CN113829124A - Six-axis linkage machining center for machining aviation materials - Google Patents
Six-axis linkage machining center for machining aviation materials Download PDFInfo
- Publication number
- CN113829124A CN113829124A CN202111123004.5A CN202111123004A CN113829124A CN 113829124 A CN113829124 A CN 113829124A CN 202111123004 A CN202111123004 A CN 202111123004A CN 113829124 A CN113829124 A CN 113829124A
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- China
- Prior art keywords
- axis linkage
- fixedly connected
- connecting rod
- machining
- machining center
- 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.)
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- 238000003754 machining Methods 0.000 title claims abstract description 15
- 239000000463 material Substances 0.000 title claims abstract description 13
- 229910001018 Cast iron Inorganic materials 0.000 claims abstract description 13
- 230000000694 effects Effects 0.000 claims description 9
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 238000003913 materials processing Methods 0.000 claims description 2
- 239000011825 aerospace material Substances 0.000 claims 5
- 238000000034 method Methods 0.000 abstract description 13
- 230000008569 process Effects 0.000 abstract description 9
- 238000004544 sputter deposition Methods 0.000 abstract description 8
- 230000006378 damage Effects 0.000 abstract description 6
- 230000002265 prevention Effects 0.000 abstract description 6
- 208000027418 Wounds and injury Diseases 0.000 abstract description 3
- 238000004140 cleaning Methods 0.000 abstract description 3
- 208000014674 injury Diseases 0.000 abstract description 3
- 230000009471 action Effects 0.000 description 3
- 238000005452 bending Methods 0.000 description 2
- 230000003139 buffering effect Effects 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000004075 alteration Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000002699 waste material Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q11/00—Accessories fitted to machine tools for keeping tools or parts of the machine in good working condition or for cooling work; Safety devices specially combined with or arranged in, or specially adapted for use in connection with, machine tools
- B23Q11/08—Protective coverings for parts of machine tools; Splash guards
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q1/00—Members which are comprised in the general build-up of a form of machine, particularly relatively large fixed members
- B23Q1/70—Stationary or movable members for carrying working-spindles for attachment of tools or work
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Milling Processes (AREA)
Abstract
The invention discloses a six-axis linkage machining center for machining aviation materials, which comprises a cast iron workbench, wherein the top of the cast iron workbench is connected with a machine tool beam in a sliding manner, the top of the machine tool beam is connected with a six-axis swinging head in a sliding manner, the bottom of the six-axis swinging head is provided with a cutter body, the bottom of the cutter body is fixedly connected with a cutter head, the surface of the cutter body is movably sleeved with a shaft sleeve, the front end and the back end of the bottom of the shaft sleeve are both fixedly connected with connecting rods, and the bottom of the connecting rods is fixedly connected with a circular baffle. According to the six-axis linkage machining equipment, materials are placed inside the cast iron workbench by a user, and then the shaft sleeve is rotated manually, so that the problem that scraps are splashed out to cause injury because the existing six-axis linkage machining equipment does not have the sputtering prevention function in the working process is solved, the labor force for cleaning by the user is reduced, and the working efficiency of the six-axis linkage machining equipment is improved.
Description
Technical Field
The invention relates to the technical field of aviation material processing, in particular to a six-axis linkage processing center for aviation material processing.
Background
The six-axis linkage ultrasonic machining center adopts a bridge type gantry structure, a workbench of the six-axis linkage ultrasonic machining center is fixed, a beam is directly connected to an X-axis base to move a front X-axis and a back X-axis, a saddle is arranged on the beam to move a Y-axis leftwards and rightwards, a ram internally comprises a main shaft and a double-swing head to move a Z-axis on the saddle and move a Z-axis downwards, and a double-swing head A/C shaft is fixedly arranged on a clear pillow.
Six-axis linkage processing equipment is needed in the processing of aviation materials, but the existing six-axis linkage processing equipment does not have the function of sputtering prevention during working, so that scraps are splashed out to cause injury, the labor force for cleaning by a user is increased, the working efficiency of the six-axis linkage processing equipment is reduced, and the practicability of the six-axis linkage processing equipment is also reduced.
Disclosure of Invention
In order to solve the problems in the background art, the invention aims to provide a six-axis linkage machining center for aviation material machining, which has the advantage of good sputtering prevention and solves the problem that the existing six-axis linkage machining equipment does not have the sputtering prevention function in the working process, so that scraps are splashed out to cause damage.
In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a six linkage machining centers for aeronautical materials processing, includes the cast iron workstation, the top sliding connection of cast iron workstation has the lathe crossbeam, the top sliding connection of lathe crossbeam has six yaw, the bottom of six yaw is provided with the blade, the bottom fixedly connected with tool bit of blade, the axle sleeve has been cup jointed in the surface activity of blade, the equal fixedly connected with connecting rod in front end and the back of the body end of axle sleeve bottom, the circular baffle of bottom fixedly connected with of connecting rod.
Preferably, the surface of the knife body is provided with threads, the cross-sectional area of the threads is equal to that of the knife body, and the shaft sleeve is matched with the threads and correspondingly arranged.
Preferably, the left side and the right side of the surface of the shaft sleeve are fixedly connected with friction blocks, the friction blocks are rectangular, and the friction blocks are distributed uniformly.
Preferably, the bottom of the circular baffle is fixedly connected with a rubber layer, the thickness of the rubber layer is more than three millimeters, and the rubber layer and the circular baffle are correspondingly matched.
Preferably, the surface of the circular baffle is provided with a through hole, and the diameter of the through hole is larger than that of the cutter body.
Preferably, the connecting rod is made of aluminum alloy and is matched with the round baffle correspondingly.
Compared with the prior art, the invention has the following beneficial effects:
1. the invention arranges a cast iron workbench, a machine tool beam, a six-axis swinging head, a tool magazine, a tool body, a tool bit, a shaft sleeve, a connecting rod and a round baffle plate in a matching and corresponding way, a user places materials inside the cast iron workbench, then manually rotates the shaft sleeve, the shaft sleeve is matched with a friction block to increase the resistance with a palm so as to be convenient to operate, the shaft sleeve rotates clockwise and is matched with a thread to move downwards, the shaft sleeve moves downwards to drive the connecting rod to move downwards synchronously, the connecting rod moves downwards to drive the round baffle plate to move, the round baffle plate moves downwards to be close to the position of the tool bit and is fixed, finally, the machine tool is started to work so that the six-axis swinging head automatically processes according to a program, the round baffle plate is matched with a rubber layer to block waste scraps generated in the rotating work of the six-axis swinging head driving the tool body and the tool bit working tool bit, the anti-sputtering effect is realized, and the problem that the existing six-axis linkage processing equipment does not have the anti-sputtering effect in the work is solved, the problem of injury is caused to the sweeps of splashing, the labor force for cleaning a user is reduced, and the working efficiency of the six-axis linkage processing equipment is improved.
2. The invention can assist the shaft sleeve to work by arranging the threads, avoids the phenomenon of slipping in the moving process of the shaft sleeve and also increases the stability of mechanical work.
3. The friction block is arranged, so that the shaft sleeve can be assisted to work, the friction effect is increased, the slipping phenomenon in the process of manually rotating the shaft sleeve by a user is avoided, and the working convenience of the shaft sleeve is improved.
4. The rubber layer is arranged, so that the round baffle can be assisted to work, the protection and buffering effects are achieved, and the round baffle is prevented from being damaged by scrapsAppear under impact
The damage phenomenon prolongs the service life of the round baffle.
5. According to the invention, through the arrangement of the through hole, the cutter body can be assisted to work, the phenomenon that the circular baffle is blocked on the surface of the cutter body due to the over-narrow width of the through hole is avoided, and the convenience of mechanical work is also improved.
6. According to the invention, the connecting rod is made of aluminum alloy, so that the metal strength of the connecting rod can be improved, the phenomenon of bending and cracking of the connecting rod in long-time use is avoided, and the safety of mechanical work is also improved.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a front view of the blade and bit configuration of FIG. 1 in accordance with the present invention;
FIG. 3 is a cross-sectional view of the blade and cutting head configuration of FIG. 2 in accordance with the present invention;
FIG. 4 is a top view of the blade body structure of FIG. 2 in accordance with the present invention;
fig. 5 is a perspective view of the circular baffle structure of fig. 3 according to the present invention.
In the figure: 1. a cast iron workbench; 2. a machine tool cross beam; 3. swinging the head by six axes; 4. a blade body; 5. a cutter head; 6. a shaft sleeve; 7. a connecting rod; 8. a circular baffle; 9. a thread; 10. a friction block; 11. a rubber layer; 12. and a through hole.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
As shown in fig. 1 to 5, the six-axis linkage machining center for machining aviation materials provided by the invention comprises a cast iron workbench 1, wherein the top of the cast iron workbench 1 is slidably connected with a machine tool cross beam 2, the top of the machine tool cross beam 2 is slidably connected with a six-axis swinging head 3, the bottom of the six-axis swinging head 3 is provided with a cutter body 4, the bottom of the cutter body 4 is fixedly connected with a cutter head 5, the surface of the cutter body 4 is movably sleeved with a shaft sleeve 6, the front end and the back end of the bottom of the shaft sleeve 6 are both fixedly connected with a connecting rod 7, and the bottom of the connecting rod 7 is fixedly connected with a circular baffle 8.
Referring to fig. 1, the surface of the blade 4 is provided with a thread 9, the cross-sectional area of the thread 9 is equal to the cross-sectional area of the blade 4, and the bushing 6 is correspondingly provided to cooperate with the thread 9.
Adopt above-mentioned scheme: through the setting of screw thread 9, can assist axle sleeve 6 to carry out work, avoided 6 phenomena that appear skidding of removal in-process of axle sleeve, also increase mechanical work's stability.
Referring to fig. 1, friction blocks 10 are fixedly connected to both left and right sides of the surface of the shaft sleeve 6, the friction blocks 10 are rectangular, and the friction blocks 10 are distributed uniformly.
Adopt above-mentioned scheme: through the setting of clutch blocks 10, can assist axle sleeve 6 to work, play the effect of increasing friction simultaneously, avoid the phenomenon of skidding to appear in the manual rotatory in-process of axle sleeve 6 of user, also improve the convenience of axle sleeve 6 work.
Referring to fig. 4, a rubber layer 11 is fixedly connected to the bottom of the circular baffle 8, the thickness of the rubber layer 11 is greater than three millimeters, and the rubber layer 11 is correspondingly matched with the circular baffle 8.
Adopt above-mentioned scheme: through the setting on rubber layer 11, can assist circular baffle 8 to carry out work, play the effect of protection buffering simultaneously, avoided circular baffle 8 to appear hitting of sweeps and hit under hitting
The damage phenomenon prolongs the service life of the circular baffle plate 8.
Referring to fig. 4, a through hole 12 is formed on the surface of the circular baffle 8, and the diameter of the through hole 12 is larger than that of the blade 4.
Adopt above-mentioned scheme: through the setting of through-hole 12, can assist blade 4 to carry out work, the width that has avoided through-hole 12 is too narrow to lead to circular baffle 8 to appear the dead phenomenon of card on the surface of blade 4, also improves the convenience of mechanical work.
Referring to fig. 1, the connecting rod 7 is made of aluminum alloy, and the connecting rod 7 is correspondingly matched with the circular baffle 8.
Adopt above-mentioned scheme: the material through connecting rod 7 is the setting of aluminum alloy, can improve connecting rod 7's metal strength, has avoided connecting rod 7 to appear bending fracture's phenomenon in long-time use, also improves mechanical work's security.
According to the invention, materials are placed in the cast iron workbench 1, then the shaft sleeve 6 is manually rotated, the shaft sleeve 6 is matched with the friction block 10 to increase resistance with a palm, so that the operation is convenient, the shaft sleeve 6 is rotated clockwise and matched with the screw threads 9 to move downwards, the shaft sleeve 6 moves downwards to drive the connecting rod 7 to synchronously move downwards, the connecting rod 7 moves downwards to drive the circular baffle 8 to move, the circular baffle 8 moves downwards to be close to the position of the tool bit 5 to be fixed, finally, the machine tool is started to work to enable the six-shaft swinging head 3 to automatically process according to a program, the six-shaft swinging head 3 works to drive the tool body 4 and the tool bit 5 to generate scraps in the rotating work, and meanwhile, the circular baffle 8 is matched with the rubber layer 11 to block, so that the sputtering prevention effect is realized, and the problem that the existing six-shaft linkage processing equipment does not have the sputtering prevention effect in the working process is solved.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides a six-shaft linkage machining center for aeronautical materials processing, includes cast iron workstation (1), its characterized in that: the top sliding connection of cast iron workstation (1) has lathe crossbeam (2), the top sliding connection of lathe crossbeam (2) has six yaw (3), the bottom of six yaw (3) is provided with blade (4), the bottom fixedly connected with tool bit (5) of blade (4), axle sleeve (6) have been cup jointed in the surface activity of blade (4), the equal fixedly connected with connecting rod (7) of front end and the back of the body end of axle sleeve (6) bottom, the bottom fixedly connected with circular baffle (8) of connecting rod (7).
2. The six-axis linkage machining center for aerospace material machining of claim 1, wherein: the surface of the knife body (4) is provided with threads (9), the cross-sectional area of the threads (9) is equal to that of the knife body (4), and the shaft sleeve (6) is matched with the threads (9) and correspondingly arranged.
3. The six-axis linkage machining center for aerospace material machining of claim 2, wherein: the left side and the right side on axle sleeve (6) surface all fixedly connected with clutch blocks (10), the shape of clutch blocks (10) is the rectangle, the quantity of clutch blocks (10) is a plurality of, and evenly distributed.
4. The six-axis linkage machining center for aerospace material machining of claim 3, wherein: the bottom of the round baffle (8) is fixedly connected with a rubber layer (11), the thickness of the rubber layer (11) is larger than three millimeters, and the rubber layer (11) and the round baffle (8) are correspondingly matched.
5. The six-axis linkage machining center for aerospace material machining of claim 4, wherein: the surface of the circular baffle (8) is provided with a through hole (12), and the diameter of the through hole (12) is larger than that of the knife body (4).
6. The six-axis linkage machining center for aerospace material machining of claim 5, wherein: the material of connecting rod (7) is the aluminum alloy, connecting rod (7) correspond the setting with circular baffle (8) cooperation.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111123004.5A CN113829124A (en) | 2021-09-24 | 2021-09-24 | Six-axis linkage machining center for machining aviation materials |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111123004.5A CN113829124A (en) | 2021-09-24 | 2021-09-24 | Six-axis linkage machining center for machining aviation materials |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN113829124A true CN113829124A (en) | 2021-12-24 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202111123004.5A Pending CN113829124A (en) | 2021-09-24 | 2021-09-24 | Six-axis linkage machining center for machining aviation materials |
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| Country | Link |
|---|---|
| CN (1) | CN113829124A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20150004662U (en) * | 2014-06-23 | 2015-12-31 | 안숙희 | Device for preventing chip of machine from splashing |
| CN207577494U (en) * | 2017-11-08 | 2018-07-06 | 苏州卓航电子有限公司 | A kind of drilling ancillary equipment for the drilling machine for producing FPC plates |
| CN108453311A (en) * | 2018-07-11 | 2018-08-28 | 林枫 | A kind of carbide-tipped reamer |
| CN213317749U (en) * | 2020-09-24 | 2021-06-01 | 昆山欧久精密刀具有限公司 | Precision alloy cutter with noise reduction structure |
| CN214053799U (en) * | 2020-11-27 | 2021-08-27 | 常州市创锦工具有限公司 | Four-edge cutting milling cutter with dust collection cover |
-
2021
- 2021-09-24 CN CN202111123004.5A patent/CN113829124A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20150004662U (en) * | 2014-06-23 | 2015-12-31 | 안숙희 | Device for preventing chip of machine from splashing |
| CN207577494U (en) * | 2017-11-08 | 2018-07-06 | 苏州卓航电子有限公司 | A kind of drilling ancillary equipment for the drilling machine for producing FPC plates |
| CN108453311A (en) * | 2018-07-11 | 2018-08-28 | 林枫 | A kind of carbide-tipped reamer |
| CN213317749U (en) * | 2020-09-24 | 2021-06-01 | 昆山欧久精密刀具有限公司 | Precision alloy cutter with noise reduction structure |
| CN214053799U (en) * | 2020-11-27 | 2021-08-27 | 常州市创锦工具有限公司 | Four-edge cutting milling cutter with dust collection cover |
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