CN202597370U - Locating pin of blind hole - Google Patents

Locating pin of blind hole Download PDF

Info

Publication number
CN202597370U
CN202597370U CN 201220155677 CN201220155677U CN202597370U CN 202597370 U CN202597370 U CN 202597370U CN 201220155677 CN201220155677 CN 201220155677 CN 201220155677 U CN201220155677 U CN 201220155677U CN 202597370 U CN202597370 U CN 202597370U
Authority
CN
China
Prior art keywords
blind hole
locating pin
hole
shank
pin
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 201220155677
Other languages
Chinese (zh)
Inventor
邸春阳
唐宪伟
郭忠义
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 201220155677 priority Critical patent/CN202597370U/en
Application granted granted Critical
Publication of CN202597370U publication Critical patent/CN202597370U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belongs to aircraft tool manufacturing technology, and relates to a locating pin of a blind hole. The locating pin of the blind pole comprises a pin body (1) of a cylindrical shape, and is characterized in that a threaded hole (2) axially penetrates through two end surfaces of the pin body (1) in the center of the pin body (1). The locating pin of the blind hole is convenient to install and take out. Gas in the blind hole is capable of being discharged from the threaded hole (2) smoothly when the locating pin of the blind hole is installed, when the locating pin of the blind hole is taken out, a bolt is screwed into the threaded hole, so that the locating pin of the blind hole can be conveniently taken out when the bolt is taken as a carrier.

Description

A kind of blind hole locating stud
Technical field
The utility model belongs to aircraft frock manufacturing technology, relates to a kind of blind hole locating stud.
Background technique
Locating stud in the existing aircraft frock is the entity straight pin.Its shortcoming is: the first, difficult installation.In aircraft frock manufacture process, when often taking place, blind hole locating stud entering positioning hole ejected situation about can not accurately locate by residual gas.The second, take out difficulty.When the aircraft product structure is changed, need take out the locating stud that is installed in the blind hole, because locating stud and blind hole adopt interference fit, take out very difficulty, often cause the damage of aircraft tool locating part.
Summary of the invention
The purpose of the utility model is: a kind of blind hole locating stud of installing and taking out be convenient to is provided.
The technological scheme of the utility model is: a kind of blind hole locating stud, comprise columniform shank 1, and it is characterized in that; A tapped hole 2 that connects 1 two end faces of shank is vertically arranged at the center of shank 1; Maximum inner diameter d=(0.2~0.5) D of tapped hole 2, D is the external diameter of shank 1, unit is mm.
The utility model has the advantages that: be convenient to install and take out.During installation, the gas in the blind hole can be discharged from tapped hole smoothly; During taking-up, screw is screwed into tapped hole, as push rod, can takes out the blind hole locating stud easily with screw.
Description of drawings
Fig. 1 is the structural representation of the utility model.
Embodiment
Explain further details in the face of the utility model down.Referring to Fig. 1, a kind of blind hole locating stud comprises columniform shank 1; It is characterized in that a tapped hole 2 that connects 1 two end faces of shank is vertically arranged at the center of shank 1, maximum inner diameter d=(0.2~0.5) D of tapped hole 2; D is the external diameter of shank 1, and unit is mm.
When aircraft product change position, hole; Be screwed into common screw in the tapped hole 2 of shank 1; Pass through rotary screw; Make screw end head hold out against the bottom of the positioning hole of aircraft frock, continue rotary screw, the blind hole locating stud can climb away positioning hole gradually along the opposite direction that screw rod advances from the positioning hole of aircraft frock.
Following table provides 3 embodiments' parameter.
D d
Embodiment 1 6 3
Embodiment 2 10 4
Embodiment 3 15 5

Claims (1)

1. a blind hole locating stud comprises columniform shank (1), it is characterized in that; A tapped hole (2) that connects (1) two end face of shank is vertically arranged at the center of shank (1); Maximum inner diameter d=(0.2~0.5) D of tapped hole (2), D is the external diameter of shank (1), unit is mm.
CN 201220155677 2012-04-13 2012-04-13 Locating pin of blind hole Expired - Fee Related CN202597370U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201220155677 CN202597370U (en) 2012-04-13 2012-04-13 Locating pin of blind hole

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201220155677 CN202597370U (en) 2012-04-13 2012-04-13 Locating pin of blind hole

Publications (1)

Publication Number Publication Date
CN202597370U true CN202597370U (en) 2012-12-12

Family

ID=47314915

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201220155677 Expired - Fee Related CN202597370U (en) 2012-04-13 2012-04-13 Locating pin of blind hole

Country Status (1)

Country Link
CN (1) CN202597370U (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103671417A (en) * 2013-10-25 2014-03-26 浙江吉利控股集团有限公司 Locating pin capable of being pushed out
CN105299011A (en) * 2015-11-25 2016-02-03 重庆渝记涵诚机械制造有限公司 Locating pin convenient to disassemble
CN106166606A (en) * 2016-08-31 2016-11-30 乔治费歇尔汽车产品(苏州)有限公司 Automobile Hpdc mould precasting pin

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103671417A (en) * 2013-10-25 2014-03-26 浙江吉利控股集团有限公司 Locating pin capable of being pushed out
CN103671417B (en) * 2013-10-25 2018-02-16 浙江吉利罗佑发动机有限公司 A kind of desirable alignment pin
CN105299011A (en) * 2015-11-25 2016-02-03 重庆渝记涵诚机械制造有限公司 Locating pin convenient to disassemble
CN106166606A (en) * 2016-08-31 2016-11-30 乔治费歇尔汽车产品(苏州)有限公司 Automobile Hpdc mould precasting pin

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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