CN202471613U - Aviation fluorescent penetration inspection system - Google Patents
Aviation fluorescent penetration inspection system Download PDFInfo
- Publication number
- CN202471613U CN202471613U CN 201220099344 CN201220099344U CN202471613U CN 202471613 U CN202471613 U CN 202471613U CN 201220099344 CN201220099344 CN 201220099344 CN 201220099344 U CN201220099344 U CN 201220099344U CN 202471613 U CN202471613 U CN 202471613U
- Authority
- CN
- China
- Prior art keywords
- rinse bath
- tank
- aviation
- cleaning
- groove
- Prior art date
- 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.)
- Expired - Fee Related
Links
- 238000007689 inspection Methods 0.000 title abstract description 8
- 230000035515 penetration Effects 0.000 title abstract 8
- 238000004140 cleaning Methods 0.000 claims abstract description 18
- 238000001514 detection method Methods 0.000 claims abstract description 14
- 238000001035 drying Methods 0.000 claims abstract description 12
- 239000007921 spray Substances 0.000 claims abstract description 4
- 239000012466 permeate Substances 0.000 claims description 6
- 210000005056 cell body Anatomy 0.000 claims description 4
- 239000000843 powder Substances 0.000 claims description 3
- 230000007547 defect Effects 0.000 abstract 1
- 230000002950 deficient Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 238000005457 optimization Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
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- Investigating Materials By The Use Of Optical Means Adapted For Particular Applications (AREA)
Abstract
The utility model belongs to the field of aviation flight, and particularly relates to an aviation fluorescent penetration inspection system which comprises a pre-cleaning portion, a penetration portion and a post-cleaning portion. The aviation fluorescent penetration inspection system is characterized in that the pre-cleaning portion at least comprises a pre-cleaning tank and a drying box, the penetration portion comprises a penetration tank, a dripping tank, a cleaning tank, a compensating cleaning tank, a drying box and a developing cabinet, the post-cleaning portion comprises a post-cleaning tank and a drying box, each tank body is provided with an inner layer and an outer layer, and a spray device, a turning device, a lifter and a duster are fixedly arranged in each of the pre-cleaning tank, the post-cleaning tank, the penetration tank, the dripping tank, the cleaning tank and the compensating cleaning tank. Automatic and semi-automatic flaw detection of surface defects of parts can be realized, the labor intensity of an operator is reduced, and fluorescent penetration flaw detection efficiency is improved.
Description
Technical field
The utility model belongs to the aviation flight field, is specifically related to a kind of aviation fluorescent penetrant detection system.
Background technology
In Aeronautics and Astronautics, weapons system, what the detection of component surface defective major part adopted is the fluorescent penetrant inspection technology.The defective that component surface exists, like fine cracks, naked eyes are difficult to see clearly, must detect zero uncle of through the fluorescent penetrant inspection method.Often utilize simple checkout equipment at present, detect through manual mode of operation, though simple checkout equipment and the fluorescent penetrant inspection operation that can realize part hand-manipulated, labor intensity of operating personnel is big, and detection efficiency is low.
The utility model content
The technical purpose of the utility model is the deficiency to prior art, and a kind of reduction labor intensity of operating personnel is provided, and improves the aviation fluorescent penetrant detection system of fluorescent penetrant inspection efficient.
The technical scheme that realizes the utility model technical purpose is: a kind of aviation fluorescent penetrant detection system; Comprise prerinse part, permeate portion, back cleaning part; Said prerinse part comprises prerinse groove, drying baker at least; Said permeate portion comprises permeable tank, drippage groove, rinse bath, revisal rinse bath, drying baker and video picture cabinet; Said back cleaning part comprises back rinse bath and drying baker, and each cell body is provided with internal layer and skin, all is set with spray equipment, revolution dress device, lifter and duster in said prerinse groove and back rinse bath, permeable tank, drippage groove, rinse bath, the revisal rinse bath.
As the further optimization of technique scheme, said prerinse groove and back rinse bath, permeable tank, drippage groove, rinse bath, revisal rinse bath are provided with the loam cake of removable unlatching.
As the further optimization of technique scheme, said duster is the independently fluidized bed powder feeder that is installed in the display case.
Compared with prior art; The beneficial effect of a kind of aviation fluorescent penetrant of the utility model detection system mainly shows as: can realize the robotization or the semi-automatic flaw detection operation of component surface defective; Reduce labor intensity of operating personnel, improved the efficient of fluorescent penetrant inspection.
Description of drawings
The structural representation that is connected for each cell body shown in Figure 1.
Embodiment
As one of most preferred embodiment of a kind of aviation fluorescent penetrant of the utility model detection system; Referring to accompanying drawing 1; It comprises prerinse part, permeate portion, back cleaning part; Said prerinse part comprises that at least prerinse groove, drying baker, said permeate portion comprise permeable tank, drippage groove, rinse bath, revisal rinse bath, drying baker and video picture cabinet, and said back cleaning part comprises back rinse bath and drying baker; Each cell body 1 is provided with internal layer and skin, all is set with spray equipment, revolution dress device, lifter and duster in said prerinse groove and back rinse bath, permeable tank, drippage groove, rinse bath, the revisal rinse bath.
Described prerinse groove and back rinse bath, permeable tank, drippage groove, rinse bath, revisal rinse bath are provided with the loam cake 2 of removable unlatching.
Described duster is the independently fluidized bed powder feeder that is installed in the display case.
In sum; After those of ordinary skill in the art reads the utility model file; Technical scheme and technical conceive according to the utility model need not the replacement that scheme between other various corresponding conversion scheme or each embodiment of the utility model is made in creative brainwork, all belong to the scope that the utility model is protected.
Claims (3)
1. aviation fluorescent penetrant detection system; It is characterized in that; Comprise prerinse part, permeate portion, back cleaning part, it is characterized in that said prerinse part comprises prerinse groove, drying baker at least; Said permeate portion comprises permeable tank, drippage groove, rinse bath, revisal rinse bath, drying baker and video picture cabinet; Said back cleaning part comprises back rinse bath and drying baker, and each cell body is provided with internal layer and skin, all is set with spray equipment, revolution dress device, lifter and duster in said prerinse groove and back rinse bath, permeable tank, drippage groove, rinse bath, the revisal rinse bath.
2. a kind of aviation fluorescent penetrant detection system according to claim 1 is characterized in that, said prerinse groove and back rinse bath, permeable tank, drippage groove, rinse bath, revisal rinse bath are provided with the loam cake of removable unlatching.
3. a kind of aviation fluorescent penetrant detection system according to claim 1 is characterized in that, said duster is the independently fluidized bed powder feeder that is installed in the display case.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220099344 CN202471613U (en) | 2012-03-16 | 2012-03-16 | Aviation fluorescent penetration inspection system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220099344 CN202471613U (en) | 2012-03-16 | 2012-03-16 | Aviation fluorescent penetration inspection system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202471613U true CN202471613U (en) | 2012-10-03 |
Family
ID=46919765
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220099344 Expired - Fee Related CN202471613U (en) | 2012-03-16 | 2012-03-16 | Aviation fluorescent penetration inspection system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202471613U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102980898A (en) * | 2012-11-12 | 2013-03-20 | 西安航空动力股份有限公司 | Method for detecting permeability of turbine blade |
| CN103308528A (en) * | 2012-03-16 | 2013-09-18 | 苏州春兴精工股份有限公司 | Aerial fluorescent penetration detection method |
| CN104122269A (en) * | 2013-04-24 | 2014-10-29 | 哈尔滨飞机工业集团有限责任公司 | Aperture interior surface fluorescence detection method |
| US10191479B2 (en) | 2015-09-29 | 2019-01-29 | General Electric Company | Methods and systems for network-based detection of component wear |
| US10726543B2 (en) | 2018-11-27 | 2020-07-28 | General Electric Company | Fluorescent penetrant inspection system and method |
| US10746667B2 (en) | 2018-11-27 | 2020-08-18 | General Electric Company | Fluorescent penetrant inspection system and method |
-
2012
- 2012-03-16 CN CN 201220099344 patent/CN202471613U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103308528A (en) * | 2012-03-16 | 2013-09-18 | 苏州春兴精工股份有限公司 | Aerial fluorescent penetration detection method |
| CN102980898A (en) * | 2012-11-12 | 2013-03-20 | 西安航空动力股份有限公司 | Method for detecting permeability of turbine blade |
| CN104122269A (en) * | 2013-04-24 | 2014-10-29 | 哈尔滨飞机工业集团有限责任公司 | Aperture interior surface fluorescence detection method |
| US10191479B2 (en) | 2015-09-29 | 2019-01-29 | General Electric Company | Methods and systems for network-based detection of component wear |
| US10726543B2 (en) | 2018-11-27 | 2020-07-28 | General Electric Company | Fluorescent penetrant inspection system and method |
| US10746667B2 (en) | 2018-11-27 | 2020-08-18 | General Electric Company | Fluorescent penetrant inspection system and method |
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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 |
Granted publication date: 20121003 Termination date: 20180316 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |