CN210796229U - Shock-absorbing structure of head assembly of glass fiber drawing machine - Google Patents

Shock-absorbing structure of head assembly of glass fiber drawing machine Download PDF

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Publication number
CN210796229U
CN210796229U CN201921719026.6U CN201921719026U CN210796229U CN 210796229 U CN210796229 U CN 210796229U CN 201921719026 U CN201921719026 U CN 201921719026U CN 210796229 U CN210796229 U CN 210796229U
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Prior art keywords
head assembly
assembly
shock
machine head
damping
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CN201921719026.6U
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Chinese (zh)
Inventor
李斌
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Wuyi Yongxin Glass Fiber Machinery Manufacturing Co ltd
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Wuyi Yongxin Glass Fiber Machinery Manufacturing Co ltd
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Priority to CN201921719026.6U priority Critical patent/CN210796229U/en
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Abstract

The utility model discloses a fine wire drawing machine head assembly's of glass shock-absorbing structure, including an at least set of head assembly, be provided with two sets of damper on head assembly's the axis at least, this application is provided with at least two sets of damper on head assembly, has strengthened head assembly's shock attenuation intensity greatly, and simple structure, reasonable in design.

Description

Shock-absorbing structure of head assembly of glass fiber drawing machine
Technical Field
The utility model belongs to the technical field of the fine wire drawing machine of glass, concretely relates to fine wire drawing machine head assembly's of glass shock-absorbing structure.
Background
The aircraft nose subassembly of fine wire drawing machine of glass includes the aircraft nose, the aircraft nose main shaft is connected to the aircraft nose, still include the carousel, a wire drawing machine generally is provided with two sets of aircraft nose subassemblies, convenient change is used, wherein, the aircraft nose main shaft is connected on the carousel, its rear end is unsettled state, because in the production process, the rotation of aircraft nose must lead to the vibrations of aircraft nose, therefore, must be provided with shock-absorbing structure on the aircraft nose, current shock-absorbing structure only sets up the shock attenuation ring in aircraft nose main shaft and carousel junction, if the length of aircraft nose is longer, the shock attenuation dynamics of this shock attenuation ring is just not enough, lead to equipment operation trouble.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a fine wire drawing machine head assembly's of glass shock-absorbing structure has solved the defect that above-mentioned wire drawing machine head assembly shock attenuation exists among the prior art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides a fine wire drawing machine head assembly's shock-absorbing structure of glass, includes at least a set of head assembly, be provided with two sets of shock-absorbing component on head assembly's the axis at least.
Preferably, the machine head assembly comprises a set of machine head assembly, a first damping assembly and a second damping assembly are arranged on the machine head assembly, the first damping assembly and the second damping assembly are consistent in structure and respectively comprise a fixed seat, and the fixed seat is sleeved outside the machine head assembly.
Preferably, a first damping ring is arranged between the fixed seat and the handpiece assembly.
Preferably, including two sets of aircraft nose subassemblies of symmetry setting and on the carousel, the aircraft nose subassembly is provided with third damper assembly with the junction of carousel, be provided with fourth damper assembly on aircraft nose subassembly's the end.
Preferably, the third damping assembly is sleeved on a second damping ring between the head assemblies and the turntable, the fourth damping assembly comprises a retainer, two ends of the retainer are respectively and fixedly connected to the end parts of the two groups of head assemblies, and the middle part of the retainer is fixed on a main shaft of the turntable.
Preferably, a third damping ring is arranged between the head assembly and the retainer.
Compared with the prior art, the beneficial effects of the utility model are that:
this application is provided with at least two sets of damper assembly on the aircraft nose subassembly, has strengthened aircraft nose subassembly's shock attenuation intensity greatly, and simple structure, reasonable in design.
Drawings
Fig. 1 is a schematic structural diagram of embodiment 1 of the present invention;
fig. 2 is a schematic structural diagram of embodiment 2 of the present invention.
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. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Example 1
As shown in fig. 1-2, the utility model provides a fine wire drawing machine head assembly's of glass shock-absorbing structure, including at least a set of head assembly 1, be provided with two sets of damper on head assembly's the axis at least, including a set of head assembly, be provided with first damper 2 and second damper 3 on the head assembly, first damper with second damper's structure is unanimous, all includes a fixing base 4, the fixing base cup joint in head assembly's outside, be provided with first damping ring (not shown) between fixing base and the head assembly.
Example 2
The difference from example 1 is that: including the symmetry set up with two sets of head assembly on the carousel, the junction of head assembly and carousel is provided with third damper assembly, two be provided with fourth damper assembly on head assembly's the end, third damper assembly cup joint in second damping ring 5 between head assembly and the carousel, fourth damper assembly includes holder 6, on the both ends of holder fixed connection two sets of head assembly's tip respectively, the middle part of holder is fixed on carousel main shaft 7, be provided with third damping ring 8 between head assembly and the holder.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications and variations can be made in the embodiments or in part of the technical features of the embodiments without departing from the spirit and the scope of the invention.

Claims (6)

1. The utility model provides a fine wire drawing machine head assembly's shock-absorbing structure of glass which characterized in that: the damping device comprises at least one group of head assembly, wherein at least two groups of damping assemblies are arranged on the axis of the head assembly.
2. The shock-absorbing structure of the glass fiber drawing machine head assembly according to claim 1, characterized in that: the first damping assembly and the second damping assembly are arranged on the machine head assembly, the first damping assembly and the second damping assembly are consistent in structure and respectively comprise a fixed seat, and the fixed seat is sleeved outside the machine head assembly.
3. The shock-absorbing structure of the glass fiber drawing machine head assembly according to claim 2, characterized in that: a first damping ring is arranged between the fixed seat and the machine head assembly.
4. The shock-absorbing structure of the glass fiber drawing machine head assembly according to claim 1, characterized in that: including the symmetry set up with two sets of head assembly on the carousel, the junction of head assembly and carousel is provided with third damper assembly, be provided with fourth damper assembly on head assembly's the end.
5. The shock-absorbing structure of the glass fiber drawing machine head assembly according to claim 4, characterized in that: the third damping assembly is sleeved on a second damping ring between the machine head assemblies and the rotary table, the fourth damping assembly comprises a retainer, two ends of the retainer are respectively and fixedly connected to the end parts of the two groups of machine head assemblies, and the middle part of the retainer is fixed on the main shaft of the rotary table.
6. The shock-absorbing structure of the glass fiber drawing machine head assembly according to claim 5, characterized in that: and a third damping ring is arranged between the machine head assembly and the retainer.
CN201921719026.6U 2019-10-14 2019-10-14 Shock-absorbing structure of head assembly of glass fiber drawing machine Active CN210796229U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201921719026.6U CN210796229U (en) 2019-10-14 2019-10-14 Shock-absorbing structure of head assembly of glass fiber drawing machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201921719026.6U CN210796229U (en) 2019-10-14 2019-10-14 Shock-absorbing structure of head assembly of glass fiber drawing machine

Publications (1)

Publication Number Publication Date
CN210796229U true CN210796229U (en) 2020-06-19

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201921719026.6U Active CN210796229U (en) 2019-10-14 2019-10-14 Shock-absorbing structure of head assembly of glass fiber drawing machine

Country Status (1)

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CN (1) CN210796229U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115504664A (en) * 2021-06-23 2022-12-23 武义永新玻纤机械制造有限公司 Glass fiber drawing machine capable of improving stability

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115504664A (en) * 2021-06-23 2022-12-23 武义永新玻纤机械制造有限公司 Glass fiber drawing machine capable of improving stability
CN115504664B (en) * 2021-06-23 2023-07-21 武义永新玻纤机械制造有限公司 Glass fiber wire drawing machine capable of improving stability

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