CN205086002U - Honeycomb carbon -fibre composite connecting piece - Google Patents
Honeycomb carbon -fibre composite connecting piece Download PDFInfo
- Publication number
- CN205086002U CN205086002U CN201520912457.XU CN201520912457U CN205086002U CN 205086002 U CN205086002 U CN 205086002U CN 201520912457 U CN201520912457 U CN 201520912457U CN 205086002 U CN205086002 U CN 205086002U
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- fiber layer
- carbon fiber
- keriotheca
- hole
- honeycomb
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Abstract
The utility model provides a honeycomb carbon -fibre composite connecting piece. The utility model relates to a robot end -to -end connection spare, concretely relates to honeycomb carbon -fibre composite end effector connecting piece. The utility model provides a robot terminal with various executor products when being connected, the light -weighted problem of structure that adopts. A honeycomb carbon -fibre composite connecting piece includes fibre layers, the keriotheca, lower fibre layers, two sets of riveting grommets and a plurality of hollow rivet, go up fibre layers, from top to bottom the rigid coupling is cheng integrative in proper order with lower fibre layers for the keriotheca, go up fibre layers, keriotheca and lower fibre layers's up end equipartition correspondence respectively is equipped with a plurality of connect the via hole, the outside of going up fibre layers and lower fibre layers is equipped with a set of riveting grommet respectively, in every connect the via hole respectively the cartridge have a hollow rivet, through the riveting of a plurality of hollow rivet between two sets of riveting grommets. The utility model is used for the terminal peripheral equipment of product and robot of carrying out of industrial robot.
Description
Technical field
The utility model relates to a kind of robot end's connector, is specifically related to a kind of honeycomb carbon fibre composite end effector connector.
Background technology
Industrial robot is multi-joint manipulator towards industrial circle or multivariant installations, and it can automatically perform work, is to realize a kind of machine of various function by self power and control ability.It can accept mankind commander, also can run according to the program of layout in advance, the principle guiding principle action that modern industrial robot can also be formulated according to artificial intelligence technology.Robot is generally made up of executing agency, drive unit, checkout gear and control system and complicated machinery etc.According to the difference of joint configuration and coordinates of motion form, robot actuating mechanism can be divided into the types such as Cartesian coordinate type, circular cylindrical coordinate formula, polar coordinates type and joint coordinates formula.
Existing industrial machine robot end needs connector to connect with various actuator product when being connected, as the agent structure, framework, connector etc. of fixture, these connectors adopt high-strength alloy material to be made usually, connector self is heavier, very large on the abundant use impact of robot payload, add the application cost of robot, even affect the service life of robot.
Utility model content
The utility model is large for solving existing industrial robot end connectors weight, and add the extra load of robot, payload utilization rate is low, the problem that application cost is high, and then proposes a kind of honeycomb carbon fibre composite connector.
The utility model is the technical scheme taked that solves the problem: the utility model comprises carbon fiber layer, keriotheca, lower carbon fiber layer, two groups of riveted joint grommets and multiple tubular rivet, upper carbon fiber layer, keriotheca and lower carbon fiber layer are affixed integral successively from top to bottom, upper carbon fiber layer, the upper surface of keriotheca and lower carbon fiber layer respectively uniform correspondence is provided with multiple connecting through hole, the outside of upper carbon fiber layer and lower carbon fiber layer is respectively equipped with one group of riveted joint grommet, often group riveted joint grommet is provided with multiple riveted joint through hole, the position of riveted joint through hole is corresponding with the position of connecting through hole, a tubular rivet is fitted with respectively in each connecting through hole, riveted by multiple tubular rivet between two groups of riveted joint grommets.
The beneficial effects of the utility model are: the utility model structure is simple, main body adopts carbon fiber layer and keriotheca produced with combination to form, significantly reduce the weight of connector self, adopt the connecting elements such as the agent structure of this structure, framework, connector, it is lightweight, strength and stiffness are high, achieves the lightweight of structural member, improves the payload of robot, reduce robot application cost, extend the service life of robot.
Accompanying drawing explanation
Fig. 1 is the integrally-built sectional view of the utility model;
Fig. 2 is the left view of Fig. 1;
Fig. 3 is the front view of upper carbon fiber layer 1 in the utility model;
Fig. 4 is the front view of keriotheca 2 in the utility model;
Fig. 5 is the front view of riveting grommet 4 in the utility model.
Detailed description of the invention
Detailed description of the invention one: composition graphs 1 to Fig. 5 illustrates present embodiment, described in present embodiment, a kind of honeycomb carbon fibre composite connecting elements comprises carbon fiber layer 1, keriotheca 2, lower carbon fiber layer 3, two groups of riveted joint grommets 4 and multiple tubular rivet 5, upper carbon fiber layer 1, keriotheca 2 and lower carbon fiber layer 3 are affixed integral successively from top to bottom, upper carbon fiber layer 1, the upper surface of keriotheca 2 and lower carbon fiber layer 3 respectively uniform correspondence is provided with multiple connecting through hole 6, the outside of upper carbon fiber layer 1 and lower carbon fiber layer 3 is respectively equipped with one group of riveted joint grommet 4, often group riveted joint grommet 4 is provided with multiple riveted joint through hole 4-1, the position of riveted joint through hole 4-1 is corresponding with the position of connecting through hole 6, a tubular rivet 5 is fitted with respectively in each connecting through hole 6, riveted by multiple tubular rivet 5 between two groups of riveted joint grommets 4.
Under the upper carbon fiber layer 1-keriotheca 2-of design employing like this, the sandwich structure of carbon fiber layer 3 is made into connecting elements, the outside of connecting through hole 6 is reinforced by riveted joint grommet 4, and riveted by tubular rivet 5, prevent connecting through hole 6 from deforming when being connected with other mechanisms, enhance the intensity of whole connecting elements, under upper carbon fiber layer 1-keriotheca 2-, the sandwich structure of carbon fiber layer 3 reduces the weight of its structure self, reduce unnecessary energy loss, reduce the load of power source, and adopt the connecting elements strength and stiffness of structure like this high, motion process is accurately light.
Detailed description of the invention two: composition graphs 1 to Fig. 4 illustrates present embodiment, the position of multiple connecting through hole 6 described in present embodiment is uniform is respectively arranged on carbon fiber layer 1, the edge of keriotheca 2 and lower carbon fiber layer 3 upper surface and middle part.Other composition is identical with detailed description of the invention one with connected mode.
The position of design connecting through hole 6 like this goes for the connection of connecting elements.
Detailed description of the invention three: composition graphs 1 to Fig. 5 illustrates present embodiment, described in present embodiment, often group riveted joint grommet 4 comprises external bushing ring 4-2 and inner bushing ring 4-3, external bushing ring 4-2 and inner bushing ring 4-3 is laid with multiple riveted joint through hole 4-1 respectively, external bushing ring 4-2 is arranged on the edge of carbon fiber layer 1 and lower carbon fiber layer 3, the position of the riveted joint through hole 4-1 on external bushing ring 4-2 and upper carbon fiber layer 1, the connecting through hole 6 of the edge of keriotheca 2 and lower carbon fiber layer 3 upper surface is corresponding, the position of the riveted joint through hole 4-1 on inner bushing ring 4-3 and upper carbon fiber layer 1, the connecting through hole 6 at the middle part of keriotheca 2 and lower carbon fiber layer 3 upper surface is corresponding.Other compositions are identical with detailed description of the invention two with annexation.
Design like this makes riveted joint grommet 4 be applicable to the position of connecting through hole 6, and connecting through hole 6 is connected into entirety, strengthens the intensity of whole connecting elements, effectively prevents distortion.
Detailed description of the invention four: composition graphs 1 to Fig. 3 illustrates present embodiment, upper carbon fiber layer 1 and lower carbon fiber layer 3 described in present embodiment are successively to be bondd successively the upper carbon fiber layer and lower carbon fiber layer made along cross-sectional direction by multilayer carbon fibre initial rinse fabric respectively.Other composition and connected mode and detailed description of the invention one, two or three identical.
Detailed description of the invention five: composition graphs 1 to Fig. 3 illustrates present embodiment, described in present embodiment, the number of plies of the multilayer carbon fibre initial rinse fabric of upper carbon fiber layer 1 and lower carbon fiber layer 3 is 8 layers ~ 15 layers.Other composition is identical with detailed description of the invention four with connected mode.
Detailed description of the invention six: composition graphs 1 to Fig. 3 illustrates present embodiment, described in present embodiment, the thickness of every layer of carbon fibre initial rinse fabric of upper carbon fiber layer 1 and lower carbon fiber layer 3 is 0.3mm ~ 0.8mm.Other composition is identical with detailed description of the invention five with connected mode.
Detailed description of the invention seven: composition graphs 1 to Fig. 4 illustrates present embodiment, keriotheca 2 described in present embodiment is by the keriotheca of metal, macromolecule or ceramic material.Other composition is identical with detailed description of the invention four with connected mode.
The intensity strengthening keriotheca 2 is convenient in design like this, thus strengthens the intensity of whole connecting elements.
Detailed description of the invention eight: composition graphs 1 to Fig. 4 illustrates present embodiment, described in present embodiment, the thickness of keriotheca 2 is 7mm ~ 13mm.Other composition is identical with detailed description of the invention seven with connected mode.
Detailed description of the invention nine: composition graphs 1 to Fig. 4 illustrates present embodiment, the monomer honeycomb shape in present embodiment keriotheca 2 is the polygon bodily form or cylindrical.Other composition is identical with detailed description of the invention seven or eight with connected mode.
Operation principle
When preparing connecting elements, usually realize as follows:
1, the shape of connecting elements as required, the upper carbon fiber layer 1 of preparation and lower carbon fiber layer 3 is successively pasted successively along the cross-sectional direction of connecting elements with multilayer carbon fibre initial rinse fabric, during preparation, the number of plies of the carbon fibre initial rinse fabric of upper carbon fiber layer 1 and lower carbon fiber layer 3 is generally 10 layers, multilayer carbon fibre initial rinse fabric after pasting is pushed down with upper and lower two polishing iron plates, entirety puts into vacuum bag, and vacuum high-temperature solidifies, and wherein vacuum is not less than-0.1MPa, solidification temperature 135 DEG C, hardening time 2h;
2, deviate from the iron plate of polishing up and down in step 1, obtain the upper carbon fiber layer 1 of connecting elements and lower carbon fiber layer 3;
3, according to the position of required connecting through hole 6 and size, the upper carbon fiber layer 1 in step 2 and lower carbon fiber layer 3 are punched, obtain the connecting through hole 6 on carbon fiber layer 1 and lower carbon fiber layer 3;
4, the shape of keriotheca 2 according to upper carbon fiber layer 1 and lower carbon fiber layer 3 is cut out, make the measure-alike of carbon fiber layer 1 and lower carbon fiber layer 3 on all the other;
5, punch to keriotheca 2, the position in hole is identical with the connecting through hole 6 on lower carbon fiber layer 3 with carbon fiber layer 1 upper in step 3 with size, obtains the connecting through hole 6 on keriotheca 2;
6, keriotheca 2 is connected with lower carbon fiber layer 3, adopts resin-bonded curing mode, make all positions of keriotheca 2 lower surface all with the upper surface of lower carbon fiber layer 3 by gluing bonding;
7, tubular rivet 5 is passed from the connecting through hole 6 of lower carbon fiber layer 3 and keriotheca 2;
8, tubular rivet 5 is passed from the connecting through hole 6 of upper carbon fiber layer 1, by upper carbon fiber layer 1 and the resin-bonded solidification of keriotheca 2;
9, the two ends of tubular rivet 5 are set with riveted joint grommet 4, riveted joint grommet 4 is arranged on the outside of carbon fiber layer 1 and lower carbon fiber layer 3, with riveting machine by fastening for rivet 5, riveted joint grommet 4 is closely connected with lower carbon fiber layer 3 with upper carbon fiber layer 1, the outer end of plain grinding tubular rivet 5 after riveting well, keeps the depth of parallelism and the flatness of connecting elements both sides;
10, sprayed paint in connecting elements surface, polishing, obtain final connecting elements.
Claims (9)
1. a honeycomb carbon fibre composite connector, it is characterized in that: a kind of honeycomb carbon fibre composite connector comprises carbon fiber layer (1), keriotheca (2), lower carbon fiber layer (3), two groups of riveted joints grommet (4) and multiple tubular rivet (5), upper carbon fiber layer (1), keriotheca (2) and lower carbon fiber layer (3) are affixed integral successively from top to bottom, upper carbon fiber layer (1), the upper surface of keriotheca (2) and lower carbon fiber layer (3) respectively uniform correspondence is provided with multiple connecting through hole (6), the outside of upper carbon fiber layer (1) and lower carbon fiber layer (3) is respectively equipped with one group of riveted joint grommet (4), often group riveted joint grommet (4) is provided with multiple riveted joint through hole (4-1), the position of riveted joint through hole (4-1) is corresponding with the position of connecting through hole (6), a tubular rivet (5) is fitted with respectively in each connecting through hole (6), by multiple tubular rivet (5) riveted joint between two groups of riveted joints grommet (4).
2. a kind of honeycomb carbon fibre composite connector according to claim 1, is characterized in that: the position of described multiple connecting through hole (6) is uniform is respectively arranged on carbon fiber layer (1), the edge of keriotheca (2) and lower carbon fiber layer (3) upper surface and middle part.
3. a kind of honeycomb carbon fibre composite connector according to claim 2, it is characterized in that: described often group riveted joint grommet (4) comprises external bushing ring (4-2) and inner bushing ring (4-3), external bushing ring (4-2) and inner bushing ring (4-3) are laid with multiple riveted joint through hole (4-1) respectively, external bushing ring (4-2) is arranged on the edge of carbon fiber layer (1) and lower carbon fiber layer (3), the position of the riveted joint through hole (4-1) on external bushing ring (4-2) and upper carbon fiber layer (1), the connecting through hole (6) of the edge of keriotheca (2) and lower carbon fiber layer (3) upper surface is corresponding, the position of the riveted joint through hole (4-1) on inner bushing ring (4-3) and upper carbon fiber layer (1), the connecting through hole (6) at the middle part of keriotheca (2) and lower carbon fiber layer (3) upper surface is corresponding.
4. a kind of honeycomb carbon fibre composite connector according to claim 1,2 or 3, is characterized in that: described upper carbon fiber layer (1) and lower carbon fiber layer (3) are successively to be bondd successively the upper carbon fiber layer and lower carbon fiber layer made along cross-sectional direction by multilayer carbon fibre initial rinse fabric respectively.
5. a kind of honeycomb carbon fibre composite connector according to claim 4, is characterized in that: the number of plies of the multilayer carbon fibre initial rinse fabric of described upper carbon fiber layer (1) and lower carbon fiber layer (3) is 8 layers ~ 15 layers.
6. a kind of honeycomb carbon fibre composite connector according to claim 5, is characterized in that: the thickness of every layer of carbon fibre initial rinse fabric of described upper carbon fiber layer (1) and lower carbon fiber layer (3) is 0.3mm ~ 0.8mm.
7. a kind of honeycomb carbon fibre composite connector according to claim 4, is characterized in that: described keriotheca (2) is by the keriotheca of metal, macromolecule or ceramic material.
8. a kind of honeycomb carbon fibre composite connector according to claim 7, is characterized in that: the thickness of described keriotheca (2) is 7mm ~ 13mm.
9. a kind of honeycomb carbon fibre composite connector according to claim 7 or 8, is characterized in that: the monomer honeycomb shape in keriotheca (2) is the polygon bodily form or cylindrical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520912457.XU CN205086002U (en) | 2015-11-16 | 2015-11-16 | Honeycomb carbon -fibre composite connecting piece |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520912457.XU CN205086002U (en) | 2015-11-16 | 2015-11-16 | Honeycomb carbon -fibre composite connecting piece |
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| CN205086002U true CN205086002U (en) | 2016-03-16 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201520912457.XU Expired - Fee Related CN205086002U (en) | 2015-11-16 | 2015-11-16 | Honeycomb carbon -fibre composite connecting piece |
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| CN (1) | CN205086002U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107039561A (en) * | 2017-05-18 | 2017-08-11 | 青岛三合兴华科技发展有限公司 | The preparation method of the ultralight solar cell substrate of composite |
| CN112606009A (en) * | 2020-12-09 | 2021-04-06 | 江苏集萃智能制造技术研究所有限公司 | Honeycomb interlayer lightweight structure of hydraulic quadruped robot |
| CN113799447A (en) * | 2021-09-18 | 2021-12-17 | 南通三多电子科技有限公司 | Ceramic honeycomb sandwich composite board and manufacturing method thereof |
| CN114368007A (en) * | 2022-03-22 | 2022-04-19 | 杭州博适特新材料科技有限公司 | Lightweight robot arm and preparation method thereof |
-
2015
- 2015-11-16 CN CN201520912457.XU patent/CN205086002U/en not_active Expired - Fee Related
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107039561A (en) * | 2017-05-18 | 2017-08-11 | 青岛三合兴华科技发展有限公司 | The preparation method of the ultralight solar cell substrate of composite |
| CN112606009A (en) * | 2020-12-09 | 2021-04-06 | 江苏集萃智能制造技术研究所有限公司 | Honeycomb interlayer lightweight structure of hydraulic quadruped robot |
| CN112606009B (en) * | 2020-12-09 | 2024-04-05 | 江苏集萃智能制造技术研究所有限公司 | Honeycomb interlayer lightweight structure of hydraulic four-foot robot |
| CN113799447A (en) * | 2021-09-18 | 2021-12-17 | 南通三多电子科技有限公司 | Ceramic honeycomb sandwich composite board and manufacturing method thereof |
| CN114368007A (en) * | 2022-03-22 | 2022-04-19 | 杭州博适特新材料科技有限公司 | Lightweight robot arm and preparation method thereof |
| CN114368007B (en) * | 2022-03-22 | 2022-06-24 | 杭州博适特新材料科技有限公司 | Lightweight robot arm and preparation method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20161216 Address after: 150000 room 1, unit F1, building 32-1, Xingda Road, Nangang District, Heilongjiang, Harbin Patentee after: Hou Zhiguo Address before: 150000 Songshan high tech Industrial Development Zone, Harbin hi tech innovation center, Nangang zero floor, road, room No. 410, room 5 Patentee before: HARBIN HONGXIN NC ELECTROMECHANICAL ENGINEERING CO., LTD. |
|
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160316 Termination date: 20171116 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |