CN208231793U - A kind of Multi Role Aircraft machinery claw - Google Patents
A kind of Multi Role Aircraft machinery claw Download PDFInfo
- Publication number
- CN208231793U CN208231793U CN201820614112.XU CN201820614112U CN208231793U CN 208231793 U CN208231793 U CN 208231793U CN 201820614112 U CN201820614112 U CN 201820614112U CN 208231793 U CN208231793 U CN 208231793U
- Authority
- CN
- China
- Prior art keywords
- main shaft
- gripper
- clamping jaw
- calvus
- role aircraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- Hooks, Suction Cups, And Attachment By Adhesive Means (AREA)
Abstract
The utility model discloses a kind of Multi Role Aircraft machinery claws, its structure includes lever arm, rotator, gripper, fixed screw, bottom plate, support base, fixing seat, telescopic arm, runing rest, connecting column, axis cover, movable main shaft, a kind of Multi Role Aircraft machinery claw of the utility model, structure is equipped with gripper, workpiece is clamped plus sucker using the calvus of gripper, machine is after startup power supply, the lever arm being mounted on rotator can be with voluntarily 360 degree of rotation, then movement up and down may be implemented using expansion bracket, this has clamping jaw main shaft among mechanical claw portion, it is mainly used to control opening clamping action of the poke rod to calvus of clamping jaw, also can use rotary main shaft in mechanical claw portion makes gripper realize rotation function, when calvus is clamped, sucker is equipped among two calvus, it is by pneumatic tube Air pressure suction-operated carry out absorption fixation, be fixed workpiece more in clamping jaw, workpiece will not be made to fall easily, damaged.
Description
Technical field
The utility model is a kind of Multi Role Aircraft machinery claw, belongs to manipulator manufacturing technology field.
Background technique
With the gradually development of mechanical automation, production, the mechanization degree of life are higher and higher, can be using mechanical generation
Also more and more for artificial field, nowadays, the use of mechanical arm is also more and more, and the scope of application of mechanical arm is increasingly
Extensively, also result in the functional requirement to mechanical arm also increasing, current mechanical arm is for clamping outer surface rule mostly
Object, but object irregular for outer surface, the structure not being arranged especially, the diversification for not being able to satisfy people needs
It asks.
Prior art discloses application No. is a kind of Multi Role Aircraft machinery claw of CN201710902993.5, including attachment base,
Clamping jaw cylinder is provided on attachment base, the piston of clamping jaw cylinder is connected with sliding seat, and folder is also hinged on attachment base
Pawl, is connected with clamping jaw connecting rod between clamping jaw and cylinder, guide post and fixed mechanism are provided on clamping jaw, is arranged in the outer end of guide post
Have block, spring I be provided between block and clamping jaw, be provided with the clamping plate of fixed guide post on fixed mechanism, clamping plate with lead
Suction device is provided between the inner end of column, but the clamping effect of the prior art is poor, causes gripper that cannot clamp workpiece,
It allows workpiece to fall, damages workpiece.
Utility model content
In view of the deficienciess of the prior art, the utility model aim is to provide a kind of Multi Role Aircraft machinery claw, with solution
Prior art clamping effect is poor, causes gripper that cannot clamp workpiece, the problem of allowing workpiece to fall, damage workpiece.
To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of multi-functional mechanical
Pawl, structure include lever arm, rotator, gripper, fixed screw, bottom plate, support base, fixing seat, telescopic arm, rotation branch
Frame, connecting column, axis cover, movable main shaft, the lever arm are installed on rotator, and the rotator is connected with gripper, institute
State the front end that gripper is set to fixed screw, fixed screw insertion is installed on the lower end of bottom plate, the support base and solid
Reservation is connected, and the telescopic arm is connected with runing rest, and the runing rest is installed on connecting column, the axis cover and work
Dynamic main shaft is connected, and the gripper includes calvus, poke rod, bearing, magnet, piston block, fixed ontology, positioning pin, revolution
Main shaft, upper cover, slide block, adjusting screw, clamping jaw main shaft, pneumatic tube, sucker, the calvus are connected with poke rod, and described group
Lever is installed on the front end of clamping jaw main shaft, and the bearing is located at the rear end of poke rod, and the magnet is connected with clamping jaw main shaft, institute
The left end for stating piston block is connected with the right end of magnet, and the fixed ontology is connected with positioning pin, the rotary main shaft installation
In fixed body interior, the upper cover is located at turn around the left side of main shaft, and the slide block is connected with rotary main shaft, the adjusting
Screw is connected with fixed ontology, and the clamping jaw main shaft is installed on the inside of fixed ontology, and the pneumatic tube is connected with sucker.
Further, the upper end of the bottom plate and the lower end of support base are mutually welded.
Further, the fixing seat is installed on the lower end of telescopic arm.
Further, the rotary main shaft is connected with rotator.
Further, the movable main shaft is cylindrical structure.
Further, the fixing seat is made of clean steel, is hardly damaged.
Further, the fixed ontology is made of steel alloy, has hardness high effect.
Beneficial effect
A kind of Multi Role Aircraft machinery claw of the utility model, structure are equipped with gripper, add sucker using the calvus of gripper
It is clamped workpiece, for machine after startup power supply, the lever arm being mounted on rotator can be with voluntarily 360 degree of rotation, then
Movement up and down may be implemented using expansion bracket, this has clamping jaw main shaft among mechanical claw portion, is mainly used to control folder
For the poke rod of pawl to the opening clamping action of calvus, also can use rotary main shaft in mechanical claw portion makes gripper realize rotation
Function is equipped with sucker, is inhaled by the air pressure suction-operated in pneumatic tube when calvus is clamped among two calvus
Attached fixation is fixed workpiece more in clamping jaw, workpiece will not be made to fall easily, damaged.
Detailed description of the invention
Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model
Sign, objects and advantages will become more apparent upon:
Fig. 1 is a kind of structural schematic diagram of Multi Role Aircraft machinery claw of the utility model；
Fig. 2 is a kind of cross section structure schematic diagram of gripper of the utility model.
In figure: lever arm -1, rotator -2, gripper -3, fixed screw -4, bottom plate -5, support base -6, fixing seat -
7, telescopic arm -8, runing rest -9, connecting column -10, axis cover -11, movable main shaft -12, calvus -301, poke rod -302, bearing -
303, magnet -304, piston block -305, fixed ontology -306, positioning pin -307, rotary main shaft -308, upper cover -309, slide block -
310, adjusting screw -311, clamping jaw main shaft -312, pneumatic tube -313, sucker -314.
Specific embodiment
To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below
In conjunction with specific embodiment, the utility model is further described.
Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of Multi Role Aircraft machinery claw technical solution: its structure includes lever arm
1, rotator 2, gripper 3, fixed screw 4, bottom plate 5, support base 6, fixing seat 7, telescopic arm 8, runing rest 9, connecting column
10, axis cover 11, movable main shaft 12, the lever arm 1 are installed on rotator 2, and the rotator 2 is connected with gripper 3, institute
The front end that gripper 3 is set to fixed screw 4 is stated, the fixed screw 4 is embedded in the lower end for being installed on bottom plate 5, the support base 6
It is connected with fixing seat 7, the telescopic arm 8 is connected with runing rest 9, and the runing rest 9 is installed on connecting column 10, institute
Axis cover 11 is stated to be connected with movable main shaft 12, the gripper 3 include calvus 301, poke rod 302, bearing 303, magnet 304,
Piston block 305, fixed ontology 306, positioning pin 307, rotary main shaft 308, upper cover 309, slide block 310, adjusting screw 311, folder
Pawl main shaft 312, pneumatic tube 313, sucker 314, the calvus 301 are connected with poke rod 302, and the poke rod 302 is installed on
The front end of clamping jaw main shaft 312, the bearing 303 are located at the rear end of poke rod 302, and the magnet 304 is connected with clamping jaw main shaft 312
It connecing, the left end of the piston block 305 is connected with the right end of magnet 304, and the fixed ontology 306 is connected with positioning pin 307,
The rotary main shaft 308 is installed on inside fixed ontology 306, and the upper cover 309 is located at turn around the left side of main shaft 308, and described group
Motion block 310 is connected with rotary main shaft 308, and the adjusting screw 311 is connected with fixed ontology 306, the clamping jaw main shaft 312
It is installed on the inside of fixed ontology 306, the pneumatic tube 313 is connected with sucker 314, the upper end and support bottom of the bottom plate 5
The lower end of seat 6 is mutually welded, and the fixing seat 7 is installed on the lower end of telescopic arm 8, and the rotary main shaft 308 is connected with rotator 2
It connects, the activity main shaft 12 is cylindrical structure, and the fixing seat 7 is made of clean steel, is hardly damaged, the fixed ontology 306
It is made of steel alloy, there is hardness high effect.
Gripper 3 described in this patent can be achieved on the robot components of similar human hand function.Robot hand is to use
It holds the component of workpiece or tool, is important one of executing agency, the workpiece shapes held according to robot are different, hand
Pawl can be divided mainly into three classes there are many type: mechanical paw, also known as mechanical clamp, including 2 refer to, 3 refer to and deformed finger；
Special gripper including magnetic-disc, welding gun etc.；General gripper, including 2 point to 5 fingers, the bearing 303 is in contemporary mechanical equipment
A kind of important spare part, its major function are to support mechanical rotary body, reduce the coefficient of friction in its motion process, and guarantee
Its rotating accuracy.
It is carrying out in use, being pressed from both sides using the calvus 301 of gripper 3 plus sucker 314 equipped with gripper 3 in structure
Clamping of workpieces, after startup power supply, then the lever arm 1 being mounted on rotator 2 can be utilized machine with voluntarily 360 degree of rotation
Movement up and down may be implemented in expansion bracket 8, this has clamping jaw main shaft 312 among 3 part of gripper, is mainly used to control folder
For the poke rod 302 of pawl to the opening clamping action of calvus 301, also can use rotary main shaft 308 in 3 part of gripper makes machinery
Pawl 3 realizes rotation function, when calvus 301 is clamped, sucker 314 is equipped among two calvus 301, is to pass through pneumatic tube
Air pressure suction-operated in 313 carries out absorption fixation.
The utility model solution prior art clamping effect is poor, causes gripper that cannot clamp workpiece, workpiece is allowed to fall, make
The problem of workpiece damages, the utility model are combined with each other by above-mentioned component, and the lever arm being mounted on rotator can
With voluntarily 360 degree of rotation, movement up and down then may be implemented using expansion bracket, this has folder among mechanical claw portion
Pawl main shaft is mainly used to control the poke rod of clamping jaw to the opening clamping action of calvus, also can use back in mechanical claw portion
Turning main shaft makes gripper realize rotation function, when calvus is clamped, sucker is equipped among two calvus, is to pass through pneumatic tube
In air pressure suction-operated carry out absorption fixation, be fixed workpiece more in clamping jaw, workpiece will not be made to fall easily, caused
Damage.
On the basic principles and main features of the present invention and the advantages of the present invention have been shown and described, for this
For the technical staff of field, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this reality
In the case where with novel spirit or essential attributes, the utility model can be realized in other specific forms.Therefore, no matter from
From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by appended
Claim rather than above description limit, it is intended that the institute that will be fallen within the meaning and scope of the equivalent elements of the claims
It changes and is embraced therein.Right involved in should not treating any reference in the claims as limiting is wanted
It asks.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (5)
1. a kind of Multi Role Aircraft machinery claw, it is characterised in that: its structure includes lever arm (1), rotator (2), gripper (3), consolidates
Determine screw (4), bottom plate (5), support base (6), fixing seat (7), telescopic arm (8), runing rest (9), connecting column (10), axis cover
(11), movable main shaft (12), the lever arm (1) are installed on rotator (2), and the rotator (2) is connected with gripper (3)
It connecing, the gripper (3) is set to the front end of fixed screw (4), and fixed screw (4) insertion is installed on the lower end of bottom plate (5),
The support base (6) is connected with fixing seat (7), and the telescopic arm (8) is connected with runing rest (9), the rotation branch
Frame (9) is installed on connecting column (10), and the axis cover (11) is connected with movable main shaft (12), and the gripper (3) includes pawl
Piece (301), poke rod (302), bearing (303), magnet (304), piston block (305), fixed ontology (306), positioning pin
(307), rotary main shaft (308), upper cover (309), slide block (310), adjusting screw (311), clamping jaw main shaft (312), pneumatic tube
(313), sucker (314), the calvus (301) are connected with poke rod (302), and the poke rod (302) is installed on clamping jaw master
The front end of axis (312), the bearing (303) are located at the rear end of poke rod (302), the magnet (304) and clamping jaw main shaft (312)
It is connected, the left end of the piston block (305) is connected with the right end of magnet (304), the fixed ontology (306) and positioning pin
(307) it is connected, the rotary main shaft (308) is installed on fixed ontology (306) inside, and the upper cover (309) is located at turn around master
The left side of axis (308), the slide block (310) are connected with rotary main shaft (308), and the adjusting screw (311) and fixation are originally
Body (306) is connected, and the clamping jaw main shaft (312) is installed on the inside of fixed ontology (306), the pneumatic tube (313) and suction
Disk (314) is connected.
2. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the upper end of the bottom plate (5) and support
It mutually welds the lower end of pedestal (6).
3. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the fixing seat (7) is installed on flexible
The lower end of arm (8).
4. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the rotary main shaft (308) and rotation
Device (2) is connected.
5. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the activity main shaft (12) is cylindrical body
Structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820614112.XU CN208231793U (en) | 2018-04-26 | 2018-04-26 | A kind of Multi Role Aircraft machinery claw |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820614112.XU CN208231793U (en) | 2018-04-26 | 2018-04-26 | A kind of Multi Role Aircraft machinery claw |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208231793U true CN208231793U (en) | 2018-12-14 |
Family
ID=64584480
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820614112.XU Expired - Fee Related CN208231793U (en) | 2018-04-26 | 2018-04-26 | A kind of Multi Role Aircraft machinery claw |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208231793U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109693258A (en) * | 2019-02-20 | 2019-04-30 | 吴钩科技(苏州)有限公司 | Submarine mechanical clamping jaw |
| CN110039272A (en) * | 2019-03-22 | 2019-07-23 | 青岛科技大学 | A kind of equipment of automation dismantling flex cable |
| CN110153351A (en) * | 2019-06-03 | 2019-08-23 | 重庆市綦江区宏利汽配有限公司 | Clamping pliers are used in a kind of forging |
| CN110713005A (en) * | 2019-09-25 | 2020-01-21 | 陈永生 | Article moving method and device |
| CN111113257A (en) * | 2019-12-09 | 2020-05-08 | 深圳市佳鑫一帆科技有限公司 | Rotary mechanical arm with clamping and locking capacity for machining plastic shell |
| CN111434473A (en) * | 2019-01-15 | 2020-07-21 | 上海哲开自动化科技有限公司 | Multifunctional industrial robot manipulator |
| DE102020131469A1 (en) | 2020-11-27 | 2022-06-02 | Karlsruher Institut für Technologie (Körperschaft des öffentlichen Rechts) | gripping device |
-
2018
- 2018-04-26 CN CN201820614112.XU patent/CN208231793U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111434473A (en) * | 2019-01-15 | 2020-07-21 | 上海哲开自动化科技有限公司 | Multifunctional industrial robot manipulator |
| CN109693258A (en) * | 2019-02-20 | 2019-04-30 | 吴钩科技(苏州)有限公司 | Submarine mechanical clamping jaw |
| CN109693258B (en) * | 2019-02-20 | 2024-04-09 | 吴钩科技(苏州)有限公司 | Underwater mechanical clamping jaw |
| CN110039272A (en) * | 2019-03-22 | 2019-07-23 | 青岛科技大学 | A kind of equipment of automation dismantling flex cable |
| CN110153351A (en) * | 2019-06-03 | 2019-08-23 | 重庆市綦江区宏利汽配有限公司 | Clamping pliers are used in a kind of forging |
| CN110713005A (en) * | 2019-09-25 | 2020-01-21 | 陈永生 | Article moving method and device |
| CN111113257A (en) * | 2019-12-09 | 2020-05-08 | 深圳市佳鑫一帆科技有限公司 | Rotary mechanical arm with clamping and locking capacity for machining plastic shell |
| DE102020131469A1 (en) | 2020-11-27 | 2022-06-02 | Karlsruher Institut für Technologie (Körperschaft des öffentlichen Rechts) | gripping device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181214 Termination date: 20190426 |