CN109252263A - Combined ceramic navel - Google Patents

Combined ceramic navel Download PDF

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Publication number
CN109252263A
CN109252263A CN201811292338.3A CN201811292338A CN109252263A CN 109252263 A CN109252263 A CN 109252263A CN 201811292338 A CN201811292338 A CN 201811292338A CN 109252263 A CN109252263 A CN 109252263A
Authority
CN
China
Prior art keywords
intermediate member
circumferential periphery
component
navel
periphery component
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Withdrawn
Application number
CN201811292338.3A
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Chinese (zh)
Inventor
刘光容
朱爱萍
朱曰春
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shaoxing Huayu Textile Machinery Co Ltd
Original Assignee
Shaoxing Huayu Textile Machinery Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shaoxing Huayu Textile Machinery Co Ltd filed Critical Shaoxing Huayu Textile Machinery Co Ltd
Priority to CN201811292338.3A priority Critical patent/CN109252263A/en
Publication of CN109252263A publication Critical patent/CN109252263A/en
Withdrawn legal-status Critical Current

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Classifications

    • DTEXTILES; PAPER
    • D02YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
    • D02GCRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
    • D02G1/00Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics
    • D02G1/02Producing crimped or curled fibres, filaments, yarns, or threads, giving them latent characteristics by twisting, fixing the twist and backtwisting, i.e. by imparting false twist
    • D02G1/04Devices for imparting false twist

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Ceramic Products (AREA)

Abstract

The present invention relates to a kind of Combined ceramic navels, belong to textile technology field, including connecting integral intermediate member and circumferential periphery component, after which is individually made, reconnect integral.The present invention is final to realize rotary inertia caused by the navel for reducing the rotation of production process high speed to achieve the purpose that effectively to mitigate ceramic navel weight by the way that the different intermediate member of specific gravity and circumferential periphery component to be combined.

Description

Combined ceramic navel
Technical field
The present invention relates to a kind of Combined ceramic navels, belong to textile technology field.
Background technique
Ceramic navel is key part in disk type scroll tube component on chemical fibre elasticizer.In prior art, ceramics Navel is often made of monolithic ceramic material, and in up to 20000 revs/min of high speed rotation, chemical fiber wire is processed into The weaving silk of excellent spring.Since monolithic ceramic navel weight ratio is heavier, rotary inertia is just very big when high speed rotation, center The load that bearing is received is just big, is also easy to produce abrasion and influences to run well.To solve this problem, thus this case generates.
Summary of the invention
For the weight for effectively mitigating ceramic navel, improve the operating condition of disk type scroll tube, the present invention provides one Kind Combined ceramic navel.
In order to achieve the above objectives, the technical scheme adopted by the invention is as follows:
A kind of Combined ceramic navel, including intermediate member and circumferential periphery component, after which is individually made, It reconnects integral.
As the further setting of above-metioned scheme, the intermediate member is that (i.e. intermediate member selects gold to metal intermediate member Belong to material to be made) or non-metallic intermediate element (i.e. intermediate member selects nonmetallic materials to be made).The raw material of intermediate member selects The ceramic material that specific gravity makes navel compared to the prior art is light.
The intermediate member is by aluminium alloy intermediate member (i.e. intermediate member selects aluminium alloy to be made).Intensity of aluminum alloy height, Light specific gravity.
The circumferential periphery component is by ceramic excircle circumferential component (i.e. circumferential periphery component Ceramics material is made).
The circumferential periphery component is that (i.e. circumferential periphery component selects toughening oxygen to reinforced alumina ceramic circumferential periphery component Change aluminium ceramic material to be made).
It is integral using mechanical structure connection between the intermediate member and circumferential periphery component, or be bonded using colloid It is integral or integral using mechanical structure association colloid bonding connection.
Faying face between the intermediate member and circumferential periphery component is stepped or planar, and intermediate member with Colloid is coated between the faying face of circumferential periphery component.
Faying face between the intermediate member and circumferential periphery component is stepped, and intermediate member and circumferential periphery Colloid is coated between the faying face of component, meanwhile, by intermediate member at the inner wall port of the big bottom surface side of circumferential periphery component It withholds ipsilateral bottom surface.
Faying face between the intermediate member and circumferential periphery component is stepped, and intermediate member and circumferential periphery It is bolted between component.
Faying face between the intermediate member and circumferential periphery component is stepped, the big bottom surface side of circumferential periphery component Inner wall port at withheld by the ipsilateral bottom surface of intermediate member.
Navel in the prior art is resolved into middle section and circumferential periphery two by Combined ceramic navel of the present invention Part after the two parts are individually made, reconnects integral.The present invention is by by the different intermediate member of specific gravity and outer circle Circumferential component is combined, and to achieve the purpose that effectively to mitigate ceramic navel weight, final realization reduces high in production process Rotary inertia caused by the navel of speed rotation.
Below in conjunction with the drawings and specific embodiments, the invention will be further described.
Detailed description of the invention
Fig. 1 is the structural diagram of the present invention one;
Fig. 2 is structural schematic diagram two of the invention;
Fig. 3 is structural schematic diagram three of the invention;
Fig. 4 is structural schematic diagram four of the invention;
Fig. 5 is structural schematic diagram five of the invention.
Specific embodiment
Embodiment 1
Combined ceramic navel of the present invention, including connecting integral intermediate member 1 and circumferential periphery component 2.Two portions After part is individually made, reconnect integral.
Intermediate member 1 is aluminium alloy intermediate member.
Circumferential periphery component 2 is ceramic excircle circumferential component.In the present embodiment, circumferential periphery component 2 is preferably toughening oxygen Change aluminium ceramic excircle circumferential component.
It is integral that mechanical structure connection can be used between intermediate member 1 and circumferential periphery component 2, colloid bonding can also be used It is integral, it is integral that mechanical structure association colloid bonding connection also can be used.
It is Nian Jie integral using colloid between intermediate member 1 and circumferential periphery component 2 in the present embodiment, specific as follows:
As shown in connection with fig. 1, the faying face between intermediate member 1 and circumferential periphery component 2 is stepped, and intermediate member 1 and outer Colloid 3 is coated between the faying face of circumferential edge component 2.
Certainly, the faying face between intermediate member 1 and circumferential periphery component 2 can also be in planar, as shown in Figure 2.
Embodiment 2
Combined ceramic navel of the present invention, including connecting integral intermediate member 1 and circumferential periphery component 2.Two portions After part is individually made, reconnect integral.
Intermediate member 1 is aluminium alloy intermediate member.
Circumferential periphery component 2 is ceramic excircle circumferential component.In the present embodiment, circumferential periphery component 2 is preferably toughening oxygen Change aluminium ceramic excircle circumferential component.
It is integral that mechanical structure connection can be used between intermediate member 1 and circumferential periphery component 2, colloid bonding can also be used It is integral, it is integral that mechanical structure association colloid bonding connection also can be used.
It is integral using mechanical structure connection between intermediate member 1 and circumferential periphery component 2 in the present embodiment, specifically such as Under:
As shown in connection with fig. 3, the faying face between intermediate member 1 and circumferential periphery component 2 is stepped, and intermediate member 1 and outer (for clearer expression structure, bolt is not shown) is bolted between circumferential edge component 2.In the present embodiment, It is provided with screw hole 4 on intermediate member 1, through-hole 5 and counter sink 6 are provided on circumferential periphery component 2, bolt passes through screw hole 4, through-hole 5 and counter sink 6 intermediate member 1 is fixedly connected with circumferential periphery component 2.
Embodiment 3
Combined ceramic navel of the present invention, including connecting integral intermediate member 1 and circumferential periphery component 2.Two portions After part is individually made, reconnect integral.
Intermediate member 1 is aluminium alloy intermediate member.
Circumferential periphery component 2 is ceramic excircle circumferential component.In the present embodiment, circumferential periphery component 2 is preferably toughening oxygen Change aluminium ceramic excircle circumferential component.
It is integral that mechanical structure connection can be used between intermediate member 1 and circumferential periphery component 2, colloid bonding can also be used It is integral, it is integral that mechanical structure association colloid bonding connection also can be used.
It is integral using mechanical structure connection between intermediate member 1 and circumferential periphery component 2 in the present embodiment, specifically such as Under:
As shown in connection with fig. 4, the faying face between intermediate member 1 and circumferential periphery component 2 is stepped, and circumferential periphery component 2 is big It is withheld at the inner wall port of bottom surface side by the ipsilateral bottom surface of intermediate member 1, is to be accomplished by the following way in the present embodiment: Chamfering 7 is set on circumferential periphery component 2, the calendering of aluminium alloy intermediate member is entered, to realize the external circumferential edge of intermediate member 1 The left-hand thread of component 2.
Embodiment 4
Combined ceramic navel of the present invention, including connecting integral intermediate member 1 and circumferential periphery component 2.Two portions After part is individually made, reconnect integral.
Intermediate member 1 is aluminium alloy intermediate member.
Circumferential periphery component 2 is ceramic excircle circumferential component.In the present embodiment, circumferential periphery component 2 is preferably toughening oxygen Change aluminium ceramic excircle circumferential component.
It is integral that mechanical structure connection can be used between intermediate member 1 and circumferential periphery component 2, colloid bonding can also be used It is integral, it is integral that mechanical structure association colloid bonding connection also can be used.
In the present embodiment, between intermediate member 1 and circumferential periphery component 2 using mechanical structure association colloid bonding connection at It is whole, specific as follows:
As shown in connection with fig. 5, the faying face between intermediate member 1 and circumferential periphery component 2 is stepped, and intermediate member 1 and outer Colloid 3 is coated between the faying face of circumferential edge component 2.Meanwhile at the inner wall port of the big bottom surface side of circumferential periphery component 2 in Between the ipsilateral bottom surface of component 1 withhold, be to be accomplished by the following way in the present embodiment: setting is fallen on outer circumferential edge component 2 The calendering of aluminium alloy intermediate member is entered at angle 7, to realize the left-hand thread of the circumferential component 2 to foreign round of intermediate member 1.
Above-described embodiment is only used for illustrating inventive concept of the invention, rather than the restriction to rights protection of the present invention, It is all to be made a non-material change to the present invention using this design, protection scope of the present invention should all be fallen into.

Claims (10)

1. a kind of Combined ceramic navel, it is characterised in that: including intermediate member and circumferential periphery component, two components point After separately made, reconnect integral.
2. Combined ceramic navel as described in claim 1, it is characterised in that: the intermediate member is metal intermediate member Or non-metallic intermediate element.
3. Combined ceramic navel as claimed in claim 2, it is characterised in that: the intermediate member is aluminium alloy middle part Part.
4. the Combined ceramic navel as described in claims 1 or 2 or 3, it is characterised in that: the circumferential periphery component is pottery Porcelain circumferential periphery component.
5. Combined ceramic navel as claimed in claim 4, it is characterised in that: the circumferential periphery component is toughening oxidation Aluminium ceramic excircle circumferential component.
6. Combined ceramic navel as described in claim 1, it is characterised in that: the intermediate member and excircle edge It is integral using mechanical structure connection between part or integral using colloid bonding, or be bonded using mechanical structure association colloid It connects integral.
7. Combined ceramic navel as claimed in claim 6, it is characterised in that: the intermediate member and excircle edge Faying face between part is stepped or planar, and glue is coated between intermediate member and the faying face of circumferential periphery component Body.
8. Combined ceramic navel as claimed in claim 6, it is characterised in that: the intermediate member and excircle edge Faying face between part is stepped, and colloid is coated between intermediate member and the faying face of circumferential periphery component, meanwhile, outside It is withheld at the inner wall port of circumferential edge component outsole surface side by the ipsilateral bottom surface of intermediate member.
9. Combined ceramic navel as claimed in claim 6, it is characterised in that: the intermediate member and excircle edge Faying face between part is stepped, and is bolted between intermediate member and circumferential periphery component.
10. Combined ceramic navel as claimed in claim 6, it is characterised in that: the intermediate member and circumferential periphery Faying face between component is stepped, by the ipsilateral bottom surface of intermediate member at the inner wall port of the big bottom surface side of circumferential periphery component It withholds.
CN201811292338.3A 2018-11-01 2018-11-01 Combined ceramic navel Withdrawn CN109252263A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201811292338.3A CN109252263A (en) 2018-11-01 2018-11-01 Combined ceramic navel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201811292338.3A CN109252263A (en) 2018-11-01 2018-11-01 Combined ceramic navel

Publications (1)

Publication Number Publication Date
CN109252263A true CN109252263A (en) 2019-01-22

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CN201811292338.3A Withdrawn CN109252263A (en) 2018-11-01 2018-11-01 Combined ceramic navel

Country Status (1)

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CN (1) CN109252263A (en)

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2056884A (en) * 1979-08-07 1981-03-25 Vogt G Coatings on textile machinery
JPH06184849A (en) * 1992-12-15 1994-07-05 Yamauchi Corp Frictional false twisting disc
JPH0941230A (en) * 1995-07-25 1997-02-10 Nitta Ind Corp Disk for frictional false twisting
JPH09256232A (en) * 1996-03-21 1997-09-30 Chichibu Onoda Cement Corp False-twisting disk
JPH10102332A (en) * 1996-09-25 1998-04-21 Murata Mach Ltd Disk unit
GB9809671D0 (en) * 1998-05-06 1998-07-01 Heberlein Fibertechnology Inc Twist disc and process for producing a twist disc
JP2001073240A (en) * 1999-08-31 2001-03-21 Kyocera Corp Drawing and false-twisting disk and drawing and false- twisting machine using the same
US20070012019A1 (en) * 2002-08-06 2007-01-18 Akira Suzuki Disk for temporary twisting
CN201136929Y (en) * 2007-11-21 2008-10-22 四川福斯表面技术有限公司 False twisting friction disc
JP2017115268A (en) * 2015-12-25 2017-06-29 京セラ株式会社 Disc for false-twisting machine

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2056884A (en) * 1979-08-07 1981-03-25 Vogt G Coatings on textile machinery
JPH06184849A (en) * 1992-12-15 1994-07-05 Yamauchi Corp Frictional false twisting disc
JPH0941230A (en) * 1995-07-25 1997-02-10 Nitta Ind Corp Disk for frictional false twisting
JPH09256232A (en) * 1996-03-21 1997-09-30 Chichibu Onoda Cement Corp False-twisting disk
JPH10102332A (en) * 1996-09-25 1998-04-21 Murata Mach Ltd Disk unit
GB9809671D0 (en) * 1998-05-06 1998-07-01 Heberlein Fibertechnology Inc Twist disc and process for producing a twist disc
JP2001073240A (en) * 1999-08-31 2001-03-21 Kyocera Corp Drawing and false-twisting disk and drawing and false- twisting machine using the same
US20070012019A1 (en) * 2002-08-06 2007-01-18 Akira Suzuki Disk for temporary twisting
CN201136929Y (en) * 2007-11-21 2008-10-22 四川福斯表面技术有限公司 False twisting friction disc
JP2017115268A (en) * 2015-12-25 2017-06-29 京セラ株式会社 Disc for false-twisting machine

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
朱军,赵建明: "高性能陶瓷假捻盘的应用研究", 《北京纺织》, pages 34 - 37 *

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Application publication date: 20190122

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