CN208529099U - A kind of Multi Role Aircraft machinery claw - Google Patents
A kind of Multi Role Aircraft machinery claw Download PDFInfo
- Publication number
- CN208529099U CN208529099U CN201820179291.9U CN201820179291U CN208529099U CN 208529099 U CN208529099 U CN 208529099U CN 201820179291 U CN201820179291 U CN 201820179291U CN 208529099 U CN208529099 U CN 208529099U
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- clamp arm
- arm
- role aircraft
- multi role
- bar
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Abstract
The utility model discloses a kind of Multi Role Aircraft machinery claws, the support arm is fixed in mounting base, the sub-arm is connected with the tail end of support arm by big shaft, the big shaft side is equipped with driving motor A, one end of the interlocking bar is fixed in mounting base, and the other end of the interlocking bar is connected with driving structure；The clamp arm includes clamp arm and dynamic clamp arm, the clamp arm is fixed on the side of fixing seat, the other side of the fixing seat is equipped with cavity, the dynamic clamp arm is mounted in cavity, and screw rod is fixed in dynamic clamp arm, the screw rod tail end passes through fixing seat, and is equipped with driving motor C in its tail end, and the clamp arm side wall is equipped with several suckers.The utility model not only can be used for carrying workpiece, but also can serve as fixture, while sucker is arranged in originally idle clamp arm side wall, can rotate the angle of clamp arm, so that sucker is contacted with workpiece, the carrying of workpiece is realized, it is multiple functional, the structure operation is simple, and rationally, cost is relatively low for design.
Description
Technical field
The utility model relates to a kind of Multi Role Aircraft machinery claws.
Background technique
Manipulator is the certain holding functions that can imitate manpower and arm, grabs to press fixed routine, carries object, or
The automatic pilot of operational instrument.Manipulator is the industrial robot occurred earliest, and the modern machines people occurred earliest,
It can replace the heavy labor of people to realize the mechanization and automation of production, can operate under hostile environment to protect the person
Safety, thus it is widely used in the departments such as machine-building, metallurgy, electronics, light industry and atomic energy.
Gripper is common manipulator ancillary equipment, is mainly used for grabbing object, due to the gripper of different field, tool
There is different constructions.For the gripper in mechanical processing process, the charging & discharging for being typically different workpiece is needed using different
Claw type, therefore in process, same gripper can be only applied to a kind of equipment processing, need constantly with changing pawl arm, or
Person directly replaces gripper, which influences production efficiency.
Utility model content
The purpose of this utility model is to provide a kind of Multi Role Aircraft machinery claws, to solve mentioned above in the background art ask
Topic.
To achieve the above object, the utility model provides the following technical solutions:
A kind of Multi Role Aircraft machinery claw, including mounting base, serial verb construction and driving structure, the serial verb construction include support
Arm, sub-arm and interlocking bar, the support arm are fixed in mounting base, and the tail end of the sub-arm and support arm passes through big shaft
Connection, the big shaft side are equipped with driving motor A, and one end of the interlocking bar is fixed in mounting base, the interlocking bar
The other end is connected with driving structure；
The driving structure includes fixing seat, clamp arm and driving motor C, and the clamp arm includes clamp arm and dynamic clamp arm, institute
The side that clamp arm is fixed on fixing seat is stated, the other side of the fixing seat is equipped with cavity, and the dynamic clamp arm is mounted in cavity,
And screw rod is fixed in dynamic clamp arm, the screw rod tail end passes through fixing seat, and is equipped with driving motor C, the folder in its tail end
Arm side wall is equipped with several suckers.
Preferably, the sucker is fixed by screws on clamp arm side wall, and the other side of the clamp arm is equipped with air pump, described
Air pump is connected with sucker.Clamp arm is responsible for grabbing pipe fitting, and the sucker of clamp arm side can then grab sheet and plate workpiece, and gas
Pump is that grabbing workpiece provides adsorption capacity, increase can grabbing workpiece weight range.
Preferably, the sub-arm and secondary bar tail end are equipped with linkage board, and driving motor B is equipped in the linkage board, described
The tail end of driving motor B is equipped with support rod, and the support rod passes through linkage board, and is equipped with fixing seat in its tail end.
Preferably, the cavity inside shape is in rectangle, and one end for being connected with driving motor C of the cavity is equipped with limit
Block, the limited block are in cylindrical body, and the screw rod passes through limited block.
Preferably, the limited block inner wall is equipped with internal screw thread, and the screw rod is equipped with matched external screw thread.
Preferably, the sucker center is equipped with tracheae, and the air pump is connected with tracheae.
Preferably, spring is equipped between the dynamic clamp arm and clamp arm.
Preferably, the interlocking bar includes mobile jib, special-shaped bar and secondary bar, and one end of the mobile jib is hinged in mounting base,
The other end of the mobile jib and special-shaped bar are hinged, the special-shaped bar again it is hinged with big shaft and secondary bar respectively, the secondary bar it is another
One end is hinged with fixing seat.
Preferably, the special-shaped bar is triangular in shape.
Compared with prior art, the utility model has the beneficial effects that
1, script is only had a kind of gripper equipment of pawl arm by the utility model, is adjusted to multi-functional pawl arm, the pawl arm
Including a kind of clamp arm for facilitating adjusting, which can be used for grabbing the workpiece of tubulose or solid, be arranged in the clamp arm side
Several suckers, the sucker can adsorb the workpiece of some plates, be suitable for various process, not only save manpower, but also solve
The carrying problems of various workpieces；
2, the utility model both can be used for carrying workpiece by screw drive to drive the clamping and release of dynamic clamp arm,
Can serve as fixture again, while sucker is arranged in originally idle clamp arm side wall, the angle of clamp arm can be rotated so that sucker with
Workpiece contact, realizes the carrying of workpiece, and multiple functional, the structure operation is simple, and rationally, cost is relatively low for design；
3, for the utility model by motor driven, the entirety of mechanical arm is realized in combined operation between interlocking bar and support arm
Position adjustment, and the gripper in driving structure realize the crawl to workpiece, and to the fixed function for workpieces processing, one
Machine is dual-purpose, equipment diversification.
Detailed description of the invention
Fig. 1 is a kind of Multi Role Aircraft machinery claw schematic diagram；
Fig. 2 is clamp arm side view.
In figure: 1- mounting base, 2- support arm, the big shaft of 3-, 4- driving motor A, 5- mobile jib, 6- special-shaped bar, 7- secondary bar, 8-
Sub-arm, 9- driving motor B, 10- linkage board, 11- fixing seat, 12- clamp arm, 13- move clamp arm, 14- screw rod, 15- driving electricity
Machine C, 16- sucker, 17- air pump.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
A kind of Multi Role Aircraft machinery claw referring to FIG. 1-2, including mounting base 1, serial verb construction and driving structure, the gearing
Structure includes support arm 2, sub-arm 8 and interlocking bar, and the support arm 2 is fixed in mounting base 1, the sub-arm 8 and support
The tail end of arm 2 is connected by big shaft 3, and big 3 side of shaft is equipped with driving motor A 4, and one end of the interlocking bar is fixed
In mounting base 1, the other end of the interlocking bar is connected with driving structure；
The driving structure includes fixing seat 11, clamp arm and driving motor C 15, and the clamp arm includes clamp arm 12 and moves
Clamp arm 13, the clamp arm 12 are fixed on the side of fixing seat 11, and the other side of the fixing seat 11 is equipped with cavity, the dynamic folder
Arm 13 is mounted in cavity, and screw rod 14 is fixed in dynamic clamp arm 13, and 14 tail end of screw rod passes through fixing seat 11, and at it
Tail end is equipped with driving motor C 15, and the clamp arm side wall is equipped with several suckers 16.
Preferably, the sucker 16 is fixed by screws on clamp arm side wall, and the other side of the clamp arm is equipped with air pump 17,
The air pump 17 is connected with sucker 16.Clamp arm is responsible for grabbing pipe fitting, and the sucker 16 of clamp arm side can then grab sheet and plate
Shape workpiece, and air pump 17 provides adsorption capacity for grabbing workpiece, increase can grabbing workpiece weight range.
Preferably, the sub-arm 8 and 7 tail end of secondary bar are equipped with linkage board 10, are equipped with driving motor B in the linkage board 10
The tail end of 9, the driving motor B 9 are equipped with support rod, and the support rod passes through linkage board 10, and is equipped with fixing seat in its tail end
11。
Preferably, the cavity inside shape is in rectangle, and one end for being connected with driving motor C 15 of the cavity is equipped with
Limited block, the limited block are in cylindrical body, and the screw rod 14 passes through limited block.
Preferably, the limited block inner wall is equipped with internal screw thread, and the screw rod 14 is equipped with matched external screw thread.
Preferably, 16 center of sucker is equipped with tracheae, and the air pump 17 is connected with tracheae.
Preferably, spring is equipped between the dynamic clamp arm 13 and clamp arm 12, inner wall is equipped with non-slip mat between clamp arm.
Preferably, the interlocking bar includes mobile jib 5, special-shaped bar 6 and secondary bar 7, and one end of the mobile jib 5 is hinged on mounting base
On 1, the other end and special-shaped bar 6 of the mobile jib 5 are hinged, and the special-shaped bar 6 is again hinged with big shaft 3 and secondary bar 7 respectively, described
The other end and fixing seat 11 of secondary bar 7 are hinged.
Preferably, the special-shaped bar 6 is triangular in shape.
It is obvious to a person skilled in the art that the present invention is not limited to the details of the above exemplary embodiments, and
And without departing substantially from the spirit or essential attributes of the utility model, it can realize that this is practical new in other specific forms
Type.Therefore, in all respects, the present embodiments are to be considered as illustrative and not restrictive, this is practical new
The range of type is indicated by the appended claims rather than the foregoing description, it is intended that containing for the equivalent requirements of the claims will be fallen in
All changes in justice and range are embraced therein.It should not treat any reference in the claims as limiting
Related claim.
Claims (9)
1. a kind of Multi Role Aircraft machinery claw, including mounting base (1), serial verb construction and driving structure, it is characterised in that: the gearing knot
Structure includes support arm (2), sub-arm (8) and interlocking bar, and the support arm (2) is fixed on mounting base (1), the sub-arm
(8) it is connected with the tail end of support arm (2) by big shaft (3), big shaft (3) side is equipped with driving motor A (4), described
One end of interlocking bar is fixed on mounting base (1), and the other end of the interlocking bar is connected with driving structure；
The driving structure includes fixing seat (11), clamp arm and driving motor C (15), and the clamp arm includes clamp arm (12) and moves
Clamp arm (13), the clamp arm (12) are fixed on the side of fixing seat (11), and the other side of the fixing seat (11) is equipped with cavity,
The dynamic clamp arm (13) is mounted in cavity, and is fixed with screw rod (14) on dynamic clamp arm (13), and screw rod (14) tail end is worn
It crosses fixing seat (11), and is equipped with driving motor C (15) in its tail end, the clamp arm side wall is equipped with several suckers (16).
2. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the sucker (16) is fixed by screw
On clamp arm side wall, the other side of the clamp arm is equipped with air pump (17), and the air pump (17) is connected with sucker (16).
3. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the sub-arm (8) and secondary bar (7) tail
End is equipped with linkage board (10), is equipped with driving motor B (9) in the linkage board (10), and the tail end of the driving motor B (9) is equipped with
Support rod, the support rod pass through linkage board (10), and are equipped with fixing seat (11) in its tail end.
4. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the cavity inside shape is in rectangle,
One end for being connected with driving motor C (15) of the cavity is equipped with limited block, and the limited block is in cylindrical body, the screw rod (14)
Across limited block.
5. a kind of Multi Role Aircraft machinery claw according to claim 4, it is characterised in that: the limited block inner wall is equipped with interior spiral shell
Line, the screw rod (14) are equipped with matched external screw thread.
6. a kind of Multi Role Aircraft machinery claw according to claim 2, it is characterised in that: sucker (16) center is equipped with gas
Pipe, the air pump (17) are connected with tracheae.
7. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the dynamic clamp arm (13) and clamp arm
(12) spring is equipped between.
8. a kind of Multi Role Aircraft machinery claw according to claim 1, it is characterised in that: the interlocking bar includes mobile jib (5), different
One end of shape bar (6) and secondary bar (7), the mobile jib (5) is hinged on mounting base (1), the other end and abnormity of the mobile jib (5)
Bar (6) hingedly, the special-shaped bar (6) again respectively with big shaft (3) and secondary bar (7) hingedly, the other end of the secondary bar (7) with consolidate
Reservation (11) is hinged.
9. a kind of Multi Role Aircraft machinery claw according to claim 8, it is characterised in that: the special-shaped bar (6) is triangular in shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820179291.9U CN208529099U (en) | 2018-02-01 | 2018-02-01 | A kind of Multi Role Aircraft machinery claw |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820179291.9U CN208529099U (en) | 2018-02-01 | 2018-02-01 | A kind of Multi Role Aircraft machinery claw |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208529099U true CN208529099U (en) | 2019-02-22 |
Family
ID=65399488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820179291.9U Active CN208529099U (en) | 2018-02-01 | 2018-02-01 | A kind of Multi Role Aircraft machinery claw |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208529099U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111673782A (en) * | 2020-06-12 | 2020-09-18 | 西安外事学院 | Mechanical automation grabbing device |
-
2018
- 2018-02-01 CN CN201820179291.9U patent/CN208529099U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111673782A (en) * | 2020-06-12 | 2020-09-18 | 西安外事学院 | Mechanical automation grabbing device |
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