CN211846645U - Aerospace is with high temperature resistant installation wire device that winds - Google Patents
Aerospace is with high temperature resistant installation wire device that winds Download PDFInfo
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- CN211846645U CN211846645U CN202020459183.4U CN202020459183U CN211846645U CN 211846645 U CN211846645 U CN 211846645U CN 202020459183 U CN202020459183 U CN 202020459183U CN 211846645 U CN211846645 U CN 211846645U
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- 238000009434 installation Methods 0.000 title claims abstract description 29
- 238000004804 winding Methods 0.000 claims abstract description 89
- 230000005540 biological transmission Effects 0.000 claims description 12
- 230000000712 assembly Effects 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 abstract description 30
- 238000005096 rolling process Methods 0.000 abstract description 20
- 230000000694 effects Effects 0.000 description 5
- 239000011148 porous material Substances 0.000 description 2
- 230000001360 synchronised effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
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Abstract
The utility model discloses an aerospace is with high temperature resistant around package installation wire device, including bottom plate and motor, two risers of the upper end fixedly connected with of bottom plate, motor fixed mounting is on the lateral wall of one riser wherein, the same diaphragm of fixedly connected with between two risers, be equipped with same winding mechanism between two risers, the lower extreme of diaphragm be equipped with winding mechanism assorted winding displacement mechanism, winding displacement mechanism's drive end and winding mechanism's drive end all rotate run through with motor fixed connection's riser setting, winding displacement mechanism's drive end and the terminal fixed connection of output shaft of motor, be equipped with same drive mechanism between winding mechanism's drive end and the output shaft of motor. The utility model discloses can not only carry out winding displacement and rolling around the package mounting wire to aerospace with high temperature resistant effectively, can also reduce aerospace with high temperature resistant friction that produces when winding package mounting wire winding displacement and rolling effectively.
Description
Technical Field
The utility model relates to a wire and cable wire winding technical field especially relates to an aerospace is with high temperature resistant around package installation wire device.
Background
The aerospace technology is a series of advanced and complex construction operation procedures, and relates to the severe academic operation such as equipment and instrument assembly, installation and use, and the like, because of the special working environment of aerospace, the requirement on the aerospace wire and cable is very high, and the requirement has the performances of high transmission type, high and low temperature resistance and the like, if the high-temperature-resistant winding installation wire is a wire and cable frequently used in aerospace, the aerospace high-temperature-resistant winding installation wire is frequently required to be wound in the production process, and a general winding device does not have the wire arranging function, or the friction generated on the wire and cable during wire arrangement is large, so that the wire and cable is easily damaged.
Most of aerospace high-temperature-resistant wrapping installation wire devices used in the market can not effectively wind and arrange wires of aerospace high-temperature-resistant wrapping installation wires, and can not effectively reduce friction generated when the aerospace high-temperature-resistant wrapping installation wires are wound and arranged.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving among the prior art aerospace with high temperature resistant around package installation wire device can not carry out rolling and winding displacement processing around the package installation wire to aerospace with high temperature resistant most effectively, and can not reduce the phenomenon of the friction that aerospace produced when package installation wire rolling and winding displacement are wound with high temperature resistant effectively, and the aerospace with high temperature resistant around package installation wire device that proposes, it can not only carry out winding displacement and rolling around package installation wire to aerospace with high temperature resistant effectively, can also reduce the friction that aerospace produced when package installation wire winding displacement and rolling with high temperature resistant effectively.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides an aerospace is with high temperature resistant around package mounting wire device, includes bottom plate and motor, two risers of the upper end fixedly connected with of bottom plate, motor fixed mounting is on the lateral wall of one riser wherein, two the same diaphragm of fixedly connected with between the riser, two be equipped with same winding mechanism between the riser, the lower extreme of diaphragm be equipped with winding mechanism assorted winding displacement mechanism, winding displacement mechanism's drive end and winding mechanism's drive end all rotate run through with motor fixed connection's riser setting, winding displacement mechanism's drive end and the terminal fixed connection of output shaft of motor, be equipped with same drive mechanism between winding mechanism's drive end and the output shaft of motor.
Preferably, winding mechanism is including rotating the same wind-up roll of connecting on two riser relative lateral walls, the one end of wind-up roll rotate run through with motor fixed connection's riser setting and with drive mechanism fixed connection, be located two coaxial fixedly connected with polylith limiting plate on the wind-up roll between the riser, winding mechanism's setting has realized the rolling effect to aerospace with high temperature resistant package assembly line.
Preferably, winding displacement mechanism is including setting up in a plurality of spouts of diaphragm lower extreme, and is a plurality of all be equipped with assorted slider with it in the spout, the polylith the slider all communicates on the part that is located outside the spout and is equipped with the rectangular hole, and is a plurality of equal fixedly connected with slip subassembly all around the inner wall of rectangular hole, and is a plurality of it has same root reciprocating lead screw to run through to rotate on the spout, reciprocating lead screw's one end is rotated run through with motor fixed connection's riser setting and with the output shaft end fixed connection of motor, winding displacement mechanism's setting has realized the winding displacement effect when winding the mounting wire rolling to aerospace with high temperature resistant, and it has improved the degree of consistency when winding the mounting wire rolling with high temperature resistant effectively.
Preferably, drive mechanism includes two respectively with motor output shaft and wind-up roll fixed connection's belt pulley, two drive connection through same root belt between the belt pulley, drive mechanism's setting has improved the utilization ratio to the motor.
Preferably, the sliding assembly comprises a fixed pulley fixedly connected to the inner wall of the rectangular hole, an arc-shaped groove is formed in the side wall of the wheel body of the fixed pulley, and friction generated during winding and arranging of the high-temperature-resistant winding installation wire for aerospace is effectively reduced due to the arrangement of the sliding assembly.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses a set up bottom plate, motor, riser, diaphragm, wind-up roll, limiting plate, spout, slider, rectangular hole, slip subassembly, reciprocal lead screw and belt pulley etc. realized with high temperature resistant winding package mounting wire and winding displacement effect to aerospace, wherein the setting of winding displacement mechanism has improved the degree of consistency when aerospace is with high temperature resistant winding package mounting wire rolling effectively, and drive mechanism's setting has improved the utilization ratio of motor in addition.
2. The utility model discloses a set up bottom plate, motor, riser, diaphragm, wind-up roll, limiting plate, spout, slider, rectangular hole, slip subassembly, reciprocal lead screw and belt pulley etc. reduced the friction that produces effectively when aerospace is with high temperature resistant winding package mounting wire rolling and winding displacement, and then reduced effectively the aerospace with high temperature resistant damage that causes when winding package mounting wire rolling and winding displacement.
Drawings
Fig. 1 is a perspective view of a high temperature resistant winding installation wire device for aerospace use according to the present invention;
fig. 2 is a schematic view of an external structure of a high temperature resistant winding installation wire device for aerospace use according to the present invention;
fig. 3 is a partially enlarged view of a portion a of fig. 1.
In the figure: the winding machine comprises a base plate 1, a motor 2, a vertical plate 3, a transverse plate 4, a winding roller 5, a limiting plate 6, a sliding chute 7, a sliding block 8, a rectangular hole 9, a sliding assembly 10, a reciprocating screw rod 11, a belt pulley 12, a belt 13, a fixed pulley 14 and an arc-shaped groove 15.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments.
Referring to fig. 1-3, a high temperature resistant package installation wire device for aerospace, including bottom plate 1 and motor 2, two risers 3 of upper end fixedly connected with of bottom plate 1, motor 2 fixed mounting is on the lateral wall of one riser 3 among them, the same diaphragm 4 of fixedly connected with between two risers 3, be equipped with same winding mechanism between two risers 3, the lower extreme of diaphragm 4 is equipped with winding mechanism assorted winding displacement mechanism, the drive end of winding displacement mechanism and the drive end of winding mechanism all rotate run through with motor 2 fixed connection's riser 3 setting, the drive end of winding displacement mechanism and the terminal fixed connection of output shaft of motor 2, be equipped with same drive mechanism between the drive end of winding mechanism and the output shaft of motor 2.
The winding mechanism comprises the same winding roller 5 which is rotatably connected on the opposite side walls of two vertical plates 3, one end of the winding roller 5 is rotatably arranged to penetrate through the vertical plate 3 fixedly connected with the motor 2 and fixedly connected with the transmission mechanism, a plurality of limiting plates 6 are coaxially and fixedly connected on the winding roller 5 positioned between the two vertical plates 3, the winding mechanism is arranged to realize the winding effect on the high-temperature-resistant winding installation line for aerospace, the winding mechanism comprises a plurality of chutes 7 arranged at the lower end of a transverse plate 4, sliding blocks 8 matched with the chutes 7 are arranged in the chutes 7, rectangular holes 9 are respectively communicated with the parts of the sliding blocks 8 positioned outside the chutes 7, sliding components 10 are respectively and fixedly connected around the inner walls of the rectangular holes 9, the same reciprocating screw rod 11 is rotatably arranged to penetrate through the chutes 7, one end of the reciprocating screw rod 11 is rotatably arranged to penetrate through the vertical plate 3 fixedly connected with the motor 2 and fixedly connected with the tail end of an output shaft of, the setting of winding displacement mechanism has realized the winding displacement effect when rolling up aerospace with high temperature resistant package installation wire, and it has improved the degree of consistency when aerospace is with high temperature resistant package installation wire rolling effectively, need explain that be equipped with wire and cable tension adjusting equipment (not shown in the figure) between winding displacement mechanism and the winding mechanism, wire and cable tension adjusting equipment can adjust the tension when rolling up wire and cable winding displacement effectively, and this is prior art, no longer gives unnecessary details here.
The transmission mechanism comprises two belt pulleys 12 respectively fixedly connected with an output shaft of the motor 2 and the winding roller 5, the two belt pulleys 12 are in transmission connection through a same belt 13, the transmission mechanism is arranged, the utilization rate of the motor is improved, it needs to be explained that the diameter ratio of the two belt pulleys 12 on the transmission mechanism can be adjusted, the diameter ratio can be selected according to needs, the diameter ratio is the prior art and is not repeated, the sliding component 10 comprises a fixed pulley 14 fixedly connected on the inner wall of the rectangular hole 9, an arc-shaped groove 15 is arranged on the side wall of a wheel body of the fixed pulley 14, the arrangement of the sliding component 10 effectively reduces the friction generated during winding and winding of the high-temperature-resistant winding installation wire for aerospace, it needs to be explained that, as shown in figure 3, one side opposite to a plurality of arc-shaped grooves 15 on the same sliding component 10 is integrally arranged in a circular shape, thereby form circular pore, when the cable passed circular pore and when removing, the wheel body on a plurality of fixed pulleys 14 all can rotate along with it, and then received friction when having reduced wire and cable rolling and winding displacement effectively, it should explain that, a plurality of spouts 7 are equallyd divide respectively and are corresponded the setting with the part of wind-up roll 5 between two adjacent limiting plates 6, and then the device of being convenient for carries out synchronous rolling to many wire and cable.
It should be noted that, the reciprocating screw rod 11 is provided with a plurality of sections of threads which are arranged in one-to-one correspondence with the plurality of sliding chutes 7, and the threads are arranged in sections, so that when the reciprocating screw rod 11 rotates, the plurality of sliding blocks 8 respectively move horizontally in the corresponding sliding chutes 7 in a reciprocating manner.
In the utility model, when the aerospace high temperature resistant wrapping installation wire needs to be rolled, as shown in fig. 3, one end of the cable is arranged through a circular hole formed on one of the sliding components 10, and one end of the cable passing through the circular hole is arranged through a wire and cable tension adjusting device (not shown in the figure), the wire and cable tension adjusting device can effectively adjust the tension when the wire and cable is rolled and wound, which is the prior art, and is not repeated herein, finally, one end of the cable passing through the wire and cable tension adjusting device is fixed and wound on the winding roller 5 between two corresponding limiting plates 6, after the cable is fixed, the motor 2 and the wire and cable tension adjusting device are started to work, the motor 2 rotates to drive the reciprocating screw rod 11 to rotate, and the transmission mechanism transmits, the reciprocating screw rod 11 rotates to enable a plurality of sliders 8 to horizontally reciprocate in the corresponding sliding chute 7 along the reciprocating screw rod 11, and then drive the cable and be horizontal reciprocating motion, carry out even winding displacement, drive mechanism's transmission makes wind-up roll 5 rotate, and wind-up roll 5 rotates the cable after the winding displacement and carries out even rolling, is equipped with a plurality of spouts 7 in the device, and a plurality of spouts 7 equally divide do not correspond the setting with the part of wind-up roll 5 between two adjacent limiting plates 6, and then the device of being convenient for carries out synchronous rolling and winding displacement to many electric wire and cable to the efficiency of cable rolling has been improved to the device.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.
Claims (5)
1. A high-temperature-resistant lapping and mounting wire device for aerospace comprises a bottom plate (1) and a motor (2), it is characterized in that the upper end of the bottom plate (1) is fixedly connected with two vertical plates (3), the motor (2) is fixedly arranged on the side wall of one vertical plate (3), the same transverse plate (4) is fixedly connected between the two vertical plates (3), the same winding mechanism is arranged between the two vertical plates (3), the lower end of the transverse plate (4) is provided with a wire arranging mechanism matched with the winding mechanism, the driving end of the wire arranging mechanism and the driving end of the winding mechanism are both rotatably arranged through a vertical plate (3) fixedly connected with the motor (2), the driving end of the winding mechanism is fixedly connected with the tail end of the output shaft of the motor (2), and the same transmission mechanism is arranged between the driving end of the winding mechanism and the output shaft of the motor (2).
2. The aerospace high temperature resistant winding installation wire device according to claim 1, wherein the winding mechanism comprises a same winding roller (5) rotatably connected to opposite side walls of two risers (3), one end of the winding roller (5) is rotated to run through the riser (3) fixed connected with the motor (2) and is fixedly connected with the transmission mechanism, and is located two coaxial fixed connection multiple limiting plates (6) are arranged on the winding roller (5) between the risers (3).
3. The aerospace high-temperature-resistant winding installation wire device according to claim 1, wherein the wire arranging mechanism comprises a plurality of sliding grooves (7) formed in the lower end of the transverse plate (4), sliding blocks (8) matched with the sliding grooves are arranged in the sliding grooves (7), a plurality of sliding blocks (8) are communicated with parts, located outside the sliding grooves (7), of the sliding blocks (8) to form rectangular holes (9), sliding assemblies (10) are fixedly connected to the periphery of the inner wall of each rectangular hole (9), a plurality of reciprocating screw rods (11) penetrate through the sliding grooves (7) in a rotating mode, and one ends of the reciprocating screw rods (11) penetrate through vertical plates (3) fixedly connected with the motor (2) in a rotating mode and are fixedly connected with the tail ends of output shafts of the motor (2).
4. The aerospace high-temperature-resistant winding installation wire device according to claim 2, wherein the transmission mechanism comprises two belt pulleys (12) fixedly connected with an output shaft of the motor (2) and the winding roller (5), and the two belt pulleys (12) are in transmission connection through the same belt (13).
5. The aerospace high temperature resistant winding installation wire device according to claim 3, wherein the sliding assembly (10) comprises a fixed pulley (14) fixedly connected to the inner wall of the rectangular hole (9), and an arc-shaped groove (15) is formed in the side wall of a wheel body of the fixed pulley (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020459183.4U CN211846645U (en) | 2020-04-01 | 2020-04-01 | Aerospace is with high temperature resistant installation wire device that winds |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020459183.4U CN211846645U (en) | 2020-04-01 | 2020-04-01 | Aerospace is with high temperature resistant installation wire device that winds |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211846645U true CN211846645U (en) | 2020-11-03 |
Family
ID=73144258
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020459183.4U Expired - Fee Related CN211846645U (en) | 2020-04-01 | 2020-04-01 | Aerospace is with high temperature resistant installation wire device that winds |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211846645U (en) |
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2020
- 2020-04-01 CN CN202020459183.4U patent/CN211846645U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201103 |
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| CF01 | Termination of patent right due to non-payment of annual fee |