CN106514343A - Positioning tool and method for automatic drilling and riveting of aircraft panels - Google Patents
Positioning tool and method for automatic drilling and riveting of aircraft panels Download PDFInfo
- Publication number
- CN106514343A CN106514343A CN201611155347.9A CN201611155347A CN106514343A CN 106514343 A CN106514343 A CN 106514343A CN 201611155347 A CN201611155347 A CN 201611155347A CN 106514343 A CN106514343 A CN 106514343A
- Authority
- CN
- China
- Prior art keywords
- positioning
- locating
- product
- plate
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q3/00—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
- B23Q3/02—Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
- B23Q3/06—Work-clamping means
- B23Q3/062—Work-clamping means adapted for holding workpieces having a special form or being made from a special material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21J—FORGING; HAMMERING; PRESSING METAL; RIVETING; FORGE FURNACES
- B21J15/00—Riveting
- B21J15/38—Accessories for use in connection with riveting, e.g. pliers for upsetting; Hand tools for riveting
- B21J15/42—Special clamping devices for workpieces to be riveted together, e.g. operating through the rivet holes
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Automatic Assembly (AREA)
- Connection Of Plates (AREA)
- Drilling And Boring (AREA)
Abstract
The invention provides a positioning tool and method for automatic drilling and riveting of aircraft panels. The positioning tool comprises a frame, connecting plates, positioning plates, positioning clamping plates, positioning connecting bases, contour positioning parts and skin compressing parts. The positioning tool can meet the positioning requirement for automatic drilling and riveting of different aircraft panel products by adjusting positions of the clamping plates on the frame and adjusting the contour positioning parts installed on the clamping plates, use is convenient and rapid, errors are not prone to occur, and tool storage space is greatly saved. Identifications, corresponding to product objects, of the positioning clamping plates, the positioning plates, positioning holes and positioning holes of the adjustable contour positioning parts on the frame are clear, and all the components are not prone to be wrongly used; and adjustment of the positions of the clamping plates and adjustment of positions of positioning shaft ends of the contour positioning parts are both achieved through sliding rails, use is convenient, and operation is easy.
Description
Technical field
The application is related to aircraft manufacturing technical field, and particularly a kind of aircraft target ship automatic punching rivets positioning tool and determines
Position method.
Background technology
In present generation aircraft manufacture process, for the efficiency and required precision more and more higher of Standard connection, thus with certainly
Dynamicization punching system, automatization's drilling connection equipment that automatic Drilling/Riveting system is representative have been obtained in aircraft assembling process extensively
Application.Have that drilling/riveting quality is good, production efficiency is high, labor condition good due to automatization's drilling and automatic Drilling/Riveting Technology,
The features such as operation is easily grasped, thus the development of China's aeronautical manufacture riveting technology is greatly facilitated.
The either automatization's punching system based on industrial robot or large-size numerical control machine, or by automatic Drilling/Riveting
The automatic Drilling/Riveting system that machine and numerical control bracket are constituted, it is necessary to which having, aircraft product component is carried out the positioning tool of positioning clamping.
The traditional structure forms of such frock have two kinds：A kind of is the joint angle for being provided for connecting on universal bracket profile clamp
Seat, for different product objects, the different locating clamp plate of more transducer set；Another kind is the form of " big frame covers little frame ", i.e., just
It is that little frame is arranged in big general peripheral frame fixes to clamp dress for each different product, the little frame of positioning of design specialized
Put.This two kinds of versions have application in practice, but also expose some problems：For clamp plate type is changed, due to difference
The different locating clamp plate of product needed, clamp quantity are more, change clamp when in use and carefully must recognize, clamp changes workload
Greatly, and easily malfunction；For " big frame covers little frame " formula, different product object has special positioning tool, not error-prone during use,
But as a brill riveting system needs to undertake the brill riveter works of multiple types, numerous wall-board products so that the quantity of little peripheral frame
It is huge many, and then the floor space for causing little peripheral frame storage needs very big, in addition every time use when need little peripheral frame to be lifted to big
In peripheral frame, as little peripheral frame is rigidly poor, location and installation is difficult, and installation period is long.
For case above, need to design, manufacture one kind and can facilitate operative, reduce error probability, and can save
Parking space, and the aircraft target ship automatic punching riveting positioning tool structure that manufacturing cost is greatly reduced, to adapt to the modern times
The new demand of aircraft manufacturing technology development.
The content of the invention
In order to solve the above problems, the invention provides a kind of positioning tool knot for the riveting of aircraft target ship automatic punching
Structure, the structure can be just suitable for by adjusting the profile keeper of position of the clamp on framework and adjustment on clamp
The positioning requirements of different aircraft target ship product automatic punching rivetings, it is convenient to use, it is not error-prone, and greatly save frock
Memory space.
A kind of positioning tool of aircraft target ship automatic punching riveting, including it is framework, connecting plate, location-plate, locating clamp plate, fixed
Position connecting seat, profile keeper, compacting skin part, framework are rectangular frame structure, and framework termination is provided with connecting plate, with system automatically
Hole riveting system support frame connection；Two longitudinal beam upper surfaces of framework are provided with two parallel guide rails, are provided with the outside of guide rail
Location-plate, is formed with the location hole of correspondence difference wall-board product, and identifies product information on location-plate, a bottom that is located by connecting is provided with
The slide block that can be slided on guide rail；The seat that is located by connecting is provided with for fixing the connecting hole of its position on framework, is located by connecting
Seat is fixed by fastening screw with location-plate；Locating clamp plate across between two longerons, locating clamp plate two ends and two guide rails
The upper corresponding seat connection that is located by connecting, determines the lengthwise position of locating clamp plate according to the position of location-plate upper Positioning holes, per block
Multiple profile keepers are installed on locating clamp plate, each profile keeper is provided with one and can stretch along the carrying out of profile normal direction
The locating shaft of adjustment, while adjusting the locating shaft on multiple profile keepers so as to position the wall that shaft end forms corresponding position
Panel products shape, product are fitted in the positioning shaft end of profile keeper, and the compacting skin part installed in locating clamp plate two ends will be produced
Product are compressed, and complete product orientation.Profile keeper is fixed by base plate, locating axle seat, locating shaft, guide finger, spacer pin and hemispherical
Position shaft end composition, base plate are connected on locating clamp plate, are suitable for profile keeper by using different dowel holes different
Product configuration, locating axle seat are used to support locating shaft and have guide effect, by leading thereon when locating shaft bounces back and be overhanging
Movement locus are limited to groove and the guide finger being installed on locating axle seat, locating shaft is overhanging to fix its position using spacer pin in place afterwards
Put, the termination of locating shaft is provided with the hemispherical positioning shaft end for supporting product design.
The method positioned using the positioning tool, is comprised the following steps：
1 according to the location hole identification information for being arranged on framework upper location-plate, by all locating clamp plate position adjustments to needs
Bore the product space of riveting.
On 2 pairs of each locating clamp plates, the positioning shaft end of profile keeper is adjusted according to location hole mark.
After 3 check that all dowel holes are consistent with the mark that need to bore riveting product object, wall-board product is placed in into positioning
In frock, position of the wallboard in frock is determined using wallboard edge block piece, by the wallboard profile on locating clamp plate
Compacting skin is fitted in the positioning shaft end of profile keeper by compacting skin part, implements drilling with riveting.
4 when the hole hindered to locating clamp plate gear carries out brill riveting, first by the positioning shaft end retraction of profile keeper on clamp, from
Open product, then clamp along guide rail to vertically moving, with the location hole positioning of corresponding product on location-plate, then profile is positioned
Part is adjusted to the position of drilled product, can implement to supplement drilling riveting work after compressing eyelid covering.
The mark of locating clamp plate, location-plate, location hole and adjustable profile keeper location hole corresponding product object on framework
Know clear, not easy-to-use mistake；And the adjustment of clamp position and profile keeper locating shaft end position is realized by slide rail, is used
It is convenient, it is simple to operate.
Description of the drawings
Fig. 1 is aircraft target ship automatic punching riveting positioning tool structural representation.
Fig. 2 is circuit theory schematic diagram.
Fig. 3 is locating clamp plate structural representation.
Fig. 4 is profile keeper schematic diagram.
Fig. 5 is compacting skin part schematic diagram.
Fig. 6 is the holder structure schematic diagram that is located by connecting.
Fig. 7 is wallboard edge block piece schematic diagram.
Fig. 8 is profile keeper schematic diagram.
In Fig. 1 to Fig. 8：1st, framework；2nd, guide rail；3rd, locating clamp plate；4th, be located by connecting seat；5th, location-plate；6th, fastening screw；
7th, profile keeper；8th, compacting skin part；10th, slide block；11st, wallboard edge block piece；12nd, base plate；13rd, locating axle seat；14th, position
Axle；15th, guide finger；16th, limit bolt；17th, hemispherical positioning shaft end
Specific embodiment
Below in conjunction with accompanying drawing, the present invention is described in further detail.
As Figure 1-Figure 8, it is a kind of positioning tool of aircraft target ship automatic punching riveting, including framework 1, connecting plate, fixed
Position plate 5, locating clamp plate 3, the seat 4 that is located by connecting, profile keeper 7, compacting skin part 8, framework is rectangular frame structure, frame end
Head is provided with connecting plate, is connected with automatic punching riveting system support frame；1 two longitudinal beam upper surfaces of framework be provided with two it is parallel
Guide rail 2, location-plate 5 is provided with the outside of guide rail 2, the location hole of correspondence difference wall-board products is formed with location-plate 5, and product is identified
Product information, 4 bottom of seat that is located by connecting are provided with the slide block 10 that can be slided on guide rail 2；It is located by connecting on seat and 4 is provided with for fixing which
The connecting hole of position on framework 1, the seat 4 that is located by connecting are fixed by fastening screw 6 with location-plate 5；Locating clamp plate 3 is across two
Between bar longeron, 3 two ends of locating clamp plate the be located by connecting seat 4 corresponding with two guide rails 2 connects, according to fixed on location-plate 5
The position in position hole determines the lengthwise position of locating clamp plate 3, is provided with multiple profile keepers 7, outside each on every piece of locating clamp plate 3
Shape keeper 7 is provided with one can be along the locating shaft 14 of the flexible adjustment of the carrying out of profile normal direction, while adjusting multiple profile positioning
Locating shaft 14 on part 7 so as to position the wall-board product shape that shaft end forms corresponding position, product is fitted in profile keeper
Product is compressed by 7 positioning shaft end, the compacting skin part 8 installed in 3 two ends of locating clamp plate, completes product orientation.
As shown in figure 8, profile keeper 7 is by base plate 12, locating axle seat 13, locating shaft 14, guide finger 15,16 and of spacer pin
Hemispherical positioning shaft end 17 constitutes, and base plate 12 is connected on locating clamp plate 3, positions profile by using different dowel holes
Part 7 is suitable for different product configurations, and locating axle seat 13 is used to support locating shaft 14 and with guide effect, locating shaft 14 bounce back and
Movement locus are limited by gathering sill thereon and the guide finger 15 being installed on locating axle seat 13 when overhanging, locating shaft 14 is overhanging
Its position is fixed using spacer pin 16 afterwards in place, the termination of locating shaft 14 is provided with the hemispherical positioning shaft end for supporting product design
17。
When being positioned using the positioning tool
1st, according to the location hole identification information for being arranged on 1 upper location-plate 5 of framework, by 3 position adjustment of all locating clamp plates extremely
Need to bore the product space of riveting,
2nd, the positioning shaft end of profile keeper 7 on each locating clamp plate 3 is adjusted according to location hole mark
3rd, after checking that all dowel holes are consistent with the mark that need to bore riveting product object, wall-board product is placed in into this fixed
In the frock of position, position of the wallboard in frock is determined using wallboard edge block piece 11, by the eyelid covering on locating clamp plate 3
Compacting skin is fitted in the positioning shaft end of profile keeper 7 by compressing member 8, implements drilling with riveting
4th, when the hole hindered to the gear of locating clamp plate 3 carries out brill riveting, first by the locating shaft of profile keeper 7 on locating clamp plate 3
End retraction, leave product, then locating clamp plate 3 along guide rail 2 to vertically moving, with the location hole of corresponding product on location-plate 3
Positioning, then profile keeper 7 is adjusted to the position of drilled product, can implement to supplement drilling riveting work after compressing eyelid covering
Make.
Claims (3)
1. the positioning tool that a kind of aircraft target ship automatic punching is riveted, including framework, connecting plate, location-plate, locating clamp plate, positioning
Connecting seat, profile keeper, compacting skin part, framework are rectangular frame structure, and framework termination is provided with connecting plate, with automatic punching
Riveting system support frame connects；Two longitudinal beam upper surfaces of framework are provided with two parallel guide rails, are provided with fixed on the outside of guide rail
Position plate, is formed with the location hole of correspondence difference wall-board product, and identifies product information on location-plate, a bottom that is located by connecting is provided with can
The slide block slided on guide rail；The seat that is located by connecting is provided with for fixing the connecting hole of its position on framework, and be located by connecting seat
Fixed by fastening screw with location-plate；Locating clamp plate across between two longerons, on locating clamp plate two ends and two guide rails
The corresponding seat connection that is located by connecting, determines the lengthwise position of locating clamp plate according to the position of location-plate upper Positioning holes, fixed per block
Multiple profile keepers are installed on the clamp of position, each profile keeper is provided with one can be along the flexible tune of the carrying out of profile normal direction
Whole locating shaft, while adjusting the locating shaft on multiple profile keepers so as to position the wallboard that shaft end forms corresponding position
Shape of product, product are fitted in the positioning shaft end of profile keeper, and the compacting skin part installed in locating clamp plate two ends is by product
Compress, complete product orientation.
2. the positioning tool structure that a kind of aircraft target ship automatic punching according to claim 1 is riveted, it is characterised in that institute
The profile keeper stated is made up of base plate, locating axle seat, locating shaft, guide finger, spacer pin and hemispherical positioning shaft end, and base plate connects
It is connected on locating clamp plate, makes profile keeper be suitable for different product configurations, locating axle seat by using different dowel holes
For supporting locating shaft and there is guide effect, locating shaft retraction and it is overhanging when by gathering sill thereon and being installed on locating shaft
Guide finger on seat limits movement locus, and locating shaft is overhanging to fix its position, the termination peace of locating shaft using spacer pin in place afterwards
Equipped with the hemispherical positioning shaft end for supporting product design.
3. usage right requires the method that positioned of positioning tool of the aircraft target ship automatic punching riveting described in 1, including with
Lower step：
3-1 according to installed in framework upper location-plate location hole identification information, by all locating clamp plate position adjustments to need bore
The product space of riveting,
3-2 is adjusted according to location hole mark to the positioning shaft end of profile keeper on each locating clamp plate
After 3-3 checks that all dowel holes are consistent with the mark that need to bore riveting product object, wall-board product is placed in into positioning work
Load onto, position of the wallboard in frock is determined using wallboard edge block piece, covered by the wallboard profile on locating clamp plate
Compacting skin is fitted in the positioning shaft end of profile keeper by skin compressing member, implements drilling with riveting
3-4, is left first by the positioning shaft end retraction of profile keeper on clamp when the hole hindered to locating clamp plate gear carries out brill riveting
Product, then clamp along guide rail to vertically moving, with the location hole positioning of corresponding product on location-plate, then profile keeper
The position of drilled product is adjusted to, can implement to supplement drilling riveting work after compressing eyelid covering.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611155347.9A CN106514343A (en) | 2016-12-14 | 2016-12-14 | Positioning tool and method for automatic drilling and riveting of aircraft panels |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611155347.9A CN106514343A (en) | 2016-12-14 | 2016-12-14 | Positioning tool and method for automatic drilling and riveting of aircraft panels |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106514343A true CN106514343A (en) | 2017-03-22 |
Family
ID=58339928
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611155347.9A Pending CN106514343A (en) | 2016-12-14 | 2016-12-14 | Positioning tool and method for automatic drilling and riveting of aircraft panels |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106514343A (en) |
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| CN107414711A (en) * | 2017-07-31 | 2017-12-01 | 中航通飞华南飞机工业有限公司 | A kind of new rear body is glued assembling jig |
| CN107499530A (en) * | 2017-08-21 | 2017-12-22 | 大连四达高技术发展有限公司 | Aircraft target ship Digital manufacturing assembly system |
| CN107498326A (en) * | 2017-07-04 | 2017-12-22 | 西安飞机工业（集团）有限责任公司 | A kind of flexible frock and localization method for automatic drill riveter |
| CN107717779A (en) * | 2017-10-11 | 2018-02-23 | 北京星航机电装备有限公司 | A kind of outer heat-insulated Rigid ceramic tile cemented in place method |
| CN108131369A (en) * | 2017-12-05 | 2018-06-08 | 北京星航机电装备有限公司 | A kind of cemented in place method of thermal protection component |
| CN108131368A (en) * | 2017-12-05 | 2018-06-08 | 北京星航机电装备有限公司 | A kind of adhesive positioning device of thermal protection component |
| CN108145060A (en) * | 2017-12-22 | 2018-06-12 | 衢州华睿工业设计有限公司 | U-shaped part riveting fixture and U-shaped part clinching method |
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| CN110216611A (en) * | 2019-06-03 | 2019-09-10 | 西安飞机工业（集团）有限责任公司 | A kind of reconfigurable flexible protects type frame and guarantor's type method |
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| CN107498326A (en) * | 2017-07-04 | 2017-12-22 | 西安飞机工业（集团）有限责任公司 | A kind of flexible frock and localization method for automatic drill riveter |
| CN107414711A (en) * | 2017-07-31 | 2017-12-01 | 中航通飞华南飞机工业有限公司 | A kind of new rear body is glued assembling jig |
| CN107414711B (en) * | 2017-07-31 | 2023-12-22 | 中航通飞华南飞机工业有限公司 | Novel assembly jig for cementing of rear machine body |
| CN107499530A (en) * | 2017-08-21 | 2017-12-22 | 大连四达高技术发展有限公司 | Aircraft target ship Digital manufacturing assembly system |
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Application publication date: 20170322 |