CN203937867U - A kind of accuracy controlling device of adjusting for wing wallboard attitude - Google Patents
A kind of accuracy controlling device of adjusting for wing wallboard attitude Download PDFInfo
- Publication number
- CN203937867U CN203937867U CN201420380798.2U CN201420380798U CN203937867U CN 203937867 U CN203937867 U CN 203937867U CN 201420380798 U CN201420380798 U CN 201420380798U CN 203937867 U CN203937867 U CN 203937867U
- Authority
- CN
- China
- Prior art keywords
- framework
- leading screw
- rotating shaft
- screw
- wallboard
- 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 - Lifetime
Links
- 244000309464 bull Species 0.000 claims description 13
- 238000000034 method Methods 0.000 abstract description 4
- 230000001360 synchronised effect Effects 0.000 description 16
- 238000005553 drilling Methods 0.000 description 4
- 238000000926 separation method Methods 0.000 description 4
- 230000004913 activation Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 241000252254 Catostomidae Species 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000004140 cleaning Methods 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 230000002452 interceptive effect Effects 0.000 description 2
- 238000010030 laminating Methods 0.000 description 2
- 230000002093 peripheral effect Effects 0.000 description 2
- 238000004080 punching Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 229910001069 Ti alloy Inorganic materials 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000000712 assembly Effects 0.000 description 1
- 238000000429 assembly Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000012827 research and development Methods 0.000 description 1
Landscapes
- Conveying And Assembling Of Building Elements In Situ (AREA)
Abstract
The utility model provides a kind of accuracy controlling device of adjusting for wing wallboard attitude, comprise the conformal framework (11) being cascading, X-direction framework (23), Y-direction framework (33), Z-direction framework (48) and Z-direction fixed disc (44), conformal framework (11) is fixedly connected with X-direction framework (23), also comprise and can make Z-direction framework (48) with the Z-direction driven unit of the first rotating shaft rotation perpendicular to Z-direction fixed disc (44), can make Y-direction framework (33) to be parallel to the Y-direction driven unit and the X-direction driven unit that can make X-direction framework (23) rotate to be parallel to the 3rd rotating shaft of Y-direction framework (33) of the second rotating shaft rotation of Z-direction framework (48).Should for the accuracy controlling device of wing wallboard attitude adjustment, can be used for the assembling of medium and small aircraft wing wallboard, and can realize the attitude accurate adjustment at fitting process wing centre section wallboard, can effectively improve efficiency of assembling and assembly quality.
Description
Technical field
The utility model relates to aircraft manufacturing equipment technical field, and concrete is a kind of accuracy controlling device of adjusting for wing wallboard attitude.
Background technology
During the assembling of aircraft wing wallboard, first the skeleton that comprises the parts such as wing root, titanium alloy beam and aluminum alloy beams is installed on fixed frame, again the composites wallboard and the skeleton that comprise the parts such as wing cover, wall and long purlin are fitted, because the difficult processing of composite material is to reach one-time-reach-place, can there is the position with skeleton interference.To there is the position of interfering, demarcate, after separating is repaired demarcated interference position, again involutoryly carry out interference position inspection, demarcation, separation is repaired ... until repaired all interference position, to integral panel and the skeleton location of again fitting, and wing wallboard is carried out to drilling, after drilling completes, integral panel is departed to work such as carrying out dedusting, clear bits, cleaning and gluing with skeleton from fixed frame, involutory with skeleton afterwards, carry out being connected of wallboard and skeleton.
It is domestic when wing wallboard assembles, mostly adopt manual mode to carry out the attitude adjustment between wing wallboard and fixed frame, work is waited in laminating location, need first with lifting device, wing wallboard to be hung in the air, the laminating location of wallboard and skeleton is manually adjusted and carried out to the mode that adopts rope to pull to the attitude of wallboard, to there is the position of interfering, demarcate, wing wallboard is sling and carried out separation again, after separating is repaired demarcated interference position, again sling and carry out the involutory of wing wallboard, carry out interference position inspection, demarcate, the wallboard separation of slinging is repaired ... until repaired all interference position, sling wallboard and the skeleton location of fitting, carry out drilling, after drilling completes, with lifting device, wallboard is sling, carry out separation, dedusting, after the work such as clear bits and cleaning complete, again wallboard is sling, manually wallboard and skeleton are carried out involutory, connect.
In wing wallboard assembling, adopted a large amount of advanced persons' automatic assembly system abroad, but these advanced assembly systems are expensive, introducing these assembly systems needs a large amount of fund inputs, and most of advanced persons' equipment abroad blocks domestic.
The mode of the manual setting wallboard attitude that in wing wallboard assembling, the ropes that adopt pull more at home, frock that this manual mode not only needs is many, operating personal is many, and between wing and frock, rapport is complicated, needs repeatedly coordination repeatedly; Wing wallboard attitude is adjusted difficulty in addition, positional accuracy is poor, has had a strong impact on wing efficiency of assembling and assembly quality, cannot meet high efficiency, special quality requirement.
In wing fitting process, research and development along with automation punching system, demand to the wing wallboard posture adjustment registration device coordinating is with it more and more urgent, manual operations is from assembly quality or efficiency of assembling aspect all cannot adapt to it, wing wallboard posture adjustment registration device and automatic punching system need to be combined, form wing automatic assembly system, to realize the automation of wing assembling.
Utility model content
Existing for solving wing wallboard attitude adjustment difficulty in wing assembling, adjusting the poor technical matters of accuracy rate in order to solve.The utility model provides a kind of accuracy controlling device of adjusting for wing wallboard attitude, should can be used for for the accuracy controlling device of wing wallboard attitude adjustment the assembling of medium and small aircraft wing wallboard, the attitude accurate adjustment at fitting process wing centre section wallboard can be realized, efficiency of assembling and assembly quality can be effectively improved.
The utility model for solving the technical scheme of its technical matters employing is: a kind of accuracy controlling device of adjusting for wing wallboard attitude, comprise the conformal framework being cascading, X-direction framework, Y-direction framework, Z-direction framework and Z-direction fixed disc, conformal framework is fixedly connected with X-direction framework, conformal framework is provided with the wallboard locating cover for wing wallboard location, the described accuracy controlling device for the adjustment of wing wallboard attitude also comprises can make Z-direction framework with the Z-direction driven unit of the first rotating shaft rotation perpendicular to Z-direction fixed disc, can make Y-direction framework to be parallel to the Y-direction driven unit and the X-direction driven unit that can make X-direction framework rotate to be parallel to the 3rd rotating shaft of Y-direction framework of the second rotating shaft rotation of Z-direction framework, this first rotating shaft, mutually vertical between this second rotating shaft and the 3rd rotating shaft.
X-direction driven unit comprise be arranged on X-direction frame edge X-direction leading screw bearing, be arranged on the X-direction screw of Y-direction frame edge, through the X-direction leading screw of X-direction leading screw bearing and X-direction screw, X-direction leading screw is fixedly connected with the inner ring of X-direction leading screw bearing, screw thread fit between X-direction leading screw and X-direction screw, X-direction framework and Y-direction framework are rotationally connected, rotating shaft between X-direction framework and Y-direction framework is the 3rd rotating shaft, when X-direction leading screw rotates, X-direction framework can be take the 3rd rotating shaft as axle rotation.
X-direction leading screw bearing peripheral hardware has X-direction bearing seat, and X-direction bearing seat is rotationally connected with the X-direction seat supports bearing seat being arranged on X-direction framework, and X-direction screw is provided with X-direction nut seat outward, and X-direction nut seat is rotationally connected with the X-direction seat supports bearing seat being arranged on Y-direction framework.
One end of X-direction leading screw is connected with the first actuating device for driving X-direction leading screw to rotate, and the other end of X-direction leading screw is connected with anti-drop block.
This first actuating device comprises the X-direction drive motor that can drive X-direction leading screw to rotate, and X-direction drive motor is fixedly connected with X-direction bearing seat by X-direction electric machine support.
Y-direction driven unit comprise be arranged on Y-direction frame edge Y-direction leading screw bearing, be arranged on the Y-direction screw of Z-direction frame edge, through the Y-direction leading screw of Y-direction leading screw bearing and Y-direction screw, Y-direction leading screw is fixedly connected with the inner ring of Y-direction leading screw bearing, screw thread fit between Y-direction leading screw and Y-direction screw, Y-direction framework and Z-direction framework are rotationally connected, rotating shaft between Y-direction framework and Z-direction framework is this second rotating shaft, when Y-direction leading screw rotates, Y-direction framework can be take this second rotating shaft as axle rotation.
Y-direction leading screw bearing peripheral hardware has Y-direction bearing seat, and Y-direction bearing seat is rotationally connected with the Y-direction seat supports bearing seat being arranged on Y-direction framework, and Y-direction screw is provided with Y-direction nut seat outward, and Y-direction nut seat is rotationally connected with the Y-direction seat supports bearing seat being arranged on Z-direction framework.
One end of Y-direction leading screw is connected with the second actuating device for driving Y-direction leading screw to rotate, and the other end of Y-direction leading screw is connected with anti-drop block.
Z-direction driven unit comprises bull gear and the slide block being fixedly connected with Z-direction framework, the axis of bull gear is this first rotating shaft, Z-direction fixed disc is provided with the 3rd driver train for driving bull gear to rotate, and is also provided with arc-shaped guide rail on Z-direction fixed disc, and slide block is plugged in arc-shaped guide rail.
On conformal framework, be also provided with for the fixing conformal sucker of this wing wallboard, conformal sucker is adjusted screw rod by sucker and is connected with conformal framework.
The beneficial effects of the utility model are:
1, this device comprises shape-keeping frame, can realize the attitude of the wallboard of different model, different sizes adjust by different shape-keeping frames.
2, between shape-keeping frame and A frame, adopt " L " type locating surface increased pressure board location, dismounting is convenient rapidly;
3, activation point is applied to frame edge, has greatly improved the adjustment precision that attitude is adjusted, realized the accuracy controlling of attitude;
4, three layers of framework are realized three direction posture adjustments, compact conformation;
5, being provided with butt flange can be conveniently integrated with robot or other three degree of freedom mobile device.
Accompanying drawing explanation
Below in conjunction with accompanying drawing, the accuracy controlling device for the adjustment of wing wallboard attitude described in the utility model is described in further detail.
Fig. 1 is the front view of this accuracy controlling device of adjusting for wing wallboard attitude.
Fig. 2 is the left view of this accuracy controlling device of adjusting for wing wallboard attitude.
Fig. 3 is the birds-eye view of this accuracy controlling device of adjusting for wing wallboard attitude.
Fig. 4 is the front perspective view of this accuracy controlling device of adjusting for wing wallboard attitude.
Fig. 5 is the enlarged diagram at A position in Fig. 4.
Fig. 6 is the enlarged diagram at B position in Fig. 4.
Fig. 7 is the enlarged diagram of Z-direction driven unit.
Fig. 8 is the rear perspective view of this accuracy controlling device of adjusting for wing wallboard attitude.
11. conformal frameworks wherein, 12. conformal suckers, 13. adjust suckers to adjust screw rods, 14. wallboard locating covers, 15. positioning pressuring plates;
21.X is to drive motor, and 22.X is to small synchronous pulley, and 23.X is to framework, 24.X is to large synchronous pulley, and 25.X is to Timing Belt, and 26.X is to leading screw, 27.X is to electric machine support, and 28.X is to leading screw bearing, and 29.X is to bearing seat, 210.X is to screw, 211.X is to nut seat, and 213.X is to seat supports bearing seat, the outside revolving bed of 214.X, the inside revolving bed of 215.X, 216. anti-drop blocks;
31.Y is to drive motor, and 32.Y is to small synchronous pulley, and 33.Y is to framework, 34.Y is to large synchronous pulley, and 35.Y is to Timing Belt, and 36.Y is to leading screw, 37.Y is to electric machine support, and 38.Y is to leading screw bearing, and 39.Y is to bearing seat, 310.Y is to screw, 311.Y is to nut seat, and 313.Y is to seat supports bearing seat, the outside revolving bed of 314.Y, the inside revolving bed of 315.Y, 316. anti-drop blocks;
41.Z to drive motor, 42.Z is to reductor, 43.Z is to reductor support, and 44.Z is to fixed disc, 45. expansion sleeves, and 46. miniature gearss, 47. bull gears, 48.Z is to framework, 49. arc-shaped guide rails, 410. slide blocks.
The specific embodiment
Below in conjunction with accompanying drawing, the accuracy controlling device for the adjustment of wing wallboard attitude described in the utility model is described in further detail.A kind of accuracy controlling device of adjusting for wing wallboard attitude, comprise the conformal framework 11 being cascading, X-direction framework 23, Y-direction framework 33, Z-direction framework 48 and Z-direction fixed disc 44, conformal framework 11 is fixedly connected with X-direction framework 23, conformal framework 11 is provided with the wallboard locating cover 14 for wing wallboard location, the described accuracy controlling device for the adjustment of wing wallboard attitude also comprises can make Z-direction framework 48 with the Z-direction driven unit of the first rotating shaft rotation perpendicular to Z-direction fixed disc 44, can make Y-direction framework 33 to be parallel to the Y-direction driven unit and the X-direction driven unit that can make X-direction framework 23 rotate to be parallel to the 3rd rotating shaft of Y-direction framework 33 of the second rotating shaft rotation of Z-direction framework 48, this first rotating shaft, mutually vertical between this second rotating shaft and the 3rd rotating shaft, as Fig. 1, Fig. 2, Fig. 3, shown in Fig. 7 and Fig. 8.
Should by three wobble components, be formed for the accuracy controlling device of wing wallboard attitude adjustment, can carry out respectively rotating around rectangular space coordinate X, Y, tri-coordinate axlees of Z, i.e. this first rotating shaft, this second rotating shaft and the 3rd rotating shaft are equivalent to respectively tri-coordinate axlees of X, Y, Z in rectangular space coordinate, thereby carry out the attitude adjustment of X, Y, tri-directions of Z, X, Y, tri-directions of Z are respectively X, the Y in rectangular space coordinate, the direction of tri-coordinate axlees of Z.The assembling characteristics little according to wing equipment adjustment scope, accuracy requirement is high, this device is the rotation around X, Y, tri-axles of Z by three layers of framework (being respectively X-direction framework 23, Y-direction framework 33, Z-direction framework 48) implementation space, by activation point is applied to frame edge, can three be rotated accurately and be controlled, thereby realize attitude accuracy controlling, and this device end is provided with quick change conformal framework 11, by conformal framework 11, can realizes the attitude of different model wallboard and adjust.As shown in Figures 1 to 4, its working process is: the shape that realizes wallboard by conformal framework 11 keeps, by X-direction driven unit, realize wallboard around the rotation of X-axis, by Y-direction driven unit, realize wallboard around the rotation of Y-axis, by Z-direction driven unit, realize wallboard around the rotation of Z axis.
Concrete, X-direction driven unit comprises the X-direction leading screw bearing 28 that is arranged on X-direction framework 23 edges, be arranged on the X-direction screw 210 at Y-direction framework 33 edges, X-direction leading screw 26 through X-direction leading screw bearing 28 and X-direction screw 210, X-direction leading screw 26 is fixedly connected with the inner ring of X-direction leading screw bearing 28, screw thread fit between X-direction leading screw 26 and X-direction screw 210, X-direction framework 23 is rotationally connected with Y-direction framework 33, rotating shaft between X-direction framework 23 and Y-direction framework 33 is the 3rd rotating shaft, when X-direction leading screw 26 rotates, distance between X-direction leading screw bearing 28 and X-direction screw 210 can increase or reduce, thereby make X-direction framework 23 can take the 3rd rotating shaft as axle rotation.
The outer X-direction bearing seat 29 that is provided with of X-direction leading screw bearing 28, X-direction bearing seat 29 is rotationally connected with the X-direction seat supports bearing seat 213 being arranged on X-direction framework 23, the outer X-direction nut seat 211 that is provided with of X-direction screw 210, X-direction nut seat 211 is rotationally connected with the X-direction seat supports bearing seat 213 being arranged on Y-direction framework 33, as shown in Figure 5, when X-direction leading screw 26 rotates, distance between X-direction leading screw bearing 28 and X-direction screw 210 can increase or reduce, X-direction bearing seat 29 can rotate with respect to X-direction seat supports bearing seat 213, X-direction nut seat 211 can rotate with respect to X-direction seat supports bearing seat 213, thereby make X-direction bearing seat 29 remain parallel with X-direction nut seat 211.Between X-direction bearing seat 29 and X-direction seat supports bearing seat 213, by bearing, connect, between X-direction nut seat 211 and X-direction seat supports bearing seat 213, by bearing, connect.
One end of X-direction leading screw 26 is connected with the first actuating device for driving X-direction leading screw 26 to rotate, the other end of X-direction leading screw 26 is connected with anti-drop block 216, the two ends of X-direction framework 23 are respectively equipped with the outer revolving bed 214 of X-direction, the two ends of Y-direction framework 33 are respectively equipped with revolving bed 215 in X-direction, the outer revolving bed 214 of the X-direction at X-direction framework 23 two ends respectively with the X-direction at Y-direction framework 33 two ends in revolving bed 215 be rotationally connected, the rotating shaft in the outer revolving bed 214 of X-direction and X-direction between revolving bed 215 is the 3rd rotating shaft.
This first actuating device comprises the X-direction drive motor 21 that can drive X-direction leading screw 26 to rotate, and X-direction drive motor 21 is fixedly connected with X-direction bearing seat 29 by X-direction electric machine support 27.It between X-direction leading screw 26 and X-direction drive motor 21, is band transmission.In order to make driving band keep tensioned state, between X-direction electric machine support 27 and X-direction bearing seat 29, be bolted, X-direction electric machine support 27 is provided with long strip type hole, bolt is connected and fixed X-direction electric machine support 27 and X-direction bearing seat 29 through the long strip type hole on X-direction electric machine support 27, distance between the motor shaft of drive motor 21 and X-direction leading screw 26 can regulate the position in long strip type hole by adjusting bolt, as shown in Figure 5.In like manner, Y-direction electric machine support 37 has also adopted identical design, so that driving band keeps tensioned state.
Being X-direction driven unit is comprised of revolving bed 215 in X-direction drive motor 21, X-direction small synchronous pulley 22, X-direction framework 23, the large synchronous pulley 24 of X-direction, X-direction Timing Belt 25, X-direction leading screw 26, X-direction electric machine support 27, X-direction leading screw bearing 28, X-direction bearing seat 29, X-direction screw 210, X-direction nut seat 211, X-direction seat supports bearing seat 213, the outer revolving bed 214 of X-direction, X-direction etc.Described X-direction drive motor 21 is arranged on X-direction seat supports bearing seat 213 by X-direction electric machine support 27, X-direction drive motor 21 output shafts are provided with X-direction small synchronous pulley 22 and link together by X-direction Timing Belt 25 and the large synchronous pulley 24 of X-direction being arranged on X-direction leading screw 26, X-direction screw 210 is installed on X-direction leading screw 26, on X-direction screw 210, be connected with X-direction nut seat 211, X-direction nut seat 211 and X-direction bearing seat 29 are respectively by X-direction seat supports bearing, X-direction seat supports bearing seat 213 is arranged on respectively on Y-direction framework 33 and X-direction framework 23, Y-direction framework 33 and X-direction framework 23 rotate by revolving bed in X-direction 215 and the outer revolving bed 214 of X-direction respectively.During this assembly work, by X-direction drive motor 21, drive X-direction small synchronous pulley 22 to rotate, by X-direction Timing Belt 25, drive the large synchronous pulley 24 of the X-direction being arranged on X-direction leading screw 26 to rotate, and then drive X-direction screw 210 along X-direction leading screw 26 axial-movements, drive A to drive Y-direction framework 33 and X-direction framework 23 through rotating by revolving bed 214 outside revolving bed in X-direction 215 and X-direction to nut seat 211 and X-direction bearing seat 29, realize the X-direction attitude adjustment of wing wallboard, as shown in Figures 1 to 5.
Y-direction driven unit comprise be arranged on Y-direction framework 33 edges Y-direction leading screw bearing 38, be arranged on the Y-direction screw 310 at Z-direction framework 48 edges, through the Y-direction leading screw 36 of Y-direction leading screw bearing 38 and Y-direction screw 310, Y-direction leading screw 36 is fixedly connected with the inner ring of Y-direction leading screw bearing 38, screw thread fit between Y-direction leading screw 36 and Y-direction screw 310, Y-direction framework 33 is rotationally connected with Z-direction framework 48, rotating shaft between Y-direction framework 33 and Z-direction framework 48 is this second rotating shaft, when Y-direction leading screw 36 rotates, Y-direction framework 33 can be take this second rotating shaft as axle rotation.
The outer Y-direction bearing seat 39 that is provided with of Y-direction leading screw bearing 38, Y-direction bearing seat 39 is rotationally connected with the Y-direction seat supports bearing seat 313 being arranged on Y-direction framework 33, the outer Y-direction nut seat 311 that is provided with of Y-direction screw 310, Y-direction nut seat 311 is rotationally connected with the Y-direction seat supports bearing seat 313 being arranged on Z-direction framework 48, as shown in Figure 6, when Y-direction leading screw 36 rotates, distance between Y-direction leading screw bearing 38 and Y-direction screw 310 can increase or reduce, Y-direction bearing seat 39 can rotate with respect to Y-direction seat supports bearing seat 313, Y-direction nut seat 311 can rotate with respect to Y-direction seat supports bearing seat 313, thereby make Y-direction bearing seat 39 remain parallel with Y-direction nut seat 311.Between Y-direction bearing seat 39 and Y-direction seat supports bearing seat 313, by bearing, connect, between Y-direction nut seat 311 and Y-direction seat supports bearing seat 313, by bearing, connect.
One end of Y-direction leading screw 36 is connected with the second actuating device for driving Y-direction leading screw 36 to rotate, the other end of Y-direction leading screw 36 is connected with anti-drop block 316, the two ends of Y-direction framework 33 are respectively equipped with the outer revolving bed 314 of Y-direction, the two ends of Z-direction framework 48 are respectively equipped with revolving bed 315 in Y-direction, the outer revolving bed 314 of the Y-direction at Y-direction framework 33 two ends respectively with the Y-direction at Z-direction framework 48 two ends in revolving bed 315 be rotationally connected, the rotating shaft in the outer revolving bed 314 of Y-direction and Y-direction between revolving bed 315 is this second rotating shaft.
Being Y-direction driven unit is comprised of revolving bed 315 in Y-direction drive motor 31, Y-direction small synchronous pulley 32, Y-direction framework 33, the large synchronous pulley 34 of Y-direction, Y-direction Timing Belt 35, Y-direction leading screw 36, Y-direction electric machine support 37, Y-direction leading screw bearing 38, Y-direction bearing seat 39, Y-direction screw 310, Y-direction nut seat 311, Y-direction seat supports bearing seat 313, the outer revolving bed 314 of Y-direction, Y-direction etc.Described Y-direction drive motor 31 is arranged on Y-direction seat supports bearing seat 313 by Y-direction electric machine support 37, Y-direction drive motor 31 output shafts are provided with Y-direction small synchronous pulley 32 and link together by Y-direction Timing Belt 35 and the large synchronous pulley 34 of Y-direction being arranged on Y-direction leading screw 36, Y-direction screw 310 is installed on Y-direction leading screw 36, on Y-direction screw 310, be connected with Y-direction nut seat 311, Y-direction nut seat 311 and Y-direction bearing seat 39 are respectively by Y-direction seat supports bearing, Y-direction seat supports bearing seat 313 is arranged on respectively on Z-direction framework 48 and Y-direction framework 33, Y-direction framework and Y-direction framework 33 rotate by revolving bed in Y-direction 315 and the outer revolving bed 314 of Y-direction respectively.During this assembly work, by Y-direction drive motor 31, drive Y-direction small synchronous pulley 32 to rotate, by Y-direction Timing Belt 35, drive the large synchronous pulley 34 of the Y-direction being arranged on Y-direction leading screw 36 to rotate, and then drive Y-direction screw 310 along Y-direction leading screw 36 axial-movements, drive B to drive Z-direction framework 48 and Y-direction framework 33 through rotating by revolving bed 314 outside revolving bed in Y-direction 315 and Y-direction to nut seat 311 and Y-direction bearing seat 39, realize the Y-direction attitude adjustment of wing wallboard, as shown in Figures 1 to 6.
Z-direction driven unit comprises bull gear 47 and the slide block 410 being fixedly connected with Z-direction framework 48, the axis of bull gear 47 is this first rotating shaft, Z-direction fixed disc 44 is provided with the 3rd driver train for driving bull gear 47 to rotate, on Z-direction fixed disc 44, be also provided with arc-shaped guide rail 49, slide block 410 is plugged in arc-shaped guide rail 49.
Be that Z-direction driven unit is comprised of Z-direction drive motor 41, Z-direction reductor 42, Z-direction reductor support 43, Z-direction fixed disc 44, expansion sleeve 45, miniature gears 46, bull gear 47, Z-direction framework 48, arc-shaped guide rail 49, slide block 410 etc., described Z-direction drive motor 41, Z-direction reductor 42 are arranged on Z-direction fixed disc 44 by Z-direction reductor support 43, miniature gears 46 is arranged on Z-direction reductor 42 axles by expansion sleeve 45, bull gear 47 and slide block 410 are arranged on Z-direction framework 48, and the arc-shaped guide rail 49 supporting with slide block 410 is arranged on Z-direction fixed disc 44.During this assembly work, Z-direction drive motor 41 drives miniature gears 46 to rotate by Z-direction reductor 42, by miniature gears 46 and bull gear 47 engagements that are arranged on Z-direction framework 48, drive Z-direction framework 48 to slide along the arc-shaped guide rail 49 on Z-direction reaction plate 44 by slide block 410, Z-direction framework 48 and Z-direction reaction plate 44 are produced relative rotation, realize the Z-direction attitude adjustment of wing wallboard.
On conformal framework 11, be also provided with for the fixing conformal sucker 12 of this wing wallboard, conformal sucker 12 is adjusted screw rod 13 by sucker and is connected with conformal framework 11.Be that conformal framework 11 is provided with conformal sucker 12, sucker is adjusted the compositions such as screw rod 13, wallboard locating cover 14, positioning pressuring plate 15.During this assembly work, first will between conformal framework 11 and X-direction framework 23 frames, complete location, and push down with positioning pressuring plate 15, again wing wallboard and conformal framework 11 are passed through to wallboard locating cover 14, complete the location of wallboard, by sucker adjusting lever 13, conformal sucker 12 is adjusted to correct position, holds wallboard, complete the conformal of wallboard.Wallboard locating cover 14 is connected with conformal framework 11 by radius stay, and the diameter of wallboard locating cover 14 towards one end of conformal framework 11 is less than the diameter of the other end, and to facilitate this wing wallboard of location, wallboard locating cover 14 is threaded connection with radius stay.
This beneficial effect for the accuracy controlling device of wing wallboard attitude adjustment is:
1, this device comprises shape-keeping frame, can realize the attitude of the wallboard of different model, different sizes adjust by different shape-keeping frames.
2, between shape-keeping frame and A frame, adopt " L " type locating surface increased pressure board location, dismounting is convenient rapidly;
3, activation point is applied to frame edge, has greatly improved the adjustment precision that attitude is adjusted, realized the accuracy controlling of attitude;
4, three layers of framework are realized three direction posture adjustments, compact conformation;
5, being provided with butt flange can be conveniently integrated with robot or other three degree of freedom mobile device.
The above; be only specific embodiment of the utility model, can not limit the scope that utility model is implemented with it, so the displacement of its equivalent assemblies; or the equivalent variations of doing according to the utility model scope of patent protection and modification, all should still belong to the category that this patent is contained.Between technical scheme and technical scheme, all can use by independent assortment in addition, between the technical characterictic and technical characterictic in the utility model, between technical characterictic and technical scheme.
Claims (10)
1. an accuracy controlling device of adjusting for wing wallboard attitude, it is characterized in that, the described accuracy controlling device for the adjustment of wing wallboard attitude comprises the conformal framework (11) being cascading, X-direction framework (23), Y-direction framework (33), Z-direction framework (48) and Z-direction fixed disc (44), conformal framework (11) is fixedly connected with X-direction framework (23), conformal framework (11) is provided with the wallboard locating cover (14) for wing wallboard location, the described accuracy controlling device for the adjustment of wing wallboard attitude also comprises can make Z-direction framework (48) with the Z-direction driven unit of the first rotating shaft rotation perpendicular to Z-direction fixed disc (44), can make Y-direction framework (33) to be parallel to the Y-direction driven unit and the X-direction driven unit that can make X-direction framework (23) rotate to be parallel to the 3rd rotating shaft of Y-direction framework (33) of the second rotating shaft rotation of Z-direction framework (48), this first rotating shaft, mutually vertical between this second rotating shaft and the 3rd rotating shaft.
2. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 1, it is characterized in that: X-direction driven unit comprises the X-direction leading screw bearing (28) that is arranged on X-direction framework (23) edge, be arranged on the X-direction screw (210) at Y-direction framework (33) edge, X-direction leading screw (26) through X-direction leading screw bearing (28) and X-direction screw (210), X-direction leading screw (26) is fixedly connected with the inner ring of X-direction leading screw bearing (28), screw thread fit between X-direction leading screw (26) and X-direction screw (210), X-direction framework (23) is rotationally connected with Y-direction framework (33), rotating shaft between X-direction framework (23) and Y-direction framework (33) is the 3rd rotating shaft, when X-direction leading screw (26) rotates, X-direction framework (23) can be take the 3rd rotating shaft as axle rotation.
3. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 2, it is characterized in that: the outer X-direction bearing seat (29) that is provided with of X-direction leading screw bearing (28), X-direction bearing seat (29) is rotationally connected with the X-direction seat supports bearing seat (213) being arranged on X-direction framework (23), the outer X-direction nut seat (211) that is provided with of X-direction screw (210), X-direction nut seat (211) is rotationally connected with the X-direction seat supports bearing seat (213) being arranged on Y-direction framework (33).
4. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 3, it is characterized in that: one end of X-direction leading screw (26) is connected with the first actuating device for driving X-direction leading screw (26) to rotate, and the other end of X-direction leading screw (26) is connected with anti-drop block (216).
5. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 4, it is characterized in that: this first actuating device comprises the X-direction drive motor (21) that can drive X-direction leading screw (26) to rotate, and X-direction drive motor (21) is fixedly connected with X-direction bearing seat (29) by X-direction electric machine support (27).
6. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 1, it is characterized in that: Y-direction driven unit comprises the Y-direction leading screw bearing (38) that is arranged on Y-direction framework (33) edge, be arranged on the Y-direction screw (310) at Z-direction framework (48) edge, Y-direction leading screw (36) through Y-direction leading screw bearing (38) and Y-direction screw (310), Y-direction leading screw (36) is fixedly connected with the inner ring of Y-direction leading screw bearing (38), screw thread fit between Y-direction leading screw (36) and Y-direction screw (310), Y-direction framework (33) is rotationally connected with Z-direction framework (48), rotating shaft between Y-direction framework (33) and Z-direction framework (48) is this second rotating shaft, when Y-direction leading screw (36) rotates, Y-direction framework (33) can be take this second rotating shaft as axle rotation.
7. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 6, it is characterized in that: the outer Y-direction bearing seat (39) that is provided with of Y-direction leading screw bearing (38), Y-direction bearing seat (39) is rotationally connected with the Y-direction seat supports bearing seat (313) being arranged on Y-direction framework (33), the outer Y-direction nut seat (311) that is provided with of Y-direction screw (310), Y-direction nut seat (311) is rotationally connected with the Y-direction seat supports bearing seat (313) being arranged on Z-direction framework (48).
8. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 7, it is characterized in that: one end of Y-direction leading screw (36) is connected with the second actuating device for driving Y-direction leading screw (36) to rotate, and the other end of Y-direction leading screw (36) is connected with anti-drop block (316).
9. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 1, it is characterized in that: Z-direction driven unit comprises bull gear (47) and the slide block (410) being fixedly connected with Z-direction framework (48), the axis of bull gear (47) is this first rotating shaft, Z-direction fixed disc (44) is provided with the 3rd driver train for driving bull gear (47) to rotate, on Z-direction fixed disc (44), be also provided with arc-shaped guide rail (49), slide block (410) is plugged in arc-shaped guide rail (49).
10. the accuracy controlling device of adjusting for wing wallboard attitude according to claim 1, it is characterized in that: on conformal framework (11), be also provided with for the fixing conformal sucker (12) of this wing wallboard, conformal sucker (12) is adjusted screw rod (13) by sucker and is connected with conformal framework (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420380798.2U CN203937867U (en) | 2014-07-10 | 2014-07-10 | A kind of accuracy controlling device of adjusting for wing wallboard attitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420380798.2U CN203937867U (en) | 2014-07-10 | 2014-07-10 | A kind of accuracy controlling device of adjusting for wing wallboard attitude |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203937867U true CN203937867U (en) | 2014-11-12 |
Family
ID=51857206
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420380798.2U Expired - Lifetime CN203937867U (en) | 2014-07-10 | 2014-07-10 | A kind of accuracy controlling device of adjusting for wing wallboard attitude |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203937867U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275504A (en) * | 2016-10-19 | 2017-01-04 | 中航飞机股份有限公司西安飞机分公司 | A kind of conformal structure for the involutory opening of aircraft wing body two layers |
| CN107128506A (en) * | 2017-03-28 | 2017-09-05 | 浙江大学 | A kind of adaptive support meanss for composite wing wallboard |
| CN107350785A (en) * | 2017-08-14 | 2017-11-17 | 上海卫星装备研究所 | A kind of High-precision multi-dimensional degree linkage structure assembling device and assembly method |
| CN109605300A (en) * | 2019-01-22 | 2019-04-12 | 芜湖中科飞机制造有限公司 | A kind of auxiliary assembling apparatus for aircraft wing assembly and maintenance |
| CN112173161A (en) * | 2020-09-21 | 2021-01-05 | 中航复合材料有限责任公司 | Auxiliary manufacturing device for composite material fuselage wallboard |
| CN112192464A (en) * | 2020-09-11 | 2021-01-08 | 黄永恒 | Shape-preserving positioning tool for composite material wing wallboard |
-
2014
- 2014-07-10 CN CN201420380798.2U patent/CN203937867U/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275504A (en) * | 2016-10-19 | 2017-01-04 | 中航飞机股份有限公司西安飞机分公司 | A kind of conformal structure for the involutory opening of aircraft wing body two layers |
| CN106275504B (en) * | 2016-10-19 | 2019-05-14 | 中航飞机股份有限公司西安飞机分公司 | It is a kind of to be open two layers of conformal structure for aircraft wing body pairing |
| CN107128506A (en) * | 2017-03-28 | 2017-09-05 | 浙江大学 | A kind of adaptive support meanss for composite wing wallboard |
| CN107128506B (en) * | 2017-03-28 | 2019-03-26 | 浙江大学 | A kind of adaptive support device for composite wing siding |
| CN107350785A (en) * | 2017-08-14 | 2017-11-17 | 上海卫星装备研究所 | A kind of High-precision multi-dimensional degree linkage structure assembling device and assembly method |
| CN107350785B (en) * | 2017-08-14 | 2019-09-17 | 上海卫星装备研究所 | A kind of High-precision multi-dimensional degree linkage structure assembly device and assembly method |
| CN109605300A (en) * | 2019-01-22 | 2019-04-12 | 芜湖中科飞机制造有限公司 | A kind of auxiliary assembling apparatus for aircraft wing assembly and maintenance |
| CN112192464A (en) * | 2020-09-11 | 2021-01-08 | 黄永恒 | Shape-preserving positioning tool for composite material wing wallboard |
| CN112173161A (en) * | 2020-09-21 | 2021-01-05 | 中航复合材料有限责任公司 | Auxiliary manufacturing device for composite material fuselage wallboard |
| CN112173161B (en) * | 2020-09-21 | 2023-05-30 | 中航复合材料有限责任公司 | Auxiliary manufacturing device for composite material fuselage wall plate |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN203937867U (en) | A kind of accuracy controlling device of adjusting for wing wallboard attitude | |
| CN203448979U (en) | Automatic gesture regulating and positioning device for assembling wing wall plate | |
| CN207682642U (en) | Prefabricated PC concrete components tear open, Bu Mo robots and production line | |
| CN111730273A (en) | Inner and outer fork assembly butt welding tool | |
| CN104589290B (en) | A kind of framework of power distribution cabinet assembly machine and assembly method | |
| CN212399311U (en) | Flexible assembly of aircraft wallboard and confined space system hole frock | |
| CN106741308A (en) | A kind of automobile door external formula positioning installation apparatus | |
| CN105014663A (en) | Base-loaded modular mechanical arm capable of realizing multi-directional connection | |
| CN203853243U (en) | Glue coating assembly fixture of passenger car windshield | |
| CN105690336A (en) | High-precision heavy-load horizontal rotary table | |
| CN106313097A (en) | Unit combined robot wrist | |
| CN204893261U (en) | Five welding manipulators | |
| CN202542387U (en) | Steering synchronization system of multi-wheel system mobile robot | |
| CN106915392A (en) | A kind of arrangements for automotive doors positioning installation apparatus | |
| CN107433432A (en) | The complete automatic assembling apparatus of bolt and nut | |
| CN207606760U (en) | A kind of tipper for heavy workpiece overturning | |
| CN206528546U (en) | Automobile door external formula positioning installation apparatus | |
| CN205651297U (en) | Horizontal revolving platform of high accuracy high capacity | |
| CN204161512U (en) | Passenger vehicle closing device | |
| CN109605300A (en) | A kind of auxiliary assembling apparatus for aircraft wing assembly and maintenance | |
| CN206203395U (en) | A kind of streamline product inverts placing device | |
| CN201483222U (en) | Subpackage tooling of instrument panel assembly | |
| CN206795167U (en) | A kind of auto parts and components fasten erecting device | |
| CN109204875A (en) | A kind of rotating device for helicopter fuselage assembly | |
| CN102774442A (en) | Caterpillar track running device used in constrained space |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 100024 North East military villa, eight Li bridge, Chaoyang District, Beijing Patentee after: AVIC BEIJING AERONAUTICAL MANUFACTURING TECHNOLOGY Research Institute Address before: 100024 North East military villa, eight Li bridge, Chaoyang District, Beijing Patentee before: BEIJING AERONAUTICAL MANUFACTURING TECHNOLOGY Research Institute |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20141112 |