CN117381049A - Aviation pipe cyclone cutting device and cutting method thereof - Google Patents
Aviation pipe cyclone cutting device and cutting method thereof Download PDFInfo
- Publication number
- CN117381049A CN117381049A CN202311616612.9A CN202311616612A CN117381049A CN 117381049 A CN117381049 A CN 117381049A CN 202311616612 A CN202311616612 A CN 202311616612A CN 117381049 A CN117381049 A CN 117381049A
- Authority
- CN
- China
- Prior art keywords
- cutting
- cutter
- feeding
- motor
- pipe
- 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.)
- Pending
Links
- 238000005520 cutting process Methods 0.000 title claims abstract description 120
- 238000000034 method Methods 0.000 title claims abstract description 15
- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 239000000463 material Substances 0.000 claims description 5
- 238000001816 cooling Methods 0.000 claims description 4
- 239000000428 dust Substances 0.000 claims description 3
- 238000009826 distribution Methods 0.000 abstract description 2
- 238000012545 processing Methods 0.000 description 4
- 238000013459 approach Methods 0.000 description 3
- 238000013461 design Methods 0.000 description 3
- 239000002994 raw material Substances 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 229910002065 alloy metal Inorganic materials 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000001125 extrusion Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000012423 maintenance 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23D—PLANING; SLOTTING; SHEARING; BROACHING; SAWING; FILING; SCRAPING; LIKE OPERATIONS FOR WORKING METAL BY REMOVING MATERIAL, NOT OTHERWISE PROVIDED FOR
- B23D21/00—Machines or devices for shearing or cutting tubes
- B23D21/04—Tube-severing machines with rotating tool-carrier
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23D—PLANING; SLOTTING; SHEARING; BROACHING; SAWING; FILING; SCRAPING; LIKE OPERATIONS FOR WORKING METAL BY REMOVING MATERIAL, NOT OTHERWISE PROVIDED FOR
- B23D33/00—Accessories for shearing machines or shearing devices
- B23D33/02—Arrangements for holding, guiding, and/or feeding work during the operation
-
- 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
- B23Q5/00—Driving or feeding mechanisms; Control arrangements therefor
- B23Q5/02—Driving main working members
- B23Q5/04—Driving main working members rotary shafts, e.g. working-spindles
- B23Q5/10—Driving main working members rotary shafts, e.g. working-spindles driven essentially by electrical means
-
- 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
- B23Q5/00—Driving or feeding mechanisms; Control arrangements therefor
- B23Q5/22—Feeding members carrying tools or work
- B23Q5/34—Feeding other members supporting tools or work, e.g. saddles, tool-slides, through mechanical transmission
- B23Q5/38—Feeding other members supporting tools or work, e.g. saddles, tool-slides, through mechanical transmission feeding continuously
- B23Q5/46—Feeding other members supporting tools or work, e.g. saddles, tool-slides, through mechanical transmission feeding continuously with variable speed ratio
Abstract
The invention discloses an aviation pipe cyclone cutting device and a cutting method thereof, wherein the aviation pipe cyclone cutting device comprises a clamping device and a cutting head, wherein the cutting head comprises a base, a driving mechanism connected to the base and a cutting mechanism connected to the driving mechanism; the driving mechanism comprises a main motor and a feeding motor, the cutting mechanism comprises a cutter disc, a spiral rotary disc connected outside the cutter disc and a plurality of cutting tools connected between the cutter disc and the spiral rotary disc, the cutter disc is connected to and driven by the main motor, and the spiral rotary disc is connected to and driven by the feeding motor. According to the invention, the stress distribution of the pipe during cutting is changed by changing the composition and the movement mode of the traditional cutting structure, and the cutting efficiency and the automation degree of the pipe can be improved.
Description
Technical Field
The invention belongs to the technical field of pipe processing, and particularly relates to an aviation pipe cyclone cutting device and an aviation pipe cyclone cutting method.
Background
Pipeline systems of aerospace craft include causing pipeline, hydraulic pipeline, fuel pipeline, etc., pipeline system is the life line of aircraft, directly influences the overall performance of aircraft. Reliability and durability of the pipeline system are important factors for meeting the airworthiness requirements, guaranteeing the flight safety and reducing the maintenance cost.
In the prior art, most of aviation pipes are alloy metal pipes, and in the early rolling process, the length of a general single pipe body is unequal by 3-6m in order to save working procedures, so that the pipes are required to be cut according to requirements. In existing cutting devices, the tubing is typically held by a clamping jaw or other similar clamping mechanism and cut by rotating the tubing and using a grinding wheel. However, the cutting mode has certain defects, on one hand, the mode of grinding wheel cutting has high noise, and the working environment in a factory is bad; on the other hand, when the blade of the cutting grinding wheel is pressed down for cutting in the traditional cutting mode, the extrusion force is instantly increased, so that the circumferential surface of the pipe is unbalanced, the pipe can deform, and particularly the problems of uneven pipe notch and the like occur.
Disclosure of Invention
The invention aims to provide an aviation pipe cyclone cutting device, which changes the stress distribution of a pipe during cutting by changing the constitution and the movement mode of a traditional cutting structure, and can improve the cutting efficiency and the automation degree of the pipe.
In order to achieve the above purpose, the technical scheme adopted by the invention is as follows:
the aviation pipe whirlwind cutting device comprises a clamping device and a cutting head, wherein the cutting head comprises a base, a driving mechanism connected to the base and a cutting mechanism connected to the driving mechanism; the driving mechanism comprises a main motor and a feeding motor, the cutting mechanism comprises a cutter disc, a spiral rotary disc connected outside the cutter disc and a plurality of cutting tools connected between the cutter disc and the spiral rotary disc, the cutter disc is connected to and driven by the main motor, and the spiral rotary disc is connected to and driven by the feeding motor.
Further, each cutting tool comprises a tool base, a tool holder movably connected to the tool base, and a cutting blade connected to the end of the tool holder.
Further, the cutter base is fixed on the cutter head, a sliding connecting groove is formed in the cutter base, and the sliding connecting groove is matched with the cutter clamping handle in size.
Further, one end of the cutter clamping handle is slidably connected in the cutter base, a limit slider is arranged at the other end of the cutter clamping handle, and the limit slider is connected into threads of the spiral rotating disc.
Further, the device also comprises a feeding mechanism, wherein the feeding mechanism comprises a plurality of supporting rollers with adjustable heights.
Further, a dust collection port and a cooling air port are also arranged in the cutting head.
According to the cyclone cutting device for the aviation pipe, provided by the invention, the cyclone cutting method is also provided, and the feeding and retracting of the cutter can be controlled better to finish the cutting of the aviation pipe, so that the specific scheme is as follows:
the cyclone cutting method for the aviation pipe comprises the following steps:
A. the workpiece alignment, namely aligning the center of the pipe material to the center of the cutting head by lifting or lowering the supporting pipe wheel according to different pipe material diameters;
B. feeding: after the workpiece is aligned, conveying the pipe material to be cut to the corresponding position of the cutting head and clamping;
C. performing cyclone cutting: and respectively starting a feeding motor and a main motor, driving a driving belt wheel by the main motor to drive the whole body to rotate, and driving a feeding spiral turntable by a feeding servo motor through a feeding driving wheel to form a speed difference with the shell so as to realize feeding of the cutter and complete cutting of the pipe.
Further, the main motor and the feeding motor implement a certain rotation proportion according to the proportion of the spiral rotary table to the cutter head, so that the instantaneous speeds of the spiral rotary table and the cutter head are kept consistent.
Further, in the step C, when cutting feed is needed, the feeding motor is accelerated, so that the spiral turntable rotates faster than the cutter head; on the contrary, when the cutter is required to be retracted, the feeding motor is decelerated, so that the rotation speed of the spiral turntable is slower than that of the cutter head.
Further, in the step C, a speed curve of the motor to be operated needs to be planned according to the size of the pipe fitting, then the speed curve is discretized, data are divided into pieces of data every 125us, and the motion controller outputs the speed according to the time interval of every 125us, so that the output is consistent with the planned curve.
Compared with the prior art, the invention has the advantages that: according to the invention, two different driving motors are respectively used as driving sources, the main motor is used as a main driving source, the driving wheel is driven to drive the whole cutter disc to rotate, the feeding motor is used for driving the spiral rotary disc to rotate on the basis of the driving motor, the speed difference is formed between the feeding motor and the cutter disc, the tail end of a cutter for cutting is connected to the spiral rotary disc through the limiting sliding block, the front end of the cutter is fixed on the cutter disc through the cutter seat, and when the speed difference is formed between the spiral rotary disc and the cutter disc, the cutter can respectively carry out the action of retracting and feeding, so that cutting and retracting are carried out. Through the rotatory mode of cutter, but not traditional work piece rotatory mode, on the one hand has effectively improved cutting efficiency, on the other hand can avoid the deformation of tubular product wall simultaneously, improves cutting quality.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some embodiments of the present invention and should not be considered limiting the scope, and that other related drawings can be obtained according to these drawings without inventive effort for a person skilled in the art.
Fig. 1 is a schematic structural view of an aviation tube cyclone cutting device provided by the invention.
Fig. 2 is a schematic diagram of a cutterhead removing structure of the cyclone cutting device for aviation pipes.
Fig. 3 is a schematic structural view of a cutting head according to the present invention.
Fig. 4 is a schematic front view of fig. 3.
Fig. 5 is a schematic structural view of an aviation tube cutting production line employing the present invention.
Reference numerals: 1. a cutting head; 2. a support tube wheel; 3. a mechanical arm; 4. a clamping device; 5. a main motor; 6. a cutterhead; 7. a cutter base; 8. a cutter clamping handle; 9. a sliding connection groove; 10. a cutting blade; 11. a spiral turntable; 12. a feed motor; 13. and a limit sliding block.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present invention more apparent, the technical solutions of the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention, and it is apparent that the described embodiments are some embodiments of the present invention, but not all embodiments of the present invention. All other embodiments, which can be made by those skilled in the art based on the embodiments of the invention without making any inventive effort, are intended to be within the scope of the invention.
It should be noted that: like reference numerals and letters denote like items in the following figures, and thus once an item is defined in one figure, no further definition or explanation thereof is necessary in the following figures.
In the description of the present invention, it should be noted that, if the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. indicate an azimuth or a positional relationship based on that shown in the drawings, or an azimuth or a positional relationship in which the inventive product is conventionally put in use, it is merely for convenience of describing the present invention and simplifying the description, and it is not indicated or implied that the apparatus or element referred to must have a specific azimuth, be constructed and operated in a specific azimuth, and thus should not be construed as limiting the present invention.
Furthermore, the terms "first," "second," "third," and the like, if any, are used merely for distinguishing between descriptions and not for indicating or implying a relative importance.
Furthermore, the terms "horizontal," "vertical," "overhang" and the like, if any, do not denote a requirement that the component be absolutely horizontal or overhang, but rather may be slightly inclined. As "horizontal" merely means that its direction is more horizontal than "vertical", and does not mean that the structure must be perfectly horizontal, but may be slightly inclined.
In the description of the present invention, it should also be noted that, unless explicitly stated and limited otherwise, the terms "disposed," "mounted," "connected," and the like are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present invention will be understood in specific cases by those of ordinary skill in the art.
It should be noted that the features of the embodiments of the present invention may be combined with each other without conflict.
As shown in fig. 1-5, the aviation pipe whirlwind cutting device comprises a clamping device 4 and a cutting head 1, wherein the cutting head 1 comprises a base, a driving mechanism connected to the base and a cutting mechanism connected to the driving mechanism; the drive mechanism comprises a main motor 5 and a feed motor 12, the cutting mechanism comprises a cutterhead 6, a helical turntable 11 connected outside the cutterhead 6 and a plurality of cutting tools connected between the cutterhead 6 and the helical turntable 11, and the cutterhead 6 is connected to the main motor 5 and driven by the main motor 5, and the helical turntable 11 is connected to the feed motor 12 and driven by the feed motor 12.
In the prior art, for cutting of pipes or other types of workpiece processing, a cutter is generally adopted to fix and rotate the workpiece, and the cutter approaches to the workpiece rotating at a high speed to complete cutting, but for pipe processing, the pipe is generally a hollow circular pipe with limited wall thickness, and a mode that the workpiece rotates and the cutter approaches is adopted, so that on one hand, the clamping of the pipe is required, the clamping is too tight to cause the sinking of the pipe, and the loose clamping can cause the workpiece to fly and drag during cutting; on the other hand, because a fixed cutter is adopted, the cutter can cause the instantaneous stress unbalance of the workpiece when being close to the workpiece, and the pipe wall is thinner, so that the situation of accidental damage is caused. However, in the present invention, the way of processing the pipe is innovated by fixing the cutter for cutting to the cutterhead 6 and the spiral turntable 11, specifically, fixing the cutter base 7 to the large disc, and the limit slider 13 is connected to the spiral turntable 11, the tail end of the grip holder of the cutter is fixed to the spiral turntable 11, the cutting head 1 of the cutter is connected to the cutter base 7, and the sliding connection groove 9 is provided on the cutter base 7. Driven by two driving sources respectively, wherein the main motor 5 drives the cutterhead 6 to rotate as a whole, and the cutterhead 6 and the spiral turntable 11 keep consistent instantaneous speed. The feeding motor 12 drives the spiral rotary table 11 independently, when the feeding motor 12 works, an instant speed difference is generated between the spiral rotary table 11 and the cutter disc 6, and the spiral rotary table 11 forces the limiting slide block 13 connected with the spiral rotary table to drive the cutter handle to move inwards or outwards in the sliding connecting groove 9 in the screwing process, so that the cutting head 1 of the cutting tool is controlled to approach to a principle workpiece, and cutting and tool withdrawal are completed.
By adopting the cutting mode, the workpiece rotation is changed into the cutter rotation, one cutting cutter is changed into a plurality of cutting cutters to simultaneously cut from different angles, and the multidirectional feeding mode can effectively avoid the damage or the dent of the pipe fitting caused by different pressure in the cutting process to a certain extent. Meanwhile, the cutting efficiency can be effectively improved by the multidirectional feeding mode.
Each cutting tool comprises a tool base 7, a tool holder 8 movably connected to the tool base 7, and a cutting blade 10 connected to the end of the tool holder 8. The cutter base 7 is fixed on the cutter head 6, and a sliding connection groove 9 is arranged on the cutter base 7, and the sliding connection groove 9 is matched with the cutter clamping handle 8 in size. One end of the cutter clamping handle 8 is slidably connected in the cutter base 7, the other end of the cutter clamping handle is provided with a limit slide block 13, and the limit slide block 13 is connected into threads of the spiral rotating disc 11. Through the design mode of cutter base 7, spacing slider 13 and sliding connection groove 9, the front end of cutting tool is connected with the setting of cutter base 7 respectively, and the tail end of cutting tool is connected to spacing slider 13 and cutter holder 8 portion link together, make the handle of a knife holder can remove at the sliding connection groove 9 on the cutter base 7, thereby realize the operation of feeding and withdrawal.
The feeding mechanism comprises a plurality of supporting rollers with adjustable heights. The feeding mechanism is mainly used for adjusting the conveying height of the pipe and can be aligned to the height of the cyclone cutting head 1.
The cutting head 1 is also provided with a dust collection port and a cooling air port. The suction opening and the cooling air opening are of a more conventional design for machining and will not be repeated here.
According to the aviation pipe cyclone cutting device provided by the invention, the cyclone cutting method is also provided, and the feeding and retracting of the cutter can be controlled better, so that the aviation pipe can be cut, and specifically, the operation mode is as follows:
the cyclone cutting method for the aviation pipe comprises the following steps:
A. workpiece alignment, namely placing a pipe to be cut on a support pipe wheel 2 through a mechanical arm 3, and aligning the center of the pipe to the center of a cutting head 1 by lifting or lowering the support pipe wheel 2 according to different pipe diameters;
B. feeding: after the workpiece is aligned, conveying the pipe material to be cut to the corresponding position of the cutting head 1 and clamping;
C. performing cyclone cutting: the feeding motor 12 and the main motor 5 are respectively started, the main motor 5 drives the driving belt wheel to drive the whole body to rotate, and then the feeding servo motor drives the feeding spiral turntable 11 through the feeding driving wheel to form a speed difference with the shell to realize cutter feeding, and the pipe cutting is completed.
The main motor 5 and the feeding motor 12 implement a certain rotation proportion according to the proportion of the spiral rotary table 11 and the cutter head 6, so that the instantaneous speeds of the spiral rotary table 11 and the cutter head 6 are kept consistent.
In the step C, when cutting feed is needed, the feeding motor 12 is accelerated, so that the rotation of the spiral turntable 11 is faster than that of the cutterhead 6; conversely, when the cutter is required to retract, the speed of the speed reducing feed motor 12 is lower than that of the cutter head 6 by the rotating speed of the spiral rotary table 11.
In the step C, a speed curve of the motor to be operated is planned according to the size of the pipe fitting, then the speed curve is discretized, data are segmented every 125us, and the motion controller outputs the speed according to the time interval of every 125us, so that the output is consistent with the planned curve.
Specifically, for example, for an aluminum alloy part aviation pipe produced on an existing production line, a raw material pipe produced in a previous rolling process is generally 3-6m long, and the raw material pipe needs to be cut into a plurality of sections according to requirements.
The cyclone cutting device provided by the invention adopts the following steps:
main motor 5: the power is 3kw;
a feed motor 12:0.75kw;
and are all alternating current servo motors, wherein the main motor 5 drives the cutter disc 6 and the spiral turntable 11 to rotate at the same speed, and the feed motor 12 drives the spiral turntable 11 to rotate, so that a speed difference is generated between the spiral turntable 11 and the cutter disc 6. Thus, the cutting blade 10 can be advanced and retracted when the screw turntable 11 drives the cutter to move again during rotation.
The rotation speed of the main motor 5 can be changed according to the diameters of different raw material pipes by a control system. The ratio of the rotation speed of the main motor 5 to the rotation speed of the feed motor 12 is: 1:4, namely 1 rotation of the main motor 5, 4 rotations of the feeding motor 12, 750r/min of the maximum rotation speed of the main motor 5 and 3000r/min of the maximum rotation speed of the feeding motor 12, wherein the instantaneous speed (comprising acceleration and deceleration processes) of the main motor 5 and the feeding motor 12 always maintains a relation of 1:4, so that the cutter does not have feeding motion, when the speed of the main motor 5 is higher than that of the feeding motor 12, the cutter moves in a retracting manner, and when the speed of the feeding motor 12 is higher than that of the main motor 5, the cutter moves in a feeding manner.
For example: when the main motor 5 and the feeding motor 12 are started from zero at the same time, the speed ratio is always kept 1:4, when the speed of the main motor 5 reaches 600r/min, the speed of the feeding motor 12 is 2400r/min, if cutting is to be performed by feeding, the speed of the main motor 5 is kept unchanged, the speed of the feeding motor 12 is larger than 2400r/min, and after cutting is completed, the speed of the main motor 5 is kept unchanged, and the retracting can be realized by only reducing the speed of the feeding motor 12 to be lower than 2400 r/min; for the feed motor 12 to run 10 revolutions alone, the screw turntable 11 rotates 1 revolution, the tool is fed 16mm, that is to say the tool is fed or withdrawn 1.6mm for each 1 revolution of the feed motor 12 relative to the main motor 5.
In summary, the invention adopts the mode that the cutter rotates and the workpiece is fixed, a plurality of cutting cutters are driven to rotate respectively by two driving sources from different directions through a good design, and the speed difference is formed, so that the cutter feeding and the cutter retracting are respectively realized, the cutting is directly carried out from a multi-direction angle, the cutting mode is faster, and the cutting effect is obviously better than that of the traditional cutting mode.
The above embodiments are merely for illustrating the technical solution of the present application, and not for limiting the same; although the present application has been described in detail with reference to the foregoing embodiments, it should be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit and scope of the corresponding technical solutions.
Claims (10)
1. Aviation tubular product whirlwind cutting device, its characterized in that: comprises a clamping device (4) and a cutting head (1), wherein the cutting head (1) comprises a base, a driving mechanism connected to the base and a cutting mechanism connected to the driving mechanism; the driving mechanism comprises a main motor (5) and a feeding motor (12), the cutting mechanism comprises a cutter disc (6), a spiral rotary disc (11) connected outside the cutter disc (6) and a plurality of cutting tools connected between the cutter disc (6) and the spiral rotary disc (11), the cutter disc (6) is connected to the main motor (5) and driven by the main motor (5), and the spiral rotary disc (11) is connected to the feeding motor (12) and driven by the feeding motor (12).
2. The airline pipe whirlwind cutting device of claim 1, wherein: each cutting tool comprises a tool base (7), a tool clamping handle (8) movably connected to the tool base (7), and a cutting blade (10) connected to the end part of the tool clamping handle (8).
3. The airline pipe whirlwind cutting device of claim 2, wherein: the cutter base (7) is fixed on the cutter head (6), a sliding connecting groove (9) is formed in the cutter base (7), and the sliding connecting groove (9) is matched with the cutter clamping handle (8) in size.
4. The airline pipe whirlwind cutting device of claim 2, wherein: one end of the cutter clamping handle (8) is slidably connected in the cutter base (7), a limit sliding block (13) is arranged at the other end of the cutter clamping handle, and the limit sliding block (13) is connected into threads of the spiral turntable (11).
5. The airline pipe whirlwind cutting device of claim 1, wherein: the feeding mechanism comprises a plurality of supporting rollers with adjustable heights.
6. The airline pipe whirlwind cutting device of claim 1, wherein: the cutting head (1) is also provided with a dust collection opening and a cooling air opening.
7. The cyclone cutting method for the aviation pipe is characterized by comprising the following steps of:
A. the workpiece alignment, namely according to different tube diameters, the support tube wheel (2) aligns the center of the tube to the center of the cutting head (1) by lifting or lowering;
B. feeding: after the workpiece is aligned, conveying the pipe material to be cut to the corresponding position of the cutting head (1) and clamping;
C. performing cyclone cutting: and respectively starting a feeding motor (12) and a main motor (5), driving a driving belt wheel to drive the whole body to rotate by the main motor (5), and driving a feeding spiral turntable (11) to form a speed difference with the shell by a feeding servo motor through a feeding driving wheel to realize cutter feeding and complete pipe cutting.
8. The cyclone cutting method for aviation tubing according to claim 7, wherein the main motor (5) and the feeding motor (12) implement a certain rotation ratio according to the ratio of the spiral turntable (11) to the cutterhead (6), so that the instantaneous speeds of the spiral turntable (11) and the cutterhead (6) are kept consistent.
9. The cyclone cutting method of aviation tubing according to claim 7, wherein in step C, when cutting feed is required, the feeding motor (12) is accelerated to make the rotation of the spiral turntable (11) faster than the cutterhead (6); on the contrary, when the cutter is required to be retracted, the feeding motor (12) is decelerated, so that the rotating speed of the spiral rotary table (11) is slower than that of the cutter head (6).
10. The cyclone cutting method of aviation tubing according to claim 7, wherein in the step C, a speed curve of the motor to be operated is planned according to the size of the tubing, then the speed curve is discretized, each 125us is divided into one data, and the motion controller outputs the speed according to the time interval of each 125us, so that the output and the planned curve are consistent.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202311616612.9A CN117381049A (en) | 2023-11-29 | 2023-11-29 | Aviation pipe cyclone cutting device and cutting method thereof |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202311616612.9A CN117381049A (en) | 2023-11-29 | 2023-11-29 | Aviation pipe cyclone cutting device and cutting method thereof |
Publications (1)
Publication Number | Publication Date |
---|---|
CN117381049A true CN117381049A (en) | 2024-01-12 |
Family
ID=89463265
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202311616612.9A Pending CN117381049A (en) | 2023-11-29 | 2023-11-29 | Aviation pipe cyclone cutting device and cutting method thereof |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN117381049A (en) |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104923846A (en) * | 2015-03-06 | 2015-09-23 | 金华畅能机械有限公司 | Pipe cutting machine |
CN107138807A (en) * | 2017-06-22 | 2017-09-08 | 余维维 | A kind of pipe part numerical control device for being used to cut major diameter length length |
CN211304977U (en) * | 2019-11-27 | 2020-08-21 | 扬州一水机械科技有限公司 | Differential feed mechanism |
CN214720984U (en) * | 2020-12-08 | 2021-11-16 | 渤海造船厂集团有限公司 | Allowance-free fixed-length cutting and groove machining integrated device for pipes |
CN115415602A (en) * | 2022-09-30 | 2022-12-02 | 河北华工森茂特激光科技有限公司 | Nickel-based alloy pipe slotting machine |
CN116810027A (en) * | 2023-05-11 | 2023-09-29 | 北京石油化工学院 | Automatic machining equipment for outer groove of numerical control pipeline for maintaining electric heater of nuclear power voltage stabilizer |
-
2023
- 2023-11-29 CN CN202311616612.9A patent/CN117381049A/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104923846A (en) * | 2015-03-06 | 2015-09-23 | 金华畅能机械有限公司 | Pipe cutting machine |
CN107138807A (en) * | 2017-06-22 | 2017-09-08 | 余维维 | A kind of pipe part numerical control device for being used to cut major diameter length length |
CN211304977U (en) * | 2019-11-27 | 2020-08-21 | 扬州一水机械科技有限公司 | Differential feed mechanism |
CN214720984U (en) * | 2020-12-08 | 2021-11-16 | 渤海造船厂集团有限公司 | Allowance-free fixed-length cutting and groove machining integrated device for pipes |
CN115415602A (en) * | 2022-09-30 | 2022-12-02 | 河北华工森茂特激光科技有限公司 | Nickel-based alloy pipe slotting machine |
CN116810027A (en) * | 2023-05-11 | 2023-09-29 | 北京石油化工学院 | Automatic machining equipment for outer groove of numerical control pipeline for maintaining electric heater of nuclear power voltage stabilizer |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN105773264A (en) | Automatic tool changer (ATC) with manipulator and incessantly rotating spindle for machining center | |
CN103894865A (en) | Numerical control five-axis machine tool for drilling laminated materials | |
CN102744448A (en) | Numerical control processing machine tool and processing method special for double-power unit propeller | |
CN101961835A (en) | Numerical control turning-milling compound machine | |
CN111618670A (en) | Adjustable twist drill grinding device | |
CN207402919U (en) | Sevenfive axis dowel numerical control machining center | |
CN103418999A (en) | Automobile axle shaft machining technique | |
CN109333178A (en) | Symmetrical configurations precision dise knife numerically control grinder and method for grinding | |
CN214720984U (en) | Allowance-free fixed-length cutting and groove machining integrated device for pipes | |
CN104117739B (en) | Horizontal type taper-shaped chamfering machine for processing numerical control gear | |
CN206966853U (en) | A kind of efficient cutting processing equipment | |
CN117381049A (en) | Aviation pipe cyclone cutting device and cutting method thereof | |
CN210587353U (en) | Horizontal opposite vertex processingequipment of thin wall blade | |
CN215199813U (en) | Deep hole groove milling device | |
CN110842311A (en) | Electric spark one-way wire-moving cutting machining equipment for turbine disc mortise | |
CN110328564A (en) | A kind of milling cutter grinding attachment and application method | |
CN114160849B (en) | Novel special machine tool for vortex disc and machining method thereof | |
CN213497695U (en) | Milling machine processing platform of steam turbine cylinder body | |
CN112547922B (en) | Horizontal double-pair-wheel multifunctional variable-size composite flexible spinning equipment | |
CN109352027A (en) | A kind of long cone hole machine device of the duplex of magnetic tape trailer seat supports and processing method | |
CN101704122A (en) | Portable pipe orifice finisher | |
CN114799922A (en) | Numerical control turntable type multi-station tool grinding machine | |
WO2019006810A1 (en) | Numerically-controlled piston ring outer circle chamfering machine tool | |
CN105598535A (en) | Whirlwind milling device | |
CN103658981B (en) | Transverse feed mechanism of square tube laser cutting machine |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |