CN208913538U - A kind of aircraft medical aid system assembly or fitting table - Google Patents

A kind of aircraft medical aid system assembly or fitting table Download PDF

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Publication number
CN208913538U
CN208913538U CN201821539441.9U CN201821539441U CN208913538U CN 208913538 U CN208913538 U CN 208913538U CN 201821539441 U CN201821539441 U CN 201821539441U CN 208913538 U CN208913538 U CN 208913538U
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CN
China
Prior art keywords
fixed
fitting table
assembly
axis
cylinder
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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.)
Expired - Fee Related
Application number
CN201821539441.9U
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Chinese (zh)
Inventor
陈寿富
陈益强
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.)
Nanjing Zhonghao Machinery Manufacturing Co Ltd
Original Assignee
Nanjing Zhonghao Machinery Manufacturing 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
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Priority to CN201821539441.9U priority Critical patent/CN208913538U/en
Application granted granted Critical
Publication of CN208913538U publication Critical patent/CN208913538U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of aircraft medical aid system assembly or fitting tables, including clamping mechanism, transmission mechanism, elevating mechanism and certainly stubborn mechanism.Wherein, clamping mechanism includes pedestal, sliding slot, the first cylinder, column, bracket, electric cylinder and gripper;Transmission mechanism includes the X-axis cylinder for being fixed on aforementioned pedestal side, the X-axis slide rail for being installed in parallel in X-axis cylinder two sides, the sliding block being mounted in the X-axis slide rail and fixed assembly or fitting table on the slide block;Elevating mechanism includes guide post, the link block for being fixed on the guide post end, the Z axis cylinder being fixed on the link block and stretches out the L-shaped fixed plate for being fixed on the link block side;It include the gripping block being mounted on aforementioned L-shaped fixed plate and pneumatic screw driver from stubborn mechanism.The utility model relates to a kind of aircraft medical aid system assembly or fitting tables, can be automatically performed clamping, transport and the assembly working to workpiece, using double-station automatic assembling, improve assembly efficiency.

Description

A kind of aircraft medical aid system assembly or fitting table
Technical field
The utility model relates to a kind of assembly or fitting tables, and in particular to a kind of aircraft medical aid system assembly or fitting table.
Background technique
Standardization and interchangeability of the Automated assembly based on components in 19th century machinery manufacturing industry start for small-sized force The production of device and clock and watch is then applied to auto industry again.In 20th century, Ford Motor Company, the U.S. is initially set up using transport Operation break-down is carried out professional assembly manipulation in each process, shortens about assembly period by the mobile automobile assembly line of band 90%, reduce production cost.The emergence and development of interchangeability manufacture and mobile assembly line are large quantities of mass productions using automatic Change opens road, and it is simple automatic then to occur hopper-type self-feeder and screw, automatic tightening machine for nut etc. successively Makeup is set.Automatic assembling is usually single-station assembly in the prior art, and workpiece usually requires artificially to be placed on assembly or fitting table simultaneously Artificially to center, the degree of automation is not high.
Utility model content
Purpose of utility model: a kind of aircraft medical aid system assembly or fitting table is provided, under the premise of guaranteeing assembly precision By setting gripper and pneumatic screw driver, to solve the above problem of the existing technology.
A kind of technical solution: aircraft medical aid system assembly or fitting table, characterized in that include: clamping mechanism, conveyer Structure, elevating mechanism and certainly stubborn mechanism;
Wherein, clamping mechanism include pedestal, the sliding slot that the pedestal side is set, be fixed on the sliding slot end One cylinder, the column being arranged on the sliding slot, the bracket being fixed on the column, the electric cylinder of installation on the bracket And it is fixed on the gripper of the electric cylinder side;
Transmission mechanism includes the X-axis cylinder for being fixed on the aforementioned pedestal other side, is installed in parallel in X-axis cylinder two sides X-axis slide rail, fixed assembly or fitting table on the slide block, is fixed on the assembly or fitting table one at the sliding block being mounted in the X-axis slide rail The Y-axis cylinder of side and the Y-axis sliding rail for being installed in parallel in Y-axis cylinder two sides;
Elevating mechanism includes being fixed on the guide post of close X-axis slide rail side on aforementioned pedestal, being fixed on the guide post end Link block, the Z axis cylinder that is fixed on the link block and stretch out the L-shaped fixed plate for being fixed on the link block side;
Include the gripping block being mounted on aforementioned L-shaped fixed plate from stubborn mechanism and is fixed by the gripping block pneumatic Screwdriver.
In a further embodiment, the electric cylinder is planetary ball electric cylinder, for transporting the rotation of servo motor Turn changes linear motion into, and gripper is driven accurately to feed.
In a further embodiment, the pneumatic screw driver includes pneumatic motor, gun body and pipette tips, for by pneumatic electricity The torque that machine generates is screwed into or unclamps bolt.
In a further embodiment, the pipette tips are quick change pipette tips, quick for being carried out according to the bolt of different flower-shapes Replacement.
In a further embodiment, the pneumatic motor is more air inlet eccentric motors, for the compression by high pressure Air blows motor blade and rotates rotor, externally exports rotary motion.
In a further embodiment, it is provided with photoelectric sensor on the L-shaped fixed plate, for emitting optical signal.
In a further embodiment, it is provided with receiver on the assembly or fitting table, for receiving photoelectric sensor sending Optical signal.
In a further embodiment, the assembly or fitting table and pneumatic screw driver are two groups, are filled simultaneously for double-station Match.
The utility model has the advantages that the utility model relates to a kind of aircraft medical aid system assembly or fitting table, by the way that clamping mechanism is arranged, By workpiece holding to be assembled and it is transmitted to assembly or fitting table, photoelectric sensor is gone up and down for being automatically positioned the location of workpiece by setting Pneumatic screw driver is simultaneously installed on the elevating mechanism by mechanism, puts correct rear lifting mechanism when the location of workpiece and drives pneumatic screw Knife slowly declines, and generates powerful torque by the pneumatic motor on the pneumatic screw driver and twist the bolt of workpiece to be assembled Tightly.A kind of aircraft medical aid system assembly or fitting table can be automatically performed clamping, transport and assembly working to workpiece, lead to It crosses setting double-station while assembling, liberation assembly manpower improves production efficiency.
Detailed description of the invention
Fig. 1 is the perspective view of the utility model;
Fig. 2 is the partial enlarged view of the utility model;
Fig. 3 is the main view of pneumatic screw driver in the utility model;
Appended drawing reference are as follows: pedestal 1, sliding slot 2, the first cylinder 3, bracket 4, electric cylinder 5, column 6, X-axis cylinder 7, gripper 8, photoelectric sensor 9, guide post 10, receiver 11, L-shaped fixed plate 12, Z axis cylinder 13, link block 14, pneumatic screw driver 15, rifle First 151, gun body 152, gripping block 153, pneumatic motor 154, Y-axis cylinder 16, X-axis slide rail 17, Y-axis sliding rail 18, workpiece 19, assembling Platform 20, sliding block 21.
Specific embodiment
In the following description, a large amount of concrete details are given so as to provide a more thorough understanding of the present invention.So And it is obvious to the skilled person that the present invention may not need one or more of these details and be able to Implement.In other examples, in order to avoid confusion with the present invention, for some technical characteristics well known in the art not into Row description.
A kind of aircraft medical aid system assembly or fitting table 20, including clamping mechanism, transmission mechanism, elevating mechanism and certainly stubborn machine Structure, wherein clamping mechanism includes pedestal 1, and the side of the pedestal 1 is equipped with sliding slot 2, is provided with column 6 on the sliding slot 2, described Column 6 is equipped with bracket 4, is fixed with electric cylinder 5 on the bracket 4, the side of the electric cylinder 5 is equipped with gripper 8;Transmission Mechanism includes the X-axis cylinder 7 for being fixed on aforementioned 1 other side of pedestal, and 7 two sides of X-axis cylinder are equipped with a pair of X being parallel to each other Axis sliding rail 17 is equipped with sliding block 21 in the X-axis slide rail 17, assembly or fitting table 20, the assembly or fitting table 20 is equipped on the sliding block 21 Side be fixed with Y-axis cylinder 16, the two sides of the Y-axis cylinder 16 are equipped with a pair of Y-axis sliding rail 18 being parallel to each other;Elevator Structure includes the guide post 10 being fixed on aforementioned pedestal 1 close to 17 side of X-axis slide rail, and the end of the guide post 10 is equipped with link block 14, Z axis cylinder 13 is fixed on the link block 14, and the side of the link block 14 is equipped with one piece of L-shaped fixed plate 12;From twist Mechanism includes the gripping block 153 being mounted on aforementioned L-shaped fixed plate 12 and the pneumatic screw fixed by the gripping block 153 Knife 15.
When workpiece 19 needs assembled, clamping mechanism is first begin to work: first being grabbed by gripper 8, by described First cylinder 3 drives column 6 mobile, when the column 6 is moved to the X-axis cylinder 7 on one wire, electric cylinder at this time 5 start to work, and gripper 8 is driven accurately to feed, and gripper 8 unclamps after workpiece 19 is in place, and returns according to original approach.This When workpiece 19 be correctly placed on assembly or fitting table 20, transmission mechanism start to work: the X-axis cylinder 7 is with movable slider 21 along institute The movement of X-axis slide rail 17 is stated, and then drives the assembly or fitting table 20 being fixed on the sliding block 21 mobile, the 16 drive group of Y-axis cylinder Dress platform 20 is moved along the Y-axis sliding rail 18, at this time transmission mechanism complementing each other to form by X-axis cylinder 7 and Y-axis cylinder 16 Cross slid platform, control assembly or fitting table 20 are moved to suitable position.Elevating mechanism is started to work at the same time, 13 band of Z axis cylinder Dynamic L-shaped fixed plate 12 moves in the vertical direction, so that 15 liters of the pneumatic screw driver being mounted on the L-shaped fixed plate 12 Drop, the elevating mechanism and transmission mechanism cooperate, and photoelectric sensor 9 are provided on the L-shaped fixed plate 12, for emitting Optical signal is provided with receiver 11 on the assembly or fitting table 20, for receiving the optical signal of the sending of photoelectric sensor 9, the reception The position of device 11 and photoelectric sensor 9 has corrected that correctly, when receiver 11 can receive the light letter of the sending of photoelectric sensor 9 Number when, this means that assembly or fitting table 20 positioned the bolt of the workpiece 19 being correctly fixed at this time on assembly or fitting table 20 i.e. with pneumatic spiral shell Silk knife 15 is conllinear, and the pneumatic screw driver 15 of elevating mechanism control at this time slowly declines, when the pipette tips 151 of the pneumatic screw driver 15 are inserted After entering bolt, pneumatic motor 154 starts running, and pipette tips 151 is driven to rotate, and the flower-shape of pipette tips 151 and the flower-shape of bolt coincide, gas Dynamic motor 154 generates powerful torque to tighten bolt.
Preferably, the electric cylinder 5 is planetary ball electric cylinder, can convert the rotary motion of servo motor and be in line Movement drives gripper 8 accurately to feed, and accomplishes steadily, at the uniform velocity to feed.
Preferably, the pipette tips 151 are quick change pipette tips 151, carry out quick replacement, such as cross according to the bolt of different flower-shapes Shape, interior hexagon, outer-hexagonal shape, quincunx etc..
Preferably, the pneumatic motor 154 is more air inlet eccentric motors, blows motor leaf by the compressed air of high pressure Piece and rotate rotor, externally export rotary motion.
As described above, although the utility model has been indicated and described referring to specific preferred embodiment, it must not It is construed to the limitation to the utility model itself.In the spirit and scope for not departing from the utility model that appended claims define Under the premise of, it can be made a variety of changes in the form and details.

Claims (7)

1. a kind of aircraft medical aid system assembly or fitting table, it is characterized in that: including:
Clamping mechanism, including pedestal, sliding slot that the pedestal side is set, the first cylinder for being fixed on the sliding slot end, The column that is arranged on the sliding slot, the bracket being fixed on the column, installation electric cylinder on the bracket and solid It is scheduled on the gripper of the electric cylinder side;
Transmission mechanism, including the X-axis cylinder for being fixed on the aforementioned pedestal other side, the X-axis that is installed in parallel in X-axis cylinder two sides Sliding rail, fixed assembly or fitting table on the slide block, is fixed on the assembly or fitting table side at the sliding block being mounted in the X-axis slide rail Y-axis cylinder and be installed in parallel in the Y-axis sliding rails of Y-axis cylinder two sides;
Elevating mechanism, including the company for being fixed on the guide post of close X-axis slide rail side on aforementioned pedestal, being fixed on the guide post end It connects block, the Z axis cylinder that is fixed on the link block and stretch out the L-shaped fixed plate for being fixed on the link block side;
From stubborn mechanism, including the gripping block being mounted on aforementioned L-shaped fixed plate and the pneumatic spiral shell fixed by the gripping block Silk knife.
2. a kind of aircraft medical aid system assembly or fitting table according to claim 1, it is characterised in that: the electric cylinder is Planetary ball electric cylinder.
3. a kind of aircraft medical aid system assembly or fitting table according to claim 1, it is characterised in that: the pneumatic screw Knife includes pneumatic motor, gun body and pipette tips.
4. a kind of aircraft medical aid system assembly or fitting table according to claim 3, it is characterised in that: the pipette tips are fast Change pipette tips.
5. a kind of aircraft medical aid system assembly or fitting table according to claim 3, it is characterised in that: the pneumatic motor For more air inlet eccentric motors.
6. a kind of aircraft medical aid system assembly or fitting table according to claim 1, it is characterised in that: on the assembly or fitting table It is provided with receiver, is provided with photoelectric sensor on the L-shaped fixed plate.
7. a kind of aircraft medical aid system assembly or fitting table according to claim 1, it is characterised in that: the assembly or fitting table and Pneumatic screw driver is two groups.
CN201821539441.9U 2018-09-20 2018-09-20 A kind of aircraft medical aid system assembly or fitting table Expired - Fee Related CN208913538U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821539441.9U CN208913538U (en) 2018-09-20 2018-09-20 A kind of aircraft medical aid system assembly or fitting table

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821539441.9U CN208913538U (en) 2018-09-20 2018-09-20 A kind of aircraft medical aid system assembly or fitting table

Publications (1)

Publication Number Publication Date
CN208913538U true CN208913538U (en) 2019-05-31

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201821539441.9U Expired - Fee Related CN208913538U (en) 2018-09-20 2018-09-20 A kind of aircraft medical aid system assembly or fitting table

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111644835A (en) * 2020-06-06 2020-09-11 深圳市初心自动化设备有限公司 Pressure equipment of transducer
CN113459028A (en) * 2021-07-06 2021-10-01 深圳市众迈科技有限公司 Intelligent disassembling equipment for gradient utilization of power battery

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111644835A (en) * 2020-06-06 2020-09-11 深圳市初心自动化设备有限公司 Pressure equipment of transducer
CN113459028A (en) * 2021-07-06 2021-10-01 深圳市众迈科技有限公司 Intelligent disassembling equipment for gradient utilization of power battery

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GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190531

Termination date: 20200920

CF01 Termination of patent right due to non-payment of annual fee