CN202480051U - Fast-assembly tool for self-tapping screw-thread bushing - Google Patents
Fast-assembly tool for self-tapping screw-thread bushing Download PDFInfo
- Publication number
- CN202480051U CN202480051U CN2012200801307U CN201220080130U CN202480051U CN 202480051 U CN202480051 U CN 202480051U CN 2012200801307 U CN2012200801307 U CN 2012200801307U CN 201220080130 U CN201220080130 U CN 201220080130U CN 202480051 U CN202480051 U CN 202480051U
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- China
- Prior art keywords
- rod body
- ensat
- fast
- screw rod
- threaded inserts
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Abstract
The utility model relates to a fast-assembly tool for a self-tapping screw-thread bushing. The fast-assembly tool for the self-tapping screw-thread bushing is characterized of being composed of a screw rod body, a limited block and an axis pin, wherein one end of the screw rod body is provided with external threads which is matched with internal threads of the self-tapping screw-thread bushing, a middle rod body of the screw rod body is provided with a table surface which is matched with the limited block, and the limited block is fixed on the table surface of the middle rod body of the screw rod body. The other end of the screw rod body is provided with a square hole which is matched with a standard pneumatic impact wrench or a standard electric wrench. The fast-assembly tool for the self-tapping screw-thread bushing is mainly used for fast assembly of the self-tapping screw-thread bushing on a nonferrous alloy product body.
Description
Technical field
The utility model fast-assembling ENSAT THREADED INSERTS technical field.Be specifically related to a kind of screw-in fast-assembling ENSAT THREADED INSERTS instrument, be mainly used in the installation of ENSAT THREADED INSERTS.
Background technology
The screw thread inserts of the inner force part of non-ferrous alloy product; The screwed hole stressed greatly like the face that suspends upper screwed hole, drain oil and other product of engine component product, that mounting or dismounting are frequent etc.; Because of these position screwed holes bear big pulling force; And must bear frequent installation, dismounting at link screwed holes such as engine installation, vehicle use, maintainings; Aforesaid big pulling force and frequent is installed because the screwed hole that directly on the non-ferrous alloy product, processes, its screw strength can not bear, dismounting, very easily causes the screw thread screw thread to pull, wear and tear and causes whole product rejection.Be head it off; The spy has designed ENSAT THREADED INSERTS pointedly; The maximum difference of this ENSAT THREADED INSERTS and other standard thread lining is: ENSAT THREADED INSERTS Front-end Design tapering form, this tapering are convenient to when ENSAT THREADED INSERTS gets into product, play guide effect; And the ENSAT THREADED INSERTS Front-end Design become two place's symmetrical openings forms; The design of this opening mainly is to shoot product inside in order to cooperate the external screw thread smear metal of leaning on lining fully, chip removal with the product matrix, only processes the basic bottom outlet (unthreaded hole) of installation ENSAT THREADED INSERTS on the product; And other standard thread lining is a threaded engagement with cooperating of product body, on product, processes the screwed hole that cooperates with the standard thread lining earlier, through threaded engagement the standard thread lining is installed in the appointment screwed hole of product through specific purpose tool.Existing accurate screw-thread bush erecting tools can not be used for installing or the Fast Installation ENSAT THREADED INSERTS.
Summary of the invention
The purpose of the utility model is exactly to above-mentioned weak point a kind of fast-assembling ENSAT THREADED INSERTS instrument that is used for Fast Installation ENSAT THREADED INSERTS on non-ferrous alloy product body to be provided.
The technical solution of the utility model is: a kind of fast-assembling ENSAT THREADED INSERTS instrument is characterized in that: be made up of screw rod body, limited block and bearing pin; Wherein, screw rod body one end is provided with the external screw thread with the ENSAT THREADED INSERTS screw-internal thread fit, and the stage casing body of rod is provided with the table top that cooperates with limited block; Limited block is fixed on the table top of this screw rod body stage casing body of rod through bearing pin 4.
The screw rod body other end described in the technical solution of the utility model is provided with cubic hole pneumatic with standard or that the electric tool spanner cooperates.
The utility model is owing to adopt the fast-assembling ENSAT THREADED INSERTS instrument that is made up of screw rod body, limited block and bearing pin, and wherein, screw rod body one end is provided with the external screw thread with the ENSAT THREADED INSERTS screw-internal thread fit; The stage casing body of rod is provided with the table top that cooperates with limited block; Limited block is fixed on this table top through bearing pin, thereby when using, earlier the screw rod body end of thread is screwed in the ENSAT THREADED INSERTS; Again ENSAT THREADED INSERTS is put into the basic bottom outlet (unthreaded hole) of non-ferrous alloy product body; Drive the rotation of screw rod body clockwise direction through pneumatic or electric tool, when the limited block working face is adjacent to the working surface of product, represent that this ENSAT THREADED INSERTS is in place; Can should be pneumatic or electric tool counterclockwise rotate from ENSAT THREADED INSERTS and withdraw from, realization is shot the product assigned address and the degree of depth with ENSAT THREADED INSERTS fast.The utlity model has make and maintenance cost cheap, on-the-spot highly versatile can be realized arbitrarily on a covering device the different cooling velocity of same metal pattern plurality of positions, the characteristics of quick for installation, laborsaving, flexible, reliable operation.The utility model is mainly used in the Fast Installation of ENSAT THREADED INSERTS on non-ferrous alloy product body.
Description of drawings
Fig. 1 is the structural representation of the utility model.
Fig. 2 is the structural representation of ENSAT THREADED INSERTS.
The specific embodiment
Like Fig. 1, shown in Figure 2.The utility model is made up of screw rod body 5, limited block 3 and bearing pin 4.Wherein, screw rod body 5 one ends are provided with the external screw thread with the ENSAT THREADED INSERTS screw-internal thread fit, and the stage casing body of rod is provided with the table top that cooperates with limited block 3, and the other end is provided with cubic hole pneumatic with standard or that the electric tool spanner cooperates.Limited block 3 is fixed on the table top of these screw rod body 5 stage casing bodies of rod through bearing pin 4.ENSAT THREADED INSERTS 2 front ends 7 are designed to the tapering form, and this taper design is convenient to when ENSAT THREADED INSERTS gets into product, play guide effect.ENSAT THREADED INSERTS 2 front ends 7 are designed to two place's symmetrical openings, 6 forms, and 6 designs of this opening mainly are in order to cooperate the external screw thread smear metal of leaning on ENSAT THREADED INSERTS 2 fully with alloy product 1 matrix, by the opening chip removal ENSAT THREADED INSERTS 2 to be shot alloy product 1 inside.Make the screw rod body 5 of various different sizes according to the internal thread specification different designs of the ENSAT THREADED INSERTS 2 that requires on the alloy product 1.
Method for using is to screw in ENSAT THREADED INSERTS 2 on the screw rod body 5 of the utility model front end through the internal and external threads interlock; The degree of depth (this degree of depth is the degree of depth that ENSAT THREADED INSERTS 2 is shot alloy product 1 inside) of leaning on limited block 3 qualifications to be threaded into; Drive the rotation of the utility model clockwise direction through pneumatic or electric tool; When limited block 3 working faces are adjacent to the working surface of alloy product 1; Represent that this ENSAT THREADED INSERTS 2 is in place, can the utility model counterclockwise be rotated from the self tapping lining and withdraw from, realize fast ENSAT THREADED INSERTS 2 being shot alloy product 1 assigned address and the degree of depth.The utility model is a kind of easy for installation, flexible, safe and reliable fast-assembling ENSAT THREADED INSERTS instrument.
Claims (2)
1. a fast-assembling ENSAT THREADED INSERTS instrument is characterized in that: be made up of screw rod body (5), limited block (3) and bearing pin (4); Wherein, screw rod body (5) one ends are provided with the external screw thread with the ENSAT THREADED INSERTS screw-internal thread fit, and the stage casing body of rod is provided with the table top that cooperates with limited block (3); Limited block (3) is fixed on the table top of this screw rod body (5) stage casing body of rod through bearing pin (4).
2. a kind of fast-assembling ENSAT THREADED INSERTS instrument according to claim 1 is characterized in that: described screw rod body (5) other end is provided with cubic hole pneumatic with standard or that the electric tool spanner cooperates.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200801307U CN202480051U (en) | 2012-03-06 | 2012-03-06 | Fast-assembly tool for self-tapping screw-thread bushing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012200801307U CN202480051U (en) | 2012-03-06 | 2012-03-06 | Fast-assembly tool for self-tapping screw-thread bushing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202480051U true CN202480051U (en) | 2012-10-10 |
Family
ID=46954511
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2012200801307U Expired - Fee Related CN202480051U (en) | 2012-03-06 | 2012-03-06 | Fast-assembly tool for self-tapping screw-thread bushing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202480051U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103273459A (en) * | 2012-03-06 | 2013-09-04 | 新兴重工湖北三六一一机械有限公司 | Fast-installed self-tapping threaded bushing tool |
| CN105822648A (en) * | 2015-03-31 | 2016-08-03 | 湖北博士隆科技有限公司 | Chip storage space communicating type chipless self-tapped thread sleeve |
| CN106272245A (en) * | 2016-08-31 | 2017-01-04 | 中船澄西船舶修造有限公司 | Thread bush installation method |
| CN106671026A (en) * | 2016-08-31 | 2017-05-17 | 中船澄西船舶修造有限公司 | Threaded sleeve installation tool |
| CN107598834A (en) * | 2017-09-29 | 2018-01-19 | 江西昌河航空工业有限公司 | A kind of installation bulging instrument of non-dismountable screw-thread bush |
| US11529901B2 (en) | 2018-09-28 | 2022-12-20 | Ka Group Ag | Grab bar assembly for a vehicle |
-
2012
- 2012-03-06 CN CN2012200801307U patent/CN202480051U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103273459A (en) * | 2012-03-06 | 2013-09-04 | 新兴重工湖北三六一一机械有限公司 | Fast-installed self-tapping threaded bushing tool |
| CN105822648A (en) * | 2015-03-31 | 2016-08-03 | 湖北博士隆科技有限公司 | Chip storage space communicating type chipless self-tapped thread sleeve |
| CN106272245A (en) * | 2016-08-31 | 2017-01-04 | 中船澄西船舶修造有限公司 | Thread bush installation method |
| CN106671026A (en) * | 2016-08-31 | 2017-05-17 | 中船澄西船舶修造有限公司 | Threaded sleeve installation tool |
| CN107598834A (en) * | 2017-09-29 | 2018-01-19 | 江西昌河航空工业有限公司 | A kind of installation bulging instrument of non-dismountable screw-thread bush |
| US11529901B2 (en) | 2018-09-28 | 2022-12-20 | Ka Group Ag | Grab bar assembly for a vehicle |
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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: 20121010 Termination date: 20140306 |