CN202592310U - Bushing extractor - Google Patents

Bushing extractor Download PDF

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Publication number
CN202592310U
CN202592310U CN 201220155816 CN201220155816U CN202592310U CN 202592310 U CN202592310 U CN 202592310U CN 201220155816 CN201220155816 CN 201220155816 CN 201220155816 U CN201220155816 U CN 201220155816U CN 202592310 U CN202592310 U CN 202592310U
Authority
CN
China
Prior art keywords
gland
pin
lining
endoporus
diameter
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.)
Expired - Fee Related
Application number
CN 201220155816
Other languages
Chinese (zh)
Inventor
李辉
林钢
敬伟
韩雪峰
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.)
Harbin Aircraft Industry Group Co Ltd
Original Assignee
Harbin Aircraft Industry Group 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 Harbin Aircraft Industry Group Co Ltd filed Critical Harbin Aircraft Industry Group Co Ltd
Priority to CN 201220155816 priority Critical patent/CN202592310U/en
Application granted granted Critical
Publication of CN202592310U publication Critical patent/CN202592310U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belong to the technology of airplane assembly, relates to a bushing extractor for taking a bushing of a tool positioning member out of an installation hole. The bushing extractor is characterized in that the extractor comprises a pin [1] and a pressing sleeve [2]; the pin [1] is a cylindrical shaft; a convex shoulder [1a] is arranged at the upper end of the pin [1]; the pressing sleeve [2] is a sleeve with a multi-step shaft shape. The bushing extractor has the advantages that the bushing extractor can prevent the positioning hole of the tool positioning member from being damaged during taking out the bushing, avoids adding the repair procedures of expanding the positioning hole and the like, and ensures the positioning accuracy and quality of the product.

Description

A kind of bush extractor
Technical field
The utility model belongs to the aircraft mounting technology, relates to a kind of bush extractor that lining on the tool locating part is taken out from installing hole.
Background technology
Lining is a kind of part commonly used in the aircraft tool locating part, through using for a long time, usually has the lining internal diameter overproof, and the phenomenon that can not satisfy positioning requirements occurs, and needs overproof lining to be taken out the lining that more renews.Mostly the method for taking out lining now is directly lining to be knocked with hammer; Easy like this damage is caused in the tool locating hole; Influence the precision of locating hole; Need position the repair procedure such as reaming in hole, not only increase processing cost but also influenced frock quality and positioning accuracy, and then influence product orientation precision and quality.
Summary of the invention
The purpose of the utility model is: a kind of bush extractor that can prevent to damage tool locating part locating hole is provided, to avoid increasing the repair procedure such as reaming of locating hole, guarantees the positioning accuracy and the quality of product.
The technical scheme of the utility model is: a kind of bush extractor; It is characterized in that; It is made up of pin 1 and gland 2; Pin 1 is a cylinder axis, and the endoporus matched in clearance of lining 3 to be removed on the diameter of this cylinder axis and the tool locating part 4 has the convex shoulder 1a of a diameter greater than pin 1 diameter in the upper end of pin 1; Gland 2 is the sleeves with step axle profile; The external diameter of the epimere 2a of gland 2 is greater than the external diameter of the hypomere 2b of gland 2; The external diameter of gland 2 hypomere 2b is less than the external diameter of lining 3 to be removed, and the diameter of bore of gland 2 hypomere 2b equals the internal diameter of lining 3 to be removed, and the endoporus of gland 2 epimere 2a is a stepped hole; The aperture of the last sector hole of this stepped hole is greater than the external diameter of pin 1 convex shoulder 1a, and the endoporus of the following sector hole of this stepped hole and gland 2 hypomere 2b is same hole; In the endoporus of the cylinder axis insertion gland 2 hypomere 2b of pin 1 and the endoporus of lining to be removed 3; The step end face of lower surface and gland 2 epimere 2a endoporus of 1 convex shoulder 1a of pinning is fitted; The pin upper surface of 1 convex shoulder 1a flushes with the upper surface of gland 2, and the length of gland 2 hypomere 2b is greater than the length of lining 3 to be removed.
The utility model has the advantages that: can prevent to damage the locating hole of tool locating part when taking out lining, avoid increasing the repair procedure such as reaming of locating hole, guarantee the positioning accuracy and the quality of product.
Description of drawings
Fig. 1 is the structural representation of the utility model.
The specific embodiment
Explain further details in the face of the utility model down.Referring to Fig. 1, a kind of bush extractor is characterized in that; It is made up of pin 1 and gland 2; Pin 1 is a cylinder axis, and the endoporus matched in clearance of lining 3 to be removed on the diameter of this cylinder axis and the tool locating part 4 has the convex shoulder 1a of a diameter greater than pin 1 diameter in the upper end of pin 1; Gland 2 is the sleeves with step axle profile; The external diameter of the epimere 2a of gland 2 is greater than the external diameter of the hypomere 2b of gland 2; The external diameter of gland 2 hypomere 2b is less than the external diameter of lining 3 to be removed, and the diameter of bore of gland 2 hypomere 2b equals the internal diameter of lining 3 to be removed, and the endoporus of gland 2 epimere 2a is a stepped hole; The aperture of the last sector hole of this stepped hole is greater than the external diameter of pin 1 convex shoulder 1a, and the endoporus of the following sector hole of this stepped hole and gland 2 hypomere 2b is same hole; In the endoporus of the cylinder axis insertion gland 2 hypomere 2b of pin 1 and the endoporus of lining to be removed 3; The step end face of lower surface and gland 2 epimere 2a endoporus of 1 convex shoulder 1a of pinning is fitted; The pin upper surface of 1 convex shoulder 1a flushes with the upper surface of gland 2, and the length of gland 2 hypomere 2b is greater than the length of lining 3 to be removed.
The method for using of the utility model is: in the endoporus of the 1 insertion gland 2 of at first will pinning; To pin then 1 insert lining 3 to be removed endoporus; The lower surface and lining to be removed 3 end faces of gland 2 are fitted, knock bush extractor with hammer, because location, the guiding function of pin 1 are arranged; Lining 3 to be removed is just by vertical taking-up, thereby avoided the damage to lining 3 installing holes on the tool locating part.
Embodiment 1: the external diameter of lining 3 to be removed is φ 15r6, and the internal diameter of lining 3 is φ 10H7, and the length of lining 3 is 10mm.The external diameter of pin 1 is φ 10r6.The external diameter of gland 2 is φ 13, and the internal diameter of gland 2 is φ 10H7, and length is 15mm.
Embodiment 2: the external diameter of lining 3 to be removed is φ 20r 6, and the internal diameter of lining 3 is φ 15H7, and the length of lining 3 is 15mm.The external diameter of pin 1 is φ 15r 6.The external diameter of gland 2 is φ 18, and the internal diameter of gland 2 is φ 15H7, and length is 20mm.
Embodiment 3: the external diameter of lining 3 to be removed is φ 10r6, and the internal diameter of lining 3 is φ 6H7, and the length of lining 3 is 10mm.The external diameter of pin 1 is φ 4r6.The external diameter of gland 2 is φ 8, and the internal diameter of gland 2 is φ 4H7, and length is 15mm.

Claims (1)

1. bush extractor; It is characterized in that; It is made up of pin [1] and gland [2]; Pin [1] is a cylinder axis, and the diameter of this cylinder axis and tool locating part [4] are gone up the endoporus matched in clearance of lining to be removed [3], and the convex shoulder [1a] of a diameter greater than pin [1] diameter arranged in the upper end of pin [1]; Gland [2] is a sleeve with step axle profile; The external diameter of the epimere [2a] of gland [2] is greater than the external diameter of the hypomere [2b] of gland [2]; The external diameter of gland [2] hypomere [2b] is less than the external diameter of lining to be removed [3]; The diameter of bore of gland [2] hypomere [2b] equals the internal diameter of lining to be removed [3]; The endoporus of gland [2] epimere [2a] is a stepped hole, and the aperture of the last sector hole of this stepped hole is greater than the external diameter of pin [1] convex shoulder [1a], and the endoporus of the following sector hole of this stepped hole and gland [2] hypomere [2b] is same hole; In the endoporus of cylinder axis insertion gland [2] hypomere [2b] of pin [1] and the endoporus of lining to be removed [3]; The lower surface of pin [1] convex shoulder [1a] and the step end face of gland [2] epimere [2a] endoporus are fitted; The upper surface of pin [1] convex shoulder [1a] flushes with the upper surface of gland [2], and the length of gland [2] hypomere [2b] is greater than the length of lining to be removed [3].
CN 201220155816 2012-04-13 2012-04-13 Bushing extractor Expired - Fee Related CN202592310U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220155816 CN202592310U (en) 2012-04-13 2012-04-13 Bushing extractor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220155816 CN202592310U (en) 2012-04-13 2012-04-13 Bushing extractor

Publications (1)

Publication Number Publication Date
CN202592310U true CN202592310U (en) 2012-12-12

Family

ID=47309894

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220155816 Expired - Fee Related CN202592310U (en) 2012-04-13 2012-04-13 Bushing extractor

Country Status (1)

Country Link
CN (1) CN202592310U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106345894A (en) * 2016-09-30 2017-01-25 安徽江淮汽车股份有限公司 Method for position adjustment processing of piercing punch and die structure
CN108838945A (en) * 2018-09-05 2018-11-20 红塔烟草(集团)有限责任公司 The inspection of box mould connecting rod and its dismantling device of copper sheathing

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106345894A (en) * 2016-09-30 2017-01-25 安徽江淮汽车股份有限公司 Method for position adjustment processing of piercing punch and die structure
CN108838945A (en) * 2018-09-05 2018-11-20 红塔烟草(集团)有限责任公司 The inspection of box mould connecting rod and its dismantling device of copper sheathing

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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: 20121212

Termination date: 20180413

CF01 Termination of patent right due to non-payment of annual fee