CN103754751B - The erecting by overhang of a kind of aircraft skin part handling - Google Patents
The erecting by overhang of a kind of aircraft skin part handling Download PDFInfo
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- CN103754751B CN103754751B CN201410047883.1A CN201410047883A CN103754751B CN 103754751 B CN103754751 B CN 103754751B CN 201410047883 A CN201410047883 A CN 201410047883A CN 103754751 B CN103754751 B CN 103754751B
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- slide rail
- slide
- slide block
- slide bar
- rail beam
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Abstract
A kind of erecting by overhang for the handling of aircraft skin part, containing slide rail beam, slide bar, fast-dismounting self-locking presss from both sides, connect suspension ring, the upside of slide rail beam is fixed with connection suspension ring, the downside of slide rail beam is the shape of falling T slide rail, the body of slide rail beam is provided with multiple knock hole perpendicular to slide rail direction, slide bar is rigidity bearing rod, slide block is fixed with in the middle part of it, slide block has the cross section of inlaying with slide rail, slide block is provided with the connecting through hole corresponding with knock hole, slide bar is embedded on slide rail by the slide block at middle part, the line of centers of slide bar is vertical with slide rail direction, the middle part of slide bar and two ends are provided with the hook of fixing fast-dismounting self-locking folder.
Description
Technical field
The present invention relates to the hoisting technology in aeronautical manufacture, is directly erecting by overhang during a kind of aircraft skin part handling, a kind of adjustable bedstead structure of handling covering.
Background technology
In the manufacturing process of aircraft skin, often need to forward covering to another station by a station week, and usually use traverse crane in factory building to lift by crane when carrying out covering turnover.Because covering is thin-slab structure (for ARJ21 aircraft target ship covering, its oad is 1.6 × 1500 × 7000mm), its poor rigidity, when using crane handling covering in production process, the vertical of its vertical handling is hung mode by adopt more.But be shaped at covering and in digital control milling process, often need covering level to be carried on service platform.Existing handling mode or a dead lift is adopted easily to make covering fracture or produce folding line.
Summary of the invention
The object of the present invention is to provide a kind of novel erecting by overhang conveniently hanging aircraft skin.
A kind of erecting by overhang for the handling of aircraft skin part, containing slide rail beam, slide bar, fast-dismounting self-locking presss from both sides, connect suspension ring, it is characterized in that the upside of described slide rail beam is fixed with connection suspension ring, the downside of slide rail beam is the shape of falling T slide rail, the body of slide rail beam is provided with multiple knock hole perpendicular to slide rail direction, the line of centres of this knock hole is parallel with the slide rail of slide rail beam, slide bar is rigidity bearing rod, slide block is fixed with in the middle part of it, slide block has the cross section of inlaying with slide rail, slide block is provided with the connecting through hole corresponding with knock hole, slide bar is embedded on slide rail by the slide block at middle part, the line of centers of slide bar is vertical with slide rail direction, the middle part of slide bar and two ends are provided with the hook of fixing fast-dismounting self-locking folder.
The beneficial effect of the application is: 1) hoisting point position of this erecting by overhang is adjustable, is applicable to the sheet material hanging of all size; 2) aircraft skin can be realized flat to hang, vertically hang function, meet the actual needs of aircraft skin production scene; 3) light structure is simple, and steadily flat the hanging conveniently realizing the thick skin part of the handling of skin part, particularly large scale is hung with vertical.
Below in conjunction with accompanying drawing, this embodiment is described in further detail.
Accompanying drawing explanation
Fig. 1 is erecting by overhang structural representation.
Fig. 2 is the operating diagram that device puts down when hanging.
Fig. 3 is the operating diagram that device stands when hanging.
Fig. 4 is that slide block installs cross-sectional view.
Fig. 5 is that cross-sectional view installed by slide bar.
Number description: 1 slide rail beam, 2 connect suspension ring, 3 fast-dismounting self-locking folders, 4 slide bars, 5 lifting ropes, 6 slide blocks, 7 knock holees, 8 aircraft skins, 9 hooks.
Specific embodiment
See accompanying drawing, the erecting by overhang for the handling of aircraft skin part of the application, containing slide rail beam 1, slide bar 4, fast-dismounting self-locking folder 2, connect suspension ring 2, described slide rail beam 1 is an i-shaped beams structure, be fixed with on the upside of it and connect suspension ring 2 for being connected with crane, the downside of slide rail beam 1 is the shape of falling T slide rail, the body of slide rail beam is provided with multiple knock hole 7 perpendicular to slide rail direction, the line of centres of this knock hole is parallel with the slide rail of slide rail beam, slide bar 4 is rigidity bearing rods, slide block 6 is fixed with in the middle part of it, slide block 6 has the cross section of inlaying with slide rail, slide block is provided with the connecting through hole corresponding with knock hole, in enforcement, slide bar is embedded on slide rail by the slide block at middle part, the line of centers of slide bar is vertical with slide rail direction, the middle part of slide bar and two ends are provided with the hook 9 of fixing fast-dismounting self-locking folder.In enforcement, slide block also can be embedded in separately on slide rail, the fast-dismounting self-locking folder 3 of hook 9 and lifting rope connection is provided with equally in the bottom of slide block, the slide bar no matter being independent slide block or being fixed by slide block, its position on slide rail beam can regulate as required, after adjustment puts in place, by locating dowel pin, the knock hole on the connecting bore on slide block and slide rail beam is connected and fixed, hurry up self-locking clip 3 to be the finished product clamp gripping members lifting ropes 5 be connected on hook 9 for clamping skin part 8 be preferably flexible strand.
During use, select different structures according to different suspending ways, put down choice for use slide bar when hanging, stand when hanging and select to be used alone slide block.Determine rational hoisting point position and quantity according to covering size, the position of adjustment slide bar or slide block is also fixing fast.After hanging up properly the lifting rope of band fast-dismounting self-locking folder according to the principle of hoisting point position symmetry, can handling covering.
Claims (1)
1. the erecting by overhang for the handling of aircraft skin part, containing slide rail beam, slide bar, fast-dismounting self-locking presss from both sides, connect suspension ring, it is characterized in that the upside of described slide rail beam is fixed with connection suspension ring, the downside of slide rail beam is the shape of falling T slide rail, the body of slide rail beam is provided with multiple knock hole perpendicular to slide rail direction, the line of centres of this knock hole is parallel with the slide rail of slide rail beam, slide bar is rigidity bearing rod, slide block is fixed with in the middle part of it, slide block has the cross section of inlaying with slide rail, slide block is provided with the connecting through hole corresponding with knock hole, slide bar is embedded on slide rail by the slide block at middle part, the line of centers of slide bar is vertical with slide rail direction, the middle part of slide bar and two ends are provided with the hook of fixing fast-dismounting self-locking folder, slide block is also had to be embedded in separately on slide rail, the fast-dismounting self-locking folder of hook and lifting rope connection is provided with equally in the bottom of slide block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410047883.1A CN103754751B (en) | 2014-02-11 | 2014-02-11 | The erecting by overhang of a kind of aircraft skin part handling |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410047883.1A CN103754751B (en) | 2014-02-11 | 2014-02-11 | The erecting by overhang of a kind of aircraft skin part handling |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103754751A CN103754751A (en) | 2014-04-30 |
| CN103754751B true CN103754751B (en) | 2015-08-26 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410047883.1A Active CN103754751B (en) | 2014-02-11 | 2014-02-11 | The erecting by overhang of a kind of aircraft skin part handling |
Country Status (1)
| Country | Link |
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| CN (1) | CN103754751B (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105013911A (en) * | 2015-06-29 | 2015-11-04 | 巨万飞 | Punching device with discharge function |
| CN106517048B (en) * | 2016-10-19 | 2018-12-14 | 中航飞机股份有限公司西安飞机分公司 | A kind of aircraft wing box 180 degree overturning handling method |
| CN107161842B (en) * | 2017-05-27 | 2018-11-02 | 中航成飞民用飞机有限责任公司 | Barrel-shaped skinpiston group parts lift transfer device |
| CN108910679A (en) * | 2018-07-06 | 2018-11-30 | 西安爱生技术集团公司 | A kind of unmanned plane flexible hanger |
| CN109019290A (en) * | 2018-07-24 | 2018-12-18 | 上海江南长兴造船有限责任公司 | A kind of dedicated hanging row lifting container guide rail bracket |
Family Cites Families (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2825474B2 (en) * | 1996-12-09 | 1998-11-18 | 株式会社ホクコン | Combined use |
| CN201458533U (en) * | 2009-07-15 | 2010-05-12 | 湖南广信工业纸板股份有限公司 | Insulation cardboard spreader |
| CN201703967U (en) * | 2010-05-19 | 2011-01-12 | 山东海利丰地源热泵有限责任公司 | Adjustable suspending support frame |
| CN202030435U (en) * | 2011-04-18 | 2011-11-09 | 北京航天发射技术研究所 | Multi-point self-balancing hoisting sling |
| CN202046793U (en) * | 2011-05-09 | 2011-11-23 | 上海国际港务(集团)股份有限公司宝山分公司 | Special strut for ultra-long flexible steel plate |
| CN202265308U (en) * | 2011-10-08 | 2012-06-06 | 杨国栋 | Combined hoisting device for pipeline steel plate hoisting |
-
2014
- 2014-02-11 CN CN201410047883.1A patent/CN103754751B/en active Active
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| Publication number | Publication date |
|---|---|
| CN103754751A (en) | 2014-04-30 |
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