CN104647090A - Self-adaption absorptive clamping device of airplane skin - Google Patents

Self-adaption absorptive clamping device of airplane skin Download PDF

Info

Publication number
CN104647090A
CN104647090A CN201410743421.3A CN201410743421A CN104647090A CN 104647090 A CN104647090 A CN 104647090A CN 201410743421 A CN201410743421 A CN 201410743421A CN 104647090 A CN104647090 A CN 104647090A
Authority
CN
China
Prior art keywords
framed bent
hole
covering
scale
self adaptation
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.)
Granted
Application number
CN201410743421.3A
Other languages
Chinese (zh)
Other versions
CN104647090B (en
Inventor
李迎光
郝小忠
陈耿祥
周鑫
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Nanjing University of Aeronautics and Astronautics
Original Assignee
Nanjing University of Aeronautics and Astronautics
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Nanjing University of Aeronautics and Astronautics filed Critical Nanjing University of Aeronautics and Astronautics
Priority to CN201410743421.3A priority Critical patent/CN104647090B/en
Publication of CN104647090A publication Critical patent/CN104647090A/en
Application granted granted Critical
Publication of CN104647090B publication Critical patent/CN104647090B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q3/00Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine
    • B23Q3/02Devices holding, supporting, or positioning work or tools, of a kind normally removable from the machine for mounting on a work-table, tool-slide, or analogous part
    • B23Q3/06Work-clamping means
    • B23Q3/08Work-clamping means other than mechanically-actuated
    • B23Q3/088Work-clamping means other than mechanically-actuated using vacuum means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23QDETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
    • B23Q2703/00Work clamping
    • B23Q2703/02Work clamping means
    • B23Q2703/10Devices for clamping workpieces of a particular form or made from a particular material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Hooks, Suction Cups, And Attachment By Adhesive Means (AREA)

Abstract

The invention discloses a self-adaption absorptive clamping device of an airplane skin. The clamping device is characterized by comprising a frame, bent frames and self-adaption absorptive columns, wherein the upper and lower beams of the frame are provided with racks, and the two ends of each bent frame are arranged on the racks and can move along the racks; each bent frame is internally provided with a linear guide rail in a vertical direction, and each group of bent frames is provided with a certain amount of self-adaption adsorption columns and can move along the linear guide rail respectively; each adsorption column comprises a rotary vacuum chuck, a self-adaption telescopic link and a scale column. According to the clamping provided by the invention, the layout of the bent frames and the self-adaption absorptive columns can be adjusted by aiming at the shape of the skin, the absorption height can be adjusted by the scale columns and the self-adaption telescopic links, and the skin can be absorbed by the vacuum suckers; furthermore, the clamping device is applicable to clamping the skins of various shapes and sizes, the comprehensive cost can be reduced, the frock preparation period and production period can be shortened, and the production efficiency can be improved.

Description

Aircraft skin self adaptation absorption clamping device
Technical field
The present invention relates to fixture, especially a kind of aircraft skin clamping device, specifically a kind of aircraft skin self adaptation absorption clamping device.
Background technology
Aircraft skin forms the appearance part of Aerodynamic Configuration of Aireraft, and its size is large, kind is many, complex-shaped various and batch is little, is the strength member ensureing aircraft aerodynamics performance.In aircraft manufacturing process, need to carry out various processing to covering, because the rigidity of covering is poor, thickness is less, adds and is easily out of shape man-hour, and existing covering processing adopts multi-point flexibly absorption mounting and clamping system usually.During covering forming, certain error can be produced, existing multi-point flexibly adsorbent equipment adopts motor or hydraulic pressure accurately to control absorption position usually, adsorption site location is carried out according to theoretical shape, the existence of form error makes true form and theoretical shape not be inconsistent, and cannot adsorb covering according to the hi-Fix of theoretical shape.
Summary of the invention
The present invention is directed to prior art and according to the problem of covering forming error self-adaptative adjustment absorption position, a kind of aircraft skin self adaptation absorption clamping device cannot be designed.
Technical scheme of the present invention is:
A kind of aircraft skin self adaptation absorption clamping device, is characterized in that the upper underbeam that it comprises framework A, framed bent B and self adaptation adsorption column C, framework A is equipped with tooth bar respectively; Framed bent B is between upper underbeam, and the two ends up and down of framed bent B are engaged with corresponding tooth bar respectively, and motor is equipped with respectively in the two ends up and down of framed bent B, and two motor in synchrony motions can make framed bent move along the tooth bar on framework A, and between framed bent B, cooperative motion is avoided interfering; The length direction of framed bent B is provided with ball-screw and upright guide rail, often organize on framed bent B and several self adaptation adsorption columns are housed, each self adaptation adsorption column can move up and down along upright guide rail under the driving of ball-screw; Self adaptation adsorption column C comprises can turn to vacuum cup, self-adapting stretching bar and scale post; Described turned to vacuum cup can unload and change covering locating piece into locate covering; Whole device can according to the layout of covering Adjusting Shape self adaptation adsorption column and absorption height.
Described framework A comprises: framework upper beam 1, frame supported post 2, chassis base 3, framework underbeam 4 and tooth bar 5, and framework upper beam 1 and framework underbeam 4 are that tooth bar 5 is all housed, and the gears meshing of tooth bar 5 and framed bent B end, framed bent B can move along tooth bar direction.
Described framed bent B comprises: framed bent shell 6, protective cover 7, framed bent bonnet 8, scale hole slot 9, upright guide rail 10, ball-screw 11, travel switch 12, travelling gear 13 and motor I 14, the travelling gear 13 that framed bent shell about 6 two ends are installed engages with the tooth bar 5 on the framework upper beam 1 of framework A and framework underbeam 4 respectively, and travelling gear 13 is driven by motor I 14; Protective cover 7 is equipped with on framed bent shell 6 width both sides respectively, prevents adding the chip produced man-hour and falls into framed bent internal damage internal structure; Scale hole slot 9 is positioned on framed bent bonnet 8, and framed bent bonnet 8 is arranged on framed bent shell 6 by screw; Upright guide rail 10 is housed in framed bent shell 6 inside and ball-screw 11 vertically moves to drive self adaptation adsorption column C; Framed bent shell 6 both sides are equipped with travel switch 12 respectively, and between framed bent B or when colliding between framed bent B and framework A, travel switch triggers and makes framed bent B stop X-direction motion or change the direction of motion.
Described self adaptation adsorption column C comprises: pressure sensor 15, vacuum cup 16 can be turned to, fixture 17, Vacuum connector 18, vacuumize pore 19, motor II 20, electric pushrod 21, guide rail sleeve 22, scale post 23, fixed base plate 24, set bolt 25, motor II I26, travel switch 27, scale hole 28, pressure column 29, piston boit 30, vacuum cavity 31, sealing ring 32, guide rod 33, stopper slot 34, limited block 35, locating hole 36, spring 37, eccentric cam 38, guide rod hole 39, first pressure air cavity 40, piston boit through hole 41, piston boit groove 42, guide rod boss 43 and the second pressure air cavity 44, pressure sensor 15 is fixed by screws in and can turns on vacuum cup 16, vacuum cup 16 lower end can be turned to have external screw thread, with between fixture 15 for being threaded, fixture 17, to connect with bolt between Vacuum connector 18 and piston boit 30, electric pushrod 21 lower end motor part is bolted on pressure column 29 both sides, is connected between upper end pusher section with fixture 17, it is inner that pressure column 29 is arranged on scale post 23, limited block 35 on pressure column can move forward and backward in the stopper slot 34 of scale post 23 inside, stopper slot 34 upper end closed, lower end is open, during installation, pressure column 29 loads from scale post 23 lower end, then installs fixed base plate 24 by screw, for limiting limited block 35 extreme lower position, fixed base plate 24 has circular hole, when limited block 35 is positioned at lower position, the extended fixed base plate 24 in pressure column 29 lower end, pressure column 29 lower end has at least two locating holes 36, and scale post 23 side has at least 3 equidistant scale holes 28, and the distance between scale hole 28 is equal with the distance between locating hole 36, and the stroke of piston boit 30 is greater than the distance between scale hole 28, each scale hole 28 indicates scale to scale post 23, suitable scale hole 28 can be selected according to adsorption site Z-direction absorption position, movement pressure post 29 position, selected scale hole 28 is connected by set bolt 25 with between locating hole 36, guide rod 33 upper end has guide rod hole 39, the output shaft of motor II 20 is equipped with eccentric cam 38, and the rotation of eccentric cam 38 in guide rod hole 39 can drive the lifting of guide rod 33, vacuum cup 16 can be turned to rotate according to skin shape any direction within 45 degree of scopes, there is guide rail sleeve 22 scale post 23 side, is arranged on upright guide rail 10, motor II I26 controls self adaptation adsorption column C motion in the Y direction by transmission mechanism and ball-screw 11, when colliding between self adaptation adsorption column C, travel switch 27 triggers and makes self adaptation adsorption column C stop Y-direction moving or change moving direction.
When vacuum cup 16 can be turned to not to be stressed, spring 37 is in compressive state, motor II 20 drives eccentric cam 38 that guide rod 33 is pushed into lower position, now, it is outside that guide rod boss 43 is in piston boit groove 42, first pressure air cavity 40 is connected with the second pressure air cavity 44, and piston rod 30 is in free state, is controlled to make piston rod 30 move to extreme higher position by electric pushrod 21, when mounting and clamping system installs covering, covering is pushed to self adaptation absorption clamping device, covering can turn to vacuum cup 16 to press backward according to own profile, covering applied pressure experienced by pressure sensor 15, when the pressure experienced is greater than setting threshold value, electric pushrod 21 controls to turn to vacuum cup 16 to move backward in real time, when covering is installed to correct position, the pressure that pressure sensor 15 is experienced is less than the threshold value of setting, electric pushrod 21 quits work, controlling motor II 20 drives eccentric cam 38 to rotate, guide rod 33 is made to move to high position, guide rod boss 43 and piston boit groove 42 are closely linked, make the gas before the first pressure air cavity 40 and the second pressure air cavity 44 isolated, the position of piston boit 30 is locked, now vacuumized by vacuum pumping hole 19, vacuum cup 16 pairs of coverings can be turned to carry out absorption clamping.
Described covering locating piece comprises: retaining thread hole 45, covering locating hole 46, covering locating piece is by being connected between retaining thread hole 45 and fixture 17, covering locating piece there is covering locating hole 46, can according to the position of covering installation site adjustment framed bent B and self adaptation adsorption column C, by pin, covering locating hole 46 is connected with the fabrication hole on covering, as machining benchmark point.
Beneficial effect of the present invention is:
1, the present invention can realize the self-adaptative adjustment of absorption position according to the exact shape of covering, and absorption success rate is high.
2, the present invention realizes coarse positioning by scale post, realizes fine positioning by pressure sensor, and reduce the requirement to parts precision, cost is low.
3, vacuum cup can be turned to change covering locating piece location covering into, improve positioning precision.
4, there is auto-lock function, good rigidly, highly versatile.
Accompanying drawing explanation
fig. 1 is covering self adaptation clamping device overall schematic of the present invention.
Fig. 2 is block schematic illustration of the present invention.
In figure: 1 is framework upper beam, 2 live for frame supported, and 3 is chassis base, and 4 is framework underbeam, and 5 is tooth bar.
Fig. 3 is the structural representation of framed bent of the present invention.
In figure: 6 is framed bent shell, 7 is protective cover, and 8 is framed bent bonnet, and 9 is scale hole slot, and 10 is upright guide rail, and 11 is ball-screw, and 12 is travel switch, and 13 is travelling gear, and 14 is motor I.
Fig. 4 is the appearance schematic diagram of self adaptation adsorption column of the present invention.
In figure: 15 is pressure sensor, and 16 for can turn to vacuum cup, 17 is fixture, and 18 is Vacuum connector, and 19 for vacuumizing pore, and 20 is motor 2, and 21 is electric pushrod, and 22 is guide rail sleeve, and 23 is scale post; 24 is fixed base plate, and 25 is set bolt, and 26 is motor II I, and 27 is travel switch, and 28 is scale hole, and 29 is pressure column.
Fig. 5 is the internal structure schematic diagram of self adaptation adsorption column of the present invention.
Figure comprises: 20 is motor II, and 30 is piston boit, and 31 is vacuum cavity, 32 is sealing ring, and 33 is guide rod, and 34 is stopper slot, 35 is limited block, and 36 is locating hole, and 37 is spring, 38 is eccentric cam, and 39 is guide rod hole, and 40 is the first pressure air cavity, 41 is piston boit through hole, 42 is piston boit groove, and 43 is guide rod boss, and 44 is the second pressure air cavity.
Fig. 6 is covering locating piece schematic diagram of the present invention
In figure: 45 is screw thread locating hole, and 46 is covering locating hole.
Fig. 7 is the structural representation of fixture 17 in Fig. 3.
Fig. 8 is the structural representation of piston boit 30 in Fig. 3.
Fig. 9 is the schematic diagram that can turn to vacuum cup 16 different rotation angle.
Figure 10 is the locating hole on pressure column and the hole on scale post and hole fixing, piston boit is positioned at minimum stroke position view.
Figure 11 is the locating hole on pressure column and the hole on scale post and hole fixing, piston boit is positioned at highest line journey position view.
Figure 12 is the locating hole on pressure column and the hole on scale post and hole fixing, piston boit is positioned at highest line journey position view.
Figure 13 is that guide rod is in high position piston boit locking state schematic diagram.
Figure 14 is that guide rod is in lower position piston boit and is in free state schematic diagram.
specific implementation method
Below in conjunction with drawings and Examples, the present invention is done to the explanation of a step, but the invention is not restricted to this embodiment.
A kind of covering self adaptation absorption clamping device, be applicable to the clamping of the various shape of aircraft, size covering, it comprises framework A, framed bent B and self adaptation adsorption column C.As shown in Figure 1, the upper underbeam of its middle frame is equipped with tooth bar respectively; Framed bent is between upper underbeam, all being engaged by respective teeth wheel and rack up and down of framed bent, the upper and lower two ends of framed bent are equipped with driven wheel respectively and are rotated thus drive framed bent on framework as the motor I of horizontal direction movement, two motor I are synchronized with the movement and framed bent can be made to move along the tooth bar on framework, and need cooperative motion to avoid interfering between framed bent; In framed bent, ball-screw and upright guide rail are vertically housed, often organize self adaptation adsorption column framed bent being equipped with some, each self adaptation adsorption column can move up and down along upright guide rail; Self adaptation adsorption column comprises can turn to vacuum cup, self-adapting stretching bar and scale post; Turned to vacuum cup on self adaptation adsorption column unloads and can change covering locating piece into locate covering.Whole device can according to the layout of covering Adjusting Shape self adaptation adsorption column and absorption height.Framework A comprises: framework upper beam 1, and frame supported lives 2, chassis base 3, framework underbeam 4, tooth bar 5, and as shown in Figure 2, on framework, underbeam is equipped with tooth bar 5 respectively, for installing framed bent B, framed bent B can be made to move along tooth bar direction.Framed bent B comprises: framed bent shell 6, protective cover 7, framed bent bonnet 8, scale hole slot 9, upright guide rail 10, ball-screw 11, travel switch 12, travelling gear 13, motor I 14, as shown in Figure 3.Framed bent shell about 6 two ends are arranged on (Fig. 2 enlarged drawing) on tooth bar corresponding to framework A 5 respectively by the gear of both sides; Protective cover 7 is equipped with on framed bent shell 6 width both sides respectively, prevents adding the chip produced man-hour and falls into framed bent internal damage internal structure; Framed bent bonnet 8 is arranged on framed bent shell 6 by screw; Upright guide rail 10 and ball-screw are equipped with in framed bent shell 6 inside, and self adaptation adsorption column C can be made vertically to move; Framed bent shell 6 both sides are equipped with travel switch 10 respectively, and between framed bent B or when colliding between framed bent B and framework A, travel switch 12 triggers and makes framed bent B stop X-direction motion or change the direction of motion.
As shown in Figure 4,5, it comprises described self adaptation adsorption column C: pressure sensor 15, can turn to vacuum cup 16, fixture 17, and Vacuum connector 18 vacuumizes pore 19, motor 220, electric pushrod 21, guide rail sleeve 22, scale post 23; Fixed base plate 24, set bolt 25, motor 326, travel switch 27, scale hole 28, pressure column 29, piston boit 30, vacuum cavity 31, sealing ring 32 guide rod 33, stopper slot 34, limited block 35, locating hole 36, spring 37, eccentric cam 38, guide rod hole 39, the first pressure air cavity 40, piston boit through hole 41, piston boit groove 42, guide rod boss 43, second pressure air cavity 44.Pressure sensor 15 is fixed by screws in and can turns on vacuum cup 16; Vacuum cup 16 lower end can be turned to have external screw thread, with between fixture 15 for being threaded; Fixture 17, to connect with bolt between Vacuum connector 18 and piston boit 30; Electric pushrod 21 lower end motor part is bolted on pressure column 29 both sides, is connected between upper end pusher section with fixture 17; It is inner that pressure column 29 is arranged on scale post 23, limited block 35 on pressure column 29 can move forward and backward in the stopper slot 34 of scale post 23 inside, stopper slot 34 upper end closed, lower end is open, during installation, pressure column 29 loads from scale post 23 lower end, then installs fixed base plate 24 by screw, for limiting limited block 35 extreme lower position; Fixed base plate 24 has circular hole, when limited block 35 is positioned at lower position, the extended fixed base plate 24 in pressure column 29 lower end; Pressure column 29 lower end has at least two locating holes 36, and scale post 23 side has at least 3 equidistant scale holes 28, and the distance between scale hole 28 is equal with the distance between locating hole 36, and the stroke of piston boit 30 is greater than the distance between scale hole 28; Each scale hole 28 indicates scale to scale post 23, suitable scale hole 28 can be selected according to adsorption site Z-direction absorption position, movement pressure post 29 position, selected scale hole 28 is connected by set bolt 25 with between locating hole 36; Guide rod upper end has guide rod hole 39, and axle is equipped with eccentric cam 38 to motor II 20, and the rotation of eccentric cam 38 in guide rod hole 39 can drive the lifting of guide rod 33; Vacuum cup 16 can be turned to can to rotate according to skin shape any direction within 45 degree of scopes; There is guide rail sleeve 22 scale post 23 side, is arranged on upright guide rail 10; Motor II I26 controls self adaptation adsorption column C motion in the Y direction by transmission mechanism and ball-screw 11; Self adaptation adsorption column C is equipped with travel switch 27, and when colliding between self adaptation adsorption column C, travel switch 27 triggers and makes self adaptation adsorption column C stop Y-direction moving or change moving direction.
The operation principle of described self adaptation adsorption column C is: when vacuum cup 16 can be turned to not to be stressed, spring 37 is in compressive state, motor 220 drives eccentric cam 38 that guide rod 33 is pushed into lower position, now, it is outside that guide rod boss 43 is in piston boit groove 42, first pressure air cavity 40 is connected with the second pressure air cavity 44, and piston rod 30 is in free state, is controlled to make piston rod 30 move to extreme higher position by electric pushrod 21, when mounting and clamping system installs covering, covering is pushed to self adaptation absorption clamping device, covering can turn to vacuum cup 16 to press backward according to own profile, covering applied pressure experienced by pressure sensor 15, when the pressure experienced is greater than setting threshold value, electric pushrod 21 controls to turn to vacuum cup 16 to move backward in real time, when covering is installed to correct position, the pressure that pressure sensor 15 is experienced is less than the threshold value of setting, electric pushrod 21 quits work, controlling motor 220 drives eccentric cam 38 to rotate, guide rod 33 is made to move to high position, guide rod boss 43 and piston boit groove 42 are closely linked, make the gas before the first pressure air cavity 40 and the second pressure air cavity 44 isolated, the position of piston boit 30 is locked, now vacuumized by vacuum pumping hole 19, vacuum cup 16 pairs of coverings can be turned to carry out absorption clamping.
As shown in Figure 6, it comprises described covering locating piece: retaining thread hole 45, covering locating hole (46).Covering locating piece is by being connected between retaining thread hole 45 and fixture 17, covering locating piece there is covering locating hole 46, can according to the position of covering installation site adjustment framed bent B and self adaptation adsorption column C, by screw, covering locating hole 46 is connected with the fabrication hole on covering, as machining benchmark point.
Using method of the present invention is as follows:
1, according to covering geomery, the selected framed bent of needs and the quantity of self adaptation adsorption column, calculate suitable adsorption site layout.
As shown in Figure 3, framed bent B comprises: framed bent shell 6, protective cover 7, framed bent bonnet 8, scale hole slot 9, upright guide rail 10, ball-screw 11, travel switch 12, travelling gear 13, motor I 14.Framed bent shell about 6 two ends are arranged on the tooth bar 5 of framework A respectively; Protective cover 7 is equipped with on framed bent shell 6 width both sides respectively, prevents adding the chip produced man-hour and falls into framed bent internal damage internal structure; Framed bent bonnet 8 is arranged on framed bent shell 6 by screw; Upright guide rail 10 and ball-screw are equipped with in framed bent shell 6 inside, and self adaptation adsorption column C can be made vertically to move; Framed bent shell 6 both sides are equipped with travel switch 12 respectively, and between framed bent B or when colliding between framed bent B and framework A, travel switch 12 triggers and makes framed bent B stop X-direction motion or change the direction of motion.
When covering is located jointly by auricle clamping and many framed bents vacuum suction, framed bent can affect the moving area of supporting device, therefore needs to carry out Region dividing in conjunction with covering actual size, and mirror image milling, by mobile framed bent absorption location, is carried out in each region.Process ensures the distance of shoring head and framed bent, collision free.In the vacuum framed bent moving process of area transformation, at least ensure that 2 framed bents are fixed, ensure the positioning precision of part on lathe, other framed bents carry out X to adjustment according to machining area, and therefore framed bent quantity must not be less than 3.
As shown in Figure 4, Figure 5, self adaptation adsorption column C comprises: pressure sensor 15, can turn to vacuum cup 16, fixture 17, and Vacuum connector 18 vacuumizes pore 19, motor II 20, electric pushrod 21, guide rail sleeve 22, scale post 23; Fixed base plate 24, set bolt 25, motor II I26, travel switch 27, scale hole 28, pressure column 29, piston boit 30, vacuum cavity 31, sealing ring 32 guide rod 33, stopper slot 34, limited block 35, locating hole 36, spring 37, eccentric cam 38, guide rod hole 39, the first pressure air cavity 40, piston boit through hole 41, piston boit groove 42, guide rod boss 43, second pressure air cavity 44.Pressure sensor 15 is fixed by screws in and can turns on vacuum cup 16; Vacuum cup 16 lower end can be turned to have external screw thread, with between fixture 15 for being threaded; As shown in Figure 7, Figure 8, fixture 17, connect with bolt between Vacuum connector 18 and piston boit 30; Electric pushrod 21 lower end motor part is bolted on pressure column 29 both sides, is connected between upper end pusher section with fixture 17; It is inner that pressure column 29 is arranged on scale post 23, limited block 35 on pressure column can move forward and backward in the stopper slot 34 of scale post 23 inside, stopper slot 34 upper end closed, lower end is open, during installation, pressure column 29 loads from scale post 23 lower end, then installs fixed base plate 24 by screw, for limiting limited block 35 extreme lower position; Fixed base plate 24 has circular hole, when limited block 35 is positioned at lower position, the extended fixed base plate 24 in pressure column 29 lower end; Guide rod upper end has guide rod hole 39, and axle is equipped with eccentric cam 38 to motor II 20, and the rotation of eccentric cam 38 in guide rod hole 39 can drive the lifting of guide rod 33; As shown in Figure 9, vacuum cup 16 can be turned to can to rotate according to skin shape any direction within 45 degree of scopes; There is guide rail sleeve 22 scale post 23 side, is arranged on upright guide rail 10; Motor II I26 controls self adaptation adsorption column C motion in the Y direction by transmission mechanism and ball-screw 11; Self adaptation adsorption column C is equipped with travel switch 27, and when colliding between self adaptation adsorption column C, travel switch triggers and makes self adaptation adsorption column C stop Y-direction moving or change moving direction.
2, design quantity and the position of covering anchor point, the rotatable vacuum cup of relevant position is unloaded and changes covering locating piece into, covering locating hole 46 and the fabrication hole on covering are connected by screw, to locate covering.
As shown in Figure 6, covering locating piece comprises: retaining thread hole 45, covering locating hole 46.Covering locating piece is by being connected between retaining thread hole 45 and fixture 17, covering locating piece there is covering locating hole 46, can according to the position of covering installation site adjustment framed bent B and self adaptation adsorption column C, by screw, covering locating hole 46 is connected, as anchor point with the fabrication hole on covering.
3, according to covering theoretical shape, coarse positioning is carried out to each adsorption column Z-direction position.
As shown in Figure 4, Figure 5, pressure column 29 lower end of self adaptation adsorption column C has at least two locating holes 36, scale post 23 side has at least 3 equidistant scale holes 28, distance between scale hole 28 is equal with the distance between locating hole 36, and the stroke of piston boit 30 is greater than the distance between scale hole 28; Each scale hole 28 indicates scale to scale post 23.
First the Z-direction position of each adsorption site is calculated according to the theoretical shapometer of covering, corresponding scale hole 28 can be drawn, secondly all self adaptation adsorption columns are moved to scale hole slot 9 position, by scale hole slot 9, selected scale hole 28 is connected by set bolt 25 with between locating hole 36, finally more each adsorption column is moved to the placement position calculated.Be the locating hole 36 on pressure column 29 and the hole on scale post 23 as shown in figure 11 and hole fixing, be the locating hole 36 on pressure column 29 and the hole on scale post 23 as shown in figure 12 and hole fixing, namely by selected different scale hole 28, coarse positioning is carried out to the absorption position of each adsorption site.
4, on coarse positioning basis according to covering exact shape self-adaptative adjustment absorption position, realize accurately location absorption covering.
As shown in figure 14, when vacuum cup 16 can be turned to not to be stressed, spring 37 is in compressive state, motor II 20 drives eccentric cam 38 that guide rod 33 is pushed into lower position, now, it is outside that guide rod boss 43 is in piston boit groove 42, and the first pressure air cavity 40 is connected with the second pressure air cavity 44, piston rod 30 is in free state, is controlled to make piston rod 30 move to highest line journey position as shown in Figure 10 as shown in figure 11 by low travel position by electric pushrod 21, when mounting and clamping system installs covering, covering is pushed to self adaptation absorption clamping device, covering can turn to vacuum cup 16 to press backward according to own profile, covering applied pressure experienced by pressure sensor 15, when the pressure experienced is greater than setting threshold value, electric pushrod 21 controls to turn to vacuum cup 16 to move backward in real time, when covering is installed to correct position, the pressure that pressure sensor 15 is experienced is less than the threshold value of setting, electric pushrod 21 quits work, controlling motor II 20 drives eccentric cam 38 to rotate, guide rod 33 is made to move to high position, guide rod boss 43 and piston boit groove 42 are closely linked, make the gas before the first pressure air cavity 40 and the second pressure air cavity 44 isolated, the position of piston boit 30 is locked, as shown in figure 13, now vacuumized by vacuum pumping hole 19, vacuum cup 16 pairs of coverings can be turned to carry out absorption clamping.
5, after machining, stop vacuumizing, control motor 220 and drive eccentric cam 38 rotation to make guide rod 33 move to lower position, make piston boit 30 be in free state, as shown in figure 14.
Using method of the present invention can be summarized as:
Step one: according to covering shape and size, the quantity of design covering anchor point and position, unload the rotatable vacuum cup of relevant position and change covering locating piece into.
Step 2: according to skin shape, design adsorption site position and quantity, calculate the X-direction position of each framed bent, self adaptation adsorption column position in the Y direction, and the Z-direction absorption position of each adsorption site.
Step 3: select corresponding scale hole to carry out coarse positioning according to the Z-direction absorption position of each adsorption site, self adaptation adsorption column is moved to the position of scale hole slot, selected scale hole is connected by set bolt with between locating hole.
Step 4: control the position that each framed bent and self adaptation adsorption column move to setting, install covering, the real-time control piston post of electric pushrod moves backward.
Step 5: when covering is mounted to desired location, by the piston boit of the locked each self adaptation adsorption column of Electric Machine Control, vacuumizes and makes to turn to vacuum cup to hold aircraft skin.
Step 6: after machining, stops vacuumizing, unloads covering, then unclamps the piston boit of each self adaptation adsorption column by Electric Machine Control.
The part that the present invention does not relate to prior art that maybe can adopt same as the prior art is realized.

Claims (6)

1. an aircraft skin self adaptation absorption clamping device, it is characterized in that it comprises framework (A), framed bent (B) and self adaptation adsorption column (C), the upper underbeam of framework (A) is equipped with tooth bar respectively; Framed bent (B) is between upper underbeam, the two ends up and down of framed bent (B) are engaged with corresponding tooth bar respectively, motor is equipped with respectively in the two ends up and down of framed bent (B), and two motor in synchrony motions can make framed bent move along the tooth bar on framework (A), and between framed bent (B), cooperative motion is avoided interfering; The length direction of framed bent (B) is provided with ball-screw and upright guide rail, and often organize on framed bent (B) and several self adaptation adsorption columns are housed, each self adaptation adsorption column can move up and down along upright guide rail under the driving of ball-screw; Self adaptation adsorption column (C) comprises can turn to vacuum cup, self-adapting stretching bar and scale post; Described turned to vacuum cup can unload and change covering locating piece into locate covering; Whole device can according to the layout of covering Adjusting Shape self adaptation adsorption column and absorption height.
2. device according to claim 1, it is characterized in that described framework (A) comprising: framework upper beam (1), frame supported post (2), chassis base (3), framework underbeam (4) and tooth bar (5), framework upper beam (1) and framework underbeam (4) are that tooth bar (5) is all housed, and the gears meshing of tooth bar (5) and framed bent (B) end, framed bent (B) can move along tooth bar direction.
3. device according to claim 1, it is characterized in that described framed bent (B) comprising: framed bent shell (6), protective cover (7), framed bent bonnet (8), scale hole slot (9), upright guide rail (10), ball-screw (11), travel switch (12), travelling gear (13) and motor I (14), framed bent shell (6) the up and down travelling gear (13) installed of two ends engages with the tooth bar (5) on the framework upper beam (1) of framework (A) and framework underbeam (4) respectively, and travelling gear (13) is driven by motor I (14); Protective cover (7) is equipped with on framed bent shell (6) width both sides respectively, prevents adding the chip produced man-hour and falls into framed bent internal damage internal structure; Scale hole slot (9) is positioned on framed bent bonnet (8), and framed bent bonnet (8) is arranged on framed bent shell (6) by screw; Upright guide rail (10) is housed in framed bent shell (6) inside and ball-screw (11) vertically moves to drive self adaptation adsorption column (C); Framed bent shell (6) both sides are equipped with travel switch (12) respectively, and between framed bent (B) or when colliding between framed bent (B) and framework (A), travel switch triggers and makes framed bent (B) stop X-direction moving or change the direction of motion.
4. device according to claim 1, it is characterized in that described self adaptation adsorption column (C) comprising: pressure sensor (15), vacuum cup (16) can be turned to, fixture (17), Vacuum connector (18), vacuumize pore (19), motor II (20), electric pushrod (21), guide rail sleeve (22), scale post (23), fixed base plate (24), set bolt (25), motor II I(26), travel switch (27), scale hole (28), pressure column (29), piston boit (30), vacuum cavity (31), sealing ring (32), guide rod (33), stopper slot (34), limited block (35), locating hole (36), spring (37), eccentric cam (38), guide rod hole (39), first pressure air cavity (40), piston boit through hole (41), piston boit groove (42), guide rod boss (43) and the second pressure air cavity (44), pressure sensor (15) is fixed by screws in and can turns on vacuum cup (16), vacuum cup (16) lower end can be turned to have external screw thread, with between fixture (15) for being threaded, fixture (17), to connect with bolt between Vacuum connector (18) and piston boit (30), electric pushrod (21) lower end motor part is bolted on pressure column (29) both sides, is connected between upper end pusher section with fixture (17), it is inner that pressure column (29) is arranged on scale post (23), limited block (35) on pressure column can be movable in the stopper slot (34) that scale post (23) is inner, stopper slot (34) upper end closed, lower end is open, during installation, pressure column (29) loads from scale post (23) lower end, then installs fixed base plate (24) by screw, for limiting limited block (35) extreme lower position, (24) have circular hole to fixed base plate, when limited block (35) is positioned at lower position, and the extended fixed base plate in pressure column (29) lower end (24), pressure column (29) lower end has at least two locating holes (36), scale post (23) side has at least 3 equidistant scale holes (28), distance between scale hole (28) is equal with the distance between locating hole (36), and the stroke of piston boit (30) is greater than the distance between scale hole (28), the upper each scale hole (28) of scale post (23) indicates scale, suitable scale hole (28) can be selected according to adsorption site Z-direction absorption position, movement pressure post (29) position, is connected selected scale hole (28) by set bolt (25) with between locating hole (36), guide rod (33) upper end has guide rod hole (39), the output shaft of motor II (20) is equipped with eccentric cam (38), and the rotation of eccentric cam (38) in guide rod hole (39) can drive the lifting of guide rod (33), vacuum cup (16) can be turned to rotate according to skin shape any direction within 45 degree of scopes, there is guide rail sleeve (22) scale post (23) side, is arranged on upright guide rail (10), motor II I(26) control self adaptation adsorption column (C) motion in the Y direction by transmission mechanism and ball-screw (11), when colliding between self adaptation adsorption column (C), travel switch (27) triggers and makes self adaptation adsorption column (C) stop Y-direction moving or change moving direction.
5. device according to claim 1, when it is characterized in that turning to vacuum cup (16) not to be stressed, spring (37) is in compressive state, motor II (20) drives eccentric cam (38) that guide rod (33) is pushed into lower position, now, it is outside that guide rod boss (43) is in piston boit groove (42), first pressure air cavity (40) is connected with the second pressure air cavity (44), piston rod (30) is in free state, is controlled to make piston rod (30) move to extreme higher position by electric pushrod (21), when mounting and clamping system installs covering, covering is pushed to self adaptation absorption clamping device, covering can turn to vacuum cup (16) to press backward according to own profile, covering applied pressure experienced by pressure sensor (15), when the pressure experienced is greater than setting threshold value, electric pushrod (21) controls to turn to vacuum cup (16) to move backward in real time, when covering is installed to correct position, the pressure that pressure sensor (15) is experienced is less than the threshold value of setting, electric pushrod (21) quits work, controlling motor II (20) drives eccentric cam (38) to rotate, guide rod (33) is made to move to high position, guide rod boss (43) and piston boit groove (42) are closely linked, make the gas before the first pressure air cavity (40) and the second pressure air cavity (44) isolated, the position of piston boit (30) is locked, now vacuumized by vacuum pumping hole (19), vacuum cup (16) can be turned to carry out absorption clamping to covering.
6. device according to claim 1, it is characterized in that described covering locating piece comprises: retaining thread hole (45), covering locating hole (46), covering locating piece is by being connected between retaining thread hole (45) and fixture (17), covering locating piece there is covering locating hole (46), the position of framed bent (B) and self adaptation adsorption column (C) can be adjusted according to covering installation site, covering locating hole (46) is connected, as machining benchmark point with the fabrication hole on covering by pin.
CN201410743421.3A 2014-12-08 2014-12-08 Aircraft skin self adaptation absorption clamping device Active CN104647090B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201410743421.3A CN104647090B (en) 2014-12-08 2014-12-08 Aircraft skin self adaptation absorption clamping device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201410743421.3A CN104647090B (en) 2014-12-08 2014-12-08 Aircraft skin self adaptation absorption clamping device

Publications (2)

Publication Number Publication Date
CN104647090A true CN104647090A (en) 2015-05-27
CN104647090B CN104647090B (en) 2016-09-14

Family

ID=53239001

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201410743421.3A Active CN104647090B (en) 2014-12-08 2014-12-08 Aircraft skin self adaptation absorption clamping device

Country Status (1)

Country Link
CN (1) CN104647090B (en)

Cited By (35)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105058109A (en) * 2015-07-17 2015-11-18 大连四达高技术发展有限公司 Flexible tool unit and flexible lattice tool system
CN105382741A (en) * 2015-12-31 2016-03-09 上海理工大学 Air pressure flexible clamping device of frame-shaped parts with thin walls, and clamping method of air pressure flexible clamping device
CN105522420A (en) * 2016-01-21 2016-04-27 南京理工大学 Flexible clamp suitable for positioning and clamping complex curved surfaces of parts
CN105690298A (en) * 2016-03-31 2016-06-22 苏州市合叶精密机械有限公司 Clamp
CN106808384A (en) * 2015-11-27 2017-06-09 成都飞机工业(集团)有限责任公司 A kind of large-scale band toothed edge covering positioner and its localization method
CN106944848A (en) * 2017-04-18 2017-07-14 天津大学 A kind of pneumatic variation rigidity mirror image milling flexible supporting device of the real-time thickness measuring of integrated form
CN107214550A (en) * 2017-06-12 2017-09-29 芜湖天航科技(集团)股份有限公司 Plate cutting method
CN107263137A (en) * 2017-06-20 2017-10-20 合肥太通制冷科技有限公司 A kind of machining center Autonomous test fixture
CN107817434A (en) * 2017-11-20 2018-03-20 上海御渡半导体科技有限公司 A kind of application method of suction jig frock for test circuit plate
CN108188779A (en) * 2018-01-05 2018-06-22 清华大学深圳研究生院 A kind of chucking appliance system for being suitable for large-scale siding class thin-wall part
CN108214002A (en) * 2017-12-29 2018-06-29 清华大学深圳研究生院 A kind of weak rigid machining distortion for aeronautical monolithic component control method
CN109626194A (en) * 2018-11-23 2019-04-16 南昌航空大学 A kind of flexible active hanging apparatus of the big covering of aircraft and its hanging method
CN109764848A (en) * 2019-01-31 2019-05-17 西北工业大学 A kind of flexible frock towards skin-covering face scanning
CN109848892A (en) * 2019-01-23 2019-06-07 南昌航空大学 A kind of fixture unit and operating method clamping thin-walled parts
CN110039345A (en) * 2019-05-16 2019-07-23 沈阳飞机工业(集团)有限公司 A kind of flexible fixture platform for planer-type Five Axis metal plate CNC milling machine milling
CN110255348A (en) * 2019-07-03 2019-09-20 南京航空航天大学 A kind of demoulding lifting device dedicated for aircraft skin
WO2019184559A1 (en) * 2018-03-29 2019-10-03 广州瑞松北斗汽车装备有限公司 Adaptive adhesion system for rolling and over-edging system
CN110508852A (en) * 2019-09-24 2019-11-29 太原理工大学 A kind of processing of structural member, assembly and detection Trinity hole location determine method
CN110561475A (en) * 2018-06-05 2019-12-13 C.R.F.阿西安尼顾问公司 suction type clamping device
CN110877221A (en) * 2019-12-04 2020-03-13 北京神工科技有限公司 Stringer skin tool structure
CN110900481A (en) * 2019-11-06 2020-03-24 浙江大学 Flexible array aircraft skin adsorbs frock
CN110937133A (en) * 2019-11-11 2020-03-31 浙江大学 Vacuum adsorption electric control telescopic device with pressure monitoring function
CN111545907A (en) * 2020-05-13 2020-08-18 南京航空航天大学 Flexible multi-point adsorption device and method for double-laser-beam bilateral synchronous welding of T-shaped wallboard structure
CN112045750A (en) * 2020-08-25 2020-12-08 湖南亚太实业有限公司 Plastic uptake mechanical cutting fixing device
CN112197719A (en) * 2020-09-27 2021-01-08 南京航空航天大学 Deformation data monitoring method and device suitable for single-side contact clamping
CN113146507A (en) * 2021-04-16 2021-07-23 彩虹(合肥)液晶玻璃有限公司 Static electricity eliminating device for processing glass substrate
CN114043284A (en) * 2021-11-25 2022-02-15 成都飞机工业(集团)有限责任公司 Vacuum clamping device
CN114228071A (en) * 2022-02-28 2022-03-25 烟台精锐模具有限公司 Nondestructive demoulding device for injection mould
CN114620481A (en) * 2022-04-21 2022-06-14 安徽巨一科技股份有限公司 Multi-vehicle-type flexible stepless self-adaptive switching and carrying device and control method thereof
CN115556025A (en) * 2022-12-05 2023-01-03 成都市鸿侠科技有限责任公司 Skin infiltration of self-adaptation camber detects bracket
CN115958318A (en) * 2023-01-20 2023-04-14 中航西安飞机工业集团股份有限公司 Aircraft skin chemical milling machine tool fixing device
CN116237795A (en) * 2023-01-05 2023-06-09 意特利(滁州)智能数控科技有限公司 Vacuum adsorption table top
CN116619090A (en) * 2023-07-25 2023-08-22 云科智能制造(沈阳)有限公司 Horizontal machining center convenient to clamping work piece
CN116673849A (en) * 2023-07-31 2023-09-01 大儒科技(苏州)有限公司 Flexible intelligent polishing device for machining
CN117300214A (en) * 2023-11-28 2023-12-29 成都弘林机械有限公司 Panel processing drilling machine convenient to it is fixed

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020152598A1 (en) * 2000-09-18 2002-10-24 Branko Sarh Cacuum clamp device to vacuum clamp device
EP1563958A1 (en) * 2004-02-10 2005-08-17 AIRBUS France Method and device for holding a thin and flexible pannel with a plurality of vacuum cups
CN101269466A (en) * 2008-04-11 2008-09-24 清华大学 Roboticized intelligent fixture system
CN102554662A (en) * 2011-12-22 2012-07-11 上海三一精机有限公司 Self-centering and work piece clamping device for working table and control method of self-centering and work piece clamping device
CN102554595A (en) * 2012-01-13 2012-07-11 清华大学 Skin manufacturing assembly system for airplane

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20020152598A1 (en) * 2000-09-18 2002-10-24 Branko Sarh Cacuum clamp device to vacuum clamp device
EP1563958A1 (en) * 2004-02-10 2005-08-17 AIRBUS France Method and device for holding a thin and flexible pannel with a plurality of vacuum cups
CN101269466A (en) * 2008-04-11 2008-09-24 清华大学 Roboticized intelligent fixture system
CN102554662A (en) * 2011-12-22 2012-07-11 上海三一精机有限公司 Self-centering and work piece clamping device for working table and control method of self-centering and work piece clamping device
CN102554595A (en) * 2012-01-13 2012-07-11 清华大学 Skin manufacturing assembly system for airplane

Cited By (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105058109A (en) * 2015-07-17 2015-11-18 大连四达高技术发展有限公司 Flexible tool unit and flexible lattice tool system
CN106808384A (en) * 2015-11-27 2017-06-09 成都飞机工业(集团)有限责任公司 A kind of large-scale band toothed edge covering positioner and its localization method
CN105382741A (en) * 2015-12-31 2016-03-09 上海理工大学 Air pressure flexible clamping device of frame-shaped parts with thin walls, and clamping method of air pressure flexible clamping device
CN105382741B (en) * 2015-12-31 2017-04-26 上海理工大学 Air pressure flexible clamping device of frame-shaped parts with thin walls, and clamping method of air pressure flexible clamping device
CN105522420A (en) * 2016-01-21 2016-04-27 南京理工大学 Flexible clamp suitable for positioning and clamping complex curved surfaces of parts
CN105690298A (en) * 2016-03-31 2016-06-22 苏州市合叶精密机械有限公司 Clamp
CN106944848B (en) * 2017-04-18 2019-01-22 天津大学 A kind of pneumatic variation rigidity mirror image milling flexible supporting device of the real-time thickness measuring of integrated form
CN106944848A (en) * 2017-04-18 2017-07-14 天津大学 A kind of pneumatic variation rigidity mirror image milling flexible supporting device of the real-time thickness measuring of integrated form
CN107214550A (en) * 2017-06-12 2017-09-29 芜湖天航科技(集团)股份有限公司 Plate cutting method
CN107263137A (en) * 2017-06-20 2017-10-20 合肥太通制冷科技有限公司 A kind of machining center Autonomous test fixture
CN107817434A (en) * 2017-11-20 2018-03-20 上海御渡半导体科技有限公司 A kind of application method of suction jig frock for test circuit plate
CN108214002A (en) * 2017-12-29 2018-06-29 清华大学深圳研究生院 A kind of weak rigid machining distortion for aeronautical monolithic component control method
CN108188779A (en) * 2018-01-05 2018-06-22 清华大学深圳研究生院 A kind of chucking appliance system for being suitable for large-scale siding class thin-wall part
WO2019184559A1 (en) * 2018-03-29 2019-10-03 广州瑞松北斗汽车装备有限公司 Adaptive adhesion system for rolling and over-edging system
CN110561475A (en) * 2018-06-05 2019-12-13 C.R.F.阿西安尼顾问公司 suction type clamping device
CN109626194A (en) * 2018-11-23 2019-04-16 南昌航空大学 A kind of flexible active hanging apparatus of the big covering of aircraft and its hanging method
CN109848892A (en) * 2019-01-23 2019-06-07 南昌航空大学 A kind of fixture unit and operating method clamping thin-walled parts
CN109764848A (en) * 2019-01-31 2019-05-17 西北工业大学 A kind of flexible frock towards skin-covering face scanning
CN110039345A (en) * 2019-05-16 2019-07-23 沈阳飞机工业(集团)有限公司 A kind of flexible fixture platform for planer-type Five Axis metal plate CNC milling machine milling
CN110039345B (en) * 2019-05-16 2024-01-23 沈阳飞机工业(集团)有限公司 Flexible clamp platform for milling of gantry type five-coordinate metal plate numerical control milling machine
CN110255348A (en) * 2019-07-03 2019-09-20 南京航空航天大学 A kind of demoulding lifting device dedicated for aircraft skin
CN110255348B (en) * 2019-07-03 2020-10-13 南京航空航天大学 Demoulding lifting device special for aircraft skin
CN110508852A (en) * 2019-09-24 2019-11-29 太原理工大学 A kind of processing of structural member, assembly and detection Trinity hole location determine method
CN110900481A (en) * 2019-11-06 2020-03-24 浙江大学 Flexible array aircraft skin adsorbs frock
CN110937133A (en) * 2019-11-11 2020-03-31 浙江大学 Vacuum adsorption electric control telescopic device with pressure monitoring function
CN110937133B (en) * 2019-11-11 2021-09-21 浙江大学 Vacuum adsorption electric control telescopic device with pressure monitoring function
CN110877221A (en) * 2019-12-04 2020-03-13 北京神工科技有限公司 Stringer skin tool structure
CN110877221B (en) * 2019-12-04 2021-11-09 北京神工科技有限公司 Stringer skin tool structure
CN111545907A (en) * 2020-05-13 2020-08-18 南京航空航天大学 Flexible multi-point adsorption device and method for double-laser-beam bilateral synchronous welding of T-shaped wallboard structure
CN112045750A (en) * 2020-08-25 2020-12-08 湖南亚太实业有限公司 Plastic uptake mechanical cutting fixing device
CN112197719A (en) * 2020-09-27 2021-01-08 南京航空航天大学 Deformation data monitoring method and device suitable for single-side contact clamping
CN112197719B (en) * 2020-09-27 2021-09-21 南京航空航天大学 Deformation data monitoring method and device suitable for single-side contact clamping
CN113146507A (en) * 2021-04-16 2021-07-23 彩虹(合肥)液晶玻璃有限公司 Static electricity eliminating device for processing glass substrate
CN114043284A (en) * 2021-11-25 2022-02-15 成都飞机工业(集团)有限责任公司 Vacuum clamping device
CN114228071A (en) * 2022-02-28 2022-03-25 烟台精锐模具有限公司 Nondestructive demoulding device for injection mould
CN114228071B (en) * 2022-02-28 2022-07-05 烟台精锐模具有限公司 Nondestructive demoulding device for injection mould
CN114620481A (en) * 2022-04-21 2022-06-14 安徽巨一科技股份有限公司 Multi-vehicle-type flexible stepless self-adaptive switching and carrying device and control method thereof
CN115556025A (en) * 2022-12-05 2023-01-03 成都市鸿侠科技有限责任公司 Skin infiltration of self-adaptation camber detects bracket
CN116237795A (en) * 2023-01-05 2023-06-09 意特利(滁州)智能数控科技有限公司 Vacuum adsorption table top
CN116237795B (en) * 2023-01-05 2023-09-12 意特利(滁州)智能数控科技有限公司 Vacuum adsorption table top
CN115958318A (en) * 2023-01-20 2023-04-14 中航西安飞机工业集团股份有限公司 Aircraft skin chemical milling machine tool fixing device
CN116619090A (en) * 2023-07-25 2023-08-22 云科智能制造(沈阳)有限公司 Horizontal machining center convenient to clamping work piece
CN116619090B (en) * 2023-07-25 2023-09-19 云科智能制造(沈阳)有限公司 Horizontal machining center convenient to clamping work piece
CN116673849A (en) * 2023-07-31 2023-09-01 大儒科技(苏州)有限公司 Flexible intelligent polishing device for machining
CN116673849B (en) * 2023-07-31 2023-10-10 大儒科技(苏州)有限公司 Flexible intelligent polishing device for machining
CN117300214A (en) * 2023-11-28 2023-12-29 成都弘林机械有限公司 Panel processing drilling machine convenient to it is fixed
CN117300214B (en) * 2023-11-28 2024-02-06 成都弘林机械有限公司 Panel processing drilling machine convenient to it is fixed

Also Published As

Publication number Publication date
CN104647090B (en) 2016-09-14

Similar Documents

Publication Publication Date Title
CN104647090A (en) Self-adaption absorptive clamping device of airplane skin
WO2021238980A1 (en) Flexible multi-point site multi-degree-of-freedom suction position tool
CN102009340B (en) Aircraft engine mounting vehicle
CN105436882B (en) Front-end module general assembly auxiliary mould
CN103862309B (en) A kind of for machining support milling face with the fixture of boring
CN101745905B (en) Multi-degree of freedom adjustable assembling platform used for butt joint of aircraft wings
CN205148435U (en) Cantilever type case and bag bead cutter that punches
CN203765385U (en) Double-station computer numerical control machining center
CN202393563U (en) Lamination and air-tightness detection device for front fog lamp of automobile
CN103921116A (en) Flexible assembly system for aircraft panel
CN103009073A (en) Automatic intermittent cycle worktable
CN103495767A (en) Piano mark back plate machining machine
CN107052736A (en) Self-adapting flexible dress calibration system based on mechanism
CN107984203B (en) With collaboration posture adjustment, collision prevention and the Automated assembly equipment for tightening function
CN206445797U (en) A kind of large-scale horizontal manipulator out of shape
CN204171763U (en) A kind of machining center cutter-exchange mechanism
CN108526252B (en) Integrated mechanical shaping equipment
CN204221369U (en) The two main shaft turning-milling complex processing lathe of aeroplane engine casing processing
CN109822673A (en) A kind of moulding integrated equipment of stamping die
CN103028952B (en) The working slider of automatic intermittent circulating work platform moves stopping means
CN109759764A (en) A kind of two-way movable clamp plate of automobile welding robot
CN206280877U (en) The adjusting part and illumination and/or signal indicating device of light source
CN108788831A (en) A kind of double limit detent mechanisms
CN104723134B (en) A kind of vertical supporting device using servo electric jar to drive
CN204727779U (en) A kind of locating device being applicable to the upper ledge mechanism of hollow glass pressing machine

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant