CN105881451A - Self-tapping thread bushing tool - Google Patents

Self-tapping thread bushing tool Download PDF

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Publication number
CN105881451A
CN105881451A CN201410746546.1A CN201410746546A CN105881451A CN 105881451 A CN105881451 A CN 105881451A CN 201410746546 A CN201410746546 A CN 201410746546A CN 105881451 A CN105881451 A CN 105881451A
Authority
CN
China
Prior art keywords
self
ensat
tapping thread
thread bushing
casting
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.)
Pending
Application number
CN201410746546.1A
Other languages
Chinese (zh)
Inventor
陈锦
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to CN201410746546.1A priority Critical patent/CN105881451A/en
Publication of CN105881451A publication Critical patent/CN105881451A/en
Pending legal-status Critical Current

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Abstract

The invention discloses a self-tapping thread bushing tool, and belongs to the technical field of control equipment in the casting production process. The self-tapping thread bushing tool mainly solves the problems that according to a traditional cooling method, different cooling speeds required by parts of a casting in a die cavity cannot be accurately met, and hole shrinkage, shrinkage porosity, cracks and other casting defects are extremely prone to happening to key parts of the casting due to too high or too low cooling speed. Different cooling speeds for multiple positions of the same metal die can be achieved at will through a set of device, and the self-tapping thread bushing tool has the beneficial effects of being fast in installation, capable of saving labor, flexible and reliable in work and is mainly used for cooling of various metal dies.

Description

ENSAT THREADED INSERTS instrument
Technical field
Fast-assembling ENSAT THREADED INSERTS technical field of the present invention.
Background technology
As relatively big in suspension face upper screwed hole, drain oil and the other products stress of engine component product, Mounting or dismounting screwed hole frequently etc., because these position screwed holes bear bigger pulling force, and install at electromotor, The link screwed holes such as vehicle use, maintaining must endure as frequently installing, dismantling, owing to directly existing The screwed hole processed on non-ferrous alloy product, its screw strength can not bear the biggest Pulling force and frequently installation, dismounting, easily cause screw thread to pull, wear and tear and cause one integral piece product report Useless.
Summary of the invention
The purpose of the present invention is aiming at above-mentioned weak point and provides a kind of ENSAT THREADED INSERTS instrument.
The technical solution of the present invention is: a kind of ENSAT THREADED INSERTS instrument, it is characterized in that: by screw rod Body, limited block and bearing pin are constituted;Wherein, screw body one end is provided with and joins with ENSAT THREADED INSERTS female thread The external screw thread closed, the stage casing body of rod is provided with the table top coordinated with limited block;Limited block is solid by bearing pin 4 It is scheduled on the table top of this screw body stage casing body of rod.
The screw body other end described in the technical solution of the present invention is provided with pneumatic with standard or electronic Four square holes that tool wrench coordinates.
Due to the fact that and use the fast-assembling ENSAT THREADED INSERTS work being made up of screw body, limited block and bearing pin Tool, wherein, screw body one end is provided with and the external screw thread of ENSAT THREADED INSERTS screw-internal thread fit, stage casing bar Body is provided with the table top coordinated with limited block, and limited block is fixed on this table top by bearing pin, thus makes Used time, first the screw body end of thread is screwed in ENSAT THREADED INSERTS, then ENSAT THREADED INSERTS is placed with In the basic bottom outlet (unthreaded hole) of color alloy product body, drive screw body by pneumatic or electric tool It is rotated clockwise, when limited block work surface is adjacent to the working surface of product, represents this self tapping spiral shell Stricture of vagina lining is installed and is put in place, this is pneumatic or electric tool can counterclockwise rotate and serve as a contrast from tapping screw thread Set exits, it is achieved quickly ENSAT THREADED INSERTS is shot product and specifies position and the degree of depth.The present invention has There are making and maintenance cost cheap, on-the-spot highly versatile, arbitrarily can realize same in set of device The rate of cooling that metal pattern plurality of positions is different, quick for installation, laborsaving, flexible, the spy of reliable operation Point.Present invention is mainly used for ENSAT THREADED INSERTS Fast Installation on non-ferrous alloy product ontology.
Accompanying drawing explanation
Fig. 1 is the structural representation of the present invention.
Fig. 2 is the structural representation of ENSAT THREADED INSERTS.
Detailed description of the invention
Screw body 5 one end is provided with and the external screw thread of ENSAT THREADED INSERTS screw-internal thread fit, on the body of rod of stage casing Being provided with the table top coordinated with limited block 3, the other end is provided with or electric tool spanner pneumatic with standard and coordinates Four square holes.Limited block 3 is fixed on the table top of this screw body 5 stage casing body of rod by bearing pin 4.From Tapping lining 2 front end 7 is designed to tapering form, and this taper design is easy to enter at ENSAT THREADED INSERTS Guide effect is played when entering product.ENSAT THREADED INSERTS 2 front end 7 is designed to symmetrical openings 6 shape at two Formula, this opening 6 is mainly designed to serve as a contrast by tapping screw thread completely with alloy product 1 base mate Overlap the external screw thread chip of 2, by opening chip removal, ENSAT THREADED INSERTS 2 shot in alloy product 1 Portion.Female thread specification different designs system according to the ENSAT THREADED INSERTS 2 required on alloy product 1 Make the screw body 5 of various different size.

Claims (2)

1. ENSAT THREADED INSERTS instrument, is characterized in that: by screw body (5), limited block (3) and bearing pin (4) Constitute;Wherein, screw body (5) one end is provided with and the external screw thread of ENSAT THREADED INSERTS screw-internal thread fit, The stage casing body of rod is provided with and limited block 3) table top that coordinates;Limited block (3) is fixed by bearing pin (4) On the table top of this screw body (5) the stage casing body of rod.
ENSAT THREADED INSERTS instrument the most according to claim 1, is characterized in that: described screw body (5) The other end is provided with four square holes that or electric tool spanner pneumatic with standard coordinates.
CN201410746546.1A 2014-12-08 2014-12-08 Self-tapping thread bushing tool Pending CN105881451A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410746546.1A CN105881451A (en) 2014-12-08 2014-12-08 Self-tapping thread bushing tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410746546.1A CN105881451A (en) 2014-12-08 2014-12-08 Self-tapping thread bushing tool

Publications (1)

Publication Number Publication Date
CN105881451A true CN105881451A (en) 2016-08-24

Family

ID=56699593

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410746546.1A Pending CN105881451A (en) 2014-12-08 2014-12-08 Self-tapping thread bushing tool

Country Status (1)

Country Link
CN (1) CN105881451A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106759936A (en) * 2016-12-12 2017-05-31 周兆弟 For automatic control absolute altitude and the erector being automatically separated
US11529901B2 (en) 2018-09-28 2022-12-20 Ka Group Ag Grab bar assembly for a vehicle

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106759936A (en) * 2016-12-12 2017-05-31 周兆弟 For automatic control absolute altitude and the erector being automatically separated
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
C06 Publication
PB01 Publication
WD01 Invention patent application deemed withdrawn after publication
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20160824