CN109551442A - The outer integrated corrosion repair kit of field portable of aircraft and corrosion repair method - Google Patents
The outer integrated corrosion repair kit of field portable of aircraft and corrosion repair method Download PDFInfo
- Publication number
- CN109551442A CN109551442A CN201811469926.XA CN201811469926A CN109551442A CN 109551442 A CN109551442 A CN 109551442A CN 201811469926 A CN201811469926 A CN 201811469926A CN 109551442 A CN109551442 A CN 109551442A
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- Prior art keywords
- corrosion
- repair
- polishing
- aircraft
- pen
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25H—WORKSHOP EQUIPMENT, e.g. FOR MARKING-OUT WORK; STORAGE MEANS FOR WORKSHOPS
- B25H3/00—Storage means or arrangements for workshops facilitating access to, or handling of, work tools or instruments
- B25H3/02—Boxes
- B25H3/021—Boxes comprising a number of connected storage elements
- B25H3/022—Boxes comprising a number of connected storage elements in fixed relationship
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
Abstract
The invention discloses the integrated corrosion repair kits of field portable outside aircraft, including cabinet, cleaning agent, battery charging polishing pen and grinding head suit, plug-in polishing pen, dial depth gauge, surface oxidation pen, Self-leveling sealant suit, Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electric erosion agent, aluminum oxide sandpaper, file, Sticky Gauze, scouring pad are provided in cabinet.Tool box of the invention easily and fast to repair aircraft structure corrosion damage under conditions of outfield lacks Corrosion Maintenance repaired item and measure.
Description
Technical field
The invention belongs to aircraft structure corrosion maintenance and repair technical fields, and in particular to a kind of outer field portable collection of aircraft
At the method changed corrosion repair kit and carry out Aircraft Corrosion damage repair using the tool box.
Background technique
Environmental corrosion has used aircraft safety and the performance of the fighting capacity of military secret constitutes serious threat.Corrosion damage
Can cause the fracture toughness of housing construction material reduces, and accelerates the formation and extension of crackle, to seriously reduce aircaft configuration
Residual intensity and service life, or even the unexpected fracture without omen is generated, aircraft and the safety of crew are seriously threatened, corrosion
In the presence of the rate of attendance and safety for having seriously affected aircraft, be especially parked in the severe outfield of the high salt fog of the high temperature and humidity such as the South Sea with
And the aircraft under islands and reefs environment, lack Corrosion Maintenance repaired item and measure, it is easier to corrode, how quickly to repair outfield aircraft
Etching problem, guarantees aircraft operational readiness and safety is pendulum letter key subjects to be solved in face of aircaft configuration engineers.
In recent years, it as corrosion damage service technique and product are more and more mature, is mentioned for outfield fast erosion damage repair
Technical support has been supplied, repair outfit and repair material have been integrated in corrosion repair kit, it can be quick and easy, efficiently right
Aircraft Corrosion damage places under repair, and the existing research achievement both at home and abroad in this field is less, there is not yet the paper of correlative study
And achievement.
Summary of the invention
Goal of the invention
The technical problem to be solved by the present invention is to lack Corrosion Maintenance repaired item in outfield and under conditions of measure, just
Aircraft structure corrosion damage is rapidly repaired in victory, guarantees aircraft safety and the rate of attendance.
Inventive technique solution
In order to achieve the above-mentioned object of the invention, the present invention uses following technical solutions:
The integrated corrosion repair kit of the outer field portable of aircraft, which is characterized in that including cabinet, be provided in cabinet clear
Lotion, battery charging polishing pen and grinding head suit, plug-in polishing pen, dial depth gauge, surface oxidation pen, gravity flow plain seal
Agent suit, Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electric erosion agent, aluminum oxide sand
Paper, file, Sticky Gauze, scouring pad.
Preferably, it is separated into several individual housing units in cabinet, places a kind of tool in each housing unit.
Preferably, the cleaning agent: trade mark TFQX-3；The battery charging polishing pen and grinding head suit: include electrification
Pond polishing pen, thick wolfram steel grinding head, thin steel grinding head, grinder buffing head, copper brush grinding head, sand paper polishing stick, sand paper polishing pad；
The plug-in polishing pen: 220V power supply, range of speeds 9000r/min~14500r/min are met；The dial depth gauge: measurement
0~12.7mm of range, resolution ratio 0.001mm；The surface oxidation pen: trade mark ALODINE 1132；The Self-leveling sealant
Suit: including HT3326 Self-leveling sealant, glue rifle and glue rifle mouth；The Rapid-Repair priming paint: trade mark B-15；It is described quickly to repair
Mend finishing coat: trade mark BF-15；The mantle corrosion inhibiter: trade mark TFHS-10；The dura mater corrosion inhibiter: trade mark TFHS-15；The electricity
Sub electrical erosion agent: trade mark TFHS-20；The aluminum oxide sandpaper: including 240#, 400#, 600# specification；The file: specification
400#；The scouring pad: trade mark 3M 7447c.
Preferably, cleaning agent, Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electronics electricity
Cavitation erosion agent is all made of sprinkling irrigation formula.
Preferably, cleaning agent, Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electronics electricity
The capacity of cavitation erosion agent is 400ml.
The integrated corrosion repair method of the outer field portable of aircraft, includes the following steps:
(a) surface clean；(b) corrosion removal product；(c) it cleaning polishing bits: is wiped with Sticky Gauze；(d) with amesdial into
Row depth measurement；(e) it is surface-treated with surface oxidation pen；(f) it spontaneously dries about after five minutes, is used according to B-15 priming paint
Method sprays B-15 priming paint；After basecoat paint 30min or so, according to BF-15 finishing coat application method, BF-15 finishing coat is sprayed；(g)
After paint layer is about 30 minutes dry, according to structure position feature, surface sprays TFHS-15 dura mater corrosion inhibiter or TFHS-10 mantle is slow
Lose agent；For spraying the electric corrosion inhibiter of TFHS-20 by electric position.
Preferably, the adoptable method of step (a) has: 1) directly being wiped with Sticky Gauze；2) TFQX-3 cleaning agent is sprayed,
It is wiped again with Sticky Gauze；3) for heavy oil dirt region, TFQX-3 cleaning agent is sprayed, then is wiped with scouring pad.
Preferably, the adoptable method of step (b) has: 1) sand paper is polished, and is polished again with fine sandpaper with coarse sandpaper；2) file
Polishing；3) the rechargeable polishing pen polishing of battery, selects suitable grinding head to polish；4) plug-in polishing pen polishing, selection
Suitable grinding head is polished；By the polishing of institute's choosing method until matrix exposes smooth surface.
Advantages of the present invention
The present invention has the advantages that
(1) repair kit is easy to carry about with one, is easy to use, can be used for the corrosion such as outfield, aircraft stationed on the island repairing, solves
Outfield or aircraft stationed on the island etc. lack the problem for corroding repair outfit and material since geographical conditions limit.
(2) the repair kit tool and material are complete, including for (surface clean, corrosion removal in corrosion repair procedures
Product, polishing bits cleaning, depth measurement, surface treatment, japanning, corrosion inhibiter application) kit and material, with completeness.
(3) cleaning agent can be used directly, without dilution in the repair kit, can completely remove weight dirt, greasy dirt etc., ring
It protects, is nontoxic, flash-point is high, using safe, and cleaning agent is in neutrality and contains corrosion inhibiter component.
(4) structure that TFHS-10 corrosion inhibiter can be used for aircraft mobile or sliding position, often dismantle in the repair kit
Part surface has very strong permeability and water substituting.
(5) TFHS-15 corrosion inhibiter is used for the non-athletic position of aircraft and inner surface structure in the repair kit, has very strong
Water substituting, film layer is hard, survivable, wear-resisting, and guard time is long.
(6) anticorrosion of the TFHS-20 corrosion inhibiter for aviation electronics electrical equipment lubricates in the repair kit, after spraying
For transparent non-sticky ultra-thin film layers, automatic briefing after failure, without removal.
(7) surface oxidation pen is used for plane aluminium alloy surface oxidation in the repair kit, easy to use, is not required to communications centre
It washes, spontaneously dries.
(8) priming paint and finishing coat are one pack system in the repair kit, and formula of spraying can be used after shaking up, easy to use.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the integrated corrosion repair kit of the outer field portable of aircraft of the invention.
Fig. 2 is the flow chart of the integrated corrosion repair method of the outer field portable of aircraft of the invention.
Specific embodiment
In conjunction with summary of the invention general introduction and attached drawing, the specific embodiment that the present invention will be described in detail.
The integrated corrosion repair kit of the outer field portable of aircraft mainly includes cleaning agent, battery charging polishing pen and is beaten
It is bistrique suit, plug-in polishing pen, dial depth gauge, surface oxidation pen, Self-leveling sealant suit, Rapid-Repair priming paint, fast
It is speed repairing finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electric erosion agent, aluminum oxide sandpaper, file, Sticky Gauze, hundred clean
Cloth.
The cleaning agent: trade mark TFQX-3, formula of spraying, capacity 400ml are used for the daily clean and maintenance in aircraft outer surface.
The battery charging polishing pen and grinding head suit: include charged pool polishing pen, thick wolfram steel grinding head, the polishing of thin steel
Head, grinder buffing head, copper brush grinding head, sand paper polishing stick, sand paper polishing pad, polish for aircraft structure corrosion product.
The plug-in polishing pen: connecing 220V power supply, and range of speeds 9000r/min~14500r/min is used for aircraft knot
The polishing of structure corrosion product.
The dial depth gauge: 0~12.7mm of measurement range, resolution ratio 0.001mm are deep for corrosion removal product post-etching
Degree measurement.
The surface oxidation pen: trade mark ALODINE 1132, weight 32g aoxidize table for plane aluminium alloy body structure surface
Surface treatment.
The Self-leveling sealant suit: include HT3326 Self-leveling sealant, glue rifle and glue rifle mouth, be used for aircraft electric appliance
The filling of the encapsulating of connector and internal local ponding region.
The Rapid-Repair priming paint: trade mark B-15, formula of spraying, capacity 400ml are repaired for aircraft surfaces corrosion damage.
The Rapid-Repair finishing coat: trade mark BF-15, formula of spraying, capacity 400ml are repaired for aircraft surfaces corrosion damage.
The mantle corrosion inhibiter: trade mark TFHS-10, formula of spraying, capacity 400ml, the spiral shell for dismountable moving part
The corrosion protection of the parts such as mother, screw thread, lock pin, pin shaft.
The dura mater corrosion inhibiter: trade mark TFHS-15, spray formula, capacity 400ml, for often do not dismantle position bolt,
The corrosion protection of the connecting portions such as rivet, structure gap.
The electric erosion agent: trade mark TFHS-20, formula of spraying, capacity 400ml, for aviation electronics electrical equipment
Anticorrosion lubrication.
The aluminum oxide sandpaper: it including 240#, 400#, 600# specification, polishes for corrosion product.
The file: specification 400# polishes for corrosion product.
The Sticky Gauze: for clean surface dust, slight dirt etc..
The scouring pad: trade mark 3M 7447c, for clean surface heavy oil dirt etc..
The method for carrying out corrosion damage repairing using the integrated corrosion repair kit of field portable outside aircraft, including it is as follows
Step:
A) surface clean.Mainly there are 3 kinds of methods: 1) directly being wiped with Sticky Gauze；2) TFQX-3 cleaning agent is sprayed, then is used
Sticky Gauze wiping；3) for heavy oil dirt region, TFQX-3 cleaning agent is sprayed, then is wiped with scouring pad.
B) corrosion removal product.Mainly have 4 kinds of methods: 1) sand paper is polished, and is polished again with fine sandpaper with coarse sandpaper；2) file is beaten
Mill；3) the rechargeable polishing pen polishing of battery, selects suitable grinding head to polish；4) plug-in polishing pen polishing, selection are closed
Suitable grinding head is polished.After the polishing of institute's choosing method, until matrix exposes smooth surface.
C) polishing bits cleaning.It is wiped with Sticky Gauze.
D) depth measurement.According to dial depth gauge application method, depth measurement is carried out.
E) it is surface-treated.According to 1132 surface oxidation application method of A Luo fourth, it is surface-treated.
F) after spontaneously drying within about 5 minutes, according to B-15 priming paint application method, B-15 priming paint is sprayed；Basecoat paint 30min is left
Behind the right side, according to BF-15 finishing coat application method, BF-15 finishing coat is sprayed.
G) after about 30 minutes paint layers are dry, according to structure position feature, surface spray TFHS-15 dura mater corrosion inhibiter or
TFHS-10 mantle corrosion inhibiter；If electric position, the electric corrosion inhibiter of TFHS-20 is sprayed.
Claims (8)
1. the integrated corrosion repair kit of the outer field portable of aircraft, which is characterized in that including cabinet, cleaning is provided in cabinet
Agent, battery charging polishing pen and grinding head suit, plug-in polishing pen, dial depth gauge, surface oxidation pen, Self-leveling sealant
Suit, Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electric erosion agent, aluminum oxide sandpaper,
File, Sticky Gauze, scouring pad.
2. the integrated corrosion repair kit of the outer field portable of aircraft as described in claim 1, which is characterized in that divide in cabinet
Several individual housing units are divided into, place a kind of tool in each housing unit.
3. the integrated corrosion repair kit of the outer field portable of aircraft as claimed in claim 2, which is characterized in that the cleaning
Agent: trade mark TFQX-3；Battery charging polishing pen and grinding head suit: comprising charged pool polishing pen, thick wolfram steel grinding head, thin
Steel grinding head, grinder buffing head, copper brush grinding head, sand paper polishing stick, sand paper polishing pad；The plug-in polishing pen: 220V is met
Power supply, range of speeds 9000r/min~14500r/min；The dial depth gauge: 0~12.7mm of measurement range, resolution ratio
0.001mm；The surface oxidation pen: trade mark ALODINE 1132；The Self-leveling sealant suit: including HT3326 Self-leveling
Sealant, glue rifle and glue rifle mouth；The Rapid-Repair priming paint: trade mark B-15；The Rapid-Repair finishing coat: trade mark BF-15；It is described
Mantle corrosion inhibiter: trade mark TFHS-10；The dura mater corrosion inhibiter: trade mark TFHS-15；The electric erosion agent: trade mark TFHS-
20；The aluminum oxide sandpaper: including 240#, 400#, 600# specification；The file: specification 400#；The scouring pad: trade mark 3M
7447c。
4. the integrated corrosion repair kit of the outer field portable of aircraft as claimed in claim 3, which is characterized in that cleaning agent,
Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, electric erosion agent are all made of sprinkling irrigation formula.
5. the integrated corrosion repair kit of the outer field portable of aircraft as claimed in claim 3, which is characterized in that cleaning agent,
Rapid-Repair priming paint, Rapid-Repair finishing coat, mantle corrosion inhibiter, dura mater corrosion inhibiter, the electric capacity for losing agent are 400ml.
6. being corroded using the outer integrated corrosion repair kit of field portable of aircraft as described in Claims 1 to 5 is any
The method of repairing, which comprises the steps of:
(a) surface clean；(b) corrosion removal product；(c) it cleaning polishing bits: is wiped with Sticky Gauze；(d) it is carried out with amesdial deep
Degree measurement；(e) it is surface-treated with surface oxidation pen；(f) it spontaneously dries about after five minutes, according to B-15 priming paint application method,
Spray B-15 priming paint；After basecoat paint 30min or so, according to BF-15 finishing coat application method, BF-15 finishing coat is sprayed；(g) paint layer
After about 30 minutes dry, according to structure position feature, surface sprays TFHS-15 dura mater corrosion inhibiter or TFHS-10 mantle corrosion inhibiter；
For spraying the electric corrosion inhibiter of TFHS-20 by electric position.
7. the integrated corrosion repair method of the outer field portable of aircraft as claimed in claim 6, which is characterized in that step (a) can
The method of use has: 1) directly being wiped with Sticky Gauze；2) TFQX-3 cleaning agent is sprayed, then is wiped with Sticky Gauze；3) for
Heavy oil dirt region sprays TFQX-3 cleaning agent, then is wiped with scouring pad.
8. the integrated corrosion repair method of the outer field portable of aircraft as claimed in claim 6, which is characterized in that step (b) can
The method of use has: 1) sand paper is polished, and is polished again with fine sandpaper with coarse sandpaper；2) file is polished；3) the rechargeable polishing pen of battery
Polishing, selects suitable grinding head to polish；4) plug-in polishing pen polishing, selects suitable grinding head to polish；It presses
The polishing of institute's choosing method is until matrix exposes smooth surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811469926.XA CN109551442A (en) | 2018-12-04 | 2018-12-04 | The outer integrated corrosion repair kit of field portable of aircraft and corrosion repair method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811469926.XA CN109551442A (en) | 2018-12-04 | 2018-12-04 | The outer integrated corrosion repair kit of field portable of aircraft and corrosion repair method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109551442A true CN109551442A (en) | 2019-04-02 |
Family
ID=65868832
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811469926.XA Pending CN109551442A (en) | 2018-12-04 | 2018-12-04 | The outer integrated corrosion repair kit of field portable of aircraft and corrosion repair method |
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| CN (1) | CN109551442A (en) |
Citations (5)
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|---|---|---|---|---|
| CN101913433A (en) * | 2010-07-20 | 2010-12-15 | 哈尔滨飞机工业集团有限责任公司 | Surface treatment method for composite material blade of helicopter |
| US20120156049A1 (en) * | 2005-12-14 | 2012-06-21 | Hong Shek C | Method and coating for protecting and repairing an airfoil surface |
| CN107214600A (en) * | 2017-06-02 | 2017-09-29 | 中国航发北京航空材料研究院 | A kind of method that novel site quickly removes corrosion product with steel matrix |
| CN107254367A (en) * | 2017-04-27 | 2017-10-17 | 中国人民解放军空军工程大学 | Aircraft skin external surface cleaning agent |
| CN107322550A (en) * | 2016-04-29 | 2017-11-07 | 国网辽宁省电力有限公司营口供电公司 | Electric power derusting combination tool case |
-
2018
- 2018-12-04 CN CN201811469926.XA patent/CN109551442A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20120156049A1 (en) * | 2005-12-14 | 2012-06-21 | Hong Shek C | Method and coating for protecting and repairing an airfoil surface |
| CN101913433A (en) * | 2010-07-20 | 2010-12-15 | 哈尔滨飞机工业集团有限责任公司 | Surface treatment method for composite material blade of helicopter |
| CN107322550A (en) * | 2016-04-29 | 2017-11-07 | 国网辽宁省电力有限公司营口供电公司 | Electric power derusting combination tool case |
| CN107254367A (en) * | 2017-04-27 | 2017-10-17 | 中国人民解放军空军工程大学 | Aircraft skin external surface cleaning agent |
| CN107214600A (en) * | 2017-06-02 | 2017-09-29 | 中国航发北京航空材料研究院 | A kind of method that novel site quickly removes corrosion product with steel matrix |
Non-Patent Citations (1)
| Title |
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| 张学军等: "飞机铝合金结构连接部位表面防护体系修理技术研究", 《装备环境工程》 * |
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| PB01 | 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 | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20190402 |