CN112045404A - Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin - Google Patents
Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin Download PDFInfo
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- CN112045404A CN112045404A CN202010986690.8A CN202010986690A CN112045404A CN 112045404 A CN112045404 A CN 112045404A CN 202010986690 A CN202010986690 A CN 202010986690A CN 112045404 A CN112045404 A CN 112045404A
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- 230000003028 elevating effect Effects 0.000 claims description 4
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- 230000000712 assembly Effects 0.000 claims description 2
- 238000000429 assembly Methods 0.000 claims description 2
- 238000011084 recovery Methods 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 238000007723 die pressing method Methods 0.000 description 3
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
- B23P19/00—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes
- B23P19/04—Machines for simply fitting together or separating metal parts or objects, or metal and non-metal parts, whether or not involving some deformation; Tools or devices therefor so far as not provided for in other classes for assembling or disassembling parts
- B23P19/06—Screw or nut setting or loosening machines
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Abstract
The invention discloses automatic fixed-torque screwing equipment for connecting a screw sleeve in an engine and a control cabin, which comprises a rack, an engine positioning and rotating device, an automatic engine sliding block position identification device, a fin tool mounting and dismounting device, a control cabin grabbing positioning and rotating device, an automatic control cabin sliding block position identification device and an automatic internal screw sleeve fixed-torque screwing device. The invention can complete the axial automatic alignment of the engine and the control cabin, ensure the simultaneous coplanarity of four pairs of wing sheet grooves, realize the fixed moment automatic tightening of the connecting inner screw sleeves of the engine and the control cabin, have high precision and good consistency, effectively reduce the number of assembling personnel, reduce the labor intensity and improve the production efficiency.
Description
Technical Field
The invention relates to a fixed-torque automatic tightening device for connection of an engine and a threaded sleeve in a control cabin.
Background
At present, production and assembly of an engine and a control cabin in domestic thin-wall products are mainly manual, and manual assembly has the defects of low efficiency, high strength, poor consistency and the like. The engine and the butt joint process of the control cabin need to ensure that four pairs of fin grooves are in a coplanar state respectively, multiple tools need to be adopted for repeated disassembly during manual assembly, and multiple persons are needed for cooperation to complete the assembly. The tightening of interior swivel nut has strict requirement to tightening torque, adopts the moment spanner to carry out exerting of moment of torsion during manual assembly, can't guarantee the uniformity of every product, and the precision is lower.
Disclosure of Invention
In order to solve the technical problems, the invention provides the automatic fixed-torque tightening equipment for connecting the engine and the threaded sleeve in the control cabin, which has the advantages of simple structure, convenience in operation and high working efficiency.
The technical scheme for solving the problems is as follows: a constant-torque automatic tightening device for connecting an engine and a threaded sleeve in a control cabin comprises a frame; the engine positioning and rotating device is arranged at the bottom of the frame and used for mounting the engine and driving the engine to rotate; the automatic engine sliding block position identification device is arranged on the rack and used for identifying the position of the engine sliding block and fixing the engine sliding block; the wing piece tool mounting and dismounting device is mounted at the bottom of the frame, symmetrically arranged at two sides of the engine positioning and rotating device and used for mounting and dismounting a wing piece tool; the control cabin grabbing and positioning and rotating device is arranged on the top of the rack in a lifting manner and is used for grabbing and fixing the control cabin and driving the control cabin to rotate; the automatic control cabin sliding block position identification device is arranged on the rack and used for identifying the position of the control cabin sliding block and fixing the control cabin sliding block; the automatic internal thread sleeve fixed torque screwing device is arranged in the middle of the rack in a lifting mode and used for screwing an internal thread sleeve mounting tool for connecting an engine and a control cabin.
The automatic fixed-torque tightening equipment is connected with the control cabin through the threaded sleeve, the engine positioning and rotating device comprises a positioning seat, a turntable bearing, a servo motor and a first speed reducer, the servo motor is fixedly installed at the bottom of the rack, the servo motor is connected with the lower end face of the turntable bearing through the first speed reducer, the positioning seat is fixedly installed on the upper end face of the turntable bearing, and the engine is placed on the positioning seat.
The engine and control cabin inner threaded sleeve is connected with fixed-torque automatic tightening equipment, the engine slide block position automatic identification device comprises an engine slide block fixing seat and a first position sensor, the first position sensor is fixed on a rack and used for identifying the position of an engine slide block, the engine slide block fixing seat is positioned above the first position sensor, a first slide rail is arranged on the rack along the vertical direction, the engine slide block fixing seat can be slidably mounted at the lower part of the first slide rail and can slide up and down along the lower part of the first slide rail, and a first driving mechanism used for driving the engine slide block fixing seat to slide on the first slide rail is arranged on the rack; after the first position sensor identifies that the engine sliding block rotates to the designated position, the engine sliding block fixing seat descends and is in matched contact with the engine sliding block, and the engine sliding block is prevented from rotating.
The automatic constant-torque tightening device is characterized in that the engine and a control cabin inner threaded sleeve are connected, the wing piece tool mounting and dismounting device comprises a guide ball, a withdrawing bolt component, a push seat, a wing piece tool and a driving cylinder, the driving cylinder is fixedly mounted on the mounting frame, the front end of the driving cylinder is connected with the push seat, and the front end of the push seat is provided with the wing piece tool; the guide balls are arranged on the upper surface and the lower surface of the wing panel tool and used for guiding the wing panel tool; the withdrawing bolt assembly is arranged on the pushing seat, so that the automatic recovery of the fin tool is realized.
The automatic fixed-torque tightening equipment is connected with the threaded sleeves in the control cabin, the number of the pin withdrawing assemblies is two, each pin withdrawing assembly comprises a telescopic cylinder, a pin is arranged at the front end of each telescopic cylinder, the pins correspond to pin holes in the fin tool, the pins are popped out and inserted into the pin holes in the fin tool under the action of the telescopic cylinders, and the fin tool is withdrawn under the action of the driving cylinders.
Above-mentioned engine is connected the automatic equipment of screwing up of fixed moment with interior swivel nut of control cabin, the control cabin snatchs location and rotary device and includes centre gripping gas claw, die-pressing cylinder, mounting panel, rotating electrical machines, second reduction gear and first elevating system, but mounting panel slidable mounting is on first slide rail upper portion and can follow first slide rail upper portion and slide from top to bottom, rotating electrical machines fixed mounting is on the mounting panel, and the rotating electrical machines passes through the second reduction gear and is connected with die-pressing cylinder, and the die-pressing cylinder lower extreme is equipped with centre gripping gas claw, first elevating system fixed mounting is connected at the frame top and with the mounting panel, drives the mounting panel and slides from top to bottom on first slide rail upper portion.
The engine and the control cabin are connected with fixed-torque automatic tightening equipment through a threaded sleeve, the control cabin sliding block position automatic identification device comprises a guide-in air cylinder, a control cabin sliding block fixing seat and a second position sensor, the second position sensor is fixed on a mounting plate and used for identifying the position of a control cabin sliding block, a second sliding rail is arranged on the mounting plate along the vertical direction, the control cabin sliding block fixing seat is located above the second position sensor, the control cabin sliding block fixing seat is slidably mounted on the second sliding rail, and the mounting plate is provided with the guide-in air cylinder used for driving the control cabin sliding block fixing seat to slide on the second sliding rail; after the second position sensor recognizes that the control cabin sliding block rotates to the designated position, the control cabin sliding block fixing seat descends and is in fit contact with the control cabin sliding block, and the control cabin sliding block is prevented from rotating.
The fixed-torque automatic tightening device is connected with the threaded sleeve in the control cabin, the internal threaded sleeve fixed-torque automatic tightening device comprises an internal threaded sleeve tightening tool, a tightening machine and a second lifting mechanism, the internal threaded sleeve tightening tool is slidably mounted in the middle of a first sliding rail and can slide up and down along the middle of the first sliding rail, the tightening machine is mounted on the internal threaded sleeve tightening tool and drives the internal threaded sleeve tightening tool to rotate through a gear set, and the second lifting mechanism is fixedly mounted at the top of the frame and connected with the internal threaded sleeve tightening tool to drive the internal threaded sleeve tightening tool to slide up and down in the middle of the first sliding rail.
The invention has the beneficial effects that:
1. the invention is provided with an engine positioning and rotating device used for installing an engine and driving the engine to rotate, an engine sliding block position automatic identification device used for identifying the position of an engine sliding block and fixing the engine sliding block, a control cabin grabbing positioning and rotating device used for grabbing and fixing a control cabin and driving the control cabin to rotate, and a control cabin sliding block position automatic identification device used for identifying the position of the control cabin sliding block and fixing the control cabin sliding block.
2. The automatic fixed-torque tightening device for the inner thread sleeve is provided with the inner thread sleeve fixed-torque mounting tool for tightening the inner thread sleeve for connecting the engine and the control cabin, can realize automatic tightening of the fixed torque of the inner thread sleeve for connecting the engine and the control cabin, has high precision and good consistency, can effectively reduce the number of assembling personnel, reduces the labor intensity and improves the production efficiency.
Drawings
FIG. 1 is a schematic structural diagram of the present invention.
Detailed Description
The invention is further described below with reference to the figures and examples.
As shown in figure 1, the constant-torque automatic tightening device for the connection of the engine and the threaded sleeve in the control cabin comprises a frame 29; the engine positioning and rotating device 1 is arranged at the bottom of the frame 29 and is used for installing the engine 25 and driving the engine 25 to rotate; an engine block position automatic recognition device 23 mounted on the frame 29 for recognizing the position of the engine block and fixing the engine block; the wing piece tool mounting and dismounting device 2 is mounted at the bottom of the frame 29, symmetrically arranged at two sides of the engine positioning and rotating device 1 and used for mounting and dismounting a wing piece tool 6; the control cabin grabbing and positioning and rotating device 13 is arranged on the top of the frame 29 in a lifting manner and is used for grabbing and fixing the control cabin 20 and driving the control cabin 20 to rotate; a control cabin slider position automatic recognition device 18 mounted on the frame 29 for recognizing the control cabin slider position and fixing the control cabin slider; and the inner sleeve fixed-torque automatic screwing device 9 is arranged in the middle of the frame 29 in a lifting manner and is used for screwing the inner sleeve mounting tool 21 for connecting the engine 25 and the control cabin 20.
The engine positioning and rotating device 1 comprises a positioning seat 28, a turntable bearing 26, a servo motor 27 and a first speed reducer, wherein the servo motor 27 is fixedly installed at the bottom of a rack 29, the servo motor 27 is connected with the lower end face of the turntable bearing 26 through the first speed reducer, the positioning seat 28 is fixedly installed on the upper end face of the turntable bearing 26, and the engine 25 is placed on the positioning seat 28.
The automatic engine block position recognition device 23 comprises an engine block fixing seat 22 and a first position sensor 24, the first position sensor 24 is fixed on a rack 29 and used for recognizing the position of an engine block, the engine block fixing seat 22 is located above the first position sensor 24, a first slide rail 30 is arranged on the rack 29 along the vertical direction, the engine block fixing seat 22 is slidably mounted at the lower part of the first slide rail 30 and can slide up and down along the lower part of the first slide rail 30, and a first driving mechanism used for driving the engine block fixing seat 22 to slide on the first slide rail 30 is arranged on the rack 29; after the first position sensor 24 recognizes that the engine block rotates to the designated position, the engine block fixing seat 22 descends and is in fit contact with the engine block, so that the engine block is prevented from rotating.
The fin tool mounting and dismounting device 2 comprises a guide ball 3, a withdrawing bolt component 4, a pushing seat 5, a fin tool 6 and a driving cylinder 7, wherein the driving cylinder 7 is fixedly mounted on a mounting frame 31, the front end of the driving cylinder 7 is connected with the pushing seat 5, and the front end of the pushing seat 5 is provided with the fin tool 6; the guide balls 3 are arranged on the upper surface and the lower surface of the wing piece tooling 6 and are used for guiding the wing piece tooling 6; the withdrawing bolt assembly 4 is installed on the pushing seat 5, and automatic withdrawing of the fin tool 6 is achieved.
It is two sets of to withdraw bolt subassembly 4 quantity, and every group withdraws bolt subassembly 4 and all includes a telescopic cylinder, and telescopic cylinder front end is equipped with the bolt, the bolt is corresponding with the bolt hole on the fin frock 6, and under telescopic cylinder's effect, the bolt pops out the bolt hole that inserts on the fin frock 6, withdraws fin frock 6 under the effect that drives actuating cylinder 7.
The control cabin grabbing, positioning and rotating device 13 comprises a clamping air claw 11, a pressure applying air cylinder 12, a mounting plate 32, a rotating motor 14, a second speed reducer and a first lifting mechanism 15, wherein the mounting plate 32 can be slidably mounted on the upper portion of a first sliding rail 30 and can slide up and down along the upper portion of the first sliding rail 30, the rotating motor 14 is fixedly mounted on the mounting plate 32, the rotating motor 14 is connected with the pressure applying air cylinder 12 through the second speed reducer, the lower end of the pressure applying air cylinder 12 is provided with the clamping air claw 11, the first lifting mechanism 15 is fixedly mounted at the top of a rack 29 and connected with the mounting plate 32, and the mounting plate 32 is driven to slide up and down on the upper portion.
The control cabin slider position automatic identification device 18 comprises a guide-in air cylinder 16, a control cabin slider fixing seat 17 and a second position sensor 19, the second position sensor 19 is fixed on a mounting plate 32 and used for identifying the position of a control cabin slider, a second slide rail is arranged on the mounting plate 32 along the vertical direction, the control cabin slider fixing seat 17 is positioned above the second position sensor 19, the control cabin slider fixing seat 17 is slidably mounted on the second slide rail, and the mounting plate 32 is provided with the guide-in air cylinder 16 used for driving the control cabin slider fixing seat 17 to slide on the second slide rail; after the second position sensor 19 recognizes that the control cabin sliding block rotates to the designated position, the control cabin sliding block fixing seat 17 descends and is in fit contact with the control cabin sliding block, so that the control cabin sliding block is prevented from rotating.
The automatic tightening device 9 with the fixed torque for the inner threaded sleeve comprises an inner threaded sleeve tightening tool 8, a tightening machine 10 and a second lifting mechanism 33, the inner threaded sleeve tightening tool 8 can be slidably mounted in the middle of a first sliding rail 30 and can slide up and down along the middle of the first sliding rail 30, the tightening machine 10 is mounted on the inner threaded sleeve tightening tool 8 and drives the inner threaded sleeve tightening tool 8 to rotate through a gear set, and the second lifting mechanism 33 is fixedly mounted at the top of a rack 29 and connected with the inner threaded sleeve tightening tool 8 to drive the inner threaded sleeve tightening tool 8 to slide up and down in the middle of the first sliding rail 30.
The first lifting mechanism 15 and the second lifting mechanism 33 have the same structure and can be realized by adopting a combined structure of a driving motor, a guide rail and a lead screw, namely, the driving motor drives the lead screw to rotate, so that the guide rail slides up and down along the lead screw, and a part to be lifted (a mounting plate 32 or an inner sleeve screwing tool 8) is fixedly connected with the guide rail and lifts up and down along with the guide rail.
The invention can automatically complete the axial automatic alignment of the engine 25 and the control cabin 20, and simultaneously carry out the fixed torque tightening on the connecting inner screw sleeve. The specific working process is as follows:
through frame manipulator equipment, carry engine 25 to positioning seat 28 in, through the first sensor measuring the slider position on engine 25, servo motor 27 drive turntable bearing 26 rotates, waits that first position sensor 24 measures the engine block and satisfies the position requirement, and engine block fixing base 22 whereabouts and engine block cooperate to confirm the position relation of engine 25, and can prevent that engine block from rotating.
Through frame manipulator equipment, carry control cabin 20 to centre gripping gas claw 11 below, centre gripping gas claw 11 carries out control cabin 20 and snatchs the operation, measure control cabin slider position through second position sensor 19, rotating electrical machines 14 can make control cabin 20 rotatory, wait that second position sensor 19 measures when control cabin slider satisfies the position requirement, control cabin slider fixing base 17 whereabouts cooperatees with the control cabin slider, prevent that the control cabin slider from rotating, thereby the control cabin 20 position relation is tentatively confirmed.
The control cabin 20 falls to just contact with the engine 25 through the first lifting mechanism 15, then the wing piece tooling 6 is automatically inserted into the two sides of the engine 25 and the control cabin 20 respectively through the wing piece tooling mounting and dismounting device 2, and two bulges at the front end of the wing piece tooling 6 are respectively inserted into the notches of the engine 25 and the control cabin 20 to accurately position the engine 25 and the control cabin 20.
An inner threaded sleeve mounting tool 21 is manually arranged at the joint of the engine 25 and the control cabin 20, the inner threaded sleeve fixed torque automatic tightening device 9 falls to the contact position of the engine 25 and the control cabin 20 through a second lifting mechanism 33, and rated torque is applied to the inner threaded sleeve mounting tool, so that the butt joint of the engine 25 and the control cabin 20 is completed.
After the butt joint is completed, the fin tool 6 is automatically retracted under the action of the retracting bolt assembly 4, the inner sleeve fixed torque automatic tightening device 9 is separated, and the product is moved back to the transmission line through the frame manipulator.
Claims (8)
1. The utility model provides an automatic equipment of screwing up of fixed moment is connected to swivel nut in engine and the control cabin which characterized in that: comprises a frame; the engine positioning and rotating device is arranged at the bottom of the frame and used for mounting the engine and driving the engine to rotate; the automatic engine sliding block position identification device is arranged on the rack and used for identifying the position of the engine sliding block and fixing the engine sliding block; the wing piece tool mounting and dismounting device is mounted at the bottom of the frame, symmetrically arranged at two sides of the engine positioning and rotating device and used for mounting and dismounting a wing piece tool; the control cabin grabbing and positioning and rotating device is arranged on the top of the rack in a lifting manner and is used for grabbing and fixing the control cabin and driving the control cabin to rotate; the automatic control cabin sliding block position identification device is arranged on the rack and used for identifying the position of the control cabin sliding block and fixing the control cabin sliding block; the automatic internal thread sleeve fixed torque screwing device is arranged in the middle of the rack in a lifting mode and used for screwing an internal thread sleeve mounting tool for connecting an engine and a control cabin.
2. The fixed-torque automatic tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 1, characterized in that: the engine positioning and rotating device comprises a positioning seat, a turntable bearing, a servo motor and a first speed reducer, wherein the servo motor is fixedly installed at the bottom of the rack, the servo motor is connected with the lower end face of the turntable bearing through the first speed reducer, the positioning seat is fixedly installed on the upper end face of the turntable bearing, and the engine is placed on the positioning seat.
3. The fixed-torque automatic tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 1, characterized in that: the automatic identification device for the position of the engine sliding block comprises an engine sliding block fixing seat and a first position sensor, wherein the first position sensor is fixed on a rack and used for identifying the position of the engine sliding block, the engine sliding block fixing seat is positioned above the first position sensor, a first sliding rail is arranged on the rack along the vertical direction, the engine sliding block fixing seat is slidably installed on the lower portion of the first sliding rail and can slide up and down along the lower portion of the first sliding rail, and a first driving mechanism used for driving the engine sliding block fixing seat to slide on the first sliding rail is arranged on the rack; after the first position sensor identifies that the engine sliding block rotates to the designated position, the engine sliding block fixing seat descends and is in matched contact with the engine sliding block, and the engine sliding block is prevented from rotating.
4. The fixed-torque automatic tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 3, characterized in that: the fin tool mounting and dismounting device comprises a guide ball, a withdrawing bolt assembly, a push seat, a fin tool and a driving cylinder, wherein the driving cylinder is fixedly mounted on the mounting frame, the front end of the driving cylinder is connected with the push seat, and the fin tool is arranged at the front end of the push seat; the guide balls are arranged on the upper surface and the lower surface of the wing panel tool and used for guiding the wing panel tool; the withdrawing bolt assembly is arranged on the pushing seat, so that the automatic recovery of the fin tool is realized.
5. The automatic fixed-torque tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 4, wherein: the retractable bolt assembly is characterized in that the retractable bolt assemblies are two in number, each retractable bolt assembly comprises a telescopic cylinder, a bolt is arranged at the front end of each telescopic cylinder, the bolt corresponds to a bolt hole in the fin tool, the bolt is popped out to be inserted into the bolt hole in the fin tool under the action of the telescopic cylinders, and the fin tool is retracted under the action of the driving cylinders.
6. The fixed-torque automatic tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 5, characterized in that: the control cabin snatchs location and rotary device includes centre gripping gas claw, air cylinder, mounting panel, rotating electrical machines, second reduction gear and first elevating system, but mounting panel slidable mounting is on first slide rail upper portion and can follow first slide rail upper portion and slide from top to bottom, rotating electrical machines fixed mounting is on the mounting panel, and the rotating electrical machines passes through the second reduction gear and is connected with the air cylinder of exerting pressure, and the air cylinder lower extreme that exerts pressure is equipped with centre gripping gas claw, first elevating system fixed mounting is connected at the frame top and with the mounting panel, drives the mounting panel and slides from top to bottom on first slide rail upper portion.
7. The fixed-torque automatic tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 6, characterized in that: the automatic control cabin slider position recognition device comprises a lead-in air cylinder, a control cabin slider fixing seat and a second position sensor, wherein the second position sensor is fixed on a mounting plate and used for recognizing the position of a control cabin slider; after the second position sensor recognizes that the control cabin sliding block rotates to the designated position, the control cabin sliding block fixing seat descends and is in fit contact with the control cabin sliding block, and the control cabin sliding block is prevented from rotating.
8. The fixed-torque automatic tightening device for connection of the engine and the threaded sleeve in the control cabin according to claim 3, characterized in that: the automatic tightening device with the fixed torque for the inner screw sleeve comprises an inner screw sleeve tightening tool, a tightening machine and a second lifting mechanism, wherein the inner screw sleeve tightening tool is slidably mounted in the middle of a first sliding rail and can slide up and down along the middle of the first sliding rail, the tightening machine is mounted on the inner screw sleeve tightening tool and drives the inner screw sleeve tightening tool to rotate through a gear set, and the second lifting mechanism is fixedly mounted at the top of a frame and connected with the inner screw sleeve tightening tool to drive the inner screw sleeve tightening tool to slide up and down in the middle of the first sliding rail.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010986690.8A CN112045404A (en) | 2020-09-18 | 2020-09-18 | Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010986690.8A CN112045404A (en) | 2020-09-18 | 2020-09-18 | Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin |
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| Publication Number | Publication Date |
|---|---|
| CN112045404A true CN112045404A (en) | 2020-12-08 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010986690.8A Pending CN112045404A (en) | 2020-09-18 | 2020-09-18 | Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112045404A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114749905A (en) * | 2022-05-27 | 2022-07-15 | 安徽巨一科技股份有限公司 | Frock is screwed up in door automatic installation |
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| JP2003145364A (en) * | 2001-11-08 | 2003-05-20 | Daihatsu Motor Co Ltd | Positioning device |
| CN104108020A (en) * | 2014-08-21 | 2014-10-22 | 芜湖莫森泰克汽车科技有限公司 | Auxiliary tool for automatic screw-driving machine |
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| KR20160135496A (en) * | 2015-05-18 | 2016-11-28 | 국방과학연구소 | Assembling apparatus for missile |
| CN111442699A (en) * | 2020-03-31 | 2020-07-24 | 中国科学院沈阳自动化研究所 | Automatic butt joint device |
| CN212398768U (en) * | 2020-09-18 | 2021-01-26 | 江南工业集团有限公司 | Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin |
-
2020
- 2020-09-18 CN CN202010986690.8A patent/CN112045404A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2003145364A (en) * | 2001-11-08 | 2003-05-20 | Daihatsu Motor Co Ltd | Positioning device |
| CN104108020A (en) * | 2014-08-21 | 2014-10-22 | 芜湖莫森泰克汽车科技有限公司 | Auxiliary tool for automatic screw-driving machine |
| KR20160135496A (en) * | 2015-05-18 | 2016-11-28 | 국방과학연구소 | Assembling apparatus for missile |
| CN204975916U (en) * | 2015-08-25 | 2016-01-20 | 马瑞利汽车零部件(芜湖)有限公司 | Valve block installation device of car air throttle |
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| CN212398768U (en) * | 2020-09-18 | 2021-01-26 | 江南工业集团有限公司 | Fixed-torque automatic tightening equipment for connection of engine and threaded sleeve in control cabin |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114749905A (en) * | 2022-05-27 | 2022-07-15 | 安徽巨一科技股份有限公司 | Frock is screwed up in door automatic installation |
| CN114749905B (en) * | 2022-05-27 | 2024-01-12 | 安徽巨一科技股份有限公司 | Automatic mounting and screwing tool for vehicle door |
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