CN110370689A - A kind of repair method of civil airplane cabin plastic components - Google Patents
A kind of repair method of civil airplane cabin plastic components Download PDFInfo
- Publication number
- CN110370689A CN110370689A CN201910619100.5A CN201910619100A CN110370689A CN 110370689 A CN110370689 A CN 110370689A CN 201910619100 A CN201910619100 A CN 201910619100A CN 110370689 A CN110370689 A CN 110370689A
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- Prior art keywords
- plastic components
- sticking patch
- epoxy resin
- paint layer
- later
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/02—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D using liquid or paste-like material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/24—Apparatus or accessories not otherwise provided for
- B29C73/26—Apparatus or accessories not otherwise provided for for mechanical pretreatment
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C73/00—Repairing of articles made from plastics or substances in a plastic state, e.g. of articles shaped or produced by using techniques covered by this subclass or subclass B29D
- B29C73/24—Apparatus or accessories not otherwise provided for
- B29C73/26—Apparatus or accessories not otherwise provided for for mechanical pretreatment
- B29C2073/262—Apparatus or accessories not otherwise provided for for mechanical pretreatment for polishing, roughening, buffing or sanding the area to be repaired
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
Abstract
The invention discloses a kind of repair methods of civil airplane cabin plastic components, it can place under repair to surface abrasion, scuffing, crackle and the civil airplane cabin of perforation plastic components, epoxy resin has been used to be repaired in repairing, 10mm is greater than for diameter and is repaired less than or equal to perforating for 50mm using the muti-piece sticking patch of production, plastic components after repairing, it is basic consistent with genuine in function in appearance.
Description
Technical field
The present invention relates to a kind of repair methods of civil airplane cabin plastic components.
Background technique
Aviation has excellent electrical insulating property, dimensional stability, chemical corrosion resistance, higher intensity and heat-resisting with plastics
Property, also have many advantages, such as self-extinguishment, fire-retardant, nontoxic, pigmentable, being widely used in aircraft cockpit chooses to install in equipment, such as: it is each
Type unit seat decorative panel, various passenger seat decorative panel, meal plate, various kitchen's interior plate, lavatory decorative panel, close to cover board
Deng.
However effective repair method of the aviation plastic components in equipment is not provided due to each equipment manufacturer, work as aircraft
When choosing to install the aviation of equipment in cockpit and being damaged with plastic components, when the case where especially perforating, it can directly replace, cause to tie up
Repair the at high cost and wasting of resources.Therefore, it is badly in need of inventing a kind of to repair the aviation in civil airplane cabin with plastic components
The method of reason.
In civilian plastics repairs field, there is the material of many repairing technologies and repairing, but is unable to satisfy middle its people
The requirement of boat office (CAAC) seaworthiness authorization.Maintenance to the aviation plastic components in civil airplane cabin both at home and abroad and maintenance are equal
Based on replacement, for the repairing technology of reference, cause aircraft cockpit choose to install the plastic components of equipment repairing renovate at
For a difficult point.
Summary of the invention
The technical problems to be solved by the invention are just to provide a kind of repair method of civil airplane cabin plastic components,
Plastic components after the above method is repaired meets the requirement of aircarrier aircraft, can save maintenance cost and resource.
Above-mentioned technical problem is solved, The technical solution adopted by the invention is as follows:
A kind of repair method of civil airplane cabin plastic components, characterized in that including the civil aviaton to following damaged condition
Aircraft cockpit plastic components places under repair:
1, it when the plastic components that navigates in civil airplane cabin is surface abrasion or scratches, places under repair through following steps:
1.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface, waits after cleaning
Remaining moisture evaporating completely on plastic components；
1.2, at least one layer of epoxy resin is smeared in the surface location of the abrasion of plastic components or scuffing, until epoxy resin is complete
The surface of abrasion or the scuffing of plastic components is filled up entirely；
1.3, film is covered in epoxy resin surface, and excludes the air between film and epoxy resin, later in room temperature
In to epoxy resin cure；
1.4, after epoxy resin cure, film is removed, is polished epoxy resin, be polishing to smooth and and plastic section
The original shape of part is identical；
1.5, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
1.6, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is completely dry to interior trim paint layer
It completes repairs after dry；
2, it when the plastic components that navigates in civil airplane cabin is cracked, places under repair through following steps:
2.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface；
2.2, stop hole is bored respectively at the both ends of crackle；
2.3, polishing crackle neighboring area, until rough surface；
2.4, plastic components surface is cleaned, remaining moisture evaporating completely on plastic components is waited after cleaning；
2.5, it is filled up completely crackle with epoxy resin, later at room temperature to epoxy resin cure；
2.6, it after epoxy resin cure, polishes epoxy resin, is polishing to smooth and original with plastic components
Shape is identical；
2.7, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
2.8, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is completely dry to interior trim paint layer
It completes repairs after dry；
3, when the plastic components that navigates in civil airplane cabin is perforated, when the diameter of perforation is less than 10mm, through following steps
It places under repair:
3.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface；
3.2, tile thin film on a work top, plastic components overturning is placed on film downward, and at this time
Film seals the port positioned at lower end of perforation；
3.3, epoxy resin is filled in perforation, later at room temperature to epoxy resin cure；
3.4, overturn plastic components, polish the surface of the perforation region of plastic components, be polishing to smoothly and
Close to the original shape of plastic components；
3.5, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
3.6, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is completely dry to interior trim paint layer
It completes repairs after dry；
4, when the plastic components that navigates in civil airplane cabin is perforated, the diameter of perforation is greater than 10mm and is less than or equal to 50mm
When, it places under repair through following steps:
4.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface, removal perforation week
The material damaged on side；
4.2, chamfering is polished along side in the external port of perforation；
4.3, polishing keyhole periphery region, until rough surface；
4.4, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
4.5, tile thin film on a workbench, by one piece of glass fabric thorough impregnation in the epoxy
Above the film to tile afterwards on the table, then in the upper surface of glass fabric tiling thin film, it is thin to exclude upper layer and lower layer
Air between film and glass fabric is fabricated to one piece of sticking patch, shears later to sticking patch, finally shears the benefit of completion
The size of piece is greater than the size of perforation；
4.6, one layer of epoxy resin is brushed at the chamfering of the external port of perforation；
4.7, the position of the corresponding perforation of the sticking patch for eliminating lower film is layered on plastic section by the lower film for removing sticking patch
Above part, the corresponding position of sticking patch is tightly attached on the inclined-plane of chamfering, and excludes the air between sticking patch and the inclined-plane of chamfering, is mended
The position corresponding with perforation of piece will be recessed into perforation, remove the topmost thin film of sticking patch later；
4.8, step 4.5 is repeated, next piece of sticking patch is made, the size after this block sticking patch is clipped is greater than previous piece of sticking patch
Size removes the lower film of this block sticking patch, is layered on above previous piece of sticking patch, and is tightly attached to above previous piece of sticking patch, exclude with
Air between previous piece of sticking patch, removes the topmost thin film of this block sticking patch later；
4.9, the laying that step 4.8 carries out sticking patch is repeated, until the thickness that the sticking patch of all layings adds up is greater than perforation
The thickness of the plastic components of position；
4.10, it after the epoxy resin cure in sticking patch, polishes sticking patch, is polishing to smooth and close to plastic components
Original shape；
4.11, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
4.12, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is complete to interior trim paint layer
It completes repairs after drying.
Further, on the glass fabric in step 4.5 after epoxy resin impregnates, epoxy resin and glass fibre
The weight ratio of fabric is 1:1.
Further, the angle on the inclined-plane and horizontal plane of the chamfering in step 4.2 is 15 °.
Further, the sticking patch after clipped is circle, and the radius of the previous piece of sticking patch of radius ratio of next piece of sticking patch is big
5mm。
Further, it is up to two layers in the level of the interior trim paint layer of plastic components surface spraying.
Further, the size that coarse region is polishing in step 4.3 is the plastic components of perforation position
Ten times of thickness.
Further, the diameter of the stop hole in step 2.2 is φ 2mm.
Compared with prior art, the invention has the following advantages:
1, the repair method of civil airplane cabin plastic components of the invention belongs to general-purpose shop, can cover and infuse in China
The airline carriers of passengers cockpit plastic components of volume, the present invention are greatly saved domestic operator and order what new part was replaced to external producer
Maintenance cost.Plastic components after being repaired by repair method of the invention, it is basic consistent with genuine in function in appearance.
2, repair method of the invention include to surface abrasion, scuffing, crackle and the repairing of perforation, can be to most of need
Plastic components to be repaired places under repair, applied widely.
Detailed description of the invention
Fig. 1 is the schematic diagram repaired in the 3rd kind of damaged condition of the invention to plastic components；
Fig. 2 is the schematic diagram that sticking patch is made in the present invention；
Fig. 3 is the schematic diagram that sticking patch is sheared in the present invention；
Fig. 4 be the 4th in the present invention in damaged condition when not repairing the perforation of plastic components schematic diagram；
Fig. 5 be the 4th in the present invention in perforation in damaged condition after step 4.2 carries out chamfering schematic diagram；
Fig. 6 be the 4th in the present invention in the schematic diagram after step 4.9 is completed in damaged condition；
Fig. 7 be the 4th in the present invention in the schematic diagram after repairing is completed in damaged condition.
Specific embodiment
The present invention is further described below with reference to embodiment.
As shown in Figure 1, Figure 2, a kind of repair method of civil airplane cabin plastic components shown in, comprising to following damage
The civil airplane cabin plastic components of degree places under repair:
1, it when the plastic components that navigates in civil airplane cabin is surface abrasion or scratches, places under repair through following steps:
1.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface, waits after cleaning
Remaining moisture evaporating completely on plastic components；
1.2, at least one layer of epoxy resin is smeared in the surface location of the abrasion of plastic components or scuffing, until epoxy resin is complete
The surface of abrasion or the scuffing of plastic components is filled up entirely；
1.3, film is covered in epoxy resin surface, and excludes the air between film and epoxy resin, later in room temperature
In to epoxy resin cure；
1.4, after epoxy resin cure, film is removed, is polished epoxy resin, be polishing to smooth and and plastic section
The original shape of part is identical；
1.5, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
1.6, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is completely dry to interior trim paint layer
It completes repairs after dry；
2, it when the plastic components that navigates in civil airplane cabin is cracked, places under repair through following steps:
2.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface；
2.2, stop hole is bored respectively at the both ends of crackle；
2.3, polishing crackle neighboring area, until rough surface；
2.4, plastic components surface is cleaned, remaining moisture evaporating completely on plastic components is waited after cleaning；
2.5, it is filled up completely crackle with epoxy resin, later at room temperature to epoxy resin cure；
2.6, it after epoxy resin cure, polishes epoxy resin, is polishing to smooth and original with plastic components
Shape is identical；
2.7, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
2.8, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is completely dry to interior trim paint layer
It completes repairs after dry；
3, as shown in Figure 1, when the plastic components that navigates in civil airplane cabin is perforated, when the diameter of perforation is less than 10mm,
It places under repair through following steps:
3.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface；
3.2, tile thin film 1 on a work top 2, and the overturning of plastic components 3 is placed in downward on film 1, and
Film 1 seals the port positioned at lower end of perforation at this time；
3.3, epoxy resin 4 is filled in perforation, is solidified at room temperature to epoxy resin 4 later；
3.4, plastic components 3 is overturn, is polished the surface of the perforation region of plastic components 3, is polishing to smooth
And close to the original shape of plastic components；
3.5, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
3.6, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is completely dry to interior trim paint layer
It completes repairs after dry；
4, when the plastic components that navigates in civil airplane cabin is perforated, the diameter of perforation is greater than 10mm and is less than or equal to 50mm
When, it places under repair through following steps:
4.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface, removal perforation week
The material damaged on side；
4.2, chamfering is polished along side in the external port of perforation；
4.3, polishing keyhole periphery region, until rough surface；
4.4, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
4.5, as shown in Figures 2 and 3, tile thin film on a workbench, by one piece of glass fabric in ring
Above the film to tile on the table after thorough impregnation in oxygen resin, then it is one layer thin in the tiling of the upper surface of glass fabric
Film excludes the air between upper layer and lower layer film and glass fabric, is fabricated to one piece of sticking patch, cuts later to sticking patch
It cuts, the size for finally shearing the sticking patch of completion is greater than the size of perforation；
4.6, one layer of epoxy resin is brushed at the chamfering of the external port of perforation；
4.7, the position of the corresponding perforation of the sticking patch for eliminating lower film is layered on plastic section by the lower film for removing sticking patch
Above part, the corresponding position of sticking patch is tightly attached on the inclined-plane of chamfering, and excludes the air between sticking patch and the inclined-plane of chamfering, is mended
The position corresponding with perforation of piece will be recessed into perforation, remove the topmost thin film of sticking patch later；
4.8, step 4.5 is repeated, next piece of sticking patch is made, the size after this block sticking patch is clipped is greater than previous piece of sticking patch
Size removes the lower film of this block sticking patch, is layered on above previous piece of sticking patch, and is tightly attached to above previous piece of sticking patch, exclude with
Air between previous piece of sticking patch, removes the topmost thin film of this block sticking patch later；
4.9, the laying that step 4.8 carries out sticking patch is repeated, until the thickness that the sticking patch of all layings adds up is greater than perforation
The thickness of the plastic components of position；
4.10, it after the epoxy resin cure in sticking patch, polishes sticking patch, is polishing to smooth and close to plastic components
Original shape；
4.11, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
4.12, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, it is complete to interior trim paint layer
It completes repairs after drying.
As shown in Figures 4 to 6 to perforate when the plastic components that navigates in civil airplane cabin, the diameter of perforation is greater than 10mm
And to the mending course of perforation when less than or equal to 50mm.
And when the plastic components that navigates in civil airplane cabin is perforated, and the diameter of perforation is greater than 50mm, directly replacement modeling
Expect component.
Wherein, preferred embodiment are as follows: on the glass fabric in step 4.5 after epoxy resin impregnates, epoxy resin with
The weight ratio of glass fabric is 1:1.The inclined-plane of chamfering in step 4.2 and the angle of horizontal plane are 15 °.After clipped
Sticking patch is round, and the big 5mm of radius of the previous piece of sticking patch of radius ratio of next piece of sticking patch.In the interior trim of plastic components surface spraying
The level of paint layer is up to two layers.The size that coarse region is polishing in step 4.3 is the plastics of perforation position
Ten times of the thickness of component.The diameter of stop hole in step 2.2 is φ 2mm.
Wherein, above-mentioned cleaning can be is cleaned by alcohol, and the method for above-mentioned exclusion air, which can be, to be passed through
Scraper plate, which put down to side, to be scraped to exclude air, and above-mentioned film can be plastic film, and above-mentioned polishing can be by beating
Grinding machine is polished, above-mentioned glass fabric can be by it is fiberglass braided at cloth.
Claims (7)
1. a kind of repair method of civil airplane cabin plastic components, which is characterized in that including the civil aviaton to following damaged condition
Aircraft cockpit plastic components places under repair:
1, it when the plastic components that navigates in civil airplane cabin is surface abrasion or scratches, places under repair through following steps:
1.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface, plastics is waited after cleaning
Remaining moisture evaporating completely on component；
1.2, at least one layer of epoxy resin is smeared in the surface location of the abrasion of plastic components or scuffing, until epoxy resin is filled out completely
Mend the surface of abrasion or the scuffing of plastic components；
1.3, cover film in epoxy resin surface, and exclude the air between film and epoxy resin, later at room temperature to
Epoxy resin cure；
1.4, after epoxy resin cure, film is removed, is polished epoxy resin, be polishing to smooth and former with plastic components
Some shapes are identical；
1.5, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
1.6, on plastic components surface spray identical with original surface paint layer color interior trim paint layer, after interior trim paint layer is completely dried
It completes repairs；
2, it when the plastic components that navigates in civil airplane cabin is cracked, places under repair through following steps:
2.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface；
2.2, stop hole is bored respectively at the both ends of crackle；
2.3, polishing crackle neighboring area, until rough surface；
2.4, plastic components surface is cleaned, remaining moisture evaporating completely on plastic components is waited after cleaning；
2.5, it is filled up completely crackle with epoxy resin, later at room temperature to epoxy resin cure；
2.6, after epoxy resin cure, polish epoxy resin, be polishing to it is smooth and with the original shape of plastic components
It is identical；
2.7, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
2.8, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, after interior trim paint layer is completely dried
It completes repairs；
3, it when the plastic components that navigates in civil airplane cabin is perforated, when the diameter of perforation is less than 10mm, is carried out through following steps
It repairs:
3.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface；
3.2, tile thin film on a work top, plastic components overturning is placed on film downward, and film at this time
Seal the port positioned at lower end of perforation；
3.3, epoxy resin is filled in perforation, later at room temperature to epoxy resin cure；
3.4, plastic components is overturn, polishes the surface of the perforation region of plastic components, is polishing to smooth and close
The original shape of plastic components；
3.5, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
3.6, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, after interior trim paint layer is completely dried
It completes repairs；
4, when the plastic components that navigates in civil airplane cabin is perforated, and the diameter of perforation is greater than 10mm and is less than or equal to 50mm,
It places under repair through following steps:
4.1, the paint layer on polishing removal plastic components surface, later cleans plastic components surface, removes keyhole periphery
The material damaged；
4.2, chamfering is polished along side in the external port of perforation；
4.3, polishing keyhole periphery region, until rough surface；
4.4, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
4.5, tile thin film on a workbench, will put down after one piece of glass fabric in the epoxy thorough impregnation
Above paving film on the table, then tile thin film in the upper surface of glass fabric, exclude upper layer and lower layer film with
Air between glass fabric is fabricated to one piece of sticking patch, shears later to sticking patch, finally shears the sticking patch of completion
Size is greater than the size of perforation；
4.6, one layer of epoxy resin is brushed at the chamfering of the external port of perforation；
4.7, the lower film for removing sticking patch, on a plastic part by the position paving for the corresponding perforation of sticking patch for eliminating lower film
The corresponding position of sticking patch is tightly attached on the inclined-plane of chamfering by face, and excludes the air between sticking patch and the inclined-plane of chamfering, sticking patch
Position corresponding with perforation will be recessed into perforation, remove the topmost thin film of sticking patch later；
4.8, step 4.5 is repeated, next piece of sticking patch is made, the size after this block sticking patch is clipped is greater than the big of previous piece of sticking patch
It is small, the lower film of this block sticking patch is removed, is layered on above previous piece of sticking patch, and is tightly attached to above previous piece of sticking patch, is excluded with before
Air between one piece of sticking patch, removes the topmost thin film of this block sticking patch later；
4.9, the laying that step 4.8 carries out sticking patch is repeated, until the thickness that the sticking patch of all layings adds up is greater than where perforation
The thickness of the plastic components of position；
4.10, it after the epoxy resin cure in sticking patch, polishes sticking patch, is polishing to smooth and original close to plastic components
Shape；
4.11, plastic components surface is cleaned again, later to moisture evaporating completely remaining on plastic components；
4.12, interior trim paint layer identical with original surface paint layer color is sprayed on plastic components surface, is completely dried to interior trim paint layer
After complete repairs.
2. the repair method of civil airplane cabin plastic components according to claim 1, it is characterised in that: in step 4.5
On glass fabric after epoxy resin impregnates, the weight ratio of epoxy resin and glass fabric is 1:1.
3. the repair method of civil airplane cabin plastic components according to claim 1, it is characterised in that: in step 4.2
Chamfering inclined-plane and horizontal plane angle be 15 °.
4. the repair method of civil airplane cabin plastic components according to claim 1, it is characterised in that: after clipped
Sticking patch is round, and the big 5mm of radius of the previous piece of sticking patch of radius ratio of next piece of sticking patch.
5. the repair method of civil airplane cabin plastic components according to claim 1, it is characterised in that: in plastic components
The level of the interior trim paint layer of surface spraying is up to two layers.
6. the repair method of civil airplane cabin plastic components according to claim 1, it is characterised in that: in step 4.3
The size for being polishing to coarse region is to perforate ten times of thickness of plastic components of position.
7. the repair method of civil airplane cabin plastic components according to claim 1, it is characterised in that: in step 2.2
Stop hole diameter be φ 2mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910619100.5A CN110370689A (en) | 2019-07-10 | 2019-07-10 | A kind of repair method of civil airplane cabin plastic components |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910619100.5A CN110370689A (en) | 2019-07-10 | 2019-07-10 | A kind of repair method of civil airplane cabin plastic components |
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| Publication Number | Publication Date |
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| CN110370689A true CN110370689A (en) | 2019-10-25 |
Family
ID=68250863
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910619100.5A Withdrawn CN110370689A (en) | 2019-07-10 | 2019-07-10 | A kind of repair method of civil airplane cabin plastic components |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113478832A (en) * | 2021-07-27 | 2021-10-08 | 贵州航天天马机电科技有限公司 | Process method for post-treatment repair of SLA parts |
| CN114851603A (en) * | 2022-03-28 | 2022-08-05 | 国营芜湖机械厂 | Method for repairing damage of organic glass broken hole of cockpit cover of outfield airplane |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4133913A (en) * | 1977-08-25 | 1979-01-09 | Bruce R. Moore | Method for providing automobile dashboards and the like with a texturized finish |
| JP2018114721A (en) * | 2017-01-20 | 2018-07-26 | 三菱重工業株式会社 | Method for repairing composite material |
| CN109604928A (en) * | 2019-01-22 | 2019-04-12 | 芜湖中科飞机制造有限公司 | A kind of composite material body structural member damage rehabilitation method |
-
2019
- 2019-07-10 CN CN201910619100.5A patent/CN110370689A/en not_active Withdrawn
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4133913A (en) * | 1977-08-25 | 1979-01-09 | Bruce R. Moore | Method for providing automobile dashboards and the like with a texturized finish |
| JP2018114721A (en) * | 2017-01-20 | 2018-07-26 | 三菱重工業株式会社 | Method for repairing composite material |
| CN109604928A (en) * | 2019-01-22 | 2019-04-12 | 芜湖中科飞机制造有限公司 | A kind of composite material body structural member damage rehabilitation method |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113478832A (en) * | 2021-07-27 | 2021-10-08 | 贵州航天天马机电科技有限公司 | Process method for post-treatment repair of SLA parts |
| CN114851603A (en) * | 2022-03-28 | 2022-08-05 | 国营芜湖机械厂 | Method for repairing damage of organic glass broken hole of cockpit cover of outfield airplane |
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Application publication date: 20191025 |
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| WW01 | Invention patent application withdrawn after publication |