
Strand etc..Fork strand is old-fashioned wire twisting equipment, and construction features is not suitable for running up, inefficient.Replace
The frame winch of fork turntable has that structure is strong, rotating speed high, has obtained applying more widely, has been current
The main flow equipment of twisted wire without back twist.Frame winch drum is arranged in the outside of main shaft, the radius of gyration about 800mm,
Rotary inertia is relatively big, and it sometimes appear that the asymmetric and inequality of drum wiring amount of drum distributed number
Situation, causes the imbalance of centrifugal force, so limiting the further raising of frame winch rotating speed, typically 200
Below Zhuaning；Cage winch is due to the restriction of structure, and rotating speed is lower, only tens turns.Pipe twisting machine is mainly used in raw
Produce the stranded conductor of small bore.It addition, above wire twisting equipment has a process shutting down upper and lower drum,
Production efficiency is restricted.
Utility model content
Technical problem to be solved in the utility model is just to provide a kind of flying-wing device, it is to avoid wire twisting machine is shut down
The appearance of upper and lower drum situation, improves production efficiency.
For solving above-mentioned technical problem, this utility model adopts the following technical scheme that a kind of flying-wing device, bag
Including the all-wing aircraft body being sleeved on main shaft, described all-wing aircraft body connects all-wing aircraft swivel head, and described all-wing aircraft rotates
Head is rotationally connected with all-wing aircraft body, is provided with retaining mechanism between described all-wing aircraft swivel head and all-wing aircraft body, described
Flying-wing device is provided with all-wing aircraft guide wheel assembly.
As preferably, described all-wing aircraft head is provided with rotary jack, and described all-wing aircraft swivel head is provided with rotary connector,
Described rotary connector inserts rotary jack.
As preferably, between described rotary connector and all-wing aircraft swivel head main part, it is provided with radial transition portion, described
Retaining mechanism is several locking nuts that radially transition part is circumferentially disposed.
As preferably, described all-wing aircraft swivel head includes runing rest and all-wing aircraft top guide, and described all-wing aircraft top guide is to water
Flat protruding outside, described all-wing aircraft guide wheel assembly includes the first guide wheel group being located on all-wing aircraft top guide and is located at rotation
The second guide wheel group on support.
As preferably, described flying-wing device is provided with upper machine body and lower body, and described upper machine body and lower body pass through
Hafu-type structural clamp is on main shaft, and described upper machine body and lower body are connected by bolt and main shaft are fixing, institute
State upper machine body and lower body head is provided with all-wing aircraft swivel head, described upper machine body and lower body near main shaft
Side is provided with the 3rd guide wheel group.
Flying-wing device of the present utility model can be adjusted, and is adjusted by all-wing aircraft swivel head to not affecting after-combustion and leads
The position of line, can carry out after-combustion wire, after wire after-combustion is on storage line capstan winch, is adjusted by all-wing aircraft swivel head
To unwrapping wire position, then the wire in storage line capstan winch can be proceeded to by flying-wing device the hollow interior releasing of main shaft,
Until the front end guide wheel of main shaft goes to the outside of main shaft, controlled by the tension force of monofilament tension-adjusting gear, really
Protect the uniform tension in order of every monofilament, complete quick twisted wire subsequently into noseplate, due to by flying-wing device
Regulation, storage line capstan winch can realize wire after-combustion and twisted wire, it is to avoid shuts down the appearance of upper and lower drum situation,
Improve production efficiency.
Accompanying drawing explanation
With detailed description of the invention, this utility model is further described below in conjunction with the accompanying drawings:
Fig. 1 is the structural representation of concentric lay conductor machine；
Fig. 2 is the structural representation of twisted wire system；
Fig. 3 is the structural representation one of flying-wing device；
Fig. 4 is the structural representation two of flying-wing device.
Detailed description of the invention
As it is shown in figure 1, a kind of concentric lay conductor machine, including paying off system 6, twisted wire system 2, die seat system 3,
Trailer system 4, winding system 5.The ring type monofilament wire drawn by wire drawing machine is positioned on paying off system 6,
Paying off system 6 is released by tenslator, guide roller device, bunch cage assembly etc., is then passed through tool
Enter twisted wire system 2 after having the guide wheel that disc brake controls and carry out wire after-combustion or strand system.Wire wind after through all-wing aircraft
The devices such as device, monofilament tension adjustment are released and carry out strand system, complete quick twisted wire, the line warp that strand has been made
Crossing mould in die seat system 3 and press molding, gone out the strand cable core after mould and entered trailer system 4, strand makes
Cable core finally enter winding system 5 rolling and complete.
As in figure 2 it is shown, twisted wire system 2 includes that main shaft 20 and flying-wing device 1, main shaft 20 are hollow axle,
Main shaft 20 is provided with the groove 203 entering for wire or passing, and main shaft 20 is supported on main shaft bearing 201,
It is rotatably connected to store up line capstan winch 21 on described main shaft 20, between storage line capstan winch 21 and main shaft, is provided with storage line capstan winch
Bearing, the wire that paying off system 6 is released enters storage line capstan winch 21 after after-combustion guide wheel 22 and completes wire again
Around, storage line capstan winch is divided into 2 dish storage line capstan winches and 4 dishes, two kinds of line capstan winch of storage, respectively can be with after-combustion 2 dish, 4 dishes
Wire, often dish strand body at most can simultaneously 3 wires of after-combustion.
Described main shaft 20 is driven by spindle motor, and described storage line capstan winch 21 is driven by storage line motor.Described master
First end of axle is fixed with the first synchronous pulley 202, and described main shaft is in the axial side of storage line capstan winch 21 side by side
It is provided with and stores up the second fixing synchronous pulley 211 of line capstan winch 21, described first synchronous pulley 202 and main shaft
By the first toothed belt transmission between motor, same by second between described second synchronous pulley and storage line motor
Step V belt translation, the axial side of storage line capstan winch 21 is provided with pneumatically operated brake 212.
Axial second side of main shaft 20 is provided with monofilament tension-adjusting gear 23, noseplate 24, and main shaft 20 exists
Monofilament tension-adjusting gear 23 first side is provided with derivation wheel 231 and wire disk 232, and conductor monofilament is through groove 203
The derivation wheel that place is arranged leads to outside main shaft, then passes through wire disk upper conductor hole, is adjusted by monofilament tension force
The tension force of regulating device 23 controls, it is ensured that the uniform tension in order of every monofilament, completes soon subsequently into noseplate 24
Speed twisted wire.
Monofilament tension-adjusting gear 23 includes Wire guide roller and regulation roller, and wire monofilament is from Wire guide roller and regulation roller
Passing, realize wire monofilament tension adjustment by the spacing of regulation regulation roller with Wire guide roller, regulation roller connects to be had
Making the spring of regulation roll-in guiding line roller, noseplate is provided with the tapered flanges to the second side opening, tapered flanges
Circumferentially arranged separated time hole, wire seal wire passes from separated time hole.
As shown in Figure 3 and Figure 4, described flying-wing device 1 includes the all-wing aircraft body 11 being sleeved on main shaft 20,
Described all-wing aircraft body connects has all-wing aircraft swivel head 12, described all-wing aircraft swivel head to be rotationally connected with all-wing aircraft body, institute
State and between all-wing aircraft swivel head and all-wing aircraft body, be provided with retaining mechanism, all-wing aircraft swivel head can with 360 degree of rotations,
There are 4 positions can be fixed by retaining mechanism, for switching and the switching of after-combustion unwrapping wire of draw drum.
Described flying-wing device 1 is provided with all-wing aircraft guide wheel assembly 13.Described all-wing aircraft head is provided with rotary jack, described
All-wing aircraft swivel head is provided with rotary connector, and described rotary connector inserts rotary jack.Described rotary connector and all-wing aircraft
Being provided with radial transition portion between swivel head main part, described retaining mechanism is that radially transition part is circumferentially disposed
Several locking nuts 121.
Described all-wing aircraft swivel head 12 includes runing rest and all-wing aircraft top guide, and described all-wing aircraft top guide is to horizontal outer side
Prominent, described all-wing aircraft guide wheel assembly includes the first guide wheel group 131 being located on all-wing aircraft top guide and is located at rotation
The second guide wheel group 132 on frame.Described flying-wing device is provided with upper machine body 112 and lower body 111, described upper machine
Body and lower body are by Hafu-type structural clamp on main shaft, and described upper machine body and lower body are by bolt 113
Fixing with main shaft and be connected, described upper machine body and lower body head are provided with all-wing aircraft swivel head, described upper machine body
It is being provided with the 3rd guide wheel group 133 near main shaft side with lower body.
As shown in Figures 2 and 3, it is provided with 2 storage line capstan winches 21, when storage line capstan winch 21 after-combustion wire 101
Time, must adjust all-wing aircraft swivel head 12 to the first guide wheel group 131 and the second guide wheel group 132 not affect and store up line strand
The position of dish 12, locks locking nut 121, carries out wire after-combustion.After after-combustion completes, all-wing aircraft is rotated
12 half-twists, make the first guide wheel group 131 and the second guide wheel group 132 in alignment with the position of storage line capstan winch 21
Putting, lock locking nut 121, wire 101, by first guide wheel group the 131, second guide wheel group 132, passes through
All-wing aircraft body, the 3rd guide wheel group 133, groove 203, in entering main shaft 20 and pull out forward entrance monofilament and open
The systems such as apparatus for adjusting force 23, noseplate 24.Each guide wheel group is formed by 3 guide wheels, so can be simultaneously
3 wires in storage line capstan winch are released.
In storage line capstan winch, the releasing of wire is to be realized by the speed difference of control storage line capstan winch and all-wing aircraft, flies
Swing device, with main axis, wire tension on-line real-time measuremen, feeds back to storage wire system motor and is controlled,
Ensure stablizing of laying tension.Concrete, described twisted wire system is provided with the pressure transducer of detection wire tension.
Described storage line motor controls rotating speed according to pressure transducer feedack, makes to produce between storage line capstan winch and main shaft
Raw speed difference, it is ensured that solid conductor maximum tension 15kg.Storage line motor is by Frequency Converter Control.
Described storage line capstan winch is provided with protective cover, and described protective cover connects travel switch, when protective cover is opened,
Travel switch disconnects.Protective cover acts primarily as safeguard protection effect, and when protective cover is opened, travel switch disconnects,
Complete machine can not start, and when protective cover closes, travel switch closes, and complete machine could start.
Strand belongs to not back twist wire twisting equipment with one heart, is suitable for the strand system of various round wire conductors, due to core after-combustion
On the drum of main shaft, therefore, rotary inertia is minimum, square being directly proportional of rotary inertia and radius, phase
To wire twisting equipments such as the frame winch in past, cage winch, rotary inertia is the most minimum, adds without week favourable turn
With drum, therefore, in the energy consumption of unit product, this product compares minimum.But also solve arbitrarily simultaneously
Phenomenon is laid particular stress on during the unwrapping wire of dish number.Strand body uses concentric type structure (in draw drum center and strand body revolution
The heart overlaps), therefore strand body rotating speed is high, and twisting speed is fast, and production efficiency is high.Built-in drum on equipment, no
Need to have enough to meet the need drum and the handling system of drum.Application multi cord principle, every drum puts three or more
Heart yearn, compact conformation, floor space is little；Strand body is stranded and after-combustion can be carried out individually or simultaneously.Individually enter
OK, device length can be shortened；Carry out simultaneously, substantially reduce downtime.
It addition, this concentric lay conductor machine has single-deck pattern and double plate pattern two kinds.
Single-deck pattern: when single-deck uses, each drum individually controls with an all-wing aircraft, and two drums are simultaneously
Carry out unwrapping wire or after-combustion, twisted wire and after-combustion alternately.After-combustion speed can make production week far above twisted wire speed
Phase is the longest, it is adaptable to strand makes substantial amounts of wire.
Double plate pattern: when double plate uses, all-wing aircraft top guide can with 360 ° rotate and can position correspondence the left side or
The drum on the right carries out unwrapping wire.Drum on one side carries out unwrapping wire, and the drum of another side can carry out in after-combustion simultaneously
Line, twisted wire and after-combustion are carried out simultaneously, and downtime can be made the shortest, and product is the highest.
Concentric lay conductor owner of the present utility model to be formed 4+4+ by 1 section of 2 dish strand body and 3 section of 4 dish strand body
(4+2) production line, 4+2 strand body in its posterior segment is composed in series by 4 dish strand bodies and 2 dishes strand body, shares one
Motor is run simultaneously by ground shaft transmission system, with clutch in drive system, double for 19 heart yearns
Dish pattern is disengagable 2 dish strand body individual operations time stranded.Every section of strand body has a set of after-combustion bus cable device respectively,
By ring type after-combustion pay off rack by wire after-combustion to twisting in internal storage wire system, each storage wire system is
How can 3 wires of after-combustion, separate electrical motor screw mandrel winding displacement.2 dish strand body 2 disk storage lines of suit, 1 group of all-wing aircraft,
4 dish strand body 4 disk storage lines of suit, 2 groups of all-wing aircrafts.Strand body each two disk storage line shares one group of all-wing aircraft, is arranged on
Between two dishes, control 2 disk storage line unwrapping wire.
During stranded 19 cores (1+6+12), use double plate pattern, after-combustion and stranded can simultaneously carry out.By putting
Coil holder ring type releases a heart yearn as centrage；6 core cablings are released 6 lines by first paragraph strand body and are completed
Stranded；12 core cablings are respectively released 6 lines by second segment and the 3rd section of strand body, carry out synchronously completing stranded.
Remaining disk storage line carries out after-combustion the most simultaneously.
During stranded 37 cores (1+6+12+18), using single-deck pattern, after-combustion and stranded needs are carried out respectively.
A heart yearn is released as centrage by pay off rack ring type；6 core cablings are released 6 lines by first paragraph strand body
Complete stranded；12 core cablings are released 12 lines by second segment 4 dish strand body and are completed stranded；18 heart yearns
Stranded being released 12 lines by the 3rd section of strand body, the 4th section of strand body is released 6 lines, is carried out synchronously completing stranded.
Claims (5)
1. a flying-wing device, including the all-wing aircraft body being sleeved on main shaft, it is characterised in that: described all-wing aircraft body
Connect have all-wing aircraft swivel head, described all-wing aircraft swivel head to be rotationally connected with all-wing aircraft body, described all-wing aircraft swivel head and
Being provided with retaining mechanism between all-wing aircraft body, described flying-wing device is provided with all-wing aircraft guide wheel assembly.
A kind of flying-wing device the most according to claim 1, it is characterised in that: described all-wing aircraft head is provided with rotation
Socket, described all-wing aircraft swivel head is provided with rotary connector, and described rotary connector inserts rotary jack.
A kind of flying-wing device the most according to claim 2, it is characterised in that: described rotary connector revolves with all-wing aircraft
Radial transition portion it is provided with, if described retaining mechanism is that radially transition part is circumferentially disposed between rotary head main part
Dry locking nut.
4. according to a kind of flying-wing device described in claims 1 to 3 any one, it is characterised in that: described all-wing aircraft
Swivel head includes runing rest and all-wing aircraft top guide, and described all-wing aircraft top guide is prominent to horizontal outer side, and described all-wing aircraft is led
Wheel assembly includes the first guide wheel group being located on all-wing aircraft top guide and the second guide wheel group being located on runing rest.
A kind of flying-wing device the most according to claim 4, it is characterised in that: described flying-wing device is provided with machine
Body and lower body, described upper machine body and lower body by Hafu-type structural clamp on main shaft, described upper machine body
Being connected by bolt and main shaft are fixing with lower body, described upper machine body and lower body head are provided with all-wing aircraft rotation
Rotary head, described upper machine body and lower body are being provided with the 3rd guide wheel group near main shaft side.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620302407.4U CN205722993U (en) | 2016-04-12 | 2016-04-12 | A kind of flying-wing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620302407.4U CN205722993U (en) | 2016-04-12 | 2016-04-12 | A kind of flying-wing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205722993U true CN205722993U (en) | 2016-11-23 |
Family
ID=57309889
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620302407.4U Active CN205722993U (en) | 2016-04-12 | 2016-04-12 | A kind of flying-wing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205722993U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105741985A (en) * | 2016-04-12 | 2016-07-06 | 浙江晨光电缆股份有限公司 | Flyer device |
| CN118692749A (en) * | 2024-08-23 | 2024-09-24 | 宁波凯特机械有限公司 | Concentric cable stranding machine |
-
2016
- 2016-04-12 CN CN201620302407.4U patent/CN205722993U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105741985A (en) * | 2016-04-12 | 2016-07-06 | 浙江晨光电缆股份有限公司 | Flyer device |
| CN118692749A (en) * | 2024-08-23 | 2024-09-24 | 宁波凯特机械有限公司 | Concentric cable stranding machine |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105719775A (en) | Concentric stranding machine | |
| CN205722992U (en) | A kind of concentric lay conductor machine | |
| CN204596540U (en) | Concentric type stranding machine and twist production line with one heart | |
| CN103413618B (en) | A kind of vertical wire twisting machine of HDMI cable | |
| CN103578652B (en) | Vertical cable former with back-twist control | |
| CN112951516B (en) | Data cable set serial production equipment | |
| CN109378129B (en) | Horizontal winding belting all-in-one | |
| CN103296840B (en) | Wire arranging device of winding machine | |
| CN207090648U (en) | A kind of cable drum carriage | |
| CN206907567U (en) | Wire twisting machine with guide bracket | |
| CN116721813B (en) | Conductor stranding machine capable of eliminating torsion | |
| CN107658070A (en) | A kind of cable cabling machine | |
| CN205722993U (en) | A kind of flying-wing device | |
| CN204189519U (en) | The stranded tube-type line strander of multilayer concentric | |
| CN203174424U (en) | Paying off untwisting device for double twisting machine | |
| CN209843376U (en) | High-speed multi-strand wire stranding machine set | |
| CN105741985A (en) | Flyer device | |
| CN207052378U (en) | A kind of Double-layer vertical belting machine | |
| CN104444580B (en) | A kind of double-deck superfine wrapping machine | |
| CN108053948A (en) | A kind of twisted wire production line of cable and its cable of production | |
| CN106298088B (en) | Concentric type wire twisting machine and production line is twisted with one heart | |
| CN205984437U (en) | Simple lay machine is fired to vertical returning | |
| CN103813867A (en) | An apparatus for filtering out defects in metal wires | |
| CN210735879U (en) | Traction rope reel | |
| CN207375210U (en) | A kind of hauling cage machine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A flying wing device Effective date of registration: 20201203 Granted publication date: 20161123 Pledgee: Dushangang sub branch of Zhejiang Pinghu Rural Commercial Bank Co., Ltd Pledgor: ZHEJIANG CHENGUANG CABLE Co.,Ltd. Registration number: Y2020330001100 |
|
| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210617 Granted publication date: 20161123 Pledgee: Dushangang sub branch of Zhejiang Pinghu Rural Commercial Bank Co., Ltd Pledgor: ZHEJIANG CHENGUANG CABLE Co.,Ltd. Registration number: Y2020330001100 |