CN106347710A - Quick hole repair method - Google Patents
Quick hole repair method Download PDFInfo
- Publication number
- CN106347710A CN106347710A CN201610843730.7A CN201610843730A CN106347710A CN 106347710 A CN106347710 A CN 106347710A CN 201610843730 A CN201610843730 A CN 201610843730A CN 106347710 A CN106347710 A CN 106347710A
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- Prior art keywords
- hole
- repaired
- perforations adding
- diameter
- plug
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Abstract
A quick hole repair method comprises steps as follows: firstly, a plugging cover matched with a to-be-repaired hole is produced from a nylon material according to the diameter of the to-be-repaired hole, the plugging cover comprises a hole plugging part, a hole clamping part and a clamping part, then the plugging cover extends into the to-be-repaired hole to be mounted on a structure of the to-be-repaired hole, the hole plugging part is plugged at the upper part of the structure of the to-be-repaired hole, the hole clamping part is clamped in the middle of the to-be-repaired hole, and the clamping part is fixed at the bottom of the structure of the to-be-repaired hole; finally, paint is sprayed on outer surfaces of the plugging cover and the repaired structure of the to-be-repaired hole, and thus the extra hole is repaired. The plugging cover is simple to produce, convenient to mount, higher in reliability, lower in cost, better in practicability, saves time and labor, can be widely applied to change and repair of parts of aircraft systems at the scientific research stage and has higher practical value, and waste is avoided while the safety is guaranteed.
Description
Technical field
The present invention relates to flying aircraft part recovery technique field, the method in more particularly, to a kind of quick reparation hole.
Background technology
Aircraft is during research and production, often due to the change of technical scheme, leads to the External Shape of production to occur
Change, if part rejection is remake, will result in huge waste, but by after part supplementary processing, occasionally there are unnecessary hole, must
It must be repaired, to ensure the performances such as product appearance, dust-proof, anticorrosion.
Content of the invention
Technical problem solved by the invention is to provide a kind of method in quick reparation hole, to solve above-mentioned background technology
In shortcoming.
Technical problem solved by the invention employs the following technical solutions to realize:
A kind of method in quick reparation hole, specifically comprises the following steps that
1) make matched blanking cover initially with nylon material according to the diameter of perforations adding to be repaired, blanking cover include plug-hole part,
Hole clipping part and gripping part；
2) blanking cover making in step 1) is stretched in the hole to be repaired and be arranged in the structure of perforations adding to be repaired, plug-hole part gets lodged in
The structure upper of perforations adding to be repaired, hole clipping part sticks in the middle part of the structure of perforations adding to be repaired, and gripping part is fixed on the knot of perforations adding to be repaired
Structure bottom；
3) blanking cover is carried out outer surface spray painting together with repairing the structure of the perforations adding to be repaired finishing, that is, complete unnecessary hole is repaiied
Multiple.
In the present invention, the diameter of plug-hole part 2～3mm bigger than the diameter of perforations adding to be repaired, in order to partly to fix plug-hole
In the structure of perforations adding to be repaired.
In the present invention, the diameter of hole clipping part is identical with repairing bore dia, and hole clipping segment thickness and perforations adding to be repaired
Structural thickness is consistent.
In the present invention, gripping part middle setting has the gap of 1～4mm, and gripping part is made up of elastomeric material, makes
Gripping part has certain elasticity, and to ensure that blanking cover sticks into after perforations adding to be repaired, plug-hole part is clamped with gripping part collective effect
The structure of perforations adding to be repaired.
In the present invention, plug-hole part is circular configuration.
In the present invention, the diameter of hole clipping part is less than the diameter of gripping part.
Beneficial effect: blanking cover of the present invention make simple, easy for installation, time saving and energy saving, reliability is higher, cost is relatively low, real
With property preferably, can be widely applied to the change of aircraft system scientific research stage part, reparation it is ensured that while safe, it also avoid
Waste, there is stronger practical value.
Brief description
Fig. 1 is the blanking cover front view in presently preferred embodiments of the present invention.
Fig. 2 is the blanking cover side view in presently preferred embodiments of the present invention.
Fig. 3 is the scheme of installation of presently preferred embodiments of the present invention.
Fig. 4 is that in presently preferred embodiments of the present invention, schematic diagram is repaired in unnecessary hole.
Specific embodiment
In order that technological means, creation characteristic, reached purpose and effect that the present invention realizes are easy to understand, tie below
Conjunction is specifically illustrating, and the present invention is expanded on further.
Referring to the method in a kind of quick reparation hole of Fig. 1～3, initially with nylon material according to perforations adding 5 to be repaired diameter
Make matched blanking cover, blanking cover includes plug-hole part 1, hole clipping part 2 and gripping part 3, then stretches into blanking cover to be repaired
Perforations adding 5 is interior and is arranged in the structure 4 of perforations adding to be repaired, and plug-hole part 1 gets lodged in structure 4 top of perforations adding to be repaired, and hole clipping part 2 is blocked
Enter in the middle part of perforations adding 5 to be repaired, gripping part 3 is used for blanking cover is fixed on the structure 4 of perforations adding to be repaired；Finally by blanking cover with repair
The structure 4 of the perforations adding to be repaired finishing carries out outer surface spray painting together so as to more attractive in appearance, that is, complete the reparation to unnecessary hole, in detail
As shown in Figure 4.
In the present embodiment, the diameter of plug-hole part 1 2～3mm bigger than the diameter of perforations adding 5 to be repaired, in order to by plug-hole part 1
It is fixed in the structure 4 of perforations adding to be repaired.
In the present embodiment, the diameter of hole clipping part 2 is identical with repairing hole 5 diameter, and hole clipping part 2 thickness with to be repaired
Structure 4 consistency of thickness in hole.
In the present embodiment, gripping part 3 middle setting has the gap of 3mm, and gripping part 3 is made up of elastomeric material,
Gripping part 3 is made to have certain elasticity, to ensure that blanking cover sticks into after perforations adding 5 to be repaired, plug-hole part 1 is made jointly with gripping part 3
With clamping the structure 4 of perforations adding to be repaired, blanking cover is promoted to be securely fixed in the structure 4 of perforations adding to be repaired.
In the present embodiment, plug-hole part 1 is circular configuration.
In the present embodiment, the diameter of hole clipping part 2 is less than gripping part 3 diameter, because gripping part 3 has elasticity, therefore
After hole clipping part 2 sticks into perforations adding 5 to be repaired, gripping part 3 can be fixed in the structure 4 of perforations adding to be repaired.
In the present embodiment it is also possible to the method repairs unnecessary hole.
Ultimate principle and principal character and the advantages of the present invention of the present invention have been shown and described above.The technology of the industry
, it should be appreciated that the present invention is not restricted to the described embodiments, the simply explanation described in above-described embodiment and description is originally for personnel
The principle of invention, without departing from the spirit and scope of the present invention, the present invention also has various changes and modifications, these changes
Change and improvement both falls within scope of the claimed invention.Claimed scope by appending claims and its
Equivalent thereof.
Claims (6)
1. a kind of method in quick reparation hole is it is characterised in that concretely comprise the following steps:
1) make matched blanking cover initially with nylon material according to the diameter of perforations adding to be repaired, blanking cover include plug-hole part,
Hole clipping part and gripping part；
2) blanking cover making in step 1) is stretched in the hole to be repaired and be arranged in the structure of perforations adding to be repaired, plug-hole part gets lodged in
The structure upper of perforations adding to be repaired, hole clipping part sticks in the middle part of the structure of perforations adding to be repaired, and gripping part is fixed on the knot of perforations adding to be repaired
Structure bottom；
3) blanking cover is carried out outer surface spray painting together with repairing the structure of the perforations adding to be repaired finishing, that is, complete unnecessary hole is repaiied
Multiple.
2. a kind of method in quick reparation hole according to claim 1 is it is characterised in that the diameter of plug-hole part is than to be repaired
Big 2～the 3mm of diameter of perforations adding.
3. a kind of method in quick reparation hole according to claim 1 is it is characterised in that the diameter of hole clipping part and repairing
Bore dia is identical, and hole clipping segment thickness is consistent with the structural thickness of perforations adding to be repaired.
4. a kind of method in quick reparation hole according to claim 1 is it is characterised in that gripping part middle setting has 1
The gap of～4mm, and gripping part is made up of elastomeric material.
5. a kind of method in quick reparation hole according to claim 1 is it is characterised in that plug-hole part is circular configuration.
6. a kind of method in quick reparation hole according to claim 1 is it is characterised in that the diameter of hole clipping part is less than card
The diameter of tight part.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610843730.7A CN106347710A (en) | 2016-09-23 | 2016-09-23 | Quick hole repair method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610843730.7A CN106347710A (en) | 2016-09-23 | 2016-09-23 | Quick hole repair method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106347710A true CN106347710A (en) | 2017-01-25 |
Family
ID=57858654
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610843730.7A Pending CN106347710A (en) | 2016-09-23 | 2016-09-23 | Quick hole repair method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106347710A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4867822A (en) * | 1987-08-04 | 1989-09-19 | The Boeing Corporation | Method for in-place fabrication of graphite epoxy bushings in graphite epoxy structures |
| US4912594A (en) * | 1986-11-03 | 1990-03-27 | The Boeing Company | Integral lightning protection repair system and method for its use |
| CN101472798A (en) * | 2006-05-19 | 2009-07-01 | 法国空中巴士公司 | Method of repairing a damaged area of an aircraft fuselage |
| CN202441192U (en) * | 2012-01-13 | 2012-09-19 | 广东贝克洛幕墙门窗系统有限公司 | Plug for auxiliary holes |
| CN202707762U (en) * | 2012-08-14 | 2013-01-30 | 潍柴动力股份有限公司 | Screw plug for engine body |
| CN103803099A (en) * | 2014-02-21 | 2014-05-21 | 山东太古飞机工程有限公司 | Technology for rapidly repairing floors |
-
2016
- 2016-09-23 CN CN201610843730.7A patent/CN106347710A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4912594A (en) * | 1986-11-03 | 1990-03-27 | The Boeing Company | Integral lightning protection repair system and method for its use |
| US4867822A (en) * | 1987-08-04 | 1989-09-19 | The Boeing Corporation | Method for in-place fabrication of graphite epoxy bushings in graphite epoxy structures |
| CN101472798A (en) * | 2006-05-19 | 2009-07-01 | 法国空中巴士公司 | Method of repairing a damaged area of an aircraft fuselage |
| CN202441192U (en) * | 2012-01-13 | 2012-09-19 | 广东贝克洛幕墙门窗系统有限公司 | Plug for auxiliary holes |
| CN202707762U (en) * | 2012-08-14 | 2013-01-30 | 潍柴动力股份有限公司 | Screw plug for engine body |
| CN103803099A (en) * | 2014-02-21 | 2014-05-21 | 山东太古飞机工程有限公司 | Technology for rapidly repairing floors |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170125 |
|
| RJ01 | Rejection of invention patent application after publication |