CN206029663U - Covering assembly fixture - Google Patents
Covering assembly fixture Download PDFInfo
- Publication number
- CN206029663U CN206029663U CN201620981024.4U CN201620981024U CN206029663U CN 206029663 U CN206029663 U CN 206029663U CN 201620981024 U CN201620981024 U CN 201620981024U CN 206029663 U CN206029663 U CN 206029663U
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- Prior art keywords
- covering
- frame
- utility
- model
- correction
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Abstract
The utility model provides an improve that covering assembly fixture belongs to airplane assembling frock, fixture device technical field, especially relates to a covering assembly fixture structure. The utility model provides a convenient operation is simple, has the covering locate function, covering assembly fixture that the product percent of pass is high. The utility model discloses a both ends are provided with the end rib locator in the frame, frame, and the top is provided with nodical locator, flange cardboard and roof beam locator in the frame, and in the frame transversely arrange and be provided with six appearance cardboards in the bottom, rib locator in the middle of being provided with on the appearance cardboard, its characterized in that: be provided with two covering calibration card boards between the three appearance cardboard in left side, also be provided with two covering calibration card boards between the three appearance cardboard in right side, covering calibration card board includes the connecting seat that links to each other with the frame, and the connecting seat top is provided with the correction frame, is provided with on the upper beam of correction frame and avoids the hole.
Description
Technical field
This utility model belongs to aircraft rigger dress, grip device technical field, more particularly to a kind of eyelid covering assembly tooling
The improvement of structure.
Background technology
It is well known that in any machining, can all allow certain range of error.Certainly, in assembling process
Also still allow for certain error to produce, but these little errors can all be superimposed and all of error will all be accumulated to finally
In one procedure.Carry out in assembling process in eyelid covering, produced error includes：1st, each part is entered by fabrication hole in frock
During row positioning, some tiny errors will be produced.
When the 2nd, setting-out and drilling is carried out on each part, can produce operating error.
When the hole on rib and beam being led system on eyelid covering the 3, operating error will be produced.
When the 4th, being attached eyelid covering and other parts by the form for riveting, operating error will be also produced.
Above-mentioned deviation accumulation can not look down upon to together, cannot but avoid.
When carrying out the eyelid covering last one procedure of processing in traditional frock, its way is directly to carry out picture on one layer of eyelid covering
Line and hole is drilled, as traditional frock self-condition is limited so as to eyelid covering cannot be corrected, the control of hole position, base at all
Originally determined by the proficiency and experience of workman.So eyelid covering is after undercarriage riveting, it will be found that eyelid covering is due to originals such as error stress
Because it is caused agitate, bend, assembling assembly is unsatisfactory for technical requirements the problems such as, the problems referred to above will cause product be reprocessed,
The serious product that will cause directly is scrapped.
The content of the invention
This utility model is aiming at the problems referred to above, there is provided a kind of easy to operate simple, with eyelid covering positioning function, product
The high eyelid covering assembly tooling of qualification rate.
In order to realize above-mentioned purpose of the present utility model, this utility model is adopted the following technical scheme that, this utility model bag
Framework is included, two ends are provided with top in end rib localizer, framework and are provided with intersection point localizer, flange clamp and beam positioning in framework
Device, laterally arrangement is provided with six profile clamps to framework inner bottom part, is provided with intermediate rib localizer on profile clamp, and its feature exists
In：Two eyelid covering correction clamps are provided between the three profile clamps in left side, are also equipped with two between the profile clamp of three, right side
Individual eyelid covering corrects clamp；The eyelid covering correction clamp includes the connecting seat being connected with framework, is provided with correction box above connecting seat,
It is provided with the upper beam of correction box and hides hole.
As a kind of preferred version of the present utility model, positioning convex and lightening grooves on the upper beam, are additionally provided with.
Used as another kind of preferred version of the present utility model, the correction box is connected with connecting seat by handle nut.
The beneficial effects of the utility model：1st, this utility model is easy to operate simple, and control is accurate, accurately and reliably, safety
Property high, low cost, cost performance is high.
2nd, when this utility model is used, eyelid covering and correction box are clamped by clamping element, so as to be capable of achieving the school to eyelid covering
Just, the hole of hiding in correction box is recycled to drill eyelid covering, it is ensured that, on preferable position, eyelid covering is in riveting for hole position
Afterwards, be not in produced problem in traditional frock, conforming product rate is improved significantly.
3rd, this utility model can make this utility model coordinate other to set by arranging positioning convex on the upper beam of correction box
It is standby to be positioned, so as to can further improve the positioning precision of eyelid covering；And this utility model is arranged on the upper beam of correction box
Lightening grooves, can mitigate weight of the present utility model.
Description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the partial enlarged drawing of Fig. 1.
In accompanying drawing 1 be profile clamp, 2 be rib localizer, 3 be intersection point localizer, 4 be flange clamp, 5 be beam localizer, 6
For eyelid covering correction clamp, 7 be framework, 8 be connecting seat, 9 be handle nut, 10 be correction box, 11 for hide hole, 12 be upper beam,
13 is lightening grooves, 14 is positioning convex.
Specific embodiment
This utility model includes framework 7, and in framework 7, two ends are provided with end rib localizer, and in framework 7, top is provided with intersection point
Localizer 3, flange clamp 4 and beam localizer 5, laterally arrangement is provided with six profile clamps 1, profile clamp 1 to 7 inner bottom part of framework
On be provided with intermediate rib localizer, it is characterised in that：Two eyelid covering correction clamps 6 are provided between the three profile clamps 1 in left side,
Two eyelid covering correction clamps 6 are also equipped between the three profile clamps 1 in right side；The eyelid covering correction clamp 6 includes and 7 phase of framework
Connecting seat 8 even, is provided with correction box 10, is provided with and hides hole 11 on the upper beam 12 of correction box 10 above connecting seat 8.
As a kind of preferred version of the present utility model, positioning convex 14 and lightening grooves on the upper beam 12, are additionally provided with
13。
Used as another kind of preferred version of the present utility model, the correction box 10 passes through handle nut 9 and 8 phase of connecting seat
Even.
Eyelid covering restocking is adjusted by this utility model when last one procedure is carried out, and corrects clamp by four eyelid coverings
6, using clamping tool（It is not shown）Eyelid covering is clamped with eyelid covering correction clamp 6, the correction of eyelid covering is carried out.Now, eyelid covering has been
It is corrected in normal scope, then hides hole 11 by the hole drill system on eyelid covering by what is opened up on eyelid covering correction clamp 6
Out.Now, then carry out undercarriage rivet when, hole position is all on preferable position.So, after being riveted, be not in
Problem in traditional frock.
It is understood that above with respect to specific descriptions of the present utility model, be merely to illustrate this utility model and not
The technical scheme being limited to described by this utility model embodiment, it will be understood by those within the art that, still can be with
This utility model is modified or equivalent, to reach identical technique effect；As long as satisfaction uses needs, all in this reality
Within new protection domain.
Claims (3)
1. a kind of eyelid covering assembly tooling, including framework（7）, framework（7）Interior two ends are provided with end rib localizer, framework（7）On interior
Side is provided with intersection point localizer（3）, flange clamp（4）With beam localizer（5）, framework（7）Laterally arrangement is provided with six to inner bottom part
Individual profile clamp（1）, profile clamp（1）On be provided with intermediate rib localizer, it is characterised in that：The three profile clamps in left side（1）
Between be provided with two eyelid coverings correction clamps（6）, three, right side profile clamp（1）Between be also equipped with two eyelid coverings correction clamps
（6）；The eyelid covering corrects clamp（6）Including with framework（7）Connected connecting seat（8）, connecting seat（8）Top is provided with correction box
（10）, correction box（10）Upper beam（12）On be provided with and hide hole（11）.
2. a kind of eyelid covering assembly tooling according to claim 1, it is characterised in that：The upper beam（12）On be additionally provided with it is fixed
Position is raised（14）And lightening grooves（13）.
3. a kind of eyelid covering assembly tooling according to claim 1, it is characterised in that：The correction box（10）By handle spiral shell
It is female（9）With connecting seat（8）It is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620981024.4U CN206029663U (en) | 2016-08-30 | 2016-08-30 | Covering assembly fixture |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620981024.4U CN206029663U (en) | 2016-08-30 | 2016-08-30 | Covering assembly fixture |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206029663U true CN206029663U (en) | 2017-03-22 |
Family
ID=58302239
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620981024.4U Expired - Fee Related CN206029663U (en) | 2016-08-30 | 2016-08-30 | Covering assembly fixture |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206029663U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382605A (en) * | 2018-03-05 | 2018-08-10 | 江苏恒神股份有限公司 | A kind of assembling jig of carbon fibre composite aircraft door |
| CN108928502A (en) * | 2018-07-05 | 2018-12-04 | 南京航空航天大学 | Assemble the tooling of composite material wing box and the method using tooling assembly wing box |
| CN109866055A (en) * | 2019-04-03 | 2019-06-11 | 西安飞机工业（集团）有限责任公司 | A kind of watchfully rib machine positioning drill jig and localization method |
| CN109877746A (en) * | 2019-04-03 | 2019-06-14 | 西安飞机工业（集团）有限责任公司 | A kind of intensive style leading edge tooling and its assembly method |
| CN112223177A (en) * | 2020-10-11 | 2021-01-15 | 王美娟 | Auxiliary assembly tool for airtight floor test piece |
| CN112373717A (en) * | 2020-10-30 | 2021-02-19 | 哈尔滨飞机工业集团有限责任公司 | Assembly method for variable-curvature welding part structure of airplane |
-
2016
- 2016-08-30 CN CN201620981024.4U patent/CN206029663U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382605A (en) * | 2018-03-05 | 2018-08-10 | 江苏恒神股份有限公司 | A kind of assembling jig of carbon fibre composite aircraft door |
| CN108928502A (en) * | 2018-07-05 | 2018-12-04 | 南京航空航天大学 | Assemble the tooling of composite material wing box and the method using tooling assembly wing box |
| CN108928502B (en) * | 2018-07-05 | 2021-03-19 | 南京航空航天大学 | Tool for assembling composite material wing box and method for assembling wing box by using tool |
| CN109866055A (en) * | 2019-04-03 | 2019-06-11 | 西安飞机工业（集团）有限责任公司 | A kind of watchfully rib machine positioning drill jig and localization method |
| CN109877746A (en) * | 2019-04-03 | 2019-06-14 | 西安飞机工业（集团）有限责任公司 | A kind of intensive style leading edge tooling and its assembly method |
| CN109866055B (en) * | 2019-04-03 | 2020-12-29 | 西安飞机工业（集团）有限责任公司 | Wing rib positioning and drilling clamp and positioning method |
| CN109877746B (en) * | 2019-04-03 | 2023-06-23 | 西安飞机工业（集团）有限责任公司 | Intensive front edge tool and assembly method thereof |
| CN112223177A (en) * | 2020-10-11 | 2021-01-15 | 王美娟 | Auxiliary assembly tool for airtight floor test piece |
| CN112373717A (en) * | 2020-10-30 | 2021-02-19 | 哈尔滨飞机工业集团有限责任公司 | Assembly method for variable-curvature welding part structure of airplane |
| CN112373717B (en) * | 2020-10-30 | 2022-10-11 | 哈尔滨飞机工业集团有限责任公司 | Assembly method for variable-curvature welding part structure of 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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170322 Termination date: 20210830 |