CN202140389U - Ventilating long circular sleeve - Google Patents

Ventilating long circular sleeve Download PDF

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Publication number
CN202140389U
CN202140389U CN 201120188802 CN201120188802U CN202140389U CN 202140389 U CN202140389 U CN 202140389U CN 201120188802 CN201120188802 CN 201120188802 CN 201120188802 U CN201120188802 U CN 201120188802U CN 202140389 U CN202140389 U CN 202140389U
Authority
CN
China
Prior art keywords
long circular
positioning
oval
ventilating
circular sleeve
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 201120188802
Other languages
Chinese (zh)
Inventor
郭忠义
邸春阳
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 201120188802 priority Critical patent/CN202140389U/en
Application granted granted Critical
Publication of CN202140389U publication Critical patent/CN202140389U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model belongs to the manufacturing technology of airplane frocks, particularly a ventilating long circular sleeve used for the positioning purpose, wherein a working long circular hole is arranged at the center of the long circular sleeve. The upper and lower cylindrical surfaces of the working outer circle of the long circular sleeve are respectively equipped with a spacing semicircular hole and a ventilating groove. Due to the adoption of the ventilating long circular sleeve, a long circular positioning pin can be conveniently inserted into a positioning long circular blind hole. Meanwhile, the problems of the inclined positioning of the positioning long circular pin and the difficult insertion of the positioning long circular pin due to the blocked gas emission inside the blind hole are solved, so that the installation precision of a frock is ensured.

Description

Ventilative oval cover
Technical field
The utility model belongs to aircraft frock manufacturing technology, particularly relates to a kind of ventilative oval cover that is used to locate.
Background technique
Existing being installed in located oval cover in the blind hole, when the oval pin in location inserts slotted hole work, because the residual gas in the blind hole of part does not have discharging, make the insertion fully of locating stud cause difficulty, even cause locating stud tiltedly to locate the positioning hole that destroys part.
Summary of the invention
The purpose of the utility model is: a kind of ventilative oval cover that is used to locate is provided.
The technological scheme of the utility model is:
A kind of ventilative oval cover that is used to locate has a work slotted hole 1 at the center of oval cover, at the upper and lower cylinder of work cylindrical of oval cover spacing semicircle orifice 2 and ventilating groove 3 are arranged respectively.
The utility model has the advantages that: be convenient to the oval locating stud of insertion in locating oval blind hole, avoided oblique location of the oval pin in location and the interior gaseous emission of blind hole freely not to cause the oval pin insertion in location difficulty, guaranteed the frock installation precision.
Description of drawings
Fig. 1 is the schematic representation of the ventilative oval cover of the utility model, and 1 is the work slotted hole, and 2 is spacing semicircle orifice, and 3 is ventilating groove.
Embodiment:
During use, oval locating stud is inserted in the work slotted hole 1 of oval cover, as the axle center, oval locating stud slowly, is vertically inserted in the work slotted hole 1 of oval cover with the outer garden of the oval locating stud of the work slotted hole of oval cover 1 guiding.At this moment, the residual gas in the blind hole of location is discharged by the ventilating groove 3 of oval cover.Spacing semicircle orifice is used to avoid locating oval pin and tiltedly locatees.Because the residual gas in the work slotted hole 1 of the oval cover in location is smoothly exhausted, insert in the work slotted hole 1 of locating oval cover very convenient so locate oval pin.

Claims (1)

1. a ventilative oval cover is characterized in that, a work slotted hole is arranged at the center of oval cover, at the upper and lower cylinder of work cylindrical of oval cover spacing semicircle orifice and ventilating groove is arranged respectively.
CN 201120188802 2011-06-03 2011-06-03 Ventilating long circular sleeve Expired - Fee Related CN202140389U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201120188802 CN202140389U (en) 2011-06-03 2011-06-03 Ventilating long circular sleeve

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201120188802 CN202140389U (en) 2011-06-03 2011-06-03 Ventilating long circular sleeve

Publications (1)

Publication Number Publication Date
CN202140389U true CN202140389U (en) 2012-02-08

Family

ID=45551447

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201120188802 Expired - Fee Related CN202140389U (en) 2011-06-03 2011-06-03 Ventilating long circular sleeve

Country Status (1)

Country Link
CN (1) CN202140389U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104329331A (en) * 2014-08-29 2015-02-04 中国运载火箭技术研究院 Cold and hot connection structure suitable for high-temperature service environment

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104329331A (en) * 2014-08-29 2015-02-04 中国运载火箭技术研究院 Cold and hot connection structure suitable for high-temperature service environment
CN104329331B (en) * 2014-08-29 2016-03-30 中国运载火箭技术研究院 A kind of cold and hot linkage structure be applicable under high-temperature service environment

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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: 20120208

Termination date: 20160603