CN209256910U - Robot - Google Patents
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- CN209256910U CN209256910U CN201821594818.0U CN201821594818U CN209256910U CN 209256910 U CN209256910 U CN 209256910U CN 201821594818 U CN201821594818 U CN 201821594818U CN 209256910 U CN209256910 U CN 209256910U
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Abstract
The embodiment of the present application provides a kind of robot.The embodiment of the present application robot, comprising: separately positioned fuselage and pedestal, fuselage are equipped with the first connection component, and pedestal is equipped with the second connection component that can be attached with the first connection component.The fuselage and pedestal of the embodiment of the present application robot are efficient and convenient by the first connection component and the second connection component connection disassembling, and robot is convenient in logistics transportation or after-sales service.
Description
Technical field
This application involves field of artificial intelligence more particularly to a kind of robots.
Background technique
Robot is the automatic installations for executing work.It can not only receive mankind commander, but also can run preparatory volume
The program of row, can also be according to principle program action formulated with artificial intelligence technology.Its task is to assist or replace the mankind
Work, such as production industry, construction industry, or dangerous work.
Currently, the most body of robot and pedestal are integrated designs, no matter logistics transportation or after-sales service are all compared in this way
It is more inconvenient.
Utility model content
The many aspects of the application provide a kind of robot, to solve robot logistics transportation or after-sales service not
Just the technical issues of.
The embodiment of the present application provides a kind of robot, comprising: separately positioned fuselage C and pedestal D, fuselage C are equipped with the
One connection component A, pedestal D are equipped with the second connection component B that can be attached with the first connection component A.
Further, the first connection component A is installed on the bottom of fuselage C, and the second connection component B is installed on pedestal D's
Top；The first connection component A includes rotational structure 1；The second connection component B includes fastener, the fastener packet
It includes the buckle structure snapped connection with rotational structure 1 and releases the unlocking structure snapped connection with rotational structure 1；Second connection
Component B further includes guide holder 3, and guide holder 3 is that rotational structure 1 is oriented to so that rotational structure 1 buckle structure and unlocking structure it
Between switch.
Further, the second connection component B further include: magnet iron piece 4, the first connection component A and the second connection component B connect
When connecing, rotational structure 1 is acted in rotation to the guiding stroke of guide holder 3 by 4 magnetic force of magnet iron piece.
Further, the guide holder 3 includes: that guiding bottom plate 31 and protrusion are set to guiding surface 301 on guiding bottom plate 31, rotation
Rotation structure 1 is switched between buckle structure and unlocking structure by guiding surface 301.
Further, the guiding surface 301 includes that rotational structure 1 is directed to the first guiding surface of buckle structure and is incited somebody to action
Rotational structure 1 is directed to the second guiding surface of unlocking structure.
Further, first guiding surface is two, and is oppositely arranged；Second guiding surface is two, and sets relatively
It sets, four guiding surfaces 301 surround ring-type.
Further, the fastener is linear bearing seat 2, and the middle part of linear bearing seat 2 is equipped with to be passed through for rotational structure 1
Hollow cavity 211, buckle structure and unlocking structure are set to the bottom of linear bearing seat 2.
Further, the buckle structure is the snap-in groove 221 set on the bottom of linear bearing seat 2, the unlocking structure
To be arranged set on the through slot 222 of the lower end of linear bearing seat 2, through slot 222 and the perforation of hollow cavity 211.
Further, the rotational structure 1 includes rotary shaft 11 and the positioning pin 12 being installed in rotary shaft 11, positioning pin 12
Cooperate with snap-in groove 221 and the limit of through slot 222, positioning pin 12 can protrude into through slot 222 from hollow cavity 211, positioning pin
12 after the deflection of guide holder 3 with snap-in groove 221 by that can snap connection, and positioning pin 12 is installed on the lower end of rotary shaft 11.
Further, the lower end of the rotary shaft 11 is equipped with positioning pin mounting hole 111, and positioning pin 12 is from positioning pin mounting hole
111 insertion installations, the two sides of rotary shaft 11 are stretched at the both ends of positioning pin 12.
Further, the snap-in groove 221 is V-shaped groove, and the two sides of snap-in groove 221 form the first spin canting 221a,
Positioning pin 12 can slide to the bottom of V-shaped groove along the first spin canting 221a, be snapped connection with realizing.
Further, the two sides of the through slot 222 are equipped with the second spin canting 222a being rotatably assorted with positioning pin 12, fixed
Position pin 12 slides in through slot 222 along the second spin canting 222a movement, is snapped connection with releasing.
Further, the snap-in groove 221 and through slot 222 are vertically arranged.
Further, the linear bearing seat 2 includes guide bearing 21 and the mounting disc 22 for being connected to 21 lower end of guide bearing,
Hollow cavity 211 is set on guide bearing 21, and the snap-in groove 221 and through slot 222 are set on the lower surface of mounting disc 22.
Further, the fastener is linear bearing seat 2, and the linear bearing seat 2 includes guide bearing 21 and is connected to
The mounting disc 22 of 21 lower end of guide bearing, magnet iron piece installation cavity 212 is offered on the lateral wall of guide bearing 21, and magnet iron piece 4 fills
Enter magnet iron piece installation cavity 212.
Further, the first connection component A further include: sleeve assembly, the sleeve assembly include connecting bushing 5 and set
Loaded on the reset spring 13 outside connecting bushing 5, connecting bushing 5 is hollow structure, is equipped with middle through-hole in the middle part of connecting bushing 5
51, the rotational structure 1 is installed in connecting bushing 5, the first connection component A and when the second connection component B connection, connecting bushing
5 protrude into the second connection component B, and the lower end of reset spring 13 and the second connection component B are limited.
Further, the sleeve assembly further includes top nut seat 55, supporting element 53, retaining ring 54 and steel ball 52；Rotational structure 1
The end of rotary shaft 11 be equipped with buckle cap 112, the inner sidewall of the middle through-hole 51 is equipped with and the buckle limit cooperation of cap 112
Retention bead 511, steel ball 52 are set between retention bead 511 and buckle cap 112, and retaining ring 54 is connected in rotary shaft 11, support
Part 53 is set in the top for being located at retaining ring 54 in rotary shaft 11, and top nut seat 55 is installed on the upper end of connecting bushing 5.
Further, the side wall of the rotary shaft 11 is equipped with the limiting groove being clasped with retaining ring 54, and retaining ring 54 offers
With the installation gap 541 of limiting groove installation cooperation.
Further, the retaining ring 54 is plate structure, and the middle part of retaining ring 54 is equipped with the retaining ring with the installation cooperation of rotary shaft 11
Mounting hole 501, the side wall of the retaining ring mounting hole 501 are equipped with the elastic notch 502 for increasing elasticity.
Further, the guide holder 3 is fixedly connected with linear bearing seat 2, is equipped between guide holder 3 and linear bearing seat 2
Spacer column 33.
It further, further include the first screw 34, guide holder 3 is equipped with the first screw hole with the installation cooperation of the first screw 34
311, the middle part of spacer column 33 is equipped with the spacer post holes 331 with the installation cooperation of the first screw 34, and linear bearing seat 2 is equipped with and the
Second screw hole 220 of one screw 34 installation cooperation, the first screw 34 sequentially pass through the first screw hole 311,331 and of spacer post holes
Second screw hole 220 links together guide holder 3 and linear bearing seat 2.
Further, in the telescopic cavity for being installed on the bottom fuselage C of the first connection component A, the first connection component A
On be connected with for by the first connection component A stretch out fuselage C bottom elastic element, to be connected with the second connection component B
It connects.
The fuselage and pedestal of robot are separately positioned, and the first connection component is arranged on robot fuselage, at robot bottom
The second connection component is set on seat, the first connection component can be connect with the second connection component fuselage and pedestal are connected to one
It rises, the fuselage and pedestal of the embodiment of the present application robot are fast square by the first connection component and the second connection component connection disassembling
Just, robot is convenient in logistics transportation or after-sales service.
Detailed description of the invention
The drawings described herein are used to provide a further understanding of the present application, constitutes part of this application, this Shen
Illustrative embodiments and their description please are not constituted an undue limitation on the present application for explaining the application.In the accompanying drawings:
Fig. 1 is the structural schematic diagram that the application exemplary embodiment robot fuselage and pedestal link together；
Structural schematic diagram when Fig. 2 is the application exemplary embodiment robot fuselage and pedestal unlock；
Fig. 3 is the structural schematic diagram after the application exemplary embodiment robot fuselage and pedestal unlock；
Fig. 4 is that the first connection component of the application exemplary embodiment and the second connection component are in the signal snapped connection
Figure；
Fig. 5 is the bottom view of Fig. 4；
Fig. 6 is the structural representation in the first connection component of the application exemplary embodiment and the second connection component unlocking process
Figure；
Fig. 7 is the bottom view of Fig. 6；
Fig. 8 is the structural schematic diagram after the first connection component of the application exemplary embodiment and the unlock of the second connection component；
Fig. 9 is the bottom view of Fig. 8；
When Figure 10 is that the first connection component of the application exemplary embodiment and the second connection component connect, positioning pin rotate to
The structural schematic diagram of corresponding position；
Figure 11 is the bottom view of Figure 10；
Figure 12 is the structural representation of the first connection component of the application exemplary embodiment and the second connection component connection procedure
Figure；
Figure 13 is the bottom view of Figure 12；
Figure 14 is the schematic perspective view after the connection of the application exemplary embodiment connection structure；
Figure 15 is the exploded view of the application exemplary embodiment connection structure；
Figure 16 is the structural schematic diagram of the application exemplary embodiment guide holder；
Figure 17 is the structural schematic diagram of the application exemplary embodiment linear bearing seat；
Figure 18 is the structural schematic diagram in another orientation of the application exemplary embodiment linear bearing seat；
Figure 19 is the exploded view of the application exemplary embodiment rotational structure；
Figure 20 is the structural schematic diagram of the application exemplary embodiment connecting bushing；
Figure 21 is the structural schematic diagram of the application exemplary embodiment retaining ring；
Figure 22 is the exploded view of the second connection component of the application exemplary embodiment；
Figure 23 is the sectional view of the first connection component of the application exemplary embodiment；
Figure 24 is the sectional view of the second connection component of the application exemplary embodiment；
Figure 25 is the schematic cross-section that the application exemplary embodiment positioning pin is deflected by magnet iron piece suction.
Specific embodiment
To keep the purposes, technical schemes and advantages of the application clearer, below in conjunction with the application specific embodiment and
Technical scheme is clearly and completely described in corresponding attached drawing.Obviously, described embodiment is only the application one
Section Example, instead of all the embodiments.Based on the embodiment in the application, those of ordinary skill in the art are not doing
Every other embodiment obtained under the premise of creative work out, shall fall in the protection scope of this application.
For existing robot in logistics transportation or the technical problem of after-sales service inconvenience, the embodiment of the present application is provided
A kind of robot, basic ideas are: the fuselage and pedestal of robot are separately positioned, and the first connection group is arranged on robot fuselage
Part, is arranged the second connection component on robot base, and the first connection component can be connect with by fuselage with the second connection component
It links together with pedestal, the fuselage and pedestal of the embodiment of the present application robot pass through the first connection component and the second connection component
Connection disassembling is efficient and convenient, and robot is convenient in logistics transportation or after-sales service.
It should be noted that the connection structure of each embodiment of the application is not limited in the connection of robot architecture, fit
Between the object that any two for that can connect with this structure need to be attached.
Below in conjunction with attached drawing, the technical scheme provided by various embodiments of the present application will be described in detail by taking robot as an example.
It should also be noted that identical label indicates same object in following attached drawing and embodiment, therefore, once it is a certain
Object is defined in an attached drawing, then in subsequent attached drawing does not need that it is further discussed.
Fig. 1-3 is the structural schematic diagram that the embodiment of the present application robot uses connection structure to be attached.In conjunction with Fig. 1-3,
The robot includes: fuselage C, pedestal D and connection structure, and connection structure includes the first connection component A and the second connection component B,
First connection component A is fixedly connected on fuselage C, and the second connection component B is fixedly connected on pedestal D.The embodiment of the present application machine
The fuselage and pedestal of device people is separately positioned, and the first connection component is arranged on robot fuselage, and is arranged on robot base
Two connection components, the first connection component can be connect with the second connection component fuselage and pedestal to link together, the application
The fuselage and pedestal of embodiment robot are efficient and convenient by the first connection component and the second connection component connection disassembling, robot
It is convenient in logistics transportation or after-sales service
In the present embodiment, in conjunction with Figure 15, the robot further include: the second screw 37 and third screw 38, first are fixed
Plate 7 and the second fixed plate 8, the first connection component A are fixed on the first connecting plate 7 of the bottom fuselage C by the second screw 37；
Second connection component B is fixed on the second connecting plate 8 at the top of pedestal D by third screw 38.First connection component A and second
Connection component B is connect with fuselage C and pedestal D respectively by screw, and fixed structure is reliable and stable.The bottom pedestal D is also equipped with cunning
E is taken turns, robot is moved freely and gets to target position.When the present embodiment robot is installed, mobile fuselage C is needed
Or pedestal, so that after the first connection component A on fuselage C is aligned with the second connection component B on pedestal D, then carry out first
The connection of connection component A and the second connection component B.
In another embodiment, in the telescopic cavity for being installed on the bottom fuselage C of the first connection component A, the first connection
Be connected on component A for by the first connection component A stretch out fuselage C bottom elastic element, with the second connection component B into
Row connection.When the present embodiment robot is installed, since fuselage C is heavier, fuselage C is first moved to the upper surface pedestal D side,
Then it is translated to the middle part of pedestal D, the first connection component A is retracted in the cavity of the bottom fuselage C, when the first connection component A is mobile
When to the second connection component B face, the first connection component A is stretched out by the effect of elastic element elastic force to carry out with the second connection component B
Connection.
In the above-described embodiments, the connection type of the first connection component A and fuselage C, the second connection component B and pedestal D
Connection type also can be used in addition to above-mentioned screw connecting mode and snap connection.First fixed plate 7, second shown in Figure 15 is solid
Fixed board 8 is the partial schematic diagram of the respective face of fuselage C and pedestal D.In addition, the first connection component A and the second connection component B can
To be interchangeable, it is also able to achieve above-mentioned function.
The scene being likely encountered below makes an explanation to the application robot:
When robot needs to transport, the connection relationship of the first connection component A and the second connection component of robot is released,
Fuselage C and pedestal D are dismantled, transport can be sorted out, reduces volume shared by robot.
When robot base or fuselage are damaged, fuselage C and pedestal D can be dismantled, only broken parts be taken to go to tie up
It repairs, uses manpower and material resources sparingly.
Present application example provides a kind of installation method of robot:
First A robot, connection component robot is installed on to the bottom of fuselage robot C robot；
Second B robot, connection component robot is installed on to the top of D robot, pedestal robot；
Fuselage robot C robot or D robot, pedestal robot are moved by the first A robot, connection component robot
It is attached with after the alignment of the second B robot, connection component robot, by fuselage robot C robot and pedestal robot D
Robot links together.
Above-mentioned installation method is based on aforementioned each robotic embodiment, therefore the robot installation method has and above-mentioned machine
The identical technical effect of people's embodiment, details are not described herein.
After being aligned in conjunction with Fig. 1-3 fuselage C with the first connection component robot A of pedestal D and the second connection component robot B
When being snapped connection, fuselage C is pressed down on, fuselage C and pedestal D pass through the first connection component A and the second connection component B card
Button links together, and when fuselage C and pedestal D needs to dismantle, fuselage C is pressed down on, the connection of the first connection component A and second
Component B releases snapping relationship, and fuselage C is mutually disengaged with pedestal D.Tool about the first connection component A and the second connection component B
The catenation principle of body is explained in detail in the following embodiments.
Fig. 1-3 is only illustrated by taking humanoid robot as an example, and the type of the robot in the embodiment of the present application is not limited to
Humanoid robot can be in all types of robots for can be used the connection structure.The connection structure is also not limited to this
In robot.
Figure 14 is the assembling schematic diagram of the embodiment of the present application connection structure, and Figure 15 is point of the embodiment of the present application connection structure
Xie Tu.It is explained in detail below with reference to Figure 14,15 pairs of the embodiment of the present application connection structures.
As shown in figs. 14-15, which includes the first connection component A and can snap connection with the first connection component A
The second connection component B；First connection component A includes rotational structure 1；Second connection component B includes fastener, fastener packet
It includes the buckle structure snapped connection with rotational structure 1 and releases the unlocking structure snapped connection with rotational structure 1；Second connection group
Part B further includes guide holder 3, and guide holder 3 is that rotational structure 1 is oriented to so that rotational structure 1 buckle structure and unlocking structure it
Between switch.
Rotational structure, the setting of the second connection component and rotation is arranged in first connection component of the embodiment of the present application connection structure
The fastener that structure is cooperated, and be arranged on fastener the buckle structure snapped connection with rotational structure and with rotational structure solution
The unlocking structure of lock also sets up guide holder on the second connection component, can be oriented to for rotational structure so that rotational structure and card
Buckle structure and unlocking structure cooperation, the first connection component and the second connection component connection disassembling are efficient and convenient, connection structure it is whole
Body is simple and compact for structure.
Figure 15 is the decomposition diagram of the embodiment of the present application connection structure.First connection component A further include: sleeve assembly,
Sleeve assembly includes connecting bushing 5 and the reset spring 13 that is set in connecting bushing 5 outside, and connecting bushing 5 is hollow structure, company
5 middle part of spindle set is equipped with middle through-hole 51, and rotational structure 1 is installed in connecting bushing 5, the connection of the first connection component A and second
When component B connection, connecting bushing 5 is protruded into the second connection component B, and the lower end of reset spring 13 and the second connection component B are limited,
When first connection component A is acted to the second connection component B, 13 compressed energy-storage of reset spring.
In conjunction with Figure 23, the structure of the sleeve assembly of the embodiment of the present application is illustrated.The sleeve assembly further includes upper spiral shell
Base 55, supporting element 53, the end of the rotary shaft 11 of 52 rotational structure 1 of retaining ring 54 and steel ball are equipped with buckle cap 112, middle through-hole
51 inner sidewall is equipped with the retention bead 511 with the buckle limit cooperation of cap 112, and retaining ring 54 is connected in rotary shaft 11, supporting element
53 are set in the top for being located at retaining ring 54 in rotary shaft 11, and top nut seat 55 is installed on the upper end of connecting bushing 5.
In the above-described embodiments, the inner sidewall of middle through-hole 51 is equipped with the retention bead with the buckle limit cooperation of cap 112
511, retention bead 511 is used for the distance that rotary limited axis 11 moves down, and in the lower section of rotary shaft 11, retaining ring 54 is arranged in clamping,
Retaining ring 54 is used for the distance that rotary limited axis 11 moves up, retention bead 511 and retaining ring 54 for rotary limited axis 11
Bottom offset enables rotary shaft 11 in the rotary motion of 5 internal stability of connecting bushing.
Figure 19 is the structural schematic diagram of the embodiment of the present application rotational structure.The rotational structure 1 includes rotary shaft 11 and installation
In the positioning pin 12 in rotary shaft 11, positioning pin 12 and snap-in groove 221 and through slot 222, positioning pin 12 can be from hollow cavity
211 protrude into through slot 222, and positioning pin 12 can snap connection after being deflected by guide holder 3 with snap-in groove 221, and positioning pin 12 is pacified
Lower end loaded on rotary shaft 11.
In the present embodiment, the lower end of rotary shaft 11 is equipped with positioning pin mounting hole 111, and positioning pin 12 is from positioning pin mounting hole
111 insertion installations, the two sides of rotary shaft 11 are stretched at the both ends of positioning pin 12.When installation, positioning pin 12 is from positioning pin mounting hole 111
Mounting hole is packed into.In order to which the installation of the positioning pin 12 made is reliable and stable, positioning pin 12 and positioning pin mounting hole 111 can be used
It is full of cooperation, it can also be using connection types such as welding.
Figure 21 is 54 structural schematic diagram of the embodiment of the present application retaining ring.The retaining ring 54 is plate structure, and the middle part of retaining ring 54 is set
There is the retaining ring mounting hole 501 with the installation cooperation of rotary shaft 11, the side wall of rotary shaft 11 is equipped with the limit being clasped with retaining ring 54
Groove, retaining ring 54 offer the installation gap 541 with limiting groove installation cooperation, and limiting groove and the limit of installation gap 541 are matched
It closes, retaining ring 54 and the mounting structure of rotary shaft 11 are reliable and stable.The elasticity that the side wall of retaining ring mounting hole 501 is equipped with increase elasticity lacks
Mouth 502.Elastic notch 502 increases the elasticity of retaining ring 54, is caught in rotary shaft 11 so that retaining ring 54 is more convenient.
Figure 16 is the structural schematic diagram of the embodiment of the present application guide holder 3.The guide holder 3 includes: guiding bottom plate 31 and protrusion
The guiding surface 301 on guiding bottom plate 31, rotational structure 1 is by guiding surface 301 between buckle structure and unlocking structure
Switching.Guide holder it is simple and compact for structure, it is easy to process.
As shown in figure 16, guiding surface 301 includes that rotational structure 1 is directed to the first guiding surface of buckle structure and is incited somebody to action
Rotational structure 1 is directed to the second guiding surface of unlocking structure.First guiding surface is two, and is oppositely arranged；Second guiding
Inclined-plane is two, and is oppositely arranged, and four guiding surfaces 301 surround ring-type.The guiding surface 301 of the present embodiment guide holder uses
Symmetrical structure setting, it is easy to process, in addition, four guiding surfaces 301 of setting are more reliable and more stable to the guiding of rotational structure.
Obviously, guiding surface 301 can be two, and two adjacent guiding surfaces 301 are arranged, i.e., oblique by a guiding respectively
Face 301 is that rotational structure 1 is oriented between buckle structure and unlocking structure.
Figure 17,18 be the embodiment of the present application fastener different direction structural schematic diagram.In the present embodiment, fastener is
Linear bearing seat 2, the middle part of linear bearing seat 2 are equipped with the hollow cavity 211 passed through for rotational structure 1, buckle structure and unlock
Structure is set to the bottom of linear bearing seat 2.When installation, rotational structure 1 is protruded into hollow cavity 211, and one end of rotational structure 1 is stretched
Cooperate to the bottom of linear bearing seat 2 and the movement of buckle structure and unlocking structure.Fastener is not limited to above-mentioned linear bearing seat
2, it can also be other structures, can be component, or single structure part.
As shown in Figure 17,18, the embodiment of a linear bearing seat is provided, linear bearing seat is not limited thereto structure.
Linear bearing seat 2 includes guide bearing 21 and the mounting disc 22 for being connected to 21 lower end of guide bearing, and the middle part of guide bearing 21 is set
There is the hollow cavity 211 passed through for rotational structure 1, buckle structure is the snap-in groove 221 set on the bottom of linear bearing seat 2,
Unlocking structure is the through slot 222 set on the lower end of linear bearing seat 2, and through slot 222 and the perforation of hollow cavity 211 are arranged, buckle recessed
Slot 221 and through slot 222 are set to the lower surface of mounting disc 22.When installation, buckle structure passes through in the middle part of hollow cavity 211, stretches to
The bottom of linear bearing seat 2 is cooperated with snap-in groove 221 and through slot 222.
As shown in figure 18, in the above-described embodiments, snap-in groove 221 is V-shaped groove, and the two sides of snap-in groove 221 form the
One spin canting 221a, positioning pin 12 can slide to the bottom of V-shaped groove along the first spin canting 221a, be snapped connection with realizing.
The two sides of through slot 222 are equipped with the second spin canting 222a being rotatably assorted with positioning pin 12, and positioning pin 12 is along the first spin canting
221a movement slides in through slot 222, is snapped connection with releasing.The embodiment of the present application snap-in groove 221 is set as V-shaped groove, buckle
The two sides of groove 221 are respectively formed the first spin canting 221a and the second spin canting 222a.When positioning pin 12 is fallen in V-shaped groove
When, movement can rotate positioning pin 12 along the first spin canting 221a upwards, and the bottom for finally sliding to V-shaped groove snaps connection, when fixed
When position pin 12 falls within the second spin canting 222a, movement can rotate positioning pin 12 along the second spin canting 222a upwards, final sliding
To through slot 222, positioning pin 12 is snapped connection with the releasing of linear bearing seat 2.
In the embodiment of the present application, snap-in groove 221 and through slot 222 are arranged at an angle, it is preferable that snap-in groove 221
It is vertically arranged with through slot 222.When snap-in groove 221 and through slot 222 are vertically arranged, more conducively integrally-built optimization design.
Figure 22 is the structural schematic diagram that the embodiment of the present application guide holder is connected with linear bearing seat.In the present embodiment, it leads
It is fixedly connected to seat 3 with linear bearing seat 2, and is equipped with spacer column 33 between guide holder 3 and linear bearing seat 2.Spacer column 33 is protected
Linear bearing seat 2 is demonstrate,proved at a distance from guide holder 3.
Further, the second connection component B further includes the first screw 34, and guide holder 3 is equipped with matches with the installation of the first screw 34
The first screw hole 311 closed, the middle part of spacer column 33 are equipped with the spacer post holes 331 with the installation cooperation of the first screw 34, linear axis
It holds seat 2 and is equipped with the second screw hole 220 cooperated with the installation of the first screw 34, the first screw 34 sequentially passes through the first screw hole
311, spacer post holes 331 and the second screw hole 220 link together guide holder 3 and linear bearing seat 2.The present embodiment uses two
A spacer column 33 is individually directed the two sides of seat 3.Obviously, spacer column 33 can also using it is single or more.It, will be every when installation
One end of sleeve column 33 is installed in the first screw hole 311 of guide holder 3, and the other end of spacer column 33 is installed on linear bearing seat 2
The second screw hole 220 in, the first screw 34 sequentially passes through the first screw hole 311, spacer post holes 331 and the second screw hole 220
Guide holder 3 and linear bearing seat 2 are linked together.Obviously, the connection type of guide holder and linear bearing seat, can also be with other
Connection type.
The installation process of the above embodiments of the present application connection structure is illustrated with reference to the accompanying drawing:
The installation process of first connection component A: as shown in figure 15, steel ball 52 is first put into the retention bead of connecting bushing 5
On 511；Then, rotary shaft 11 is put into middle through-hole 51 from the upper end of connecting bushing 5, the buckle cap 112 of rotary shaft 11 with
The inner sidewall retention bead 511 of middle through-hole 51 limits, and steel ball 52 is located at 112 lower section of buckle cap, reduces force of rolling friction, card
Deduction cap 112 limits rotary shaft 11 and moves down, and supporting element 53 is set in rotary shaft 11 from 11 lower end of rotary shaft, and retaining ring 54 blocks
It is connected in the limiting groove of rotary shaft 11, limitation rotary shaft 11 moves up；As shown in figure 19, positioning pin 12 is installed on rotary shaft
Rotational structure is formed in the positioning pin mounting hole 111 of 11 lower end；As shown in figure 15, then by 55 company of being installed on of top nut seat
The top of spindle set 5, reset spring 13 is set on connecting bushing 5, and one end of reset spring 13 and top nut seat 55 are fixed
Connection.
The installation process of second connection component B: as shown in figure 22, one end of spacer column 33 is installed on the of guide holder 3
In one screw hole 311, the other end of spacer column 33 is installed in the second screw hole 220 of linear bearing seat 2, the first screw 34 according to
It is secondary to pass through the first screw hole 311, spacer post holes 331 and the second screw hole 220 guide holder 3 and linear bearing seat 2 are connected to one
It rises.
The specific action process of the above embodiments of the present application connection structure is illustrated with reference to the accompanying drawing:
1, as shown in Figure 4,5, the structural schematic diagram to link together for the first connection component A and the second connection component B.
2, as shown in Figure 6,7, when the first connection component A and the second connection component B needs to disassemble, press down on first
Connection component A, positioning pin 12 are fallen on the second guiding surface, under the guiding of the second guiding surface, positioning pin 12 rotation as
On unlocking structure corresponding position.
3, as shown in Figure 8,9, stop the first reset bullet of connection component A, the first connection component A in reset spring 13 of pressing
It is acted upwards under the action of power, movement continues to deflect positioning pin 12 along the second spin canting 222a upwards, finally slides to logical
In slot 222, releasing is snapped connection, and the first connection component A and the second connection component B connect relationship.
4, as shown in Figure 12,13, when the first connection component A and the second connection component B needs to connect, positioning pin 12 is revolved
The relative position of the first guiding surface is gone to, the first connection component A, guiding of the positioning pin 12 in the first guiding surface are pressed down on
Under effect, rotation to position corresponding with buckle structure stops the first connection component A, the first connection component A of pressing and is resetting bullet
It is acted upwards under the action of the reseting elasticity of spring 13, movement continues to occur partially positioning pin 12 along the first spin canting 221a upwards
Turn, slide to the bottom of V-shaped groove, is snapped connection with realizing, the first connection component A and the second connection component B link together.
In the above embodiments, the first connection component A and when the second connection component B connection, needs to revolve positioning pin 12
Go to on the first guiding surface.The structural schematic diagram of Figure 15 the application another exemplary embodiment connection structure, the connection
Structure on the basis of the above embodiments, adds magnet iron piece 4, the connection of the first connection component A and second on the second connection component B
When component B connection, rotational structure 1 is acted in rotation to the guiding stroke of guide holder 3 by 4 magnetic force of magnet iron piece.
It is worth noting that when above-described embodiment connection structure, the first connection component A and the second connection component B connection,
Rotational structure 1 is acted in the guiding stroke for being automatically rotated to guide holder 3 by 4 magnetic force of magnet iron piece, without artificially to rotational structure
It is presetting with the position progress of guiding surface, greatly improve the joint efficiency and success rate of connection structure.
Figure 17 is the embodiment of the present application magnet iron piece 4 and the structural schematic diagram that linear bearing seat 2 is installed.In the present embodiment,
Magnet iron piece 4 is installed on the lower end of the guide bearing 21 of linear bearing seat 2.Magnet iron piece peace is offered on the lateral wall of guide bearing 21
It behave affectedly 212, magnet iron piece 4 is packed into magnet iron piece installation cavity 212.When installation, magnet iron piece 4 is packed into magnet from the lateral wall of guide bearing 21
In part installation cavity 212, installation process is simple and fast.Obviously, magnet iron piece 4 can be set in the other positions of linear bearing seat 2,
Such as be set in the mounting disc 22 of linear bearing seat 2, the fixed form of magnet iron piece 4 and linear bearing seat 2 can also be with straight line
Bearing block 2 is fixedly connected, for example, magnet iron piece 4 can linear bearing seat 2 be molded when sealing inside linear bearing seat 2.
As shown in figure 25, the schematic cross-section to be deflected for the embodiment of the present application positioning pin 12 by 4 suction of magnet iron piece.Knot
Figure 10,11 are closed, in the first connection component A and the second connection component B connection, positioning pin 12 deflects close to magnet iron piece 4,
In the rotation to the line of two pieces of magnet iron pieces 4 of positioning pin 12.Wherein, there are mutually matched positions between guide holder 3 and magnet iron piece 4
Relationship, so that in the rotation to the first guiding surface of guide holder 3 of positioning pin 12.
Illustrate the specific action process of another embodiment connection structure of the application with reference to the accompanying drawing:
1, as shown in Figure 4,5, the structural schematic diagram to link together for the first connection component A and the second connection component B.
2, as shown in Figure 6,7, when the first connection component A and the second connection component B needs to disassemble, press down on first
Connection component A, positioning pin 12 are fallen on the second guiding surface, under the guiding of the second guiding surface, positioning pin 12 rotation as
On unlocking structure corresponding position.
3, as shown in Figure 8,9, stop the first reset bullet of connection component A, the first connection component A in reset spring 13 of pressing
It is acted upwards under the action of power, movement continues to deflect positioning pin 12 along the second spin canting 222a upwards, finally slides to logical
In slot 222, releasing is snapped connection, and the first connection component A and the second connection component B connect relationship.
4, as shown in Figure 10,11, when the first connection component A and the second connection component B needs to connect, positioning pin 12 is close
Magnet iron piece 4 deflects, in the rotation to the line of two pieces of magnet iron pieces 4 of positioning pin 12, the rotation of positioning pin 12 to the first guiding surface
Corresponding position on.
5, as shown in Figure 12,13, the first connection component A is pressed down on, positioning pin 12 is made in the guiding of the first guiding surface
Under, rotation to position corresponding with buckle structure stops the first connection component A of pressing, and the first connection component A is in reset spring
It being acted upwards under the action of 13 reseting elasticity, movement continues to deflect positioning pin 12 along the first spin canting 221a upwards,
The bottom of V-shaped groove is slided to, is snapped connection with realizing, the first connection component A and the second connection component B link together.
The above is only embodiments herein, are not intended to limit this application.To those skilled in the art,
Various changes and changes are possible in this application.It is all within the spirit and principles of the present application made by any modification, equivalent replacement,
Improve etc., it should be included within the scope of the claims of this application.
Claims (22)
1. a kind of robot characterized by comprising separately positioned fuselage (C) and pedestal (D), fuselage (C) are equipped with first
Connection component (A), pedestal (D) are equipped with the second connection component (B) that can be attached with the first connection component (A).
2. robot according to claim 1, which is characterized in that
First connection component (A) is installed on the bottom of fuselage (C), and the second connection component (B) is installed on the top of pedestal (D)
Portion；Robot
First connection component (A) includes rotational structure (1)；
Second connection component (B) includes fastener, and the fastener includes the buckle knot snapped connection with rotational structure (1)
Structure and the unlocking structure snapped connection with rotational structure (1) releasing；
Second connection component (B) further includes guide holder (3), and guide holder (3) is rotational structure (1) guiding, so that rotational structure (1)
Switch between buckle structure and unlocking structure.
3. robot according to claim 2, which is characterized in that second connection component (B) further include: magnet iron piece
(4), when the first connection component (A) and the second connection component (B) connect, rotational structure (1) is revolved by the effect of magnet iron piece (4) magnetic force
It goes in the guiding stroke of guide holder (3).
4. robot according to claim 2 or 3, which is characterized in that the guide holder (3) includes: guiding bottom plate (31)
It is set to guiding surface (301) in guiding bottom plate (31) with protrusion, rotational structure (1) is by guiding surface (301) in buckle structure
Switch between unlocking structure.
5. robot according to claim 4, which is characterized in that the guiding surface (301) includes by rotational structure (1)
It is directed to the first guiding surface of buckle structure and rotational structure (1) is directed to the second guiding surface of unlocking structure.
6. robot according to claim 5, which is characterized in that first guiding surface is two, and is oppositely arranged；
Second guiding surface is two, and is oppositely arranged, and four guiding surfaces (301) surround ring-type.
7. robot according to claim 2 or 3, which is characterized in that the fastener is linear bearing seat (2), straight line
The middle part of bearing block (2) is equipped with the hollow cavity (211) passed through for rotational structure (1), and buckle structure and unlocking structure are set to straight
The bottom of line bearing block (2).
8. robot according to claim 7, which is characterized in that the buckle structure is set on linear bearing seat (2)
The snap-in groove (221) of bottom, the unlocking structure are the through slot (222) set on the lower end of linear bearing seat (2), through slot
(222) it is arranged with hollow cavity (211) perforation.
9. robot according to claim 8, which is characterized in that the rotational structure (1) includes rotary shaft (11) and peace
Loaded on the positioning pin (12) on rotary shaft (11), positioning pin (12) and snap-in groove (221) and through slot (222) limit cooperate, fixed
Position pin (12) can be protruded into from hollow cavity (211) in through slot (222), and positioning pin (12) can be with after being deflected by guide holder (3)
Snap-in groove (221) snaps connection, and positioning pin (12) is installed on the lower end of rotary shaft (11).
10. robot according to claim 9, which is characterized in that pacify equipped with positioning pin the lower end of the rotary shaft (11)
It fills hole (111), positioning pin (12) is inserted into from positioning pin mounting hole (111) and installs, and rotary shaft is stretched at the both ends of positioning pin (12)
(11) two sides.
11. robot according to claim 9, which is characterized in that the snap-in groove (221) is V-shaped groove, snap-in groove
(221) two sides form the first spin canting (221a), and positioning pin (12) can slide to V-shaped groove along the first spin canting (221a)
Bottom, with realize snap connection.
12. robot according to claim 9, which is characterized in that the two sides of the through slot (222) are equipped with and positioning pin
(12) the second spin canting (222a) being rotatably assorted, positioning pin (12) slide to through slot along the second spin canting (222a) movement
(222) it in, is snapped connection with releasing.
13. robot according to claim 8, which is characterized in that the snap-in groove (221) and through slot (222) are vertical
Setting.
14. robot according to claim 9, which is characterized in that the linear bearing seat (2) includes guide bearing (21)
With the mounting disc (22) for being connected to guide bearing (21) lower end, hollow cavity (211) is set on guide bearing (21), the buckle
Groove (221) and through slot (222) are set to the lower surface of mounting disc (22).
15. robot according to claim 3, which is characterized in that the fastener is linear bearing seat (2), described straight
Line bearing block (2) includes guide bearing (21) and the mounting disc (22) for being connected to guide bearing (21) lower end, guide bearing (21)
Lateral wall on offer magnet iron piece installation cavity (212), magnet iron piece (4) be packed into magnet iron piece installation cavity (212).
16. robot according to claim 2 or 3, which is characterized in that first connection component (A) further include: axle sleeve
Component, the sleeve assembly include connecting bushing (5) and the reset spring (13) for being set in connecting bushing (5) outside, connecting shaft
Covering (5) is hollow structure, is equipped with middle through-hole (51) in the middle part of connecting bushing (5), the rotational structure (1) is installed on connecting bushing
(5) in, when the first connection component (A) and the second connection component (B) connect, connecting bushing (5) protrudes into the second connection component (B)
Interior, the lower end of reset spring (13) and the second connection component (B) are limited.
17. robot according to claim 16, which is characterized in that the sleeve assembly further include top nut seat (55),
Supporting element (53), retaining ring (54) and steel ball (52)；The end of the rotary shaft (11) of rotational structure (1) is equipped with buckle cap (112), institute
The inner sidewall for stating middle through-hole (51) is equipped with the retention bead (511) cooperated with buckle cap (112) limit, and steel ball (52) is set to limit
Between position raised (511) and buckle cap (112), retaining ring (54) is connected on rotary shaft (11), and supporting element (53) is set in rotation
It is located at the top of retaining ring (54) on axis (11), top nut seat (55) is installed on the upper end of connecting bushing (5).
18. robot according to claim 17, which is characterized in that the side wall of the rotary shaft (11) is equipped with and retaining ring
(54) limiting groove being clasped, retaining ring (54) offer the installation gap (541) with limiting groove installation cooperation.
19. robot according to claim 18, which is characterized in that the retaining ring (54) is plate structure, retaining ring (54)
Middle part be equipped with the retaining ring mounting hole (501) with rotary shaft (11) installation cooperation, the side wall of the retaining ring mounting hole (501) is equipped with
Increase the elastic notch (502) of elasticity.
20. robot according to claim 7, which is characterized in that the guide holder (3) and linear bearing seat (2) are fixed
Connection is equipped with spacer column (33) between guide holder (3) and linear bearing seat (2).
21. robot according to claim 20, which is characterized in that further include the first screw (34), guide holder is set on (3)
There is the first screw hole (311) with the first screw (34) installation cooperation, the middle part of spacer column (33) is equipped with and the first screw (34)
The spacer post holes (331) of cooperation is installed, linear bearing seat (2) is equipped with the second screw hole with the first screw (34) installation cooperation
(220), the first screw (34) sequentially passes through the first screw hole (311), spacer post holes (331) and the second screw hole (220) and will lead
It links together to seat (3) and linear bearing seat (2).
22. robot according to claim 2, which is characterized in that first connection component (A) is telescopic to be installed on
In the cavity of the bottom fuselage (C), it is connected on the first connection component (A) for the first connection component (A) to be stretched out fuselage (C)
The elastic element of bottom, to be attached with the second connection component (B).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821594818.0U CN209256910U (en) | 2018-09-28 | 2018-09-28 | Robot |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821594818.0U CN209256910U (en) | 2018-09-28 | 2018-09-28 | Robot |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209256910U true CN209256910U (en) | 2019-08-16 |
Family
ID=67553311
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821594818.0U Active CN209256910U (en) | 2018-09-28 | 2018-09-28 | Robot |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209256910U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110962107A (en) * | 2018-09-28 | 2020-04-07 | 科沃斯商用机器人有限公司 | Robot and mounting method |
| CN112975903A (en) * | 2019-12-16 | 2021-06-18 | 科沃斯商用机器人有限公司 | Connecting piece, coupling mechanism and intelligent robot |
-
2018
- 2018-09-28 CN CN201821594818.0U patent/CN209256910U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110962107A (en) * | 2018-09-28 | 2020-04-07 | 科沃斯商用机器人有限公司 | Robot and mounting method |
| CN112975903A (en) * | 2019-12-16 | 2021-06-18 | 科沃斯商用机器人有限公司 | Connecting piece, coupling mechanism and intelligent robot |
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