CN107637921B - A kind of shoe manufacturing machine people - Google Patents
A kind of shoe manufacturing machine people Download PDFInfo
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- CN107637921B CN107637921B CN201710870358.3A CN201710870358A CN107637921B CN 107637921 B CN107637921 B CN 107637921B CN 201710870358 A CN201710870358 A CN 201710870358A CN 107637921 B CN107637921 B CN 107637921B
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Abstract
The invention discloses a kind of shoe manufacturing machine people, including fuselage and switching, the scroll wheel in fuselage bottom is set, heavy access slot is equipped in body bottom surface, heavy access slot inner roof wall runs through the sliding slot of landing for being equipped with the setting that stretches upwards, the first transmission chamber of the interior setting that stretches equipped with left and right of the fuselage above slot is slipped in landing, landing is slipped transmits chamber in inner wall on the right side of slot through equipped with second, landing slips at the top of slot inner left wall to run through connects slot equipped with first, first to connect the end pin bottom that stretches on the left of groove top portion and the first transmission chamber opposite, first connects the first screw rod that the setting that stretches up and down is equipped in slot, stretch end pin and the first driver of first screw tip is connected, the setting of first driver outer surface is connected in slot inner roof wall and is fixedly connected first；The configuration of the present invention is simple, it is easy to operate, the accuracy and stability of hammer out are improved, the labor intensity of worker is alleviated, reduces the cost of transport.
Description
Technical field
The present invention relates to shoe-making field, specifically a kind of shoe manufacturing machine people.
Background technology
Shoes vamp cut seal after need further to the rough seam of heel of a shoe, too thick flanging at
Hammer out dressing operation is carried out, welt, the smooth beauty of the flanging of vamp or joint are made.Traditional hammer out mode uses man-hour manually hand-held
Tup carries out hammer out, is easy to injure operator's both hands, and inefficiency, time-consuming and laborious, speed is slow, and manually is difficult to control
It Mechanical Moving and moves.
Invention content
Technical problem to be solved by the invention is to provide a kind of shoe manufacturing machine people, can solve above-mentioned show in the art
The problem of.
The present invention is achieved through the following technical solutions：The present invention a kind of shoe manufacturing machine people, including fuselage and
The scroll wheel in the fuselage bottom is arranged in switching, and heavy access slot is equipped in the body bottom surface, and the heavy access slot inner roof wall runs through
Slot is slipped in landing equipped with the setting that stretches upwards, and the landing, which slips to be equipped in the fuselage above slot, controls the setting that stretches
First transmits chamber, and inner wall is interior through the second transmission chamber is equipped on the right side of the sliding slot of the landing, and slot inner left wall is slipped in the landing
Slot is connected through equipped with first in top, described first connects the end pin bottom phase that stretches on the left of groove top portion and the first transmission chamber
Right, described first connects the first screw rod that the setting that stretches up and down is equipped in slot, and first screw tip stretches end pin and first
Driver is connected, and the setting of first driver outer surface is connected in slot inner roof wall and is fixedly connected, institute described first
State helical line on the first screw rod be connected with described first connect the sliding cooperation of slot connect block, the landing is slipped in slot
Sliding to be combined with hammer out block, the hammer out block left end roof is fixedly connected with the block right side end pin that connects, hammer out block bottom
It is equipped with hammer out in face and slips slot, the hammer out, which slips to slip in slot, coordinates hammer out to push away extension bar, and the hammer out slips inner wall on the right side of slot
Interior to connect slot through equipped with second, described second connects the sliding-contacted rod for being slipped in slot and being combined with and controlling the setting that stretches, described sliding
The end pin that stretches on the left of bar pushes away extension bar right hand top with the hammer out and is fixedly connected, and the end pin that stretches on the right side of the sliding-contacted rod is visited to described
Second transmits intracavitary and sliding cooperation, and described second on the downside of the sliding-contacted rod, which transmits intracavitary, is equipped with and hammer out block right side
It transfers the first Coupling Shaft of cooperation, deviation wheel is fixedly installed on first Coupling Shaft outer surface, first Coupling Shaft is right
The side end pin that stretches is fixedly installed first bevel gear, and the first transmission intracavitary is equipped with to be connected with first driver
Transfer device, the second transmission chamber right side inner wall is equipped with the driving device to be connected with the transfer device, described
Fuselage top surface left part is fixedly installed transparent storage box, and the transparent storage box is separated out the different glove of multiple specifications by partition board
Slot.
Preferably technical solution, the transfer device include setting stretch in section on the left of the first transmission chamber and
The second Coupling Shaft and being arranged on the right side of the first transmission chamber of setting of stretching up and down stretches in section and the setting that stretches up and down
Third Coupling Shaft, second Coupling Shaft bottom stretch and are connected at the top of end pin and first driver, and described first passes
Second Coupling Shaft outer surface for passing intracavitary is equipped with the first transfer wheel, the institute below the section that stretches on the right side of the first transmission chamber
It states to be equipped in fuselage inner wall and connects chamber, it is described to connect sliding be combined with of intracavitary and connect block, it is described to connect helical line in block top surface and match
It closes and is connected with the second screw rod of setting of stretching upwards, second screw tip end pin that stretches is stretched with third Coupling Shaft bottom
Prolong end pin to be fixedly connected, the second transfer wheel be fixedly installed on the third Coupling Shaft outer surface of the first transmission intracavitary,
Transfer tape is connected between second transfer wheel and first transfer wheel, it is described to connect the end pin switching cooperation of block bottom
It is connected with bevel gear.
Preferably technical solution, the driving device include being arranged in the fuselage connected below chamber
Third transmits chamber, switching is equipped with transmitting assembly and the fixed setting described the transmitted in the third in chamber inner left wall
Three transmit the speed changer in inner walls on the right side of chambers, and the speed changer left side, which is connected with to visit to the third, transmits the of intracavitary
Four bevel gears, speed changer right side end pin are connected with the second driver, and end pin coordinates company on the right side of second driver
Spy is connected to the second cogwheel outside the fuselage right side, the third transmits chamber and described connect is passed through through being equipped between chamber
Wears groove, the transmitting assembly include that switching is arranged in the fuselage for transmitting between chamber and third transmission chamber described second
The 4th Coupling Shaft and the second bevel gear and third hand tap gear that are respectively fixedly disposed at left and right sides of the 4th Coupling Shaft,
The second bevel gear is located at the second transmission intracavitary below the first bevel gear, and the third hand tap gear is located at described
Third transmits intracavitary leftward position.
Preferably technical solution is fixedly installed the first cogwheel, institute on the right side of the fuselage on the scroll wheel of front side
It states and is connected with transfer chain between the first cogwheel and second cogwheel.
Preferably technical solution slips in the heavy access slot and is combined with hammer out block, at the top of the hammer out block with it is described
Hammer out is equipped between pushing away extension bar bottom end pin except shake part.
Preferably technical solution, the hammer out that the hammer out pushes away extension bar over top slip in slot equipped with spring coil.
The beneficial effects of the invention are as follows：
1. being visited to second by the end pin that stretches on the right side of sliding-contacted rod and transmitting intracavitary and sliding cooperation, second on the downside of sliding-contacted rod passes
It passs intracavitary and sets the first Coupling Shaft coordinated with the switching of hammer out block right side, fixed setting deviation is taken turns on the first Coupling Shaft outer surface,
Stretch on the right side of first Coupling Shaft end pin fixed setting first bevel gear, and the first transmission intracavitary is set to be connected with the first driver
Transfer device, the second transmission chamber right side inner wall sets the driving device to be connected with transfer device, to realize automatic control
The transmission connection and the driving work of hammer out of hammer out processed, meanwhile, realization automatically controls hammer out work, improves the accurate of hammer out
Property and stability.
2. including second turn that the setting that stretches in section on the left of the first transmission chamber and stretch up and down is arranged by transfer device
Spindle and being arranged on the right side of the first transmission chamber, which stretches, to be set in section and the third Coupling Shaft for the setting that stretches up and down, the second Coupling Shaft bottom
Portion stretches and is connected at the top of end pin and the first driver, and the first transmission is set on the second Coupling Shaft outer surface of the first transmission intracavitary
It takes turns, is set in the fuselage inner wall below the section that stretches on the right side of the first transmission chamber and connect chamber, connect the sliding cooperation of intracavitary and connect block, connect block
Helical line is connected the second screw rod of setting of stretching upwards in top surface, and the second screw tip stretches end pin and third Coupling Shaft bottom
Portion's end pin that stretches is fixedly connected, and the second transfer wheel is fixedly installed on the third Coupling Shaft outer surface of the first transmission intracavitary, second passes
The transfer tape that is connected between wheel and the first transfer wheel is passed, block bottom end pin switching mating connection bevel gear is connected, to realize
The landing work for automatically controlling hammer out block, makes the hammer out block of hammer out block bottom visit to outside the bottom surface of fuselage, meanwhile, realize the first cone
The mating connection work of gear and the second driver.
3. the configuration of the present invention is simple, easy to operate, the transmission connection for automatically controlling hammer out and the driving of hammer out can be realized
Work, meanwhile, realization automatically controls hammer out work, improves the accuracy and stability of hammer out, alleviates the labour of worker
Intensity automatically moves work in addition, can realize, reduces the cost of transport.
Description of the drawings
The present invention is described in detail by following specific embodiment and attached drawing for ease of explanation,.
Fig. 1 is overall structure diagram outside a kind of shoe manufacturing machine people of the present invention；
Fig. 2 be the present invention Fig. 1 in " A-A " sectional view；
Fig. 3 is structural schematic diagram when a kind of shoe manufacturing machine people of the invention automatically controls hammer out；
Fig. 4 is that the hammer out of the present invention pushes away the structural schematic diagram of extension bar.
Specific implementation mode
As Figure 1-Figure 4, a kind of shoe manufacturing machine people of the invention, including fuselage 8 and switching are arranged in the fuselage 8
The scroll wheel 81 of bottom is equipped with heavy access slot 83 in 8 bottom surface of the fuselage, and 83 inner roof wall of heavy access slot runs through to be equipped with to stretch upwards
Slot 82 is slipped in the landing of setting, the first biography of the setting that stretches equipped with left and right in the fuselage 8 of sliding 82 top of slot of the landing
Chamber 86 is passed, the landing is slipped through the second transmission chamber 84 is equipped in 82 right side inner wall of slot, and the landing is slipped in 82 left side of slot
Interior at the top of wall to connect slot 85 through equipped with first, described first connects 85 top of slot transmits the tail that stretches on the left of chamber 86 with described first
Tip bottom is opposite, and described first connects the first screw rod 852 that the setting that stretches up and down is equipped in slot 85, and first screw rod 852 pushes up
Stretch end pin and the first driver 853 of portion is connected, and 853 outer surface of the first driver is arranged connects slot described first
It in 85 inner roof walls and is fixedly connected, helical line is connected with that connect slot 85 with described first sliding on first screw rod 852
Cooperation connects block 851, and the landing, which slips to slip in slot 82, is combined with hammer out block 821,821 left end roof of the hammer out block with
The 851 right side end pin of block that connects is fixedly connected, and hammer out is equipped in 821 bottom surface of hammer out block and slips slot 822, the hammer out is slided
Cooperation hammer out is slipped in access slot 822 and pushes away extension bar 824, and the hammer out slips to run through in 822 right side inner wall of slot connects slot equipped with second
823, described second connects the sliding-contacted rod 825 for being slipped in slot 823 and being combined with and controlling the setting that stretches, and 825 left side of the sliding-contacted rod is stretched
Prolong end pin and push away 824 right hand top of extension bar with the hammer out and be fixedly connected, 825 right side of the sliding-contacted rod end pin that stretches is visited to described the
Two transmit in chambers 84 and sliding cooperation, and described the second of 825 downside of the sliding-contacted rod transmits and be equipped in chamber 84 and the hammer out block
First Coupling Shaft 841 of 821 right sides switching cooperation, deviation wheel is fixedly installed on 841 outer surface of the first Coupling Shaft
843, the right side of first Coupling Shaft 841 end pin that stretches is fixedly installed first bevel gear 842, is set in the first transmission chamber 86
Have a transfer device being connected with first driver 853, described second transmit 84 right side inner wall of chamber be equipped with to institute
The driving device of transfer device mating connection is stated, 8 top surface left part of the fuselage is fixedly installed transparent storage box 801, described
Bright storage box 801 is separated out the different article putting groove 803 of multiple specifications by partition board 802.
Valuably, the transfer device includes being arranged to stretch in section and stretch up and down in 86 left side of the first transmission chamber to set
The second Coupling Shaft 861 for setting and being arranged stretches on 86 right side of the first transmission chamber in section and the third for the setting that stretches up and down turns
Spindle 863,861 bottom of the second Coupling Shaft, 853 top of end pin and first driver that stretches are connected, and described first
It transmits 861 outer surface of the second Coupling Shaft in chamber 86 and is equipped with the first transfer wheel 862,86 right side of the first transmission chamber is stretched
Prolong to be equipped in 8 inner wall of the fuselage below section and connect chamber 89, it is described connect to slip to be combined in chamber 89 connect block 891, it is described
Connect the second screw rod 892 that helical line in 891 top surface of block is connected with the setting that stretches upwards, second screw rod, 892 top
End pin and 863 bottom of third the Coupling Shaft end pin that stretches that stretches are fixedly connected, and described first transmits the third in chamber 86
The second transfer wheel 864, second transfer wheel 864 and first transfer wheel 862 are fixedly installed on 863 outer surface of Coupling Shaft
Between be connected with transfer tape 865, it is described to connect 891 bottom end pin switching of block and be connected with bevel gear 893, to realize
The landing work for automatically controlling hammer out block 821, makes the hammer out block 831 of 821 bottom of hammer out block visit to outside the bottom surface of fuselage 8, meanwhile,
Realize the mating connection work of first bevel gear 842 and the second driver 874.
Valuably, the driving device includes that the third being arranged in the fuselage 8 connected below chamber 89 is transmitted
Chamber 87, switching are equipped with transmitting assembly 871 and the fixed setting described the transmitted in the third in 87 inner left wall of chamber
Three transmit the speed changer 873 in 87 right side inner wall of chamber, and 873 left side of the speed changer is connected with spy to the third and transmits
The 4th bevel gear 872 in chamber 87,873 right side end pin of the speed changer are connected with the second driver 874, and described second drives
Dynamic 874 right side end pin of device is connected with spy to the second cogwheel 875 outside 8 right side of the fuselage, and the third transmits chamber
87 and described connect run through slot 88 through being equipped between chamber 89, the transmitting assembly 871 includes that switching setting is passed described second
It passs the 4th Coupling Shaft 8710 in the fuselage 8 between chamber 84 and third transmission chamber 87 and is respectively fixedly disposed at institute
State the second bevel gear 8712 and third hand tap gear 8711 of 8710 left and right sides of the 4th Coupling Shaft, the second bevel gear 8712
Described second in 842 lower section of the first bevel gear transmits in chamber 84, and the third hand tap gear 8711 is located at third biography
Leftward position in chamber 87 is passed, the walking of fuselage 8 and hammer out work are automatically controlled to realize.
Valuably, it is fixedly installed the first cogwheel 810 on the scroll wheel 81 of the right side of the fuselage 8 front side, described first
It is connected with transfer chain 811 between cogwheel 810 and second cogwheel 875.
Valuably, it is slipped in the heavy access slot 83 and is combined with hammer out block 831,831 top of the hammer out block and the hammer out
It pushes away and is equipped between 824 bottom end pin of extension bar except shake part 826, the impact force generated when to reduce hammer out improves making for the present apparatus
Use the service life.
Valuably, the hammer out pushes away the hammer out of 824 over top of extension bar and slips and be equipped with spring coil 827 in slot 822, to
Realization is resumed work automatically.
When original state, deviation wheel 843 is influenced by its own gravity and the pressure on top surface of spring coil 827, makes the second transmission
825 bottom surface of sliding-contacted rod in chamber 84 utmostly offsets close to 841 axial line side of the first Coupling Shaft with 843 outer surfaces of wheel are biased to
It connects, meanwhile, the first screw rod 852, which drives, to be connected block 851 and connects top position in slot 85 positioned at first, at this point, by connecting block
851 drive hammer out block 821 to slip the top position in slot 82 positioned at landing, meanwhile, extension bar 824 is pushed away by hammer out and drives bottom
Hammer out block 831 is fully located in heavy access slot 83, at this point, connect block 851 utmostly connects 85 inner top position of slot positioned at first,
The first driver 853 for connecting 851 bottom end pin of block is set utmostly to connect 85 inner bottom wall of slot far from first, meanwhile, hammer out block
First bevel gear 842 on 821 right sides is utmostly far from second bevel gear 8712.
When needing to automatically control hammer out work, the rotation of the second cogwheel 875 is driven by the second driver 874 first,
It drives the first cogwheel 810 to rotate by the transfer chain 811 on the second cogwheel 875, and then front side is driven by the first cogwheel 810
Scroll wheel 81 rotate, automatically control the mobile working of fuselage 8 to realize, reduce transportation cost, needed until fuselage 8 is moved to
It wants at the position of hammer out, at this point, the second driver 874 of control stops operating, bottom is then driven by the first driver 853
Second Coupling Shaft 861 at the first screw rod 852 and top rotates, and then connects block 851 gradually along the by the drive of the first screw rod 852
One connects the sliding of 85 bottom direction of slot, meanwhile, drive hammer out block 821 gradually to slip 82 bottom side of slot along landing by connecting block 851
To sliding, the hammer out block 831 of bottom is driven gradually to visit to outside 83 bottom of heavy access slot at this point, pushing away extension bar 824 by hammer out, meanwhile, make
First bevel gear 842 on 821 right side of hammer out block is gradually slided by 8712 top side of second bevel gear, at this point, by second
The rotation of Coupling Shaft 861 drives the rotation of the first transfer wheel 862 simultaneously, and then is driven by the transfer tape 865 in the first transfer wheel 862
Second transfer wheel 864 and third Coupling Shaft 863 rotate, meanwhile, by third Coupling Shaft 863 drive bottom connect block 891 by
Gradually along the bottom direction sliding connected in chamber 89, slot 85 is connected until connecting block 851 as shown in Figure 3 and utmostly sliding into first
When interior lowest position, slipped in slot 82 at this point, driving hammer out block 821 utmostly to slide into landing by connecting block 851
Bottom position, meanwhile, extension bar 824 is pushed away by the drive hammer out of hammer out block 821 and hammer out pushes away the hammer out block 831 of 824 bottom of extension bar most
Big degree is visited to outside the bottom surface of fuselage 8, at this point, hammer out block 821 drives the first bevel gear 842 and second bevel gear on right side
8712 engagement connections, meanwhile, block 891 is connected by the drive of the second screw rod 892 and utmostly slides into the bottommost connected in chamber 89
Position, at this point, being passed through through slot 88 by the connection bevel gear 893 for connecting the drive of block 891 bottom and utmostly being visited to third biography
It passs in chamber 87 and the left and right sides of 893 bottom of connection bevel gear is made to be bored respectively with 8711 right hand top of third hand tap gear and the 4th
The engagement connection of 872 left side top of gear, at this point, the rotation of the second cogwheel 875 is driven by the second driver 874, it is embedding by second
Transfer chain 811 on gear 875 drives the rotation of the first cogwheel 810, and then the scroll wheel of front side is driven by the first cogwheel 810
81 rotations, to realize the mobile working for automatically controlling fuselage 8, meanwhile, by the second driver 874 after 873 speed change of speed changer
It drives the 4th bevel gear 872 to rotate, and then drives connection bevel gear 893 and connection bevel gear 893 left by the 4th bevel gear 872
The transmitting assembly 871 of side rotates, at this point, being driven in first bevel gear 842 and first bevel gear 842 by transmitting assembly 871
Deviation wheel 843 rotate, by be biased to wheel 843 lasting rotation and be slidably matched with 825 bottom surface top pressure of sliding-contacted rod, simultaneously as
Hammer out pushes away top pressure active force of the extension bar 824 by spring coil 827, and the hammer out block that extension bar 824 drives bottom is pushed away by hammer out to realize
831 reciprocal hammer out work.
The beneficial effects of the invention are as follows：
1. being visited to second by the end pin that stretches on the right side of sliding-contacted rod and transmitting intracavitary and sliding cooperation, second on the downside of sliding-contacted rod passes
It passs intracavitary and sets the first Coupling Shaft coordinated with the switching of hammer out block right side, fixed setting deviation is taken turns on the first Coupling Shaft outer surface,
Stretch on the right side of first Coupling Shaft end pin fixed setting first bevel gear, and the first transmission intracavitary is set to be connected with the first driver
Transfer device, the second transmission chamber right side inner wall sets the driving device to be connected with transfer device, to realize automatic control
The transmission connection and the driving work of hammer out of hammer out processed, meanwhile, realization automatically controls hammer out work, improves the accurate of hammer out
Property and stability.
2. including second turn that the setting that stretches in section on the left of the first transmission chamber and stretch up and down is arranged by transfer device
Spindle and being arranged on the right side of the first transmission chamber, which stretches, to be set in section and the third Coupling Shaft for the setting that stretches up and down, the second Coupling Shaft bottom
Portion stretches and is connected at the top of end pin and the first driver, and the first transmission is set on the second Coupling Shaft outer surface of the first transmission intracavitary
It takes turns, is set in the fuselage inner wall below the section that stretches on the right side of the first transmission chamber and connect chamber, connect the sliding cooperation of intracavitary and connect block, connect block
Helical line is connected the second screw rod of setting of stretching upwards in top surface, and the second screw tip stretches end pin and third Coupling Shaft bottom
Portion's end pin that stretches is fixedly connected, and the second transfer wheel is fixedly installed on the third Coupling Shaft outer surface of the first transmission intracavitary, second passes
The transfer tape that is connected between wheel and the first transfer wheel is passed, block bottom end pin switching mating connection bevel gear is connected, to realize
The landing work for automatically controlling hammer out block, makes the hammer out block of hammer out block bottom visit to outside the bottom surface of fuselage, meanwhile, realize the first cone
The mating connection work of gear and the second driver.
3. the configuration of the present invention is simple, easy to operate, the transmission connection for automatically controlling hammer out and the driving of hammer out can be realized
Work, meanwhile, realization automatically controls hammer out work, improves the accuracy and stability of hammer out, alleviates the labour of worker
Intensity automatically moves work in addition, can realize, reduces the cost of transport.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.Therefore, of the invention
Protection domain should be determined by the scope of protection defined in the claims.
Claims (6)
1. the scroll wheel in fuselage bottom is arranged in a kind of shoe manufacturing machine people, including fuselage and switching, it is characterised in that：Fuselage bottom
Heavy access slot is equipped in face, heavy access slot inner roof wall runs through the landing equipped with the setting that stretches upwards and slips slot, and landing is slipped above slot
It it is equipped with left and right in fuselage stretches and the first of setting transmit chamber, landing, which is slipped on the right side of slot in inner wall, transmits chamber through being equipped with second, rises
Drop is slipped at the top of slot inner left wall connects slot through equipped with first, and first connects the tail that stretches on the left of groove top portion and the first transmission chamber
Tip bottom is opposite, and first connects the first screw rod that the setting that stretches up and down is equipped in slot, and the first screw tip stretches end pin and first
Driver is connected, and the setting of the first driver outer surface is connected in slot inner roof wall and is fixedly connected first, on the first screw rod
Helical line is connected with the block that connects for connecting the sliding cooperation of slot with first, and landing, which slips to slip in slot, is combined with hammer out block, hammers into shape
Plain block left end roof is fixedly connected with end pin on the right side of block is connected, and hammer out is equipped in hammer out block bottom surface and slips slot, hammer out slips in slot
Sliding that hammer out is coordinated to push away extension bar, hammer out slips connects slot in inner wall on the right side of slot through equipped with second, and second connects sliding in slot match
The sliding-contacted rod for having left and right to stretch setting is closed, the end pin that stretches on the left of sliding-contacted rod pushes away extension bar right hand top with hammer out and is fixedly connected, and slips
The end pin that stretches on the right side of bar is visited to second and transmits intracavitary and sliding cooperation, and second on the downside of sliding-contacted rod, which transmits intracavitary, is equipped with and hammer out block
First Coupling Shaft of right side switching cooperation, is fixedly installed deviation wheel on the first Coupling Shaft outer surface, on the right side of the first Coupling Shaft
The end pin that stretches is fixedly installed first bevel gear, and the first transmission intracavitary is equipped with the transfer device being connected with the first driver,
Inner wall is equipped with the driving device to be connected with transfer device on the right side of second transmission chamber, and fuselage top surface left part is fixedly installed
Transparent storage box, transparent storage box are separated out the different article putting groove of multiple specifications by partition board.
2. a kind of shoe manufacturing machine people according to claim 1, it is characterised in that：The transfer device includes being arranged described
It stretches on the left of first transmission chamber in section and the second Coupling Shaft of the upper and lower setting that stretches and setting is transmitted described first on the right side of chamber
Stretch in the section that stretches and up and down the third Coupling Shaft of setting, and second Coupling Shaft bottom stretches end pin and first driver
Top be connected, it is described first transmit intracavitary second Coupling Shaft outer surface be equipped with the first transfer wheel, described first
It transmits to be equipped in the fuselage inner wall to stretch on the right side of chamber below section and connects chamber, it is described to connect sliding be combined with of intracavitary and connect block,
Described to connect helical line in block top surface and be connected with the second screw rod of setting of stretching upwards, second screw tip stretches tail
The tip and the third Coupling Shaft bottom end pin that stretches are fixedly connected, and described first transmits the third Coupling Shaft outer surface of intracavitary
On be fixedly installed the second transfer wheel, be connected with transfer tape between second transfer wheel and first transfer wheel, institute
It states and connects the switching of block bottom end pin and be connected with bevel gear.
3. a kind of shoe manufacturing machine people according to claim 2, it is characterised in that：The driving device includes being arranged described
The third in the fuselage below chamber is connected to transmit chamber, transfer to be equipped with and transmit the biography in chamber inner left wall in the third
The speed changer in inner wall on the right side of component and the fixed setting third transmission chamber is passed, the speed changer left side is connected with
It visits to the third and transmits the 4th bevel gear of intracavitary, end pin is connected with the second driver on the right side of the speed changer, described
End pin is connected with spy to the second cogwheel outside the fuselage right side on the right side of second driver, the third transmit chamber with
Described connect runs through slot through being equipped between chamber, and the transmitting assembly includes switching setting transmits chamber and described the described second
Three transmit the 4th Coupling Shaft in the fuselage between chambers and are respectively fixedly disposed at left and right sides of the 4th Coupling Shaft
Second bevel gear and third hand tap gear, the second bevel gear be located at below the first bevel gear it is described second transmit chamber
Interior, the third hand tap gear is located at the third and transmits intracavitary leftward position.
4. a kind of shoe manufacturing machine people stated according to claim 3, it is characterised in that：It is solid on the scroll wheel of front side on the right side of the fuselage
Surely it is provided with the first cogwheel, transfer chain is connected between first cogwheel and second cogwheel.
5. a kind of shoe manufacturing machine people according to claim 1, it is characterised in that：It is slipped in the heavy access slot and is combined with hammer out
Block, the hammer out block top and the hammer out are equipped between pushing away extension bar bottom end pin except shake part.
6. a kind of shoe manufacturing machine people according to claim 1, it is characterised in that：The hammer out pushes away the institute of extension bar over top
Hammer out is stated to slip in slot equipped with spring coil.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710870358.3A CN107637921B (en) | 2017-09-23 | 2017-09-23 | A kind of shoe manufacturing machine people |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710870358.3A CN107637921B (en) | 2017-09-23 | 2017-09-23 | A kind of shoe manufacturing machine people |
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| Publication Number | Publication Date |
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| CN107637921A CN107637921A (en) | 2018-01-30 |
| CN107637921B true CN107637921B (en) | 2018-08-03 |
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| CN201710870358.3A Active CN107637921B (en) | 2017-09-23 | 2017-09-23 | A kind of shoe manufacturing machine people |
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Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN108489524A (en) * | 2018-02-06 | 2018-09-04 | 佛山尘凡环保科技有限公司 | A kind of modified remote sensing of environment device |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB185202A (en) * | 1921-05-28 | 1922-08-28 | Basil Pomeroy Cooper | Improvements in or relating to the supporting of boots or shoes for sole levelling |
| GB897766A (en) * | 1957-06-11 | 1962-05-30 | British United Shoe Machinery | Improvements in or relating to machines suitable for levelling the bottoms of shoes |
| CN2378982Y (en) * | 1999-07-30 | 2000-05-24 | 郑豪迈 | Double top pounding machine for pounding leather-shoes |
| CN2901957Y (en) * | 2005-09-12 | 2007-05-23 | 夏正义 | High performance machine for toecap angle hammering and wrinkles-removing |
| CN104665114B (en) * | 2015-03-06 | 2016-07-27 | 东莞市联洲知识产权运营管理有限公司 | A kind of press of leather shoe surface |
| CN104814574B (en) * | 2015-05-13 | 2017-04-26 | 温州蓝海鞋业有限公司 | Horizontal vamp flatting machine |
| CN105708052A (en) * | 2016-04-01 | 2016-06-29 | 金丽秋 | Vamp flatting machine for making shoes |
-
2017
- 2017-09-23 CN CN201710870358.3A patent/CN107637921B/en active Active
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|---|---|
| CN107637921A (en) | 2018-01-30 |
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Effective date of registration: 20180621 Address after: 325036 8 Ouhai Cui Bo Road, Ouhai Economic Development Zone, Wenzhou, Zhejiang Applicant after: DESAY GROUP CO., LTD. Address before: 321000 3 3, Yingbin Avenue, Wucheng District, Jinhua, Zhejiang. Applicant before: Tong Zhongyi |
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