CN201405033Y - Narrow area riveting and pressure riveting tool - Google Patents

Narrow area riveting and pressure riveting tool Download PDF

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Publication number
CN201405033Y
CN201405033Y CN2009200136843U CN200920013684U CN201405033Y CN 201405033 Y CN201405033 Y CN 201405033Y CN 2009200136843 U CN2009200136843 U CN 2009200136843U CN 200920013684 U CN200920013684 U CN 200920013684U CN 201405033 Y CN201405033 Y CN 201405033Y
Authority
CN
China
Prior art keywords
head
riveting
bow
left end
pressure riveting
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
CN2009200136843U
Other languages
Chinese (zh)
Inventor
皇甫金旗
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.)
Shenyang Aircraft Industry Group Co Ltd
Original Assignee
Shenyang 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 Shenyang Aircraft Industry Group Co Ltd filed Critical Shenyang Aircraft Industry Group Co Ltd
Priority to CN2009200136843U priority Critical patent/CN201405033Y/en
Application granted granted Critical
Publication of CN201405033Y publication Critical patent/CN201405033Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Insertion Pins And Rivets (AREA)

Abstract

The utility model discloses a narrow area riveting and pressure riveting tool, which relates to the improvement on a riveting tool structure and is used for the riveting operation of a narrow area. The narrow area riveting and pressure riveting tool is characterized by consisting of a bow clipping body, an assistant pressure riveting head, a pressure riveting head, a compression bar and a cylinderbody, wherein the pressure riveting head is made into a blind hole with internal threads, the left end of the compression bar is provided with external threads, the assistant pressure riveting head is provided with a combined structure of cylindrical external threads and an oblate boss, the left end of the bow clipping body is provided with a screwed hole, and the right end of the bow clipping body is provided with a compression bar mounting hole; and the cylinder body is arranged on the bow clipping body, the compression bar is arranged in the compression bar mounting hole at the right end of the bow clipping body, the right end of the compression bar is connected with the cylinder body, the left end of the compression bar is provided with the pressure riveting head, and the assistant pressure riveting head is arranged in the screwed hole at the left end of the bow clipping body. The utility model has the advantages that the assistant pressure riveting head can rotate at any angle relative to the axis of the cylindrical external threads in order to adjust the pressure riveting stroke as required, the adjustment is convenient, and the riveting quality is improved.

Description

Narrow zone is riveted the instrument that presses
Technical field:
The invention is the improvement to the tool construction that presses, and is used for the riveted joint operation of narrow zone.
Background technology:
Aircraft is when the riveted joint operation, there is narrow zone, existing clincher tool can not be applied to narrow zone and rivet, have to adopt manual rammer riveting, the riveting work difficulty, two people cooperate randomness big, the degree control of riveted joint position, rivet force control, riveting molding number of times etc. all is uncertain factor, is prone to the riveted joint defective.
Summary of the invention:
The purpose of the invention provides a kind of suitable narrow zone riveted joint, reduces the narrow zone of riveted joint defective and rivets the instrument that presses; The purpose of the invention is to realize by following technical scheme: the narrow zone riveted joint instrument that presses is characterized in that being made up of press head, press head, depression bar and cylinder block of bow clamp, pair; The head that presses is made female blind hole, and depression bar left end head is shaped on external screw thread, and the pair head that presses is shaped on cylinder external screw thread and oblate boss integrated structure, bends on the clamp left end to be shaped on screwed hole, and right-hand member is shaped on the installation strut kong; Cylinder block is installed on the bow clamp, and depression bar is installed in the strut kong of bow clamp right-hand member, and the depression bar right-hand member is connected with cylinder block, and the depression bar left end is installed the head that presses, and pair presses in the screwed hole that is installed in bow clamp left end.
The advantage of the invention: the pair head that presses can arbitrarily angledly rotate relative to the cylinder axis of external thread, and is easy to adjust so that adjust the stroke that presses on demand, the raising riveting quality.
Description of drawings:
Fig. 1 is that narrow zone is riveted the tool construction schematic diagram that presses.
Among the figure: 1, bow clamp 2, pair press 3, workpiece 4, rivet 5, press 6, depression bar 7, cylinder block
The specific embodiment:
The narrow zone riveted joint instrument that presses is characterized in that being made up of press head, press head, depression bar and cylinder block of bow clamp, pair; The head that presses is made female blind hole, and depression bar left end head is shaped on external screw thread, and the pair head that presses is shaped on cylinder external screw thread and oblate boss integrated structure, bends on the clamp left end to be shaped on screwed hole, and right-hand member is shaped on the installation strut kong; Cylinder block is installed on the bow clamp, and depression bar is installed in the strut kong of bow clamp right-hand member, and the depression bar right-hand member is connected with cylinder block, and the depression bar left end is installed the head that presses, and pair presses in the screwed hole that is installed in bow clamp left end.
At the flaperon at the aircraft outer wing rear portion of aircraft narrow zone, two webs and lower arm plate riveted joint place are used about the 6th support arm in the invention, and it is even that rivet bar is upset as shape, and the composite of being riveted does not produce defectives such as layering.

Claims (1)

1, the narrow zone riveted joint instrument that presses is characterized in that being made up of press head, press head, depression bar and cylinder block of bow clamp, pair; The head that presses is made female blind hole, and depression bar left end head is shaped on external screw thread, and the pair head that presses is shaped on cylinder external screw thread and oblate boss integrated structure, bends on the clamp left end to be shaped on screwed hole, and right-hand member is shaped on the installation strut kong; Cylinder block is installed on the bow clamp, and depression bar is installed in the strut kong of bow clamp right-hand member, and the depression bar right-hand member is connected with cylinder block, and the depression bar left end is installed the head that presses, and pair presses in the screwed hole that is installed in bow clamp left end.
CN2009200136843U 2009-05-14 2009-05-14 Narrow area riveting and pressure riveting tool Expired - Fee Related CN201405033Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009200136843U CN201405033Y (en) 2009-05-14 2009-05-14 Narrow area riveting and pressure riveting tool

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009200136843U CN201405033Y (en) 2009-05-14 2009-05-14 Narrow area riveting and pressure riveting tool

Publications (1)

Publication Number Publication Date
CN201405033Y true CN201405033Y (en) 2010-02-17

Family

ID=41675954

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009200136843U Expired - Fee Related CN201405033Y (en) 2009-05-14 2009-05-14 Narrow area riveting and pressure riveting tool

Country Status (1)

Country Link
CN (1) CN201405033Y (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104942206B (en) * 2015-06-17 2016-10-26 沈阳飞机工业(集团)有限公司 Close the anti-clinching method of small space plate nut
CN106363122A (en) * 2016-11-10 2017-02-01 浙江大学 Bent riveting head for aircraft panel horizontal automatic drilling and riveting machine
CN109604508A (en) * 2018-11-27 2019-04-12 中国航发贵州黎阳航空动力有限公司 A kind of narrow ring cavity depths clinching method and send holding tool
CN110405130A (en) * 2019-07-31 2019-11-05 中国航发南方工业有限公司 For the support device and clinching method in situ for riveting middle (center) bearing oil return pipe mounting seat
CN110561312A (en) * 2019-07-25 2019-12-13 沈阳富创精密设备有限公司 Aviation part press-fitting clamp
CN112139432A (en) * 2020-09-08 2020-12-29 中国航发贵州黎阳航空动力有限公司 Riveting method and riveting tool for part with interference structure at riveting position

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104942206B (en) * 2015-06-17 2016-10-26 沈阳飞机工业(集团)有限公司 Close the anti-clinching method of small space plate nut
CN106363122A (en) * 2016-11-10 2017-02-01 浙江大学 Bent riveting head for aircraft panel horizontal automatic drilling and riveting machine
CN106363122B (en) * 2016-11-10 2018-09-28 浙江大学 A kind of flexure type of the horizontal automatic drill riveter of aircraft target ship applies riveter
CN109604508A (en) * 2018-11-27 2019-04-12 中国航发贵州黎阳航空动力有限公司 A kind of narrow ring cavity depths clinching method and send holding tool
CN110561312A (en) * 2019-07-25 2019-12-13 沈阳富创精密设备有限公司 Aviation part press-fitting clamp
CN110405130A (en) * 2019-07-31 2019-11-05 中国航发南方工业有限公司 For the support device and clinching method in situ for riveting middle (center) bearing oil return pipe mounting seat
CN112139432A (en) * 2020-09-08 2020-12-29 中国航发贵州黎阳航空动力有限公司 Riveting method and riveting tool for part with interference structure at riveting position

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100217

Termination date: 20120514