CN203245761U - Push-pull-type positioning device - Google Patents
Push-pull-type positioning device Download PDFInfo
- Publication number
- CN203245761U CN203245761U CN 201320213186 CN201320213186U CN203245761U CN 203245761 U CN203245761 U CN 203245761U CN 201320213186 CN201320213186 CN 201320213186 CN 201320213186 U CN201320213186 U CN 201320213186U CN 203245761 U CN203245761 U CN 203245761U
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- hole
- pin
- positioning
- sliding rod
- sliding bar
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Abstract
The utility model belongs to the technical field of processing equipment, and relates to a push-pull-type positioning device on airplane assembly processing equipment of the filed of aeronautical manufacturing. The positioning device comprises a fixture base body, a sliding rod, a support, a positioning pin, a limiting pin and an alignment limiting pin. The support is located on the fixture base body and is fixed; holes where the positioning pin and the alignment limiting pin are installed are formed in the support, the hole where the positioning pin is installed corresponds to a pin hole formed in the side edge of the sliding rod, and the hole of the alignment positioning pin corresponds to a positioning groove in the sliding rod; the positioning groove is formed in the sliding rod; a limiting pin hole is formed in the sliding rod; the distance between the limiting pin hole and the hole where the positioning pin is arranged equals that between the hole where the positioning pin is arranged and the end surface of the support. Because limiting and guiding of the sliding rod and the support are added, the push-pull-type positioning device achieves the purpose that a positioning piece fast and accurately reaches a theoretically correct position, simplifies the operation of workers and improves working efficiency.
Description
Technical field
The utility model belongs to the process equipment technology, relates to the plug-type positioner on the aircraft rigger skill equipment in a kind of Field of Aviation Manufacturing.
Background technology
A large amount of flat welding bearing keeper and tube-in-tube structure keepers of using in traditional aircraft rigger dress, flat part is of a great variety, dismounting and complex installation process.Tube-in-tube structure positioner sliding bar 1 all directions in sleeve 2 are free state, adjust in the process of sliding bar 1, without guiding and stopping means, sleeve 2 is not visible with the fastening screw hole of adjusting sliding bar 1, it to be adjusted to the tram very difficult, thereby strengthened workman's operation easier, greatly reduced production efficiency.Therefore just need a kind of positioner easy to use and quick for installation, accurate, simple to operate of design.
Summary of the invention
The purpose of this utility model proposes a kind of plug-type positioner easy to use and quick for installation.
Technical solution of the present utility model is: positioner comprises type frame matrix 6, sliding bar 1, bearing 2, alignment pin 3, axial limiting pin 4 and aims at spacer pin 5, bearing 2 is located on the type frame matrix 6 and fixes, the hole of alignment pin 3 being installed and aiming at spacer pin 5 is arranged on the bearing 2, the hole that alignment pin 3 is installed is corresponding with the pin-and-hole that sliding bar 1 side arranges, and the hole of aiming at alignment pin 5 is corresponding with the locating slot 7 on the sliding bar 1; Have locating slot 7 on the sliding bar 1, have limit pin hole on the sliding bar 1, the distance between the hole of limit pin hole and installation alignment pin 3 equals the hole of the installation alignment pin 3 on the bearing 2 and the distance of bearing 2 end faces.The utility model has the advantages that: the utility model is by the spacing of increase sliding bar and bearing and guiding, thereby the realization keeper fast, accurately reaches the purpose of theoretical tram.Simplified workman's operation, increase work efficiency, the utility model can make on the one hand sliding bar fast aligning location, make things convenient on the other hand the workman to operate, avoided simultaneously repeatedly a large amount of adjustment and cause because axle and cover wearing and tearing reduce positioning accuracy, the shortening frock problem in service life.The utility model can be widely used in the location of part in the aircraft rigger dress or assembly.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the cutaway view of Fig. 1.
Fig. 3 is the part top view of Fig. 1.
The specific embodiment
Below in conjunction with accompanying drawing the utility model is elaborated.Positioner comprises type frame matrix 6, sliding bar 1, bearing 2, alignment pin 3, axial limiting pin 4 and aims at spacer pin 5, bearing 2 is located on the type frame matrix 6 and fixes, the hole of alignment pin 3 being installed and aiming at spacer pin 5 is arranged on the bearing 2, the hole that alignment pin 3 is installed is corresponding with the pin-and-hole that sliding bar 1 side arranges, and the hole of aiming at alignment pin 5 is corresponding with the locating slot 7 on the sliding bar 1; Have locating slot 7 on the sliding bar 1, have limit pin hole on the sliding bar 1, the distance between the hole of limit pin hole and installation alignment pin 3 equals the hole of the installation alignment pin 3 on the bearing 2 and the distance of bearing 2 end faces.
During manufacturing, each spacing element on sliding bar 1 and the bearing 2 is respectively to insert separately the hole of alignment pin 3 as benchmark, the position of each hole and groove is corresponding one by one, that is: the locating slot 7 on the sliding bar 1 and aligning alignment pin 5 correspondences on the bearing 2, the bus of the spacer pin 4 on the sliding bar 1 is corresponding with the sleeve end face of bearing 2.
During use: bearing 2 is fixed on the type frame matrix 6, the spacer pin 5 of radially aiming on the bearing 2 is slided along the locating slot 7 on the sliding bar 1, when the end contact of axial limiting pin 4 and sleeve 2 and insert limit pin hole on the sliding bar 1, like this, basically be exactly the correct axial location of sliding bar 1, at this moment, insert the hole that alignment pin 3 is installed on the sliding bar 1 visual by inserting the hole that alignment pin 3 is installed on the bearing 2, can easily plug alignment pin 3 is installed, the location-plate 8 on the sliding bar 1 namely is in the tram that design needs at this moment.
Claims (1)
1. plug-type positioner, it is characterized in that, positioner comprises type frame matrix (6), sliding bar (1), bearing (2), alignment pin (3), spacer pin (4) and aims at spacer pin (5), it is upper and fixing that bearing (2) is located in type frame matrix (6), the hole that installation alignment pin (3) and aligning spacer pin (5) are arranged on the bearing (2), the hole that alignment pin (3) is installed is corresponding with the pin-and-hole that sliding bar (1) side arranges, and the hole of aiming at alignment pin (5) is corresponding with the locating slot (7) on the sliding bar (1); Have locating slot (7) on the sliding bar (1), sliding bar has limit pin hole on (1), and the distance between the hole of limit pin hole and installation alignment pin (3) equals the hole of the installation alignment pin (3) on the bearing (2) and the distance of bearing (2) end face.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320213186 CN203245761U (en) | 2013-04-24 | 2013-04-24 | Push-pull-type positioning device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320213186 CN203245761U (en) | 2013-04-24 | 2013-04-24 | Push-pull-type positioning device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203245761U true CN203245761U (en) | 2013-10-23 |
Family
ID=49372222
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320213186 Expired - Fee Related CN203245761U (en) | 2013-04-24 | 2013-04-24 | Push-pull-type positioning device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203245761U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103878717A (en) * | 2014-03-17 | 2014-06-25 | 沈阳飞机工业（集团）有限公司 | Novel rapid positioning supporting mechanism |
| CN104708580A (en) * | 2015-02-12 | 2015-06-17 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | Gas compressor fixed blade ring installation tool and usage method thereof |
| CN106272183A (en) * | 2016-09-22 | 2017-01-04 | 无锡威孚力达催化净化器有限责任公司 | Synchronizing moving attitude reference device |
| CN106363331A (en) * | 2016-11-30 | 2017-02-01 | 江西洪都航空工业集团有限责任公司 | Interior and exterior clamping device applied to welding of plane box section |
| CN112192481A (en) * | 2020-11-30 | 2021-01-08 | 中国航空制造技术研究院 | A dimension shape positioner for fuselage section transfers appearance |
| CN112809592A (en) * | 2020-12-07 | 2021-05-18 | 沈阳飞机设计研究所扬州协同创新研究院有限公司 | Positioning pin installation alignment system and method between detachable engine and airplane |
-
2013
- 2013-04-24 CN CN 201320213186 patent/CN203245761U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103878717A (en) * | 2014-03-17 | 2014-06-25 | 沈阳飞机工业（集团）有限公司 | Novel rapid positioning supporting mechanism |
| CN103878717B (en) * | 2014-03-17 | 2016-08-17 | 沈阳飞机工业（集团）有限公司 | Novel quick supporting mechanism for location |
| CN104708580A (en) * | 2015-02-12 | 2015-06-17 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | Gas compressor fixed blade ring installation tool and usage method thereof |
| CN104708580B (en) * | 2015-02-12 | 2019-10-01 | 北京华清燃气轮机与煤气化联合循环工程技术有限公司 | A kind of installation tool and its application method of compressor stator ring |
| CN106272183A (en) * | 2016-09-22 | 2017-01-04 | 无锡威孚力达催化净化器有限责任公司 | Synchronizing moving attitude reference device |
| CN106272183B (en) * | 2016-09-22 | 2017-11-10 | 无锡威孚力达催化净化器有限责任公司 | Synchronizing moving attitude reference device |
| CN106363331A (en) * | 2016-11-30 | 2017-02-01 | 江西洪都航空工业集团有限责任公司 | Interior and exterior clamping device applied to welding of plane box section |
| CN112192481A (en) * | 2020-11-30 | 2021-01-08 | 中国航空制造技术研究院 | A dimension shape positioner for fuselage section transfers appearance |
| CN112192481B (en) * | 2020-11-30 | 2021-04-13 | 中国航空制造技术研究院 | A dimension shape positioner for fuselage section transfers appearance |
| CN112809592A (en) * | 2020-12-07 | 2021-05-18 | 沈阳飞机设计研究所扬州协同创新研究院有限公司 | Positioning pin installation alignment system and method between detachable engine and airplane |
| CN112809592B (en) * | 2020-12-07 | 2022-05-24 | 沈阳飞机设计研究所扬州协同创新研究院有限公司 | Positioning pin installation alignment system and method between detachable engine and airplane |
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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: 20131023 Termination date: 20160424 |