CN204159813U - A kind of controlled pause device of rivet driver - Google Patents

A kind of controlled pause device of rivet driver Download PDF

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Publication number
CN204159813U
CN204159813U CN201420604762.8U CN201420604762U CN204159813U CN 204159813 U CN204159813 U CN 204159813U CN 201420604762 U CN201420604762 U CN 201420604762U CN 204159813 U CN204159813 U CN 204159813U
Authority
CN
China
Prior art keywords
main shaft
cross bar
fuselage
pin
axle sleeve
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.)
Withdrawn - After Issue
Application number
CN201420604762.8U
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Chinese (zh)
Inventor
管伟东
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZHEJIANG HAOGUO FURNITURE Co Ltd
Original Assignee
ZHEJIANG HAOGUO FURNITURE Co Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by ZHEJIANG HAOGUO FURNITURE Co Ltd filed Critical ZHEJIANG HAOGUO FURNITURE Co Ltd
Priority to CN201420604762.8U priority Critical patent/CN204159813U/en
Application granted granted Critical
Publication of CN204159813U publication Critical patent/CN204159813U/en
Withdrawn - After Issue legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

A controlled pause device for rivet driver, comprising fuselage and the main shaft for driving rivet driver to run, comprising and being rotationally connected by axle the cross bar be arranged in fuselage, one end of described cross bar arranges pedal, and the other end arranges extension spring; Described cross bar arranges on extension spring one end and connects stretching bar again, described stretching bar connects the connecting rod be piercing in outside fuselage, described connecting rod is fixedly connected with the second cross bar again, second cross bar connects on the relative other end of connecting rod at it and connects pin, described second cross bar is connected on fuselage by being rotationally connected the second rotating shaft, corresponding pin position arranges axle sleeve with described main shaft, and described axle sleeve follows spindle synchronous rotation through axle sleeve to propping up on main shaft by bolt; Described pin can be close to axle sleeve while pedal rises to range, and is stoped the rotation of main shaft by bolt blocks.This device can control the time of time-out with the custom of operating personnel, and simple to operate, suspends sensitivity strong, also can not injure machine shaft.

Description

A kind of controlled pause device of rivet driver
Technical field
The utility model relates to rivet make-up machinery field, especially for the rivet driver of the products such as the assembling chair back.
Background technology
Rivet refers in riveted joint, and utilize self-deformation or interference to connect by the part of riveting parts, it utilizes the magnitude of interference of rivet and lock body opening to rivet.And operating personnel again practical operation rivet driver carry out beat rivet work time, one as the products such as the chair back complete riveter nail step after, need change the chair back, repeat beat rivet work, the time changed in the middle of this is very short, but also required time differs according to the quantity situation of different operating personnel.The general switched electronic device that arranges stops to control motor or opens; but this extremely bothers, and motor also needs 1-2 time second from starting to normal operation, and this time may enough change chair back product; and the frequent start-stop of motor, larger to the loss ratio of motor.
Utility model content
The purpose of this utility model solves the problems of the technologies described above, and provides a kind of pause device controlled to rivet driver.
Technical solution of the present utility model is: a kind of controlled pause device of rivet driver, comprise fuselage and the main shaft for driving rivet driver to run, comprise and be rotationally connected by axle the cross bar be arranged in fuselage, one end of described cross bar arranges pedal, and the other end arranges extension spring; Described cross bar arranges on extension spring one end and connects stretching bar again, described stretching bar connects the connecting rod be piercing in outside fuselage, described connecting rod is fixedly connected with the second cross bar again, second cross bar connects on the relative other end of connecting rod at it and connects pin, described second cross bar is connected on fuselage by being rotationally connected the second rotating shaft, corresponding pin position arranges axle sleeve with described main shaft, and described axle sleeve follows spindle synchronous rotation through axle sleeve to propping up on main shaft by bolt; Described pin can be close to axle sleeve while pedal rises to range, and is stoped the rotation of main shaft by bolt blocks.
Operating personnel are when changing the product needing riveter to follow closely, and need machine to suspend for a moment, whole event is ofer short duration; if it is cumbersome to go shutdown to start shooting specially again; so a design pause device, under non-stop-machine state, change product for operating personnel, accelerate operating efficiency.
As preferably, described pin is rotationally connected with the base plate be arranged on fuselage by turning cylinder, the position that described second cross bar is fixedly connected with pin is positioned at the side of turning cylinder, and the other end of pin can enter into bolt by the adjustment of the second cross bar and follows the circular motion route of main axis or depart from this moving line.In order to strengthen the frictional force of pin to axle sleeve, so arranging base plate to strengthen the support force of pin, shortening the movement travel of pin thus strengthening active force to axle sleeve.
As preferably, the side that described second cross bar connects pin is fixedly connected with one again for being close to the friction lever of main shaft while rising to range at pedal.In order to strengthen the sensitivity of pause device further, when needs stop, can stopping immediately.So arrange a friction lever again in order to strengthen the frictional force to main shaft.
As preferred further, described friction lever comprises extension, bending part and friction head; Described bending part is extended the top to main shaft by extension, and the lower surface of friction head is contacted with the upper surface of main shaft.If the contacts side surfaces of friction head and main shaft, friction head is easily flicked, and needs larger power that friction head is contacted with main shaft.And if upper and lower faces contact, the gravity of friction head self also can become a part for frictional force.
As further preferred, the side of described friction head and the contacts side surfaces of axle sleeve.The increasing friction force by increase contact area.
As preferably, the turning cylinder on described base plate will extend to friction lever place plane, and for limiting the pendulum angle of friction lever.This is a safeguard protection design.The turning cylinder extended departs from away after rupturing with the second cross bar after may be used for preventing friction lever from being flicked by main shaft.
As preferably, described fuselage arranges motor, described motor connects driving wheel, and driving wheel is connected to the main wheel be arranged on main shaft by belt transmission.If main shaft is directly by driven by motor, and pause device directly suspends main shaft, is just easy to make the motor shaft in motor stuck.Motor shaft in present motor still can rotate, and namely drives driving wheel idle running.
The utility model beneficial effect is:
This pause device can control the time of time-out with the custom of operating personnel, and simple to operate, suspends sensitivity strong, also can not injure machine shaft.
Accompanying drawing explanation
Fig. 1 is the utility model embodiment perspective view;
Fig. 2 is the sectional structure schematic diagram of the present embodiment;
Fig. 3 is the enlarged drawing in the A portion of Fig. 1;
Fig. 4 is the syndeton schematic diagram of friction lever and main shaft.
In figure: 1-fuselage, 7-pause device, 71-connecting rod, 72-second cross bar, 73-second rotating shaft, 74-friction lever, 741-extension, 742-bending part, 743-friction head, 75-pin, 751-base plate, 752-turning cylinder, 81-main shaft, 811-axle sleeve, 812-bolt, 9-motor, 91-driving wheel, 92-main wheel, 10-pedal, 101-cross bar, 102-axle, 103-stretching bar, 104-extension spring.
Detailed description of the invention
Below in conjunction with accompanying drawing, with embodiment, the utility model is described in further detail.
This specific embodiment is only to explanation of the present utility model; it is not to restriction of the present utility model; those skilled in the art can make to the present embodiment the amendment not having creative contribution as required after reading this description, as long as but be all subject to the protection of Patent Law in right of the present utility model.
Embodiment 1, a controlled pause device for rivet driver, comprising fuselage 1 and the main shaft 81 for driving rivet driver to run, comprising and being rotationally connected by axle 102 cross bar 101 be arranged in fuselage 1, one end of described cross bar 101 arranges pedal 10, and the other end arranges extension spring 104; Described cross bar 101 arranges on extension spring 104 one end and connects stretching bar 103 again, described stretching bar 103 connects the connecting rod 71 be piercing in outside fuselage 1, described connecting rod 71 is fixedly connected with the second cross bar 72 again, second cross bar 72 connects on the relative other end of connecting rod 71 at it and connects pin 75, described second cross bar 72 is connected on fuselage 1 by being rotationally connected the second rotating shaft 73, position arranges axle sleeve 811 with described main shaft 81 corresponding pin 75, and described axle sleeve 811 follows main shaft 81 synchronous axial system through axle sleeve 811 to propping up on main shaft 81 by bolt 812; Described pin 75 can be close to axle sleeve 811 while pedal 10 rises to range, and is stopped the rotation stoping main shaft 81 by bolt 812.Described pin 75 is rotationally connected with the base plate 751 be arranged on fuselage 1 by turning cylinder 752, the position that described second cross bar 72 is fixedly connected with pin 75 is positioned at the side of turning cylinder 752, and the other end of pin 75 can enter into bolt 812 by the adjustment of the second cross bar 72 and follows the circular motion route of main shaft 81 rotation or depart from this moving line.The position relationship of pin 75 is driven by pedal 10, thus the time-out realized main shaft 81 or operation.
As shown in Figure 3, in order to increase the frictional force to main shaft, the time that main shaft is stopped operating is shorter, so the side that described second cross bar 72 connects pin 75 is fixedly connected with one again for being close to the friction lever 74 of main shaft 81 while rising to range at pedal 10.
As shown in Figure 4, described friction lever 74 comprises extension 741, bending part 742 and friction head 743; The top that described bending part 742 is extended to main shaft 81 by extension 741, and the lower surface of friction head 743 is contacted with the upper surface of main shaft 81.And the side of described friction head 743 and the contacts side surfaces of axle sleeve 811.Both can increase friction area to increase frictional force, and the interphase interaction of friction head 743 and axle sleeve 811 can have been ensured again, and friction head 743 can not be made to deflect.
As shown in Figure 3, the turning cylinder 752 on described base plate 751 will extend to friction lever 74 place plane, and for limiting the pendulum angle of friction lever 74.The turning cylinder 752 extended departs from away after rupturing with the second cross bar 72 after may be used for preventing friction lever 74 from being flicked by main shaft 81.
As illustrated in fig. 1 and 2, described fuselage 1 arranges motor 9, described motor 9 connects driving wheel 91, and driving wheel 91 is connected to the main wheel 92 be arranged on main shaft 81 by belt transmission.Drive driving wheel to rotate by motor 9, thus drive the type of drive of main axis, even if main shaft stops suddenly, the motor shaft in motor 9 still can drive driving wheel to dally, thus can not cause the damage of motor.And the motor that this pause device uses is slow speed motor, about rotating speed is at 20 ~ 30r/min.

Claims (7)

1. the controlled pause device of a rivet driver, comprise fuselage (1) and the main shaft (81) for driving rivet driver to run, it is characterized in that: comprise and be rotationally connected by axle (102) cross bar (101) be arranged in fuselage (1), one end of described cross bar (101) arranges pedal (10), and the other end arranges extension spring (104), described cross bar (101) arranges on extension spring (104) one end and connects stretching bar (103) again, the connection of described stretching bar (103) is piercing in fuselage (1) connecting rod outward (71), described connecting rod (71) is fixedly connected with the second cross bar (72) again, second cross bar (72) connects on the relative other end of connecting rod (71) at it and connects pin (75), described second cross bar (72) is connected on fuselage (1) by being rotationally connected the second rotating shaft (73), described main shaft (81) corresponding pin (75) position is arranged axle sleeve (811), described axle sleeve (811) above follows main shaft (81) synchronous axial system through axle sleeve (811) to propping up main shaft (81) by bolt (812), described pin (75) can be close to axle sleeve (811) while pedal (10) rises to range, and is stopped the rotation stoping main shaft (81) by bolt (812).
2. by the controlled pause device of a kind of rivet driver according to claim 1, it is characterized in that: described pin (75) is rotationally connected with the base plate (751) be arranged on fuselage (1) by turning cylinder (752), the position that described second cross bar (72) is fixedly connected with pin (75) is positioned at the side of turning cylinder (752), and the other end of pin (75) can enter into bolt (812) by the adjustment of the second cross bar (72) and follows circular motion route that main shaft (81) rotates or depart from this moving line.
3. by the controlled pause device of a kind of rivet driver according to claim 2, it is characterized in that: the side that described second cross bar (72) connects pin (75) is fixedly connected with one again for being close to the friction lever (74) of main shaft (81) while rising to range at pedal (10).
4., by the controlled pause device of a kind of rivet driver according to claim 3, it is characterized in that: described friction lever (74) comprises extension (741), bending part (742) and friction head (743); The top that described bending part (742) is extended to main shaft (81) by extension (741), and the lower surface of friction head (743) is contacted with the upper surface of main shaft (81).
5., by the controlled pause device of a kind of rivet driver according to claim 4, it is characterized in that: the side of described friction head (743) and the contacts side surfaces of axle sleeve (811).
6., by the controlled pause device of a kind of rivet driver according to claim 5, it is characterized in that: the turning cylinder (752) on described base plate (751) will extend to friction lever (74) place plane, and for limiting the pendulum angle of friction lever (74).
7. by the controlled pause device of a kind of rivet driver described in claim 1 or 6, it is characterized in that: described fuselage (1) is arranged motor (9), described motor (9) connects driving wheel (91), and driving wheel (91) is connected to the main wheel (92) be arranged on main shaft (81) by belt transmission.
CN201420604762.8U 2014-10-20 2014-10-20 A kind of controlled pause device of rivet driver Withdrawn - After Issue CN204159813U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420604762.8U CN204159813U (en) 2014-10-20 2014-10-20 A kind of controlled pause device of rivet driver

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420604762.8U CN204159813U (en) 2014-10-20 2014-10-20 A kind of controlled pause device of rivet driver

Publications (1)

Publication Number Publication Date
CN204159813U true CN204159813U (en) 2015-02-18

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201420604762.8U Withdrawn - After Issue CN204159813U (en) 2014-10-20 2014-10-20 A kind of controlled pause device of rivet driver

Country Status (1)

Country Link
CN (1) CN204159813U (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104353773A (en) * 2014-10-20 2015-02-18 浙江昊国家具有限公司 Controllable pause device of riveting machine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104353773A (en) * 2014-10-20 2015-02-18 浙江昊国家具有限公司 Controllable pause device of riveting machine

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C14 Grant of patent or utility model
GR01 Patent grant
AV01 Patent right actively abandoned

Granted publication date: 20150218

Effective date of abandoning: 20160120

C25 Abandonment of patent right or utility model to avoid double patenting