CN110181545A - A kind of Multi Role Aircraft machinery claw - Google Patents
A kind of Multi Role Aircraft machinery claw Download PDFInfo
- Publication number
- CN110181545A CN110181545A CN201910369832.3A CN201910369832A CN110181545A CN 110181545 A CN110181545 A CN 110181545A CN 201910369832 A CN201910369832 A CN 201910369832A CN 110181545 A CN110181545 A CN 110181545A
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- Prior art keywords
- staving
- cabinet
- rotary shaft
- block
- hole
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B25—HAND TOOLS; PORTABLE POWER-DRIVEN TOOLS; MANIPULATORS
- B25J—MANIPULATORS; CHAMBERS PROVIDED WITH MANIPULATION DEVICES
- B25J15/00—Gripping heads and other end effectors
- B25J15/02—Gripping heads and other end effectors servo-actuated
- B25J15/0206—Gripping heads and other end effectors servo-actuated comprising articulated grippers
- B25J15/0213—Gripping heads and other end effectors servo-actuated comprising articulated grippers actuated by gears
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- Engineering & Computer Science (AREA)
- Robotics (AREA)
- Mechanical Engineering (AREA)
- Jigs For Machine Tools (AREA)
- Clamps And Clips (AREA)
Abstract
The present invention provides a kind of Multi Role Aircraft machinery claws, including hold assembly and transmission parts；The hold assembly includes the first brace, claw, the first cabinet, the first staving and the second staving；2 the first braces are at least symmetrically hinged on first cabinet, each first brace top is fixedly connected with claw, and be slidably connected the first sliding block on first brace；First box top is fixedly connected with the first staving；The first staving inner top surface installs second bearing, and the second bearing supports rotary shaft one end, and screw thread pair connects the second screw shell in the rotary shaft, so that the second screw shell is moved along a straight line by rotary shaft rotation；It is hinged by the second brace between first sliding block and the second screw shell；First tank floor is fixedly connected with the second staving, and second staving bottom fixed conveyor parts, the rotary shaft other end passes through the first cabinet and the second staving is connect with transmission parts.The configuration of the present invention is simple, it is vdiverse in function, it is practical.
Description
Technical field
The present invention relates to mechanical hand technical field, in particular to a kind of Multi Role Aircraft machinery claw.
Background technique
With the progress of machinery industry, the application of gripper is more and more wider, and gripper can be engaged in some arduous and ring
The severe work in border, wide adaptation range, currently there are gripper type it is very much, most gripper all can only be real
Pick-and-place now is carried out to the same shape or shape substantially similar object, utility function is more single, in order to realize to different shape or
The pick-and-place of complex structure needs the gripper in conjunction with a variety of different function, not only increases pick-and-place cost, also time-consuming to take
Power.
Summary of the invention
For the deficiencies in the prior art, the present invention provides a kind of Multi Role Aircraft machinery claws, and structure is simple, and function is more
Sample, it is practical.
The present invention achieves the above technical objects by the following technical means.
A kind of Multi Role Aircraft machinery claw, including hold assembly and transmission parts；The hold assembly includes the first brace, card
Pawl, the first cabinet, the first staving and the second staving；2 the first braces, Mei Gesuo are at least symmetrically hinged on first cabinet
It states the first brace top and is fixedly connected with claw, be slidably connected the first sliding block on first brace；First box top
It is fixedly connected with the first staving；The first staving inner top surface installs second bearing, and the second bearing supports rotary shaft one end,
Screw thread pair connects the second screw shell in the rotary shaft, so that the second screw shell is moved along a straight line by rotary shaft rotation；It is described
It is hinged by the second brace between first sliding block and the second screw shell；First tank floor is fixedly connected with second barrel
Body, second staving bottom fixed conveyor parts, the rotary shaft other end pass through the first cabinet and the second staving and transmission
Component connection.
It further, further include traversing component and clutch part, the traversing component includes threaded rod, first sleeve, more piece
Telescopic rod and rotating cylinder；One end of hinged Multi-section telescopic rod, the other end of the Multi-section telescopic rod on each first sliding block
It is hinged with the first screw shell, the first screw shell, the first box inside wall fixed first axle are installed on the threaded rod
It holds, the first bearing supports described threaded rod one end, and the threaded rod other end connects first bevel gear；First cabinet
Inner sidewall bottom supports rotating cylinder, and second bevel gear is installed in described rotating cylinder one end, and the rotary shaft passes through rotating cylinder and second
Bevel gear, the second bevel gear are engaged at least two first bevel gear, and the rotating cylinder other end is equipped with clutch part, are used
In connection rotating cylinder and transmission parts.
Further, the clutch part includes the second cabinet, rotating disk, resilient pin mechanism and linear slide mechanism；Institute
It states rotating disk to connect with transmission of rotary axis, and the rotating disk is on the rotary shaft slidably；Rotating disk bottom surface annular is provided with
Dovetail groove, the dovetail groove are equipped at least two dovetails, and rotating disk top surface annular is evenly distributed with several square blocks；
The second inner wall of barrel annular is equipped with several resilient pin mechanisms, and the second wall box annular is equipped with several
Second through-hole, and the resilient pin mechanism is inserted into inside the second through-hole, for preventing second body pivot；Described second
Cabinet is connect with the rotating cylinder other end, and second tank floor is evenly distributed with several first through hole, and the first through hole with it is rectangular
Block corresponds, and several linear slide mechanisms, and the linear slide mechanism and first through hole one are equipped in second cabinet
One is corresponding；Enter first through hole by square block, shrinks resilient pin mechanism described in the linear slide mechanism controls；U-shaped
Bar is penetrated in the second staving and is connect respectively with two dovetails, for moving axially rotating disk；When rotating disk is axially moved
When dynamic, the square block, which enters first through hole, makes linear slide mechanism move linearly；It is equipped between the U-shaped bar and the second staving
Resetting-mechanism, for making the square block leave first through hole.
Further, the linear slide mechanism includes slide, slide bar, convex block and limited block；It is equipped in second cabinet
Slide, the slide bar are slidably connected with slide, and described slide bar one end is equipped with convex block, the convex block and resilient pin mechanism contacts,
For shrinking resilient pin mechanism；The slide bar other end is equipped with limited block, for preventing convex block to be pierced by the second through-hole；It is described
Slide bar and square block are the wedge block of pairing.
Further, the resilient pin mechanism includes groove, cross bar and second spring；It is equipped in second staving recessed
Slot, the second spring are located in groove, and described cross bar one end is connect with second spring, and it is logical that the cross bar other end passes through second
Hole and linear slide mechanism contacts.
Further, the claw side wall is fixedly connected with frosted layer.
Further, further include battery, battery is installed in second staving, the battery is energized for transmission parts.
The beneficial effects of the present invention are:
Multi Role Aircraft machinery claw of the present invention, structure is simple, vdiverse in function, practical, by setting the first brace,
Claw, frosted layer, first bearing, the first sliding block, the first staving, second bearing, the second threaded rod, the second screw shell, second
Brace, phase Induction Machines, L shape bar, retarder, rotary shaft, battery and controller can sufficiently clamp object, be convenient for object
The carrying of body, and it is provided with first bevel gear, threaded rod, the first screw shell, section telescopic bar, the second cabinet, rotating cylinder, second
Bevel gear, stop collar, slide, slide bar, limited block, convex block, third staving, transverse slat, cross bar and second spring can be to Bu Tong big
Small and shape object is clamped, and improves use scope, time-consuming and laborious so as to improve producing once again, is improved work efficiency.
Detailed description of the invention
Fig. 1 is the structure chart of Multi Role Aircraft machinery claw of the present invention.
Fig. 2 is the partial enlarged view of Multi Role Aircraft machinery claw of the present invention.
Fig. 3 is the half sectional view of the second cabinet of the present invention.
In figure:
The first cabinet of 1-；The first brace of 2-；3- claw；4- frosted layer；5- first bearing；6- threaded rod；7- first bores tooth
Wheel；The first screw shell of 8-；The first sliding block of 9-；10- Multi-section telescopic rod；The first staving of 11-；12- second bearing；13- screw thread pair；
The second screw shell of 14-；The second brace of 15-；The second staving of 16-；17- threephase asynchronous machine；18-L shape bar；19- retarder；
20- rotary shaft；21- battery；22- controller；23- rotating disk；24- dovetails；25- square block；26- handle；27-U shape bar；
The first spring of 28-；The second cabinet of 29-；30- rotating cylinder；31- second bevel gear；32- stop collar；33- slide；34- slide bar；35-
Limited block；36- convex block；37- third staving；38- transverse slat；39- cross bar；40- second spring；1-1- first sliding groove；11-1- second
Sliding slot；16-1- groove；23-1- dovetail groove；29-1- first through hole；29-2- first through hole.
Specific embodiment
Present invention will be further explained with reference to the attached drawings and specific examples, but protection scope of the present invention is simultaneously
It is without being limited thereto.
As shown in Figure 1, Figure 2 and Figure 3, Multi Role Aircraft machinery claw of the present invention, including hold assembly, transmission parts, cross
Move component and clutch part；
The hold assembly includes the first brace 2, claw 3, the first cabinet 1, the first staving 11 and the second staving 16；It is described
2 the first braces 2 are at least symmetrically hinged on first cabinet 1, each first brace, 2 top is fixedly connected with claw 3, institute
State 3 side wall of claw and be fixedly connected with frosted layer 4,2 section of the first brace be it is rectangular, be slidably connected on first brace 2
First sliding block 9；First cabinet, 1 top surface is fixedly connected with the first staving 11；First cabinet, 1 top surface is provided with first sliding groove
1-1；First staving, 11 inner top surface installs second bearing 12, and the second bearing 12 supports 20 one end of rotary shaft, the rotation
Shaft 20 is equipped with screw thread pair 13, and the screw thread pair 13 is threadedly coupled with the second screw shell 14, is made by the rotation of rotary shaft 20
Second screw shell 14 linear motion；First staving, 11 sidewall symmetry is provided with multiple second sliding slot 11-1, and described first is sliding
Block 9 and 15 one end of the second brace are hinged, and 15 other end of the second brace passes through the second sliding slot 11-1 and the second thread bush
Cylinder 14 is hinged；First cabinet, 1 bottom surface is fixedly connected with the second staving 16, the 16 bottom fixed conveyor portion of the second staving
Part, first sliding groove 1-1 and second staving 16 of 20 other end of rotary shaft on the first cabinet 1 are connect with transmission parts.
Second staving, 16 inner bottom surface is fixedly connected with threephase asynchronous machine 17, and 16 inner bottom surface of the second staving is symmetrically fixedly connected
There are two L shape bars 18, retarder 19,17 output end of threephase asynchronous machine and retarder are fixedly connected between two L shape bars 18
19 one end are fixedly connected, and 19 output end of retarder connects rotary shaft 20, are fixedly connected with battery in second staving 16
21,16 side wall of the second staving is fixedly connected with controller 22, and the threephase asynchronous machine 17 has control by connection
Device 22.
The traversing component includes threaded rod 6, first sleeve 8, Multi-section telescopic rod 10 and rotating cylinder 30；Each described first
The other end of one end of hinged Multi-section telescopic rod 10 on sliding block 9, the Multi-section telescopic rod 10 passes through first sliding groove 1-1 and the first spiral shell
Line sleeve 8 is hinged, and the first screw shell 8 is installed on the threaded rod 6, and 1 inner sidewall of the first cabinet fixes first bearing 5,
The first bearing 5 supports described 6 one end of threaded rod, and 6 other end of threaded rod connects first bevel gear 7；First case
1 inner sidewall bottom of body supports rotating cylinder 30, and second bevel gear 31 is installed in described 30 one end of rotating cylinder, and the rotary shaft 20 passes through rotation
Rotating cylinder 30 and second bevel gear 31, the second bevel gear 31 are engaged at least two first bevel gear 7, and the rotating cylinder 30 is another
One end is equipped with clutch part, for connecting rotating cylinder 30 and transmission parts.The rotating cylinder 30 is equipped with two stop collars 32, is used for
Prevent rotating cylinder 30 from moving axially on the first cabinet 1, the stop collar 32 is axis circlip.
The clutch part includes the second cabinet 29, rotating disk 23, resilient pin mechanism and linear slide mechanism；The rotation
Turntable 23 and rotary shaft 20 are sequentially connected, and the rotating disk 23 in rotary shaft 20 slidably；The rotating disk 23 and rotation
Axis 20 can be keyed, and the gap of keyway is become larger and the rotating disk 23 can be achieved in rotary shaft 20 slidably, also can achieve
The effect of transmission；The 23 bottom surface annular of rotating disk is provided with dovetail groove 23-1, and the dovetail groove 23-1 is equipped at least two dovetails
Block 24, the 23 top surface annular of rotating disk are evenly distributed with several square blocks 25；
Wall circular is equipped with several resilient pin mechanisms in second staving 16, and the 29 side wall annular of the second cabinet is equipped with
Several second through-hole 29-2, and the resilient pin mechanism is inserted into inside the second through-hole 29-2, for preventing second cabinet
29 rotations；Second cabinet 29 is connect with 30 other end of rotating cylinder, and 29 bottom surface of the second cabinet is evenly distributed with several first through hole
29-1, and the first through hole 29-1 and square block 25 correspond, and are equipped with several linear slide machines in second cabinet 29
Structure, and the linear slide mechanism and first through hole 29-1 are corresponded；Enter first through hole 29-1 by square block 25, makes institute
State the contraction of resilient pin mechanism described in linear slide mechanism controls；Second staving, 16 bottom surface is fixedly connected with handle 26, institute
It states 16 bottom surface of the second staving and is installed with U-shaped bar 27, U-shaped bar 27 penetrates in the second staving 16 to be connected with two dovetails 24 respectively
It connects, for moving axially rotating disk 23；26 top surface of handle is fixedly connected with the first spring 28,28 end of the first spring
It is fixedly connected with 27 cross bar top surface of U-shaped bar；When rotating disk 23 moves axially, the square block 25 makes into first through hole 29-1
The linear movement of linear slide mechanism；Resetting-mechanism is equipped between the U-shaped bar 27 and the second staving 16, for making the square block
25 leave first through hole 29-1.
The linear slide mechanism includes slide 33, slide bar 34, convex block 36 and limited block 35；It is set in second cabinet 29
There is slide 33, the slide bar 34 is slidably connected with slide 33, and described 34 one end of slide bar is equipped with convex block 36, the convex block 36 and elasticity
Bolt mechanism contact, for shrinking resilient pin mechanism；34 other end of slide bar is equipped with limited block 35, for preventing convex block
36 are pierced by the second through-hole 29-2；The slide bar 34 and square block 25 are the wedge block of pairing.
The resilient pin mechanism includes groove 16-1, cross bar 39 and second spring 40；It is equipped in second staving 16
Staving 37 is fixedly connected in groove 16-1, the groove 16-1, fitting sliding has transverse slat 38, the transverse slat in the staving 37
38 one side walls are fixedly connected with cross bar 39, and 39 other end of cross bar is pierced by staving 37 across the second through-hole 29-2 and 36 side of convex block
Wall fitting, the cross bar 39 are slidably connected with staving 37, are equipped with second spring 40, the second spring 40 1 in the staving 37
End is bonded with the second staving 16.
First brace 2 is made of alloy steel material.
The model ye3-315l-4 of the threephase asynchronous machine 17.
Working principle: it when object needs to clamp mobile, when manual handling inconvenience, is carried using the present apparatus, this is filled
Two claws 3 set are placed into the object both ends for needing to carry, and then operate controller 22 and threephase asynchronous machine 17 is made to start work
To make, 17 output end of threephase asynchronous machine drives rotary shaft 20 to rotate by retarder 19, and rotary shaft 20 drives rotating disk 23 to rotate,
Rotary shaft 20 drives the second screw shell 14 mobile, and the second screw shell 14 drives the second brace 15 mobile, 15 band of the second brace
Dynamic first sliding block 9 rotation, the first sliding block 9 drive the rotation of the first brace 2, and the first brace 2 drives claw 3 mobile, and two claws 3 are by object
Body is clamped, and the setting of frosted layer 4 effectively prevents object from sliding, and is carried handle 26 and is moved the present apparatus, to reach
To the purpose of mobile object, when object is moved to appropriate location, operation controller 22 reversely rotates threephase asynchronous machine 17,
Two claws 3 are separated with object, to realize the movement of object.
When object volume is too small, with hand pinching U-shaped bar 27, U-shaped bar 27 drives rotating disk 23 to move in rotary shaft 20,
Square block 25 is slowly inserted into the first through hole 29-1 of the second cabinet 29, pushes slide bar 34 mobile, slide bar 34 drives convex block
36 is mobile, and it is mobile that convex block 36 pushes cross bar 39, so that cross bar 39 is skidded off from the second through-hole 29-2, square block 25 and limited block 35
It offsets, convex block 36 and 16 inner wall of the second staving are tangent at this time, and the second cabinet 29 is integrated with rotating disk 23, and rotating disk 23 drives
The rotation of second cabinet 29, the second cabinet 29 drive rotating cylinder 30 to rotate, and rotating cylinder 30 drives second bevel gear 31 to rotate, the second cone
Gear 31 drives first bevel gear 7 to rotate, and first bevel gear 7 drives threaded rod 6 to rotate, and threaded rod 6 drives the first screw shell 8
Mobile, the first screw shell 8 drives Multi-section telescopic rod 10 mobile to two sides, and Multi-section telescopic rod 10 drives the first sliding block obliquely upward
Mobile, rotary shaft 20 drives the second screw shell 14 to move up at the same time, and the second screw shell 14 pushes the second brace 15
It moves obliquely upward, so that the first cylinder 9 moves obliquely upward, then unclamps U-shaped bar 27, so that U-shaped bar 27 is to moving down
Dynamic, U-shaped bar 27 drives rotating disk 23 to move down, and rotating disk 23 drives square block 25 to move down, and square block 25 is logical from first
It is skidded off in the 29-1 of hole, so that rotating disk 23 is separated with the second cabinet 29, second spring 40 pushes transverse slat 38 mobile at this time, horizontal
Plate 38 pushes cross bar 39 mobile, and 39 other end of cross bar is re-inserted into the second through-hole 29-2, to obtain the second cabinet indirectly
Then 29 fixation operates controller 22 again and threephase asynchronous machine 17 is rotated in the forward direction, carry out aforesaid operations be clamped with
And movement prevents object, when object is too big, carries out the inverse operation of aforesaid operations, and after object clamps movement, operation control
Device 22 processed makes threephase asynchronous machine 17 stop working.
The embodiment is a preferred embodiment of the present invention, but present invention is not limited to the embodiments described above, not
In the case where substantive content of the invention, any conspicuous improvement that those skilled in the art can make, replacement
Or modification all belongs to the scope of protection of the present invention.
Claims (7)
1. a kind of Multi Role Aircraft machinery claw, which is characterized in that including hold assembly and transmission parts；The hold assembly includes first
Brace (2), claw (3), the first cabinet (1), the first staving (11) and the second staving (16)；On first cabinet (1) at least
2 the first braces (2) symmetrically are hinged with, each first brace (2) top is fixedly connected with claw (3), and described first tiltedly
Be slidably connected the first sliding block (9) on bar (2)；First cabinet (1) top surface is fixedly connected with the first staving (11)；Described first
Staving (11) inner top surface installs second bearing (12), and the second bearing (12) supports rotary shaft (20) one end, the rotary shaft
(20) screw thread pair connection the second screw shell (14) on transports the second screw shell (14) straight line by rotary shaft (20) rotation
It is dynamic；It is hinged by the second brace (15) between first sliding block (9) and the second screw shell (14)；First cabinet (1)
Bottom surface is fixedly connected with the second staving (16), the second staving (16) bottom fixed conveyor parts, and the rotary shaft (20) is another
One end passes through the first cabinet (1) and the second staving (16) is connect with transmission parts.
2. Multi Role Aircraft machinery claw according to claim 1, which is characterized in that further include traversing component and clutch part, institute
Stating traversing component includes threaded rod (6), first sleeve (8), Multi-section telescopic rod (10) and rotating cylinder (30)；Each described first is sliding
One end of hinged Multi-section telescopic rod (10) on block (9), the other end and the first screw shell (8) hinge of the Multi-section telescopic rod (10)
It connects, is installed the first screw shell (8) on the threaded rod (6), the first cabinet (1) inner sidewall is fixed first bearing (5), institute
It states first bearing (5) and supports described threaded rod (6) one end, threaded rod (6) other end connects first bevel gear (7)；It is described
First cabinet (1) inner sidewall bottom supports rotating cylinder (30), and second bevel gear (31) are installed in described rotating cylinder (30) one end, described
Rotary shaft (20) passes through rotating cylinder (30) and second bevel gear (31), and the second bevel gear (31) and at least two first bore tooth
(7) engagement is taken turns, rotating cylinder (30) other end is equipped with clutch part, for connecting rotating cylinder (30) and transmission parts.
3. Multi Role Aircraft machinery claw according to claim 2, which is characterized in that the clutch part includes the second cabinet
(29), rotating disk (23), resilient pin mechanism and linear slide mechanism；The rotating disk (23) and rotary shaft (20) transmission connect
Connect, and the rotating disk (23) on rotary shaft (20) slidably；Rotating disk (23) bottom surface annular is provided with dovetail groove (23-
1), the dovetail groove (23-1) is equipped at least two dovetails (24), and rotating disk (23) the top surface annular is uniformly distributed several rectangular
Block (25)；
The interior wall circular of second staving (16) is equipped with several resilient pin mechanisms, and the second cabinet (29) side wall annular is equipped with
Several second through-holes (29-2), and resilient pin mechanism insertion the second through-hole (29-2) is internal, for preventing described second
Cabinet (29) rotation；Second cabinet (29) connect with rotating cylinder (30) other end, and the second cabinet (29) bottom surface is uniformly distributed
Several first through hole (29-1), and the first through hole (29-1) and square block (25) correspond, second cabinet (29)
It is interior to be equipped with several linear slide mechanisms, and the linear slide mechanism and first through hole (29-1) are corresponded；Pass through square block
(25) enter first through hole (29-1), shrink resilient pin mechanism described in the linear slide mechanism controls；U-shaped bar (27) is worn
Enter and connect respectively with two dovetails (24) in the second staving (16), for moving axially rotating disk (23)；Work as rotation
When disk (23) moves axially, the square block (25), which enters first through hole (29-1), makes linear slide mechanism move linearly；The U
Resetting-mechanism is equipped between shape bar (27) and the second staving (16), for making the square block (25) leave first through hole (29-
1)。
4. Multi Role Aircraft machinery claw according to claim 3, which is characterized in that the linear slide mechanism includes slide
(33), slide bar (34), convex block (36) and limited block (35)；Slide (33) are equipped in second cabinet (29), the slide bar
(34) it is slidably connected with slide (33), described slide bar (34) one end is equipped with convex block (36), the convex block (36) and resilient pin machine
Structure contact, for shrinking resilient pin mechanism；Slide bar (34) other end is equipped with limited block (35), for preventing convex block
(36) it is pierced by the second through-hole (29-2)；The slide bar (34) and square block (25) are the wedge block of pairing.
5. Multi Role Aircraft machinery claw according to claim 3, which is characterized in that the resilient pin mechanism includes groove (16-
1), cross bar (39) and second spring (40)；It is equipped with groove (16-1) in second staving (16), second spring (40) position
In groove (16-1), described cross bar (39) one end is connect with second spring (40), and cross bar (39) other end passes through second
Through-hole (29-2) and linear slide mechanism contacts.
6. Multi Role Aircraft machinery claw according to claim 1-5, which is characterized in that claw (3) side wall is fixed
It is connected with frosted layer (4).
7. Multi Role Aircraft machinery claw according to claim 1-5, which is characterized in that it further include battery (21), it is described
Battery (21) are installed in second staving (16), the battery (21) energizes for transmission parts.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910369832.3A CN110181545B (en) | 2019-05-06 | 2019-05-06 | Multifunctional mechanical claw |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910369832.3A CN110181545B (en) | 2019-05-06 | 2019-05-06 | Multifunctional mechanical claw |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN110181545A true CN110181545A (en) | 2019-08-30 |
| CN110181545B CN110181545B (en) | 2021-05-25 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201910369832.3A Active CN110181545B (en) | 2019-05-06 | 2019-05-06 | Multifunctional mechanical claw |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107695461A (en) * | 2017-11-13 | 2018-02-16 | 中车集团四川丹齿零部件有限公司 | A kind of robot manipulator structure of gear grinding machines |
| CN111055272A (en) * | 2019-12-17 | 2020-04-24 | 南京昱晟机器人科技有限公司 | Machine claw with strong control performance |
| CN112157902A (en) * | 2020-09-11 | 2021-01-01 | 深圳市利航电子有限公司 | Full-automatic production line for backlight source |
| CN112454405A (en) * | 2021-01-26 | 2021-03-09 | 广东顺力智能物流装备股份有限公司 | Intelligent material carrying manipulator |
| CN114229456A (en) * | 2022-01-27 | 2022-03-25 | 中原工学院 | A novel mechanical clamping jaw for machine-building |
| CN114604622A (en) * | 2022-04-01 | 2022-06-10 | 南通制桶厂有限公司 | A centre gripping lifts up device for iron bucket assembly line |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0134819A1 (en) * | 1978-08-01 | 1985-03-27 | Grisebach, Hans-Theodor | Gripping head with an electric clasping drive |
| CN103878763A (en) * | 2014-03-14 | 2014-06-25 | 江苏大学 | Three-freedom degree manipulator |
| CN106584496A (en) * | 2017-01-18 | 2017-04-26 | 瑞安市智造科技有限公司 | Mechanical paw convenient to quickly adjust |
| CN106826896A (en) * | 2017-01-18 | 2017-06-13 | 赵浩琛 | A kind of manipulator for being easy to adjustment width |
| KR20180012447A (en) * | 2016-07-27 | 2018-02-06 | (주)주강로보테크 | The gripping device |
| CN108327911A (en) * | 2018-04-22 | 2018-07-27 | 南通雾图信息技术有限公司 | A kind of unmanned plane device with crawl function |
| CN207682400U (en) * | 2017-10-12 | 2018-08-03 | 淮海工学院 | A kind of multifunction manipulator |
| CN208117849U (en) * | 2018-03-21 | 2018-11-20 | 广安职业技术学院 | A kind of mechanical arm |
| CN109015728A (en) * | 2018-09-11 | 2018-12-18 | 湖州奥驿汽车服务有限公司 | Auxiliary clamp is used in a kind of detection of motor vehicle components |
| CN109600971A (en) * | 2018-12-12 | 2019-04-09 | 郑州云海信息技术有限公司 | Server cabinet cooling device |
-
2019
- 2019-05-06 CN CN201910369832.3A patent/CN110181545B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0134819A1 (en) * | 1978-08-01 | 1985-03-27 | Grisebach, Hans-Theodor | Gripping head with an electric clasping drive |
| CN103878763A (en) * | 2014-03-14 | 2014-06-25 | 江苏大学 | Three-freedom degree manipulator |
| KR20180012447A (en) * | 2016-07-27 | 2018-02-06 | (주)주강로보테크 | The gripping device |
| CN106584496A (en) * | 2017-01-18 | 2017-04-26 | 瑞安市智造科技有限公司 | Mechanical paw convenient to quickly adjust |
| CN106826896A (en) * | 2017-01-18 | 2017-06-13 | 赵浩琛 | A kind of manipulator for being easy to adjustment width |
| CN207682400U (en) * | 2017-10-12 | 2018-08-03 | 淮海工学院 | A kind of multifunction manipulator |
| CN208117849U (en) * | 2018-03-21 | 2018-11-20 | 广安职业技术学院 | A kind of mechanical arm |
| CN108327911A (en) * | 2018-04-22 | 2018-07-27 | 南通雾图信息技术有限公司 | A kind of unmanned plane device with crawl function |
| CN109015728A (en) * | 2018-09-11 | 2018-12-18 | 湖州奥驿汽车服务有限公司 | Auxiliary clamp is used in a kind of detection of motor vehicle components |
| CN109600971A (en) * | 2018-12-12 | 2019-04-09 | 郑州云海信息技术有限公司 | Server cabinet cooling device |
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| CN107695461A (en) * | 2017-11-13 | 2018-02-16 | 中车集团四川丹齿零部件有限公司 | A kind of robot manipulator structure of gear grinding machines |
| CN111055272A (en) * | 2019-12-17 | 2020-04-24 | 南京昱晟机器人科技有限公司 | Machine claw with strong control performance |
| CN111055272B (en) * | 2019-12-17 | 2021-05-28 | 南京昱晟机器人科技有限公司 | Machine claw with strong control performance |
| CN112157902A (en) * | 2020-09-11 | 2021-01-01 | 深圳市利航电子有限公司 | Full-automatic production line for backlight source |
| CN112454405A (en) * | 2021-01-26 | 2021-03-09 | 广东顺力智能物流装备股份有限公司 | Intelligent material carrying manipulator |
| CN112454405B (en) * | 2021-01-26 | 2021-04-13 | 广东顺力智能物流装备股份有限公司 | Intelligent material carrying manipulator |
| CN114229456A (en) * | 2022-01-27 | 2022-03-25 | 中原工学院 | A novel mechanical clamping jaw for machine-building |
| CN114229456B (en) * | 2022-01-27 | 2023-11-03 | 中原工学院 | Novel mechanical clamping jaw for mechanical manufacturing |
| CN114604622A (en) * | 2022-04-01 | 2022-06-10 | 南通制桶厂有限公司 | A centre gripping lifts up device for iron bucket assembly line |
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