CN206885377U - Outer wing numerical control posture adjusting system in a kind of wing finishing type frame - Google Patents
Outer wing numerical control posture adjusting system in a kind of wing finishing type frame Download PDFInfo
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- CN206885377U CN206885377U CN201720764181.4U CN201720764181U CN206885377U CN 206885377 U CN206885377 U CN 206885377U CN 201720764181 U CN201720764181 U CN 201720764181U CN 206885377 U CN206885377 U CN 206885377U
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- Prior art keywords
- longitudinal
- wing
- outer wing
- screw mandrel
- numerical control
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims description 15
- 238000004891 communication Methods 0.000 claims description 3
- 230000005611 electricity Effects 0.000 claims description 2
- 238000003754 machining Methods 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000011156 evaluation Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
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Abstract
The utility model discloses a kind of wing to finish outer wing numerical control posture adjusting system in type frame, it includes horizontal mobile mechanism, movable mechanism and locator, movable mechanism is arranged on horizontal mobile mechanism, locator is provided with movable mechanism, ball head locking device is provided with locator.The beneficial effects of the utility model are：It is compact-sized, improve machining accuracy, realize in outer wing is horizontal, the adjustment of front and rear and vertical direction, simple to operate.
Description
Technical field
The technical field of the middle outer wing pose adjustment of aircraft is the utility model is related to, particularly a kind of wing finishing type frame
Middle outer wing numerical control posture adjusting system.
Background technology
In order to meet the needs of outer wing assemble flow in aircraft, wing finishes outer wing numeral posture adjusting system in type frame, uses
In China and foreign countries' cautiously box posture adjustment, the digitlization posture adjustment and processing of the thriving box in aircraft China and foreign countries are completed.The system mainly includes：Middle outer wing is adjusted
Appearance numerical control positioning system, middle outer wing guarantor type bracket, system controlling software etc..Wherein, middle outer wing numerical control posture adjusting system is used for left and right
The middle rib of outer wing 2,15 rib face millings and butt hole drill centering outer wing after the completion of the positioning of outer wing in finishing, and finishing
Detection, the evaluation of Specifications, as shown in Figure 1.Middle outer wing guarantor type bracket is used to hold up middle outer wing, middle outer wing guarantor type support
The bottom of frame is provided with bulb, bulb is connected with middle outer wing posture adjustment numerical control positioning system realize in outer wing positioning.It is however, existing
The middle outer wing numerical control posture adjusting system having is unable to the height of outer wing in accurate adjustment, moved forward and backward, left and right displacement, causes following process
Precision is not high, and bulb is locked insecure with middle outer wing posture adjustment numerical control positioning system in addition, and bulb easily loosens, and middle outer wing rocks,
Mismachining tolerance is big.
Utility model content
The shortcomings that the purpose of this utility model is to overcome prior art, there is provided a kind of compact-sized, raising machining accuracy,
Outer wing is horizontal in realization, the adjustment of front and rear and vertical direction, outer wing numerical control posture adjusting system in wing simple to operate finishing type frame.
The purpose of this utility model is achieved through the following technical solutions：Outer wing numerical control is adjusted in a kind of wing finishing type frame
Appearance system, it includes horizontal mobile mechanism, movable mechanism and locator, movable mechanism and is arranged at horizontal mobile mechanism
On, locator is provided with movable mechanism, described locator includes support base, servomotor, vertical screw mandrel and bearing,
Opening is offered at the top of support base, the cavity of open communication is provided with support base, the bottom of cavity is installed with servo
Motor, vertical screw mandrel within the cavity is connected with servo motor output shaft, bearing, bearing are threaded with vertical screw mandrel
Top is provided with ball head locking device, and ball head locking device includes pedestal, shell, trip lever, unblock briquetting and self-locking jacking block, outside
Clamshell is installed with vertical cylinder, unblock briquetting is connected with the piston rod of vertical cylinder outside pedestal in pedestal side wall, solve
The side wall of lock briquetting is provided with blind hole, trip lever is fitted with blind hole, trip lever extends housing exterior, the top of described pedestal
Portion offers spherical groove, and the self-locking jacking block positioned at spherical groove side, below cover top portion, self-locking are provided with the top of pedestal
Jacking block is provided with riser with unblock briquetting wedge-like engagement and its top, the lower surface of described cover top portion, positioned at self-locking jacking block
Top is installed with fixed block, and fixed block offers spring mounting hole with riser to opposite, and being fixed with level in spring mounting hole sets
The spring put, the other end of spring are fixed on riser, and lead is fixedly provided with spring mounting hole, and lead sequentially runs through bullet
Spring and riser are set.
Described horizontal mobile mechanism includes sliding laterally base, cross lead screw, cross motor and cross slide way, laterally electricity
Machine, which is fixedly installed in, to be slid laterally on base, and cross lead screw is arranged at horizontal cunning with cross motor output axis connection, cross slide way
The top of base is moved, is threaded with longitudinal sliding motion base on cross lead screw, longitudinal sliding motion base is slidably matched with cross slide way.
Described movable mechanism includes longitudinal motor, longitudinal rail and longitudinal screw mandrel, and longitudinal motor is fixed on longitudinal direction
On sliding bottom, longitudinal rail is arranged on longitudinal sliding motion base, longitudinal screw mandrel and longitudinal motor output axis connection, longitudinal screw mandrel
On be threaded with rebound, rebound is slidably matched with longitudinal screw mandrel.
The support base of described locator is fixedly arranged at the top of rebound.
The utility model has advantages below：The utility model is compact-sized, improves machining accuracy, outer wing water in realization
Flat, front and rear and vertical direction adjusts, is simple to operate.
Brief description of the drawings
Fig. 1 is the positioning schematic diagram of middle outer wing；
Fig. 2 is the connection diagram of horizontal mobile mechanism and movable mechanism；
Fig. 3 is the structural representation of locator；
Fig. 4 is the front view of ball head locking device；
Fig. 5 is the top view of ball head locking device；
Fig. 6 is Fig. 4 A-A sectional views；
In figure, 1- support bases, 2- servomotors, the vertical screw mandrels of 3-, 4- bearings, 5- ball head locking devices, 6- pedestals, outside 7-
Shell, 8- trip levers, 9- unblock briquettings, 10- self-locking jacking blocks, the vertical cylinders of 11-, 12- spherical grooves, 13- risers, 14- fixed blocks,
15- springs, 16- slide laterally base, 17- cross lead screws, 18- cross motors, 19- cross slide ways, 20- longitudinal sliding motion bases,
21- longitudinal motors, 22- longitudinal rails, 23- longitudinal screw mandrels, 24- rebounds, 25- leads.
Embodiment
The utility model is further described below in conjunction with the accompanying drawings, the scope of protection of the utility model be not limited to
It is lower described：
As shown in Fig. 2 ~ 6, outer wing numerical control posture adjusting system in a kind of wing finishing type frame, it include horizontal mobile mechanism,
Movable mechanism and locator, movable mechanism are arranged on horizontal mobile mechanism, and it is fixed to be provided with movable mechanism
Position device, described locator include support base 1, servomotor 2, vertical screw mandrel 3 and bearing 4, and the top of support base 1 offers out
Mouthful, the cavity of open communication is provided with support base 1, the bottom of cavity is installed with servomotor 2, and servomotor 2 exports
Vertical screw mandrel 3 within the cavity is connected with axle, bearing 4 is threaded with vertical screw mandrel 3, the top of bearing 4 is provided with ball
Head locking device 5, ball head locking device 5 include pedestal 6, shell 7, trip lever 8, unblock briquetting 9 and self-locking jacking block 10, shell 7
Cover at outside pedestal 6, vertical cylinder 11 is installed with the side wall of pedestal 6, unblock pressure is connected with the piston rod of vertical cylinder 11
Block 9, the side wall of unblock briquetting 9 are provided with blind hole, trip lever 8 are fitted with blind hole, trip lever 8 is extended outside shell 7, described
The top of pedestal 6 offer spherical groove 12, the top of pedestal 6 is provided with positioned at the side of spherical groove 12, under the top of shell 7
The self-locking jacking block 10 of side, self-locking jacking block 10 are provided with riser 13, described shell 7 with the unblock wedge-like engagement of briquetting 9 and its top
The lower surface at top, fixed block 14 is installed with above self-locking jacking block 10, fixed block 14 offers bullet with riser 13 to opposite
Spring mounting hole, horizontally disposed spring 15 is fixed with spring mounting hole, the other end of spring 15 is fixed on riser 13, spring
Lead 25 is fixedly provided with mounting hole, lead 25 is sequentially set through spring 15 and riser 13.
Described horizontal mobile mechanism includes sliding laterally base 16, cross lead screw 17, cross motor 18 and cross slide way
19, cross motor 18, which is fixedly installed in, to be slid laterally on base 16, and cross lead screw 17 exports axis connection with cross motor 18, laterally
Guide rail 19 is arranged at the top for sliding laterally base 16, and longitudinal sliding motion base 20 is threaded with cross lead screw 17, and longitudinal direction is sliding
Dynamic base 20 is slidably matched with cross slide way 19.
Described movable mechanism includes longitudinal motor 21, longitudinal rail 22 and longitudinal screw mandrel 23, and longitudinal motor 21 is solid
Due on longitudinal sliding motion base 20, longitudinal rail 22 is arranged on longitudinal sliding motion base 20, longitudinal screw mandrel 23 and longitudinal motor 21
Axis connection is exported, is threaded with rebound 24 in longitudinal screw mandrel 23, rebound 24 is slidably matched with longitudinal screw mandrel 23.
The support base 1 of described locator is fixedly arranged on the top of rebound 24.
The course of work of the present utility model is as follows：
S1, middle outer wing installation, the middle outer wing of aircraft to be processed is positioned over middle outer wing guarantor type pallet top；In middle outer wing
The bottom of guarantor's type bracket is provided with bulb, and then bulb is assemblied in spherical groove 12 from top to bottom, and spherical groove 12 is matched somebody with somebody with bulb
Close；Trip lever 8 to be extracted, then controls the vertical piston rod of cylinder 11 to stretch out, unblock briquetting 9 promotes self-locking jacking block 10 to the left, from
The lock compression spring 15 of jacking block 10 is simultaneously resisted against on bulb, so as to realize the locking of bulb, is made bulb locking more firm, is avoided
Middle outer wing rocks in process, improves the machining accuracy of middle outer wing；
When S2, control cross motor 18 rotate, cross lead screw 17 rotates, and longitudinal sliding motion base 20 is along the water of cross slide way 19
Translation is dynamic, so as to which outer wing moves horizontally in realizing；When controlling the rotation of longitudinal motor 21, longitudinal screw mandrel 23 rotates, the edge of rebound 24
It is movable longitudinal rail 22, so as to which outer wing moves forward and backward in realizing；When controlling the startup of servomotor 2, servomotor 2 drives
Vertical screw mandrel 3 rotates, and bearing 4 moves up and down along vertical screw mandrel 3, so as to which outer wing moves up and down in realizing, can accurately realize
Middle outer wing is horizontal, front and rear and vertical direction adjustment, is easy to the accurate processing of follow-up centering outer wing.
Claims (4)
- A kind of 1. outer wing numerical control posture adjusting system in wing finishing type frame, it is characterised in that：It includes horizontal mobile mechanism, front and rear Travel mechanism and locator, movable mechanism are arranged on horizontal mobile mechanism, and locator is provided with movable mechanism, Described locator includes support base（1）, servomotor（2）, vertical screw mandrel（3）And bearing（4）, support base（1）Top open Provided with opening, support base（1）The cavity of open communication is inside provided with, the bottom of cavity is installed with servomotor（2）, servo Motor（2）Vertical screw mandrel within the cavity is connected with output shaft（3）, vertical screw mandrel（3）On be threaded with bearing（4）, Bearing（4）Top is provided with ball head locking device（5）, ball head locking device（5）Including pedestal（6）, shell（7）, trip lever （8）, unblock briquetting（9）With self-locking jacking block（10）, shell（7）Cover at pedestal（6）Outside, pedestal（6）It is installed with side wall vertical To cylinder（11）, vertical cylinder（11）Piston rod on be connected with unblock briquetting（9）, unlock briquetting（9）Side wall be provided with it is blind Hole, trip lever is fitted with blind hole（8）, trip lever（8）Extend shell（7）Outside, described pedestal（6）Top offer Spherical groove（12）, pedestal（6）Top be provided with positioned at spherical groove（12）Side, positioned at shell（7）Self-locking top below top Block（10）, self-locking jacking block（10）With unlocking briquetting（9）Wedge-like engagement and its top be provided with riser（13）, described shell（7） The lower surface at top, positioned at self-locking jacking block（10）Top is installed with fixed block（14）, fixed block（14）With riser（13）To opposite Spring mounting hole is offered, horizontally disposed spring is fixed with spring mounting hole（15）, spring（15）The other end be fixed on Riser（13）On, lead is fixedly provided with spring mounting hole（25）, lead（25）Sequentially run through spring（15）And riser （13）Set.
- 2. outer wing numerical control posture adjusting system in a kind of wing finishing type frame according to claim 1, it is characterised in that：It is described Horizontal mobile mechanism include slide laterally base（16）, cross lead screw（17）, cross motor（18）And cross slide way（19）, it is horizontal To motor（18）It is fixedly installed in and slides laterally base（16）On, cross lead screw（17）With cross motor（18）Export axis connection, Cross slide way（19）It is arranged at and slides laterally base（16）Top, cross lead screw（17）On be threaded with longitudinal sliding motion base （20）, longitudinal sliding motion base（20）With cross slide way（19）It is slidably matched.
- 3. outer wing numerical control posture adjusting system in a kind of wing finishing type frame according to claim 1, it is characterised in that：It is described Movable mechanism include longitudinal motor（21）, longitudinal rail（22）And longitudinal screw mandrel（23）, longitudinal motor（21）It is fixed on Longitudinal sliding motion base（20）On, longitudinal rail（22）It is arranged at longitudinal sliding motion base（20）On, longitudinal screw mandrel（23）With longitudinal electricity Machine（21）Export axis connection, longitudinal screw mandrel（23）On be threaded with rebound（24）, rebound（24）With longitudinal screw mandrel（23） It is slidably matched.
- 4. outer wing numerical control posture adjusting system in a kind of wing finishing type frame according to claim 1, it is characterised in that：It is described Locator support base（1）It is fixedly arranged on rebound（24）Top.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720764181.4U CN206885377U (en) | 2017-06-28 | 2017-06-28 | Outer wing numerical control posture adjusting system in a kind of wing finishing type frame |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720764181.4U CN206885377U (en) | 2017-06-28 | 2017-06-28 | Outer wing numerical control posture adjusting system in a kind of wing finishing type frame |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206885377U true CN206885377U (en) | 2018-01-16 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720764181.4U Expired - Fee Related CN206885377U (en) | 2017-06-28 | 2017-06-28 | Outer wing numerical control posture adjusting system in a kind of wing finishing type frame |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206885377U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107310749A (en) * | 2017-06-28 | 2017-11-03 | 成都立航科技有限公司 | Outer wing numerical control posture adjusting system in a kind of wing finishing type frame |
| CN108296760A (en) * | 2018-02-05 | 2018-07-20 | 岳池县宇虹科技有限公司 | A kind of automatic correction device of filter resistors frame |
| CN110900483A (en) * | 2019-11-19 | 2020-03-24 | 芜湖市努尔航空信息科技有限公司 | A positioner for aircraft part frock |
-
2017
- 2017-06-28 CN CN201720764181.4U patent/CN206885377U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107310749A (en) * | 2017-06-28 | 2017-11-03 | 成都立航科技有限公司 | Outer wing numerical control posture adjusting system in a kind of wing finishing type frame |
| CN107310749B (en) * | 2017-06-28 | 2022-07-05 | 成都立航科技股份有限公司 | Outer wing numerical control posture adjustment system in wing finish machining type frame |
| CN108296760A (en) * | 2018-02-05 | 2018-07-20 | 岳池县宇虹科技有限公司 | A kind of automatic correction device of filter resistors frame |
| CN110900483A (en) * | 2019-11-19 | 2020-03-24 | 芜湖市努尔航空信息科技有限公司 | A positioner for aircraft part frock |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 610041 No. 24 Yongfeng Road, hi tech Zone, Chengdu, Sichuan, 1 Patentee after: CHENGDU LIHANG TECHNOLOGY Co.,Ltd. Address before: 610041 No. 24 Yongfeng Road, hi tech Zone, Chengdu, Sichuan, 1 Patentee before: CHENGDU LIHANG TECHNOLOGY CO.,LTD. |
|
| CP01 | Change in the name or title of a patent holder | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |