CN206459975U - A kind of blade of aviation engine Surface inspection intelligence control system - Google Patents
A kind of blade of aviation engine Surface inspection intelligence control system Download PDFInfo
- Publication number
- CN206459975U CN206459975U CN201720193278.4U CN201720193278U CN206459975U CN 206459975 U CN206459975 U CN 206459975U CN 201720193278 U CN201720193278 U CN 201720193278U CN 206459975 U CN206459975 U CN 206459975U
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- electric
- shield
- lowering
- base
- hoisting gear
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Abstract
The utility model provides a kind of blade of aviation engine Surface inspection intelligence control system, including electric box, the bottom of the electric box is provided with supporting leg and wheel group, the top of the electric box is provided with shield, the shield is internally provided with detection platform and testing agency, the testing agency is arranged on the upper end of detection platform, the testing agency includes base, the rear end of the base is provided with fixed mount, it is arranged on the electrostatic platform on base, electric-examination drafting board is provided with above the electrostatic platform, lowering or hoisting gear is provided with the electric-examination drafting board, several array probe components arranged in a uniform are provided with the electric-examination drafting board, the array probe component includes probe and the CCD camera being arranged on probe and infrared detecting set, the CCD camera and infrared detecting set are respectively connecting to data acquisition device, the data acquisition device and the host computer electric connection for being arranged on shield.
Description
Technical field
The utility model is related to a kind of detection means, is related to a kind of blade profile detection intelligence control system；Specifically relate to
And a kind of blade of aviation engine Surface inspection intelligence control system.
Background technology
The detection of current blade of aviation engine relates generally to standard jig method, Five Axis continuous mode method, Phalanx and sat
Mensuration is marked, these methods depend on detection device, the existing state-of-the-art continuous gauge head blade profile measurement of Five Axis
System takes around 6,000,000, and price is high, and volume is larger, and precision does not reach Aero-Space rigorous, and can not complete manufacture
The detection of process.
Utility model content
In view of this, main purpose of the present utility model there is provided a kind of blade of aviation engine Surface inspection and intelligently control
System processed.
The technical solution adopted in the utility model is：
A kind of blade of aviation engine Surface inspection intelligence control system, including electric box, the bottom of the electric box are set
There are a supporting leg and wheel group, the top of the electric box is provided with shield, the shield is internally provided with detection platform and detection machine
Structure, the testing agency is arranged on the upper end of detection platform, and the testing agency includes base, and the rear end of the base is provided with admittedly
Determine frame, be arranged on the electrostatic platform on base, be provided with electric-examination drafting board, the electric-examination drafting board and set above the electrostatic platform
Have lowering or hoisting gear, the lowering or hoisting gear is fixed on fixed mount, be provided with the fixed mount power knob, buzzing instrument and jerk by
Expansion link on button, the lowering or hoisting gear is fixed with electric-examination drafting board；It is arranged in a uniform that several are provided with the electric-examination drafting board
Array probe component, the array probe component includes probe and the CCD camera being arranged on probe and infrared acquisition
Instrument, the CCD camera and infrared detecting set are respectively connecting to data acquisition device, and the data acquisition device is with being arranged on shield
Host computer be electrically connected with, the host computer include memory cell, data extracting unit, processor, display unit and control
Device, the memory cell external connection data acquisition device, it internally connects data extracting unit, and the processor connects respectively
Connect display unit and data extracting unit, the lowering or hoisting gear, power knob, buzzing instrument and scram button respectively with control device
It is electrically connected with.
Further, base is provided with the host computer, the base is fixed on shield upper end.
Further, be provided with supply unit in the electric box, the supply unit respectively with power knob, buzzing instrument,
Scram button, lowering or hoisting gear, array probe component and host computer are electrically connected with.
The utility model provides a kind of blade profile detection intelligence control system of the intensive detection probe of array, the dress
That puts simple in construction, intelligent control, it is easy to operate.The manufacturing process detection of inter process is can apply to, defective products flow direction is reduced
Lower process, improves overall manufacture efficiency, shortens the manufacturing cycle.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is sectional view of the present utility model；
Fig. 3 is the structural representation of testing agency in the utility model；
Fig. 4 is the frame principle of system in the utility model.
Embodiment
Describe the utility model in detail below in conjunction with accompanying drawing and specific embodiment, herein signal of the present utility model
Property embodiment and explanation be used for explaining the utility model, but be not intended as limiting of the present utility model.
Referring to figs. 1 to Fig. 4, the utility model discloses a kind of blade of aviation engine Surface inspection intelligence control system,
Including electric box 3, the bottom of the electric box 3 is provided with supporting leg 2 and wheel group 1, and the top of the electric box 3 is provided with shield 4, institute
That states shield 4 is internally provided with detection platform and testing agency 9, and the testing agency 9 is arranged on the upper end of detection platform, described
Testing agency 9 includes base 92, and the lower section of the base 92 is provided with shock-absorbing support 91, and the shock-absorbing support 91 is fixed on detection platform
Upper end, the rear end of the base 92 is provided with fixed mount 98, is arranged on the electrostatic platform 95 on base 92, the electrostatic platform 95
Top be provided with electric-examination drafting board 93, be provided with limiting bracket 96 on the electric-examination drafting board 93, the limiting bracket 96 be used for protect electricity
Detection plate 93 avoids being pressed onto on electrostatic platform 95, the electric-examination drafting board 93 during moving up and down is provided with lowering or hoisting gear
99, the lowering or hoisting gear 99 is fixed on fixed mount 96, and the expansion link on the lowering or hoisting gear 99 is fixed with electric-examination drafting board 93, described
Lowering or hoisting gear 99 pulls electric-examination drafting board 93 to move up and down by expansion link.Several arrangements are provided with the electric-examination drafting board 93 equal
Even array probe component 94, the array probe component 94 includes probe and the CCD camera 941 being arranged on probe
With infrared detecting set 942, the CCD camera 941 and infrared detecting set 942 are respectively connecting to data acquisition device 943, the number
It is electrically connected with according to harvester 943 with being arranged on the host computer 7 of shield 4, the host computer 7 includes memory cell 71, data and carried
Take unit 72, processor 73, display unit 74 and control device 75, the external connection data acquisition device of memory cell 71
943, it internally connects data extracting unit 72, and the processor 72 connects display unit 74 and data extracting unit 72 respectively,
The lowering or hoisting gear 99, power knob 5, buzzing instrument 6 and scram button 7 are electrically connected with control device 75 respectively.The buzzing
Instrument 6 is alarmed for misoperation, and the scram button 7 is used to interrupt in operating process.
Power knob 5, buzzing instrument 6 and scram button 8, the power knob 5, buzzing instrument are provided with the fixed mount 93
6 and scram button 8 be electrically connected with respectively with host computer 7.Base is provided with the host computer 7, the base is fixed on shield 4
End.Be provided with supply unit in the electric box 2, the supply unit respectively with power knob 5, buzzing instrument 6, scram button 8, rise
Falling unit 99, array probe component 94 and host computer 7 are electrically connected with.
Its operation principle is, by the engaging means power supply of power knob 5, starts lowering or hoisting gear 99, by electric-examination drafting board 93
Move, blade is placed on the upper end of electrostatic platform 95, electrostatic platform 95 carries out Electrostatic Treatment, the interference of electrostatic prevented, after placing
Electric-examination drafting board 93 is moved down, and is stopped when array probe component 94 touches blade, is started host computer 7, is set host computer 7
Process of measurement, now, the image information and coordinate position of CCD camera 941 and infrared detecting set 942 for gathering vane section bar,
And the image information collected and coordinate position are transferred to data acquisition device 943, data acquisition device 943 is by data message
Memory cell 71 is passed to, the data that data extracting unit 72 is used in memory cell 71 are extracted and give the data transfer of extraction
Processor 73, processor 73 is modeled by the data message of collection, obtains the model of blade profile, by model analysis from
And reach the purpose of detection.And show obtained result by display unit 74.
In the utility model, manual braking device 90 is provided with the lowering or hoisting gear 99, the manual braking device 90
Electrically connected for lowering or hoisting gear 99 when bad and processing very high degree of precision needs and moves up and down electric-examination drafting board 93 manually and complete electric-examination
The manual of drafting board 93 moves up and down.
The utility model provides a kind of blade profile detection intelligence control system of the intensive detection probe of array, the dress
That puts is simple in construction, can apply to the manufacturing process detection of inter process, reduces the lower process of defective products flow direction, improves overall manufacture
Efficiency, shortens the manufacturing cycle.
The technical scheme disclosed in the utility model embodiment is described in detail above, it is used herein specifically
Embodiment is set forth to the principle and embodiment of the utility model embodiment, and the explanation of above example is only applicable to
Help understands the principle of the utility model embodiment；It is real according to the utility model simultaneously for those of ordinary skill in the art
Example is applied, be will change in embodiment and application, in summary, this specification content should not be understood
For to limitation of the present utility model.
Claims (3)
1. a kind of blade of aviation engine Surface inspection intelligence control system, including electric box, the bottom of the electric box is provided with
Supporting leg and wheel group, the top of the electric box is provided with shield, and the shield is internally provided with detection platform and testing agency,
Characterized in that, the testing agency is arranged on the upper end of detection platform, the testing agency includes base, the rear end of the base
Fixed mount is provided with, the electrostatic platform on base is arranged on, electric-examination drafting board, the electro-detection are provided with above the electrostatic platform
Lowering or hoisting gear is provided with plate, the lowering or hoisting gear is fixed on fixed mount, power knob, buzzing instrument are provided with the fixed mount
And scram button, the expansion link on the lowering or hoisting gear fixes with electric-examination drafting board；Several rows are provided with the electric-examination drafting board
Arrange uniform array probe component, the array probe component include probe and the CCD camera being arranged on probe and
Infrared detecting set, the CCD camera and infrared detecting set are respectively connecting to data acquisition device, and the data acquisition device is with setting
The host computer electric connection in shield is put, the host computer includes memory cell, data extracting unit, processor, display unit
And control device, the memory cell external connection data acquisition device, it internally connects data extracting unit, the processing
Device connects display unit and data extracting unit respectively, the lowering or hoisting gear, power knob, buzzing instrument and scram button respectively with
Control device is electrically connected with.
2. blade of aviation engine Surface inspection intelligence control system according to claim 1, it is characterised in that on described
Base is provided with the machine of position, the base is fixed on shield upper end.
3. blade of aviation engine Surface inspection intelligence control system according to claim 1, it is characterised in that the electricity
Supply unit is provided with gas tank, the supply unit respectively with power knob, buzzing instrument, scram button, lowering or hoisting gear, array
Probe assembly and host computer are electrically connected with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720193278.4U CN206459975U (en) | 2017-03-01 | 2017-03-01 | A kind of blade of aviation engine Surface inspection intelligence control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720193278.4U CN206459975U (en) | 2017-03-01 | 2017-03-01 | A kind of blade of aviation engine Surface inspection intelligence control system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206459975U true CN206459975U (en) | 2017-09-01 |
Family
ID=59690743
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720193278.4U Expired - Fee Related CN206459975U (en) | 2017-03-01 | 2017-03-01 | A kind of blade of aviation engine Surface inspection intelligence control system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206459975U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108760320A (en) * | 2018-05-11 | 2018-11-06 | 山西迪迈沃科光电工业有限公司 | A kind of blade displacement situ detection system device for aero-engine |
| CN109813839A (en) * | 2017-11-22 | 2019-05-28 | 江苏文心古籍数字产业有限公司 | A kind of ancient books fragmentation quality inspection device fixed structure |
-
2017
- 2017-03-01 CN CN201720193278.4U patent/CN206459975U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109813839A (en) * | 2017-11-22 | 2019-05-28 | 江苏文心古籍数字产业有限公司 | A kind of ancient books fragmentation quality inspection device fixed structure |
| CN108760320A (en) * | 2018-05-11 | 2018-11-06 | 山西迪迈沃科光电工业有限公司 | A kind of blade displacement situ detection system device for aero-engine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170901 Termination date: 20210301 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |