CN202037356U - Automatic curved surface drilling tail end actuator - Google Patents

Automatic curved surface drilling tail end actuator Download PDF

Info

Publication number
CN202037356U
CN202037356U CN201020666020XU CN201020666020U CN202037356U CN 202037356 U CN202037356 U CN 202037356U CN 201020666020X U CN201020666020X U CN 201020666020XU CN 201020666020 U CN201020666020 U CN 201020666020U CN 202037356 U CN202037356 U CN 202037356U
Authority
CN
China
Prior art keywords
drilling
unit
ring
axis
bolster
Prior art date
Application number
CN201020666020XU
Other languages
Chinese (zh)
Inventor
王兴松
张来喜
Original Assignee
东南大学
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 东南大学 filed Critical 东南大学
Priority to CN201020666020XU priority Critical patent/CN202037356U/en
Application granted granted Critical
Publication of CN202037356U publication Critical patent/CN202037356U/en

Links

Abstract

The utility model discloses an automatic curved surface drilling tail end actuator, which comprises a drilling unit, a pressing unit, a normal measurement unit, a positioning ring, a two-dimensional normal regulation unit and an outer support ring, wherein the drilling unit and the pressing unit are fixed on the positioning ring, the normal measurement unit is fixed on the pressing unit, a pressing head is connected onto the pressing unit through a spherical joint, the inner side of the pressing head is fixed with a measuring plate, the measuring plate can rotate along the pressing head, four displacement sensors are fixed at four corners of the pressing unit, four corners of the measuring plate are respectively in contact with the four displacement sensors, and the displacement sensors respectively measure the displacement of the four corners of the measuring plate, so the normal direction of the curved surface at the drilling coordinate part is calculated. The pressing unit is driven by a servo motor and a ball screw rod, the pressing force can be controlled through controlling the torque of the servo motor, and the positioning ring is fixed on the two-dimensional normal regulation unit and can respectively rotate around the X axis and the Y axis for completing the normal regulation. The tail end actuator in the structure can perfectly complete the curved surface drilling processing.

Description

The automatic drilling end effector of a kind of curved surface
Technical field
The utility model belongs to the automated manufacturing field, specifically, relates to the automatic drilling end effector of a kind of curved surface, is particularly useful for the automatic drilling of plane airfoil.
Background technology
The main method of attachment of aircraft structure employing at present is still mechanical connection, nearly 150~2,000,000 connectors on the large aircraft.In the various safety failures of aircraft, the number of faults of body injury has accounted for more than 30% of total failare quantity, therefore, depends mainly on the life-span of body the entire life of aircraft.Fatigue rupture is the basic reason of airframe disablement, and wherein 75%~80% fatigue rupture occurs in the connection hole of housing construction.In order to satisfy the requirement that modern large aircraft long-life, high reliability, low cost and high efficiency are made, can improve the state of the art (surface quality, fiting property, version etc.) of each tie point by various technological approaches, a large amount of long-life interconnection techniques that adopt, realize the assembling of aircaft configuration high-quality and high efficiency, one of them very important approach be to carry out automatic accurate drilling by automation equipment, improve the drilling quality.
Modern large aircraft profile, complex structure, number of spare parts many (surplus reaching 300 ten thousand), the inner space compactness, the rapport complexity, assembling and the active channel of installing are poor, and wherein aircraft assembles the amount of labour and accounts for more than 50% of the whole aircraft manufacturing amount of labour.Therefore, aircraft assembling be a technical difficulty big, relate to the many comprehensive integrated technologies of ambit, determined final mass, manufacturing cost and the cycle of aircraft to a great extent, be tap, key and the core technology of whole aircraft manufacturing process.
By means of high rigidity and structural design in advance, and advanced automatic control technology, conventional automated manufacturing technology can be controlled at mismachining tolerance within the small scope, therefore makes accurately to make or be assembled into for may.In the aircraft assembling, traditional way is to come the required lathe of customized user according to the specific matching requirements of aircraft mechanism.The structure of aircraft is generally all huger, the result of high accuracy assembling often assembly equipment maximization, high rigidity, expensive, the equipment purposes is too single-minded, and needs supporting fixed frame or automatic carriage, its investment also is huge.Along with the increase of aircraft components size, the automation of this form has been subjected to very big restriction in the middle of being assemblied in practice, in a way, because the cost of traditional automation assembling is too expensive, is obliged to retreat and adopts hand assembled.The problem of hand assembled is, along with the increase of aircraft components size, the cost of assembling also increases thereupon, and the mistake of hand assembled often causes producing high maintenance cost simultaneously, the scrapping and the delay of assembly period of parts.
Existing industrial machinery arm mainly is towards automobile, household electrical appliances, and industries such as pottery, working space is less relatively, and load capacity is lower.If exploitation on a large scale, the industrial machinery arm of heavy load, be difficult to solve the contradiction of high accuracy and big working space again.Light automation equipment provides another kind of selection for the aircraft flexible assembly.It has been sacrificed overall precision and has pursued local accuracy, and has made full use of aircraft components own characteristic and light weight on the parts aspect, more economical, can be assigned to operation field or attach on the aircraft components, do not need big fabricating yard, and the cost of equipment become cheap many.The robot hole fabrication techniques is the important application and the research direction of aircraft flexible assembly technology, because can longitudinally growing distance, automatic drilling system of robot moves, can finish the various piece of aircraft is bored riveting processing and be need not travelling workpiece, compare with traditional automatic drill riveting processing mode, improve machining accuracy and efficient greatly, therefore obtained extensive studies and application abroad.But because existing robot rigidity and precision is low, load is little makes traditional robot low in the application level of aircraft fit on.
In sum, research and development have traditional drilling robot light, reach the low advantage of cost flexibly, and have high stiffness, than heavy load holding capacity and high accuracy, the flexible curved surface drilling robot that satisfies the requirement of aircraft automation assembling is the important application and the research direction of aircraft flexible assembly technology, and multi-functional drilling end effector is one of key technology.
The utility model content
The purpose of this utility model provides can measure institute's drilling coordinate points surface normal direction, adjusts the drilling main shaft to normal orientation, and by compressing unit drilling place is implemented the automatic drilling end effector of curved surface that compresses.
The automatic drilling end effector of the utility model curved surface comprises that drilling unit 1, compressing unit 2, normal direction measuring unit 3, centring ring 4, two dimensional method are to adjustment unit 5, outer bracing ring 6; Drilling unit 1 and compressing unit 2 are fixed on the centring ring 4; Two dimensional method to adjustment unit 5 and drive its around Y-axis rotate be arranged on outside Y-axis rotational power mechanism 58 on the bracing ring 6 link to each other; It links to each other centring ring 4 and drive around the two dimensional method X-axis rotational power mechanism 54 on adjustment unit 5 that is arranged on that X-axis is rotated; Compressing unit 2 comprise the bracing frame 21 that compresses actuating unit 25, move at the drive lower edge z axle that compresses actuating unit 25, with the hold-down head 23 that bracing frame 21 is connected by ball-joint, having on the hold-down head 23 can be by the through hole 26 of drilling main shaft; The drilling main axle unit 12 that drilling unit 1 comprises the drilling actuating unit, moves at the drive lower edge of drilling actuating unit z axle; The drilling main axle unit comprises rotary drilling main shaft, and the drilling main shaft is coaxial with the ball-joint on the bracing frame 21; Normal direction measuring unit 3 comprises the drafting board 31 that is fixed on hold-down head 23 back sides, four displacement transducers 32 that are used to detect drafting board 31 displacements, and displacement transducer 32 is arranged on the bracing frame 21 and is distributed on the circumferencial direction of drilling main shaft.
The beneficial effects of the utility model: during its work, compressing engine drives bracing frame and hold-down head and moves along the z axle and move down, because hold-down head is arranged on the bracing frame and can rotates relative to bracing frame by ball-joint, so hold-down head can be pressed on the periphery that needs drilling place.And drafting board 31 is fixed on the hold-down head, moves with hold-down head, can pass through the displacement difference of the drafting board 31 of displacement transducer 32 detections like this, calculates the normal vector that curved surface is pointed out in drilling.Four displacement transducers 32 can be measured the drilling main shaft more accurately whether in normal orientation, are particularly useful for the curved surface of more complicated.At this moment driving centring ring 4 by X-axis rotational power mechanism 54 rotates around X-axis or/and rotate around Y-axis to adjustment unit 5 by Y-axis rotational power mechanism 58 drive two dimensional methods, can adjust centring ring 4 positions, be fixed on the centring ring 4 drilling unit 1 and compressing unit 2 (in the adjustment process thereby adjust, the gripper shoe action, hold-down head is motionless) attitude, make the moving of drafting board 31 that displacement transducer 32 detects equate, reach the drilling main shaft and be positioned at purpose on the normal direction.Then, drilling main axle unit 12 axially down moves at the drive lower edge of drilling actuating unit z, the drilling main shaft pass hold-down head through hole 26 and in needs drilling place drilling.Therefore, effect of the present utility model is: it can measure institute's drilling coordinate points surface normal direction, adjusts the drilling main shaft to normal orientation, and by compressing unit drilling place is implemented to compress.
The automatic drilling end effector of above-mentioned curved surface, drilling actuating unit are the drilling servomotor that is fixed on the drilling base plate 11; The drilling servomotor drives the drilling main axle unit 12 that is slidingly arranged on the drilling base plate 11 by ball-screw.
The automatic drilling end effector of above-mentioned curved surface, drilling main axle unit 12 is electric main shaft.The electricity main shaft belongs to prior art, no longer describes.
The automatic drilling end effector of above-mentioned curved surface compresses actuating unit 25 for being fixed on the servomotor that compresses that compresses on the base plate 24; Compress servomotor and be slidingly arranged in the bracing frame 21 that compresses on the base plate 24 by the ball-screw drive.Like this, can provide thrust by compressing servomotor, and by moment of torsion control control thrust.
The automatic drilling end effector of above-mentioned curved surface, two dimensional method to adjustment unit 5 be one be positioned at outside the bracing ring 51 of bracing ring 6, interior bracing ring 51 links to each other with the bolster Y that is parallel to Y-axis, bolster Y links to each other with Y-axis rotational power mechanism 58; In the bracing ring 51, centring ring 4 linked to each other with the bolster X that is parallel to X-axis in centring ring 4 was arranged on, and bolster X links to each other with X-axis rotational power mechanism 54.Employing is vertically arranged two turning cylinders (being bolster X and bolster Y) in same plane, can realize the adjustment of normal direction attitude quickly and accurately, and simple and compact for structure.
Description of drawings
Fig. 1 is a general three structural representation of the present utility model.
Fig. 2 is a drilling unit three-dimensional structural representation of the present utility model.
Fig. 3 is compressing unit of the present utility model and normal direction measuring unit three-dimensional structure schematic diagram.
Fig. 4 is the three-dimensional structure schematic diagram of two dimensional method of the present utility model to adjustment unit, outer bracing ring etc.
Fig. 5 is the hold-down head schematic diagram in the compressing unit of the present utility model.
Fig. 6 is the bracing frame schematic diagram in the compressing unit of the present utility model.
Fig. 7 is the structural representation of drilling of the present utility model unit, compressing unit, normal direction measuring unit etc.
Fig. 8 is connection diagrams such as hold-down head of the present utility model, bracing frame, retainer plate.
Among the figure,
1, drilling unit, 2, compressing unit, 3, the normal direction measuring unit, 4, centring ring, 5, two dimensional method is to adjustment unit, 6, outer bracing ring (bracing ring Y);
11, drilling base plate, 12, high-speed electric main shaft (drilling main axle unit), 13, drilling servomotor and reductor;
21, bracing frame, 22, retainer plate, 23, hold-down head, 24, compress base plate, 25, compress servomotor and reductor (compressing actuating unit), 26, through hole, 231, spherical extrinsic articulation, 211, spherical intrinsic articulation;
31, drafting board, 32, displacement transducer, 33, holder;
51, bracing ring X (interior bracing ring), 52, bolster XA, 53, bolster XB, 54, servomotor and reductor X (X-axis rotational power mechanism), 56, bolster YA, 57, bolster YB, 58, servomotor and reductor Y (Y-axis rotational power mechanism).
The specific embodiment
Describe the technical solution of the utility model in detail below in conjunction with accompanying drawing.
Shown in Fig. 1,7, the automatic drilling end effector of curved surface of the present utility model comprises that drilling unit 1, compressing unit 2, normal direction measuring unit 3, centring ring 4, two dimensional method are to adjustment unit 5, outer bracing ring 6.
Referring to Fig. 3, compressing unit 2 comprises being fixed on and compresses compressing servomotor and reductor 25, be slidingly arranged in the bracing frame 21 that compresses on the base plate 24, hold-down head 23 etc. by line slide rail along the z axle on the base plate 24.Compress servomotor and reductor 25 links to each other with ball-screw by shaft coupling, ball-screw links to each other with bracing frame 21 again.Compress servomotor and reductor 25 actions, can drive bracing frame 21 and move along the z axle.The outer surface of hold-down head 23 has spherical extrinsic articulation 231, has on the bracing frame 21 and spherical extrinsic articulation 231 corresponding spherical intrinsic articulations 211.Spherical extrinsic articulation 231 has been formed ball-joint with corresponding spherical intrinsic articulation 211.Hold-down head 23 is by on ball-joint connection and the bracing frame 21, and having on the hold-down head 23 can be by the through hole 26 of drilling main shaft.Retainer plate 22 is fixed on and prevents on the bracing frame 21 that hold-down head 23 from coming off.
Referring to Fig. 2, drilling unit 1 comprises the drilling servomotor that is fixed on the drilling base plate 11 and reductor 13, is slidingly arranged in high-speed electric main shaft 12 on the drilling base plate 11 etc. by line slide rail along the z axle.Drilling servomotor and reductor 13 link to each other with ball-screw by shaft coupling, and ball-screw links to each other with high-speed electric main shaft 12 again.Drilling servomotor and reductor 13 actions can drive high-speed electric main shaft 12 and move along the z axle.High-speed electric main shaft 12 comprises rotary drilling main shaft.The drilling main shaft is coaxial with the spherical intrinsic articulation 211 on the bracing frame 21.
Referring to Fig. 3, normal direction measuring unit 3 comprises the drafting board 31 that is fixed on hold-down head 23 back sides (inboard), four displacement transducers 32 that are used to detect drafting board 31 displacements, and displacement transducer 32 is arranged on the bracing frame 21 and is distributed on the circumferencial direction of drilling main shaft.
Referring to Fig. 4, two dimensional method to adjustment unit 5 be one be positioned at outside the bracing ring 51 of bracing ring 6, interior bracing ring 51 relative two sides link to each other with outer bracing ring 6 by the bolster YA56 parallel with Y-axis, bolster YB57 respectively, and bolster YA and bolster YB have formed bolster Y jointly; Bolster YB links to each other with servomotor and reductor Y (Y-axis rotational power mechanism) 58 on being fixed on outer bracing ring 6.Servomotor and reductor Y operation, bracing ring 51 and bolster YA and bolster YB rotate around Y-axis in driving.
In the bracing ring 51, centring ring 4 linked to each other with the bolster X that is parallel to X-axis in centring ring 4 was arranged on, and bolster X links to each other with X-axis rotational power mechanism 54.Two other opposite flank of interior bracing ring 51 links to each other with centring ring 4 by the bolster XA52 parallel with X-axis, bolster XB53 respectively, and bolster XA and bolster XB have formed bolster X jointly; Bolster XB be fixed in servomotor and reductor X (X-axis rotational power mechanism) 54 on the bracing ring 51 link to each other.Servomotor and reductor X operation drive centring ring 4 and bolster XA and bolster XB and rotate around X-axis.
Drilling unit 1 is 90 ° with compressing unit 2 and is separately fixed on two adjacent sides of centring ring 4 inside.
As shown in Figure 2, drilling unit 1 is fixed on centring ring 4 inside by drilling base plate 11, be used for given coordinate position drilling on curved surface, high-speed electric main shaft 12 is driven by drilling servomotor and reductor 13, be connected on the drilling base plate 11 by line slide rail, drilling servomotor and reductor 13 use shaft coupling to connect with ball-screw, Motor torque are converted into power, for high-speed electric main shaft 12 provides centripetal force.
As Fig. 3, Fig. 5 and shown in Figure 6, compressing unit 2 is fixed on centring ring 4 inside by compressing base plate 24, and bracing frame 21 is connected by line slide rail and compresses on the base plate 24.Compress servomotor and reductor 25 and use shaft coupling to connect, Motor torque is converted into power, for compressing unit 2 provides thrust with ball-screw.The spherical extrinsic articulation 231 of hold-down head 23 and the spherical intrinsic articulation of bracing frame 21 211 are bound up by spherical joint, and hold-down head 23 can rotate arbitrarily angled in bracing frame, and the assurance hold-down head closely contacts the drilling position.Compress the output torque of servomotor and reductor 25 by control, and consider that the Sliding mode variable structure control technology is for hold-down head provides accurately thrust because the loss of machine of torque that factors such as friction cause adopts the impedance Control technology.
Normal direction measuring unit 3 comprises drafting board 31, four displacement sensings 32, four holders 33, drafting board 31 is fixed on the inboard of hold-down head 23, change angle with hold-down head, it is parallel that drafting board plane and hold-down head end face 232 remain, and the normal orientation of drafting board has been represented the normal orientation of drilling coordinate points curved surface, four displacement transducers 32 be distributed on high-speed electric main shaft 12 around and be fixed on the bracing frame 21 by holder 33.Each displacement transducer 32 is under the effect of spring, and its end is against drafting board 31 surfaces, fully contacts with drafting board 31.
As shown in Figure 4, two dimensional method comprises bracing ring X (interior bracing ring) 51, bolster XA52, bolster XB53, servomotor and reductor X54, bolster YA56, bolster YB57, servomotor and reductor Y58 etc. to adjustment unit.Bracing ring X is bound up on the bracing ring Y (outer bracing ring) by bolster YA and bolster YB, provides power by servomotor and reductor Y, can rotate around Y-axis.Centring ring 4 is bound up on the bracing ring X by bolster XA and bolster XB, provides power by servomotor and reductor X, can rotate around X-axis.
Compared with prior art, the automatic drilling end effector of curved surface of the present utility model can be realized express method to measurement, and express method is to adjustment, and thrust is accurately controlled, and whole apparatus structure is simply compact.In the technical program, the normal direction measuring unit adopts four displacement transducers, can calculate four planes at tested curved surface, thereby can more accurately determine drilling coordinate points surface normal direction, can adapt to the normal direction drilling of more complicated curved surface simultaneously; Compressing unit adopts the mode of control servomotor moment of torsion to control thrust, need not to adopt separately the force sensor measuring thrust, and the employing impedance Control has taken into full account the frictional resistance between each component, directly provides desired thrust by the control of servomotor moment of torsion.The utility model is simple in structure, and thrust control is more accurate; Two dimensional method adopts vertically arranged two turning cylinders in same plane to adjustment unit, can realize the adjustment of normal direction attitude quickly and accurately, and simple and compact for structure.
Generally speaking, the utility model discloses the automatic drilling end effector of a kind of curved surface, comprise that drilling unit, compressing unit, normal direction measuring unit, centring ring, two dimensional method are to adjustment unit, outer bracing ring.Drilling unit and compressing unit are fixed on the centring ring; The normal direction measuring unit is fixed on the compressing unit, on compressing unit, be linked with hold-down head by spherical joint, a drafting board is fixed in the hold-down head inboard, drafting board can rotate with hold-down head, four displacement transducers of Corner Strapped at compressing unit, drafting board contacts with four displacement transducers respectively for four jiaos, and displacement transducer is measured drafting board four angular displacements respectively, thereby calculates drilling coordinate place normal to a surface direction.Compressing unit is driven by servomotor and ball-screw, and the moment of torsion of control servomotor can be controlled thrust; Centring ring is fixed on two dimensional method on adjustment unit, can rotate around X-axis and Y-axis respectively, thereby Completion Techniques is to adjustment.This structure can be measured institute's drilling coordinate points surface normal direction automatically, adjusts the drilling main shaft automatically to normal orientation, and compressing unit is implemented to compress automatically, and controlled system thrust, can finely finish curved surface drilling processing.

Claims (3)

1. the automatic drilling end effector of curved surface is characterized in that, it comprises that drilling unit (1), compressing unit (2), normal direction measuring unit (3), centring ring (4), two dimensional method are to adjustment unit (5), outer bracing ring (6);
Drilling unit (1) and compressing unit (2) are fixed on the centring ring (4);
Two dimensional method to adjustment unit (5) and drive its around Y-axis rotate be arranged on outside Y-axis rotational power mechanism (58) on the bracing ring (6) link to each other;
It links to each other centring ring (4) and drive around the two dimensional method X-axis rotational power mechanism (54) on adjustment unit (5) that is arranged on that X-axis is rotated;
Compressing unit (2) comprise the bracing frame (21) that compresses actuating unit (25), move at the drive lower edge z axle that compresses actuating unit (25), with the hold-down head (23) that bracing frame (21) is connected by ball-joint, having on the hold-down head (23) can be by the through hole (26) of drilling main shaft;
The drilling main axle unit (12) that drilling unit (1) comprises the drilling actuating unit, moves at the drive lower edge of drilling actuating unit z axle; The drilling main axle unit comprises rotary drilling main shaft, and the drilling main shaft is coaxial with the ball-joint on the bracing frame (21);
Normal direction measuring unit (3) comprises the drafting board (31) that is fixed on hold-down head (23) back side, four displacement transducers (32) that are used to detect drafting board (31) displacement, and displacement transducer (32) is arranged on bracing frame (21) and goes up and be distributed on the circumferencial direction of drilling main shaft.
2. the automatic drilling end effector of curved surface as claimed in claim 1, it is characterized in that, two dimensional method to adjustment unit (5) be one be positioned at outside the bracing ring (51) of bracing ring (6), interior bracing ring (51) links to each other with the bolster Y that is parallel to Y-axis, and bolster Y links to each other with Y-axis rotational power mechanism (58).
3. the automatic drilling end effector of curved surface as claimed in claim 2 is characterized in that, centring ring (4) is arranged in the interior bracing ring (51), and centring ring (4) links to each other with the bolster X that is parallel to X-axis, and bolster X links to each other with X-axis rotational power mechanism (54).
CN201020666020XU 2010-12-17 2010-12-17 Automatic curved surface drilling tail end actuator CN202037356U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201020666020XU CN202037356U (en) 2010-12-17 2010-12-17 Automatic curved surface drilling tail end actuator

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201020666020XU CN202037356U (en) 2010-12-17 2010-12-17 Automatic curved surface drilling tail end actuator

Publications (1)

Publication Number Publication Date
CN202037356U true CN202037356U (en) 2011-11-16

Family

ID=44964821

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201020666020XU CN202037356U (en) 2010-12-17 2010-12-17 Automatic curved surface drilling tail end actuator

Country Status (1)

Country Link
CN (1) CN202037356U (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102091799A (en) * 2010-12-17 2011-06-15 东南大学 End effector for automatically drilling curved surface
CN103639471A (en) * 2013-12-05 2014-03-19 郑州大学 Drilling end actuator for robot
CN108015312A (en) * 2017-10-27 2018-05-11 上海拓璞数控科技股份有限公司 For robot high accuracy drilling and the end effector and measuring method of counter boring
CN110216505A (en) * 2018-03-01 2019-09-10 中国商用飞机有限责任公司 Pressing force closed-loop control system and method for automatic punching equipment

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102091799A (en) * 2010-12-17 2011-06-15 东南大学 End effector for automatically drilling curved surface
CN103639471A (en) * 2013-12-05 2014-03-19 郑州大学 Drilling end actuator for robot
CN103639471B (en) * 2013-12-05 2016-01-20 郑州大学 Robot hole end effector
CN108015312A (en) * 2017-10-27 2018-05-11 上海拓璞数控科技股份有限公司 For robot high accuracy drilling and the end effector and measuring method of counter boring
CN110216505A (en) * 2018-03-01 2019-09-10 中国商用飞机有限责任公司 Pressing force closed-loop control system and method for automatic punching equipment

Similar Documents

Publication Publication Date Title
CN104589334B (en) A kind of five shaft multifunctional machinery handss
CN104698968B (en) Multi-functional automatic Drilling/Riveting end effector and automatic Drilling/Riveting method
CN102990458B (en) Three-dimensional automatic feeding, discharging and detecting device
CN102794491B (en) Device and method of automatic helical milling of hole
CN102699377B (en) A kind of lean auto-feed of replacing is bored
CN103722549B (en) Spatial cooperation heavy-loaded precision dual-arm robot
CN103990829B (en) A kind of aircraft assembles end effector and its using method of drilling
CN103056658B (en) A kind of aggregation type lathe
CN204975930U (en) A many function executing ware for airplane assembling
CN203679343U (en) Tail end hole forming actuator of robot
CN200980019Y (en) An electrically driven cylinder controlled and served by the straight movement of a piston rod
CN102000970B (en) Bolt assembly and disassembly manipulator capable of moving with three degrees of freedom
CN101633060B (en) Automatic spiral hole-milling unit
CN105500338A (en) Double-arm SCARA (selective compliance assembly robot arm) industrial robot
CN102768028A (en) Method and device for online in-situ measurement with single joint arm
CN103737577B (en) A kind of Six-DOF industrial robot driven containing ball screw assembly,
CN106041955B (en) A kind of robot automatic punching device and processing method
CN101104233A (en) Modular self-adaptive regulation clamp to weld car and its regulating method
CN201020662Y (en) High precision grinder wheel finishing device for complex section grinding wheel processing
CN101386150A (en) Numerical control polishing machine for optical elements
CN102744448B (en) Numerical control processing machine tool and processing method special for double-power unit propeller
CN103737207A (en) Parallel-serial welding robot mechanism with six degrees of freedom
CN202062167U (en) Cartesian five-degree-of-freedom welding manipulator
CN104708322A (en) Multifunctional drilling and riveting actuator and working method thereof
CN105181329A (en) Comprehensive test platform for industrial robot joint reducer

Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20111116

Effective date of abandoning: 20120822