CN205834104U - Automatic rivet bracket and the combination type frame of assembly tooling - Google Patents
Automatic rivet bracket and the combination type frame of assembly tooling Download PDFInfo
- Publication number
- CN205834104U CN205834104U CN201620746930.6U CN201620746930U CN205834104U CN 205834104 U CN205834104 U CN 205834104U CN 201620746930 U CN201620746930 U CN 201620746930U CN 205834104 U CN205834104 U CN 205834104U
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- assembly tooling
- bracket
- automatic rivet
- automatic
- rivet bracket
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- 241000538562 Banjos Species 0.000 claims abstract description 10
- 238000005553 drilling Methods 0.000 abstract description 11
- 210000000744 eyelid Anatomy 0.000 abstract description 9
- 238000010276 construction Methods 0.000 abstract description 3
- 238000000034 method Methods 0.000 abstract description 3
- 238000000926 separation method Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 4
- 230000003044 adaptive effect Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 241001074085 Scophthalmus aquosus Species 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Abstract
This utility model discloses the combination type frame of a kind of automatic rivet bracket and assembly tooling, including: assembly tooling part, automatic rivet bracket part, banjo fixing butt jointing；Described assembly tooling part is connected by banjo fixing butt jointing with automatic rivet bracket part, and described assembly tooling part is made up of frame localizer, compactor and assembling skeleton, and described automatic rivet bracket part is made up of shape clamp and bracket in stringer localizer, eyelid covering.This utility model, by automatic rivet bracket and the combination of assembly tooling and separation, makes the assembly process of aircraft target ship simplify.This utility model simple in construction, be applicable to aircraft target ship assembling, be conducive to facilitating the automatic Drilling/Riveting of aircraft target ship.
Description
Technical field
This utility model relates to the technical field of aircraft target ship subassembler dress, particularly relates to a kind of automatic rivet bracket
Combination type frame with assembly tooling.
Background technology
Along with the continuous progress of technology, the use of the automatic Drilling/Riveting equipment for assembling aircraft target ship assembly is more and more wider
General, the use for the automatic Drilling/Riveting type frame of assembling aircraft target ship assembly requires more and more higher.Form the main of aircraft target ship
Part includes deckle board, stringer and eyelid covering, after needing a set of assembly tooling that part is riveted in advance, a set of location bracket is installed on automatically
Boring and complete residue riveting on riveting equipment, the use complex procedures of two set frocks repeats.For improving aircraft target ship automatic Drilling/Riveting efficiency
And shorten the manufacturing cycle, and saving quantity and the purpose of cost of frock, those skilled in the art is devoted to exploitation one always
Simple in construction, be applicable to aircraft target ship assembling, be conducive to the automatic Drilling/Riveting torr that the automatic Drilling/Riveting operation facilitating aircraft target ship simplifies
Frame and the combination type frame of assembly tooling.
Utility model content
Because above-mentioned the deficiencies in the prior art, the utility model proposes a kind of simple in construction, be applicable to aircraft target ship dress
Join, be conducive to the combination type frame of automatic rivet bracket that the automatic Drilling/Riveting operation facilitating aircraft target ship simplifies and assembly tooling.
For achieving the above object, this utility model provides the combination type frame of a kind of automatic rivet bracket and assembly tooling,
Including: assembly tooling part, automatic rivet bracket part, banjo fixing butt jointing；Described assembly tooling part and described automatic Drilling/Riveting torr
Frame part is connected by described banjo fixing butt jointing, and described assembly tooling part is made up of frame localizer, compactor and assembling skeleton, institute
State automatic rivet bracket part to be made up of shape clamp and bracket in stringer localizer, eyelid covering.
Having the beneficial effect that of the combination type frame of a kind of automatic rivet bracket of this utility model and assembly tooling:
Automatic rivet bracket of the present utility model is simple with the combined shelf structure of assembly tooling, it is adaptable to aircraft target ship fills
Join, be conducive to the automatic Drilling/Riveting operation facilitating aircraft target ship to simplify.This utility model adaptive in described assembly tooling part and
The connection of described automatic rivet bracket part and two states of separation, it is achieved the assembling use of aircraft target ship and automatic rivet bracket
The function used.
Accompanying drawing explanation
Fig. 1 is the automatic rivet bracket combined shelf structure schematic diagram with assembly tooling of the present embodiment.
Detailed description of the invention
As shown in accompanying drawing 1, a kind of automatic rivet bracket of the present embodiment and the combination type frame of assembly tooling, including: assembling
Frock part 1, automatic rivet bracket part 2, banjo fixing butt jointing 3；Described assembly tooling part 1 is led to automatic rivet bracket part 2
Cross banjo fixing butt jointing 3 to connect, described assembly tooling part 1 by frame localizer 4, compactor 5 and assembling skeleton 6 form, described automatically
Bore riveting bracket portion 2 to be made up of shape clamp 8 in stringer localizer 7, eyelid covering and bracket 9.
A kind of automatic rivet bracket of the present embodiment is as follows with the concrete application of the combination type frame of assembly tooling:
Require adaptive in described assembly tooling part, to arrange frame localizer, compactor according to aircraft target ship trim designs
With assembling skeleton, aircraft deckle board is fixed clamping on described frame localizer, compactor, in described automatic rivet bracket part
Shape clamp in stringer localizer, eyelid covering is set, aircraft stringer and eyelid covering are fixed clamping shape in described stringer localizer, eyelid covering
On clamp, in described frame localizer, compactor, stringer localizer and eyelid covering, shape clamp is prior art generally in the art, this
Field those of ordinary skill can obviously assemble, and does not repeats them here.Workman is in automatic rivet bracket and assembling
After aircraft deckle board, stringer and eyelid covering being completed the assembly manipulations such as pre-riveting in the combination type frame of frock, with crane by described automatically
Bore the overall described banjo fixing butt jointing connected upwardly away from described assembly tooling part of riveting bracket portion and aircraft target ship, will described oneself
Dynamic brill riveting bracket portion and aircraft target ship are connected with automatic Drilling/Riveting equipment entirely through described banjo fixing butt jointing, carry out automatic drill riveter
Make.After completing product undercarriage, described automatic rivet bracket part is reinstalled and docks with described the described of assembly tooling part
Joint.Make aircraft target ship assembly process simplify by being applied in combination of frock, be effectively increased the use effect of automatic Drilling/Riveting equipment
Rate also shortens the manufacturing cycle, saves quantity and the hall space of frock, adds benefit.
Preferred embodiment of the present utility model described in detail above.Should be appreciated that the ordinary skill people of this area
Member just can make many modifications and variations according to design of the present utility model without creative work.Therefore, all technology neck
In territory, technical staff passes through logical analysis, reasoning or limited reality on the basis of existing technology according to design of the present utility model
Test available technical scheme, all should be in the protection domain being defined in the patent claims.
Claims (1)
1. an automatic rivet bracket and the combination type frame of assembly tooling, it is characterised in that including: assembly tooling part, automatic drill
Riveting bracket portion, banjo fixing butt jointing；Described assembly tooling part is connected by banjo fixing butt jointing with automatic rivet bracket part, described dress
Allotment of labor's dress part is made up of frame localizer, compactor and assembling skeleton, and described automatic rivet bracket part is by stringer localizer, illiteracy
Intradermal shape clamp and bracket composition.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620746930.6U CN205834104U (en) | 2016-07-15 | 2016-07-15 | Automatic rivet bracket and the combination type frame of assembly tooling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620746930.6U CN205834104U (en) | 2016-07-15 | 2016-07-15 | Automatic rivet bracket and the combination type frame of assembly tooling |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205834104U true CN205834104U (en) | 2016-12-28 |
Family
ID=57619961
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620746930.6U Active CN205834104U (en) | 2016-07-15 | 2016-07-15 | Automatic rivet bracket and the combination type frame of assembly tooling |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205834104U (en) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN108972422A (en) * | 2018-09-19 | 2018-12-11 | 陕西飞机工业（集团）有限公司 | A kind of general-purpose aircraft siding positioning bracket |
| CN110216235A (en) * | 2019-06-03 | 2019-09-10 | 西安飞机工业（集团）有限责任公司 | A kind of flexible fuselage wallboard assembly tooling and assembly method based on measured data |
| CN110877221A (en) * | 2019-12-04 | 2020-03-13 | 北京神工科技有限公司 | Stringer skin tool structure |
| CN111977017A (en) * | 2020-07-15 | 2020-11-24 | 成都飞机工业（集团）有限责任公司 | Airplane type frame clamping plate based on variable-proportion scissor fork mechanism |
| CN112497107A (en) * | 2020-11-26 | 2021-03-16 | 首都航天机械有限公司 | Pre-assembly method suitable for drilling and riveting of extra-large-diameter carrier rocket cabin section |
| CN112676839A (en) * | 2020-12-17 | 2021-04-20 | 中航沈飞民用飞机有限责任公司 | Composite tool for assembling and milling composite material part of airplane |
| US11866201B2 (en) | 2022-05-03 | 2024-01-09 | The Boeing Company | Method and apparatus for the application of frame to fuselage pull-up force via fuselage skin waterline tensioning |
-
2016
- 2016-07-15 CN CN201620746930.6U patent/CN205834104U/en active Active
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN107499530B (en) * | 2017-08-21 | 2023-08-25 | 大连四达高技术发展有限公司 | Digital processing and assembling system for aircraft wall panels |
| CN108972422A (en) * | 2018-09-19 | 2018-12-11 | 陕西飞机工业（集团）有限公司 | A kind of general-purpose aircraft siding positioning bracket |
| CN110216235A (en) * | 2019-06-03 | 2019-09-10 | 西安飞机工业（集团）有限责任公司 | A kind of flexible fuselage wallboard assembly tooling and assembly method based on measured data |
| CN110216235B (en) * | 2019-06-03 | 2024-02-09 | 西安飞机工业（集团）有限责任公司 | Flexible fuselage wall plate assembly tool and assembly method based on measured data |
| CN110877221A (en) * | 2019-12-04 | 2020-03-13 | 北京神工科技有限公司 | Stringer skin tool structure |
| CN110877221B (en) * | 2019-12-04 | 2021-11-09 | 北京神工科技有限公司 | Stringer skin tool structure |
| CN111977017A (en) * | 2020-07-15 | 2020-11-24 | 成都飞机工业（集团）有限责任公司 | Airplane type frame clamping plate based on variable-proportion scissor fork mechanism |
| CN112497107B (en) * | 2020-11-26 | 2022-08-23 | 首都航天机械有限公司 | Pre-assembly method suitable for drilling and riveting of extra-large-diameter carrier rocket cabin section |
| CN112497107A (en) * | 2020-11-26 | 2021-03-16 | 首都航天机械有限公司 | Pre-assembly method suitable for drilling and riveting of extra-large-diameter carrier rocket cabin section |
| CN112676839B (en) * | 2020-12-17 | 2021-12-03 | 中航沈飞民用飞机有限责任公司 | Composite tool for assembling and milling composite material part of airplane |
| CN112676839A (en) * | 2020-12-17 | 2021-04-20 | 中航沈飞民用飞机有限责任公司 | Composite tool for assembling and milling composite material part of airplane |
| US11866201B2 (en) | 2022-05-03 | 2024-01-09 | The Boeing Company | Method and apparatus for the application of frame to fuselage pull-up force via fuselage skin waterline tensioning |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 200231, 3rd floor, No. 11, Lane 100, Huaji Road, Xuhui District, Shanghai Patentee after: Shanghai Shangfei Aircraft Equipment Manufacturing Co.,Ltd. Address before: 200231, 3rd floor, No. 11, Lane 100, Huaji Road, Xuhui District, Shanghai Patentee before: SHANGHAI SHANGFEI AIRCRAFT EQUIPMENT MANUFACTURING Co.,Ltd. |
|
| CP03 | Change of name, title or address |