CN206407167U - A kind of aircraft wing automatic detection labelling apparatus - Google Patents
A kind of aircraft wing automatic detection labelling apparatus Download PDFInfo
- Publication number
- CN206407167U CN206407167U CN201720035001.9U CN201720035001U CN206407167U CN 206407167 U CN206407167 U CN 206407167U CN 201720035001 U CN201720035001 U CN 201720035001U CN 206407167 U CN206407167 U CN 206407167U
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- fluid pressure
- drive device
- pressure drive
- fixed
- scanner
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Abstract
The utility model discloses a kind of aircraft wing automatic detection labelling apparatus, including：Scanner, scanner support, some pins, the first fluid pressure drive device, the second fluid pressure drive device, the 3rd fluid pressure drive device, expansion link, turning arm, turntable, ground moving car, lifting platform, electric rotating machine, operating control device and synchronous scanning result display instrument.The pit that aircraft wing automatic detection labelling apparatus of the present utility model can be produced during aircraft maintenance to wing by shock carries out automatic detection and marked, it can realize and damage wing is scanned comprehensively, and show on display instrument the parameters such as position, depth, the diameter of each pit in real time；In addition, can also on operating control device preset threshold value, filter out the pit needed repairing, important evidence provided for engineering maintenance personnel, save a large amount of manpowers, accuracy of detection is greatly improved.
Description
Technical field
The utility model belongs to aircraft maintenance field of mechanical technique, more particularly to a kind of aircraft wing automatic detection mark dress
Put.
Background technology
At present, the wing of aircraft often meets with external impacts (such as hail, dust storm), causes pit to occur.It is existing at home
Under the conditions of some maintenances, engineering engineer relies solely on range estimation and checked, is then marked, measures and records manually, then
Judge whether pit needs repairing.The above-mentioned course of work not only needs labor intensive, and is affected by human factors larger；It is heavier
Want, precision is poor, the generation of aircraft accident can be possibly even caused when deviation is serious.
Utility model content
The purpose of this utility model is to provide a kind of aircraft wing automatic detection labelling apparatus.
Therefore, technical solutions of the utility model are as follows：
A kind of aircraft wing automatic detection labelling apparatus, including：Scanner, scanner support, some pins, the first hydraulic pressure
Drive device, the second fluid pressure drive device, the 3rd fluid pressure drive device, expansion link, turning arm, turntable, ground moving car, liter
Platform, electric rotating machine, operating control device and synchronous scanning result display instrument drop；
Wherein, lifting platform includes supporting table and is capable of the truss of folding liftable, and supporting table is horizontally fixed on the upper end of truss；
The lower end of truss is fixed on the surface of ground moving car；Lifting platform is provided with the second fluid pressure drive device, the second hydraulic-driven dress
The cylinder body lower end put is fixed on the surface of ground moving car, and push rod upper end is fixed on the bottom surface of supporting table；
Electric rotating machine is fixed in supporting table, turntable be horizontally set on above electric rotating machine and with the output of electric rotating machine
Axle is connected；
Expansion link includes fix bar and the mobile bar being nested in inside fix bar；
Lower one end of turning arm is hingedly fixed on turntable by pin, and the upper other end passes through pin and two expansion links
The end of upper fix bar is hinged；Turntable is provided with the first vertical fluid pressure drive device, the cylinder body of the first fluid pressure drive device
Lower end is fixed on the surface of turntable, and push rod upper end is fixed on turning arm；
The outer end of mobile bar is hinged by one end of pin and scanner support on two expansion links, and scanner, which is fixed on, to be swept
Retouch the free terminal of instrument support；The cylinder body outer end of 3rd fluid pressure drive device is fixed on the upper end of turning arm, and push rod outer end is with sweeping
The one end for retouching instrument support is hinged；
Operating control device is electrically connected with electric rotating machine, scanner and synchronous scanning result display instrument, and with the first hydraulic pressure
The controller electrical connection of drive device, the second fluid pressure drive device and the 3rd fluid pressure drive device.
Locking device is additionally provided with described electric rotating machine.
Compared with prior art, the aircraft wing automatic detection labelling apparatus that the utility model is provided can be in aircraft maintenance
During the pit that is produced to wing by shock carry out automatic detection and mark, damage wing can comprehensively be scanned, and
Show the detailed parameter such as position, depth, the diameter of each pit in real time on display instrument；In addition, can also be filled in operational control
Preset threshold value is put, the pit needed repairing is filtered out, important evidence is provided for engineering maintenance personnel, a large amount of people are saved
Power, accuracy of detection is greatly improved.
Brief description of the drawings
Fig. 1 is the structural representation of aircraft wing automatic detection labelling apparatus of the present utility model.
Embodiment
Below in conjunction with the accompanying drawings and specific embodiment is described further to the utility model, but following embodiments are right absolutely not
The utility model has any limitation.
As shown in figure 1, the aircraft wing automatic detection labelling apparatus includes：Scanner 2, scanner support 3, some pins
4th, the first fluid pressure drive device 51, the second fluid pressure drive device 52, the 3rd fluid pressure drive device 53, expansion link 6, turning arm 7, rotation
Turntable 8, ground moving car 9, lifting platform 11, electric rotating machine 13, operating control device 14 and synchronous scanning result display instrument 15.
Wherein, lifting platform 11 includes supporting table 10 and is capable of the truss 12 of folding liftable, and supporting table 10 is horizontally fixed on purlin
The upper end of frame 12；The lower end of truss 12 is fixed on the surface of ground moving car 9；Therefore, truss 12 both can be with stored collapsed, moreover it is possible to
The adjustment of upper-lower position is realized, so that scanner 2 is in suitable scanning height.
Lifting platform 11 is provided with the second fluid pressure drive device 52, and the cylinder body lower end of the second fluid pressure drive device 52 is fixed on ground
The surface of face locomotive 9, push rod upper end is fixed on the bottom surface of supporting table 10, so as to realize the upper and lower displacement of supporting table 10；
Electric rotating machine 13 is fixed in supporting table 10, and turntable 8 is horizontally set on the top of electric rotating machine 13 and and electric rotating
The output shaft of machine 13 is connected, and so as to realize the rotation of the planar all angles of turntable 8, turning arm 7 is realized indirectly
The planar rotation of each angle.In addition, locking device is additionally provided with electric rotating machine 13, to realize the fixation in unspecified angle.
Expansion link 6 includes fix bar and the mobile bar being nested in inside fix bar；
The lower end of turning arm 7 is hingedly fixed on turntable 8 by pin 4, and upper end passes through pin 4 and two expansion links 6
The end of upper fix bar is hinged；Turntable 8 is provided with the first vertical fluid pressure drive device 51, the first fluid pressure drive device 51
Cylinder body lower end is fixed on the surface of turntable 8, and push rod upper end is fixed on turning arm 7；Pass through the first fluid pressure drive device 51
Driving, realizes the change at the inclination angle of turning arm 7 with respect to the horizontal plane；
The outer end of mobile bar is hinged by one end of pin 4 and scanner support 3 on two expansion links 6, and scanner 2 is fixed
In the free terminal of scanner support 3；The cylinder body outer end of 3rd fluid pressure drive device 53 is fixed on the upper end of turning arm 7, push rod
Outer end and one end of scanner support 3 be hinged, and mobile bar on expansion link 6 is promoted by the 3rd fluid pressure drive device 53 provides power
Shortening or elongation, realize closely and at a distance comprehensively scanning；
Operating control device 14 is electrically connected with electric rotating machine 13, scanner 2 and synchronous scanning result display instrument 15, and with
The controller electrical connection of one fluid pressure drive device 51, the second fluid pressure drive device 52 and the 3rd fluid pressure drive device 53；Work people
Member's input instruction on the keyboard of operating control device 14, by the instruction of 14 pairs of operating control device parse after to scanning
Instrument 2, the first fluid pressure drive device 51, the second fluid pressure drive device 52 and the 3rd fluid pressure drive device 53 are controlled, and will be swept
The Real-time Monitoring Data for retouching instrument 2 is shown on synchronous scanning result display instrument 15.In addition, can also be pre- on operating control device 14
First given threshold, filters out the pit needed repairing and goes forward side by side line label.
Now the operation principle of aircraft wing automatic detection labelling apparatus of the present utility model is described below：
When needing to detect aircraft wing 1, ground moving car 9 is moved to wing 1 first by staff attached
Closely, testing inspection parameter and operational order are then inputted on operating control device 14, under the control of operating control device 14,
Electric rotating machine 13 is rotated, and makes its rotation to appropriate position and locking；Then the first fluid pressure drive device 51, the second hydraulic pressure are passed through
The controller of the fluid pressure drive device 53 of drive device 52 and the 3rd elongates or shortens push rod thereon, until making the He of supporting table 10
Turning arm 7 is in suitable height, and expansion link 6 is in suitable length.During above-mentioned continuous adjustment, scanner 2 is utilized
The surface of wing 1 is scanned, the result of scanning is then fed back into operating control device 14, at operating control device 14
By in the result simultaneous display of scanner 2 to synchronous scanning result display instrument 15 after reason；When finding pit, operating control device
14, according to the scan data of scanner 2, calculate the data such as position, depth, the diameter of pit, then with having pre-entered
The threshold value of operating control device 14 is compared, and is filtered out the position of the whole pits needed repairing and is marked, will be final
Mark result show, important foundation is provided for locomotive work personnel.Said process is repeated, until completing whole wing 1
Detection.
The utility model provide aircraft wing automatic detection labelling apparatus can during aircraft maintenance to wing 1 because
The pit for hitting and producing carries out automatic detection and marked, and can realize and damage wing is scanned comprehensively, and on display instrument
The parameters such as position, depth, the diameter of each pit are shown in real time；In addition, can also in the preset threshold value of operating control device 14,
The pit needed repairing is filtered out by being compared with the threshold value, important evidence is provided for engineering maintenance personnel, saves big
Manpower is measured, accuracy of detection is greatly improved.
Claims (2)
1. a kind of aircraft wing automatic detection labelling apparatus, it is characterised in that the aircraft wing automatic detection labelling apparatus bag
Include：Scanner (2), scanner support (3), some pins (4), the first fluid pressure drive device (51), the second fluid pressure drive device
(52), the 3rd fluid pressure drive device (53), expansion link (6), turning arm (7), turntable (8), ground moving car (9), lifting platform
(11), electric rotating machine (13), operating control device (14) and synchronous scanning result display instrument (15)；
Wherein, lifting platform (11) includes supporting table (10) and is capable of the truss (12) of folding liftable, and supporting table (10) level is fixed
Upper end in truss (12)；The lower end of truss (12) is fixed on the surface of ground moving car (9)；Lifting platform (11) is provided with second
Fluid pressure drive device (52), the cylinder body lower end of the second fluid pressure drive device (52) is fixed on the surface of ground moving car (9), push rod
Upper end is fixed on the bottom surface of supporting table (10)；
Electric rotating machine (13) is fixed in supporting table (10), turntable (8) be horizontally set on above electric rotating machine (13) and with rotation
The output shaft of rotating motor (13) is connected；
Expansion link (6) includes fix bar and the mobile bar being nested in inside fix bar；
Lower one end of turning arm (7) is hingedly fixed on turntable (8) by pin (4), and the upper other end passes through pin (4) and two
The end of fix bar is hinged on root expansion link (6)；Turntable (8) is provided with vertical the first fluid pressure drive device (51), first
The cylinder body lower end of fluid pressure drive device (51) is fixed on the surface of turntable (8), and push rod upper end is fixed on turning arm (7)；
The outer end of mobile bar is hinged by one end of pin (4) and scanner support (3) on two expansion links (6), scanner (2)
It is fixed on the free terminal of scanner support (3)；The cylinder body outer end of 3rd fluid pressure drive device (53) is fixed on turning arm (7)
Upper end, one end of push rod outer end and scanner support (3) is hinged；
Operating control device (14) is electrically connected with electric rotating machine (13), scanner (2) and synchronous scanning result display instrument (15), and
It is electrically connected with the controller of the first fluid pressure drive device (51), the second fluid pressure drive device (52) and the 3rd fluid pressure drive device (53)
Connect.
2. aircraft wing automatic detection labelling apparatus according to claim 1, it is characterised in that described electric rotating machine
(13) locking device is additionally provided with.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720035001.9U CN206407167U (en) | 2017-01-12 | 2017-01-12 | A kind of aircraft wing automatic detection labelling apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720035001.9U CN206407167U (en) | 2017-01-12 | 2017-01-12 | A kind of aircraft wing automatic detection labelling apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206407167U true CN206407167U (en) | 2017-08-15 |
Family
ID=59554881
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720035001.9U Expired - Fee Related CN206407167U (en) | 2017-01-12 | 2017-01-12 | A kind of aircraft wing automatic detection labelling apparatus |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206407167U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109557170A (en) * | 2018-12-03 | 2019-04-02 | 中国人民解放军国防科技大学 | SQUID-based wing detection system and detection method thereof |
| CN110546476A (en) * | 2018-04-27 | 2019-12-06 | 深圳市大疆创新科技有限公司 | Folding equipment |
| CN112362726A (en) * | 2020-10-09 | 2021-02-12 | 郑州大学 | Device and method for detecting internal defects of building material based on magnetic particles |
-
2017
- 2017-01-12 CN CN201720035001.9U patent/CN206407167U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110546476A (en) * | 2018-04-27 | 2019-12-06 | 深圳市大疆创新科技有限公司 | Folding equipment |
| CN109557170A (en) * | 2018-12-03 | 2019-04-02 | 中国人民解放军国防科技大学 | SQUID-based wing detection system and detection method thereof |
| CN112362726A (en) * | 2020-10-09 | 2021-02-12 | 郑州大学 | Device and method for detecting internal defects of building material based on magnetic particles |
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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: 20170815 Termination date: 20180112 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |