CN218080619U - Highlight milling cutter for machining aviation aluminum cylindrical surface - Google Patents
Highlight milling cutter for machining aviation aluminum cylindrical surface Download PDFInfo
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- CN218080619U CN218080619U CN202221254217.1U CN202221254217U CN218080619U CN 218080619 U CN218080619 U CN 218080619U CN 202221254217 U CN202221254217 U CN 202221254217U CN 218080619 U CN218080619 U CN 218080619U
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Abstract
The utility model discloses a processing aviation aluminium face of cylinder highlight milling cutter specifically is aviation aluminium processing technology field, a processing aviation aluminium face of cylinder highlight milling cutter, including the dead lever, the outside upper portion of dead lever is seted up threadedly, and the lower extreme of dead lever is fixed with the installation piece, and a plurality of fixed slots have been seted up to the bottom surface outside of installation piece, and the inboard sliding connection of fixed slot has the fixed block, and the welding groove has been seted up to the one end of fixed block, and the inboard in welding groove is fixed with the tool bit, and the below of installation piece is equipped with the fixed disk, and the top surface external fixation of fixed disk has a plurality of joint pieces, and the outside of joint piece cooperates with the inboard joint of fixed slot. The utility model has the advantages of reasonable design compactness, excellent in use effect avoids dismantling and installing the change tool bit one by one, has saved the manpower, has improved work efficiency.
Description
Technical Field
The utility model relates to an aviation aluminium processing technology field specifically is a processing aviation aluminium face of cylinder highlight milling cutter.
Background
The milling cutter is a rotary cutter which is used for milling and provided with one or more cutter teeth, the cutter teeth cut off the allowance of a workpiece intermittently in sequence during working, the milling cutter is mainly used for processing planes, steps, grooves, forming surfaces, cutting off the workpiece and the like on a milling machine, and the highlight milling cutter for processing aviation aluminum cylindrical surfaces in the prior art has the following problems:
in the use process of the highlight milling cutter for machining the aviation aluminum cylindrical surface, the milling cutter is easy to wear due to long-time friction, cutter heads need to be detached, installed and replaced one by one, time and labor are wasted, the working efficiency is reduced, and therefore the highlight milling cutter for machining the aviation aluminum cylindrical surface is provided for solving the problems.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a processing aviation aluminium face of cylinder highlight milling cutter to solve the problem that proposes in the above-mentioned background art.
In order to solve the technical problem, the utility model adopts the following technical scheme: the utility model provides a processing aviation aluminium face of cylinder highlight milling cutter, includes the dead lever, screw thread is seted up on the outside upper portion of dead lever, the lower extreme of dead lever is fixed with the installation piece, a plurality of fixed slots have been seted up to the bottom surface outside of installation piece, the inboard sliding connection of fixed slot has the fixed block, the welding groove has been seted up to the one end of fixed block, the inboard in welding groove is fixed with the tool bit, the below of installation piece is equipped with the fixed disk, the top surface external fixation of fixed disk has a plurality of joint pieces, the outside of joint piece cooperates with the inboard joint of fixed slot.
Preferably, a thread groove is formed in the middle of the outer side of the mounting block, and a threaded rod is connected to the inner side of the thread groove in a threaded manner.
Preferably, the lower extreme of threaded rod fixes the operation piece, the straight line groove has been seted up to the bottom surface of operation piece, a plurality of latch A have been seted up to the top surface of operation piece, latch A is the triangle-shaped structure.
Preferably, the fixed disk is internally provided with a through groove, the bottom surface of the fixed disk is fixed with a lantern ring, and the bottom surface of the lantern ring is provided with a latch B.
Preferably, an elastic gasket is arranged between the lantern ring and the operating block, and two sides of the elastic gasket are in sliding contact with the outer sides of the latch B and the latch A.
Compared with the prior art, the beneficial effects of the utility model reside in that:
1. the utility model discloses a dismantle the threaded rod in the thread groove, dismantle the fixed disk for separate in joint piece on the fixed disk and the fixed slot, thereby take off fixed block and the tool bit of renewal with fixed block and tool bit, then, fix the threaded rod again, fixed disk for joint piece on the fixed disk inserts the fixed slot and supports the fixed block, whole process convenient and fast has saved the manpower, has improved work efficiency.
2. The utility model discloses when fixed threaded rod, latch A on the operation piece of threaded rod one end extrudees and promotes elastic gasket, make latch B on elastic gasket and the lantern ring, because elastic gasket's elasticity influences, elastic gasket takes place to warp, latch A and latch B take place relative slip with elastic gasket, but when rotatory in the opposite direction, latch A and latch B take place the joint with elastic gasket, thereby the restriction threaded rod is to the rotation in the opposite direction, prevent it not hard up, but be limited to elastic gasket's intensity, exert great power through the manual work, can destroy elastic gasket, thereby lift the threaded rod off.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without creative efforts.
Fig. 1 is an overall schematic view of the present invention.
Fig. 2 is a schematic overall sectional view of the present invention.
Fig. 3 is an enlarged schematic view of a point a in fig. 2 according to the present invention.
In the figure: 1. fixing the rod; 2. mounting blocks; 3. fixing grooves; 4. a fixed block; 5. a cutter head; 6. fixing the disc; 7. a clamping block; 8. a thread groove; 9. a threaded rod; 10. an operation block; 11. a straight slot; 12. a latch A; 13. a through groove; 14. a collar; 15. a latch B; 16. an elastic pad.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Example (b): as shown in fig. 1-3, the high-gloss milling cutter for machining the aviation aluminum cylindrical surface comprises a fixing rod 1, wherein threads are formed in the upper portion of the outer side of the fixing rod 1, an installation block 2 is fixed to the lower end of the fixing rod 1, a plurality of fixing grooves 3 are formed in the outer portion of the bottom surface of the installation block 2, a fixing block 4 is connected to the inner side of each fixing groove 3 in a sliding mode, a welding groove is formed in one end of each fixing block 4, a cutter head 5 is fixed to the inner side of each welding groove, a fixing disc 6 is arranged below the installation block 2, a plurality of clamping blocks 7 are fixed to the outer portion of the top surface of the fixing disc 6, the outer sides of the clamping blocks 7 are in clamping fit with the inner sides of the fixing grooves 3, a threaded groove 8 is formed in the middle portion of the outer side of the installation block 2, and a threaded rod 9 is connected to the inner side of the threaded groove 8;
through dismantling threaded rod 9 in the thread groove 8, dismantle fixed disk 6 for separation in joint piece 7 on the fixed disk 6 and the fixed slot 3, thereby take off fixed block 4 and the tool bit 5 of renewal, then, fix threaded rod 9 again, fixed disk 6, make joint piece 7 on the fixed disk 6 insert fixed slot 3 and support fixed block 4, whole process convenient and fast has saved the manpower, has improved work efficiency.
Further, an operation block 10 is fixed at the lower end of the threaded rod 9, a straight groove 11 is formed in the bottom surface of the operation block 10, a plurality of clamping teeth A12 are formed in the top surface of the operation block 10, the clamping teeth A12 are of a triangular structure, a through groove 13 is formed in the fixed disc 6, a lantern ring 14 is fixed on the bottom surface of the fixed disc 6, clamping teeth B15 are formed in the bottom surface of the lantern ring 14, an elastic gasket 16 is arranged between the lantern ring 14 and the operation block 10, and two sides of the elastic gasket 16 are in sliding contact with the outer sides of the clamping teeth B15 and the clamping teeth A12;
when the threaded rod 9 is fixed, the latch A12 on the operation block 10 at one end of the threaded rod 9 extrudes and pushes the elastic gasket 16, so that the elastic gasket 16 and the latch B15 on the lantern ring 14 are enabled to slide relatively due to the elastic force of the elastic gasket 16, the elastic gasket 16 deforms, and the latch A12 and the latch B15 slide relatively with the elastic gasket 16, but when the threaded rod is rotated in the opposite direction, the latch A12 and the latch B15 are clamped with the elastic gasket 16, so that the threaded rod 9 is limited from rotating in the opposite direction, and the threaded rod is prevented from loosening, but the strength of the elastic gasket 16 is limited, and the elastic gasket 16 can be damaged by applying a large force manually, so that the threaded rod 9 is dismounted.
The working principle is as follows: the utility model discloses a through dismantling threaded rod 9 in the thread groove 8, dismantle fixed disk 6, make the joint piece 7 on the fixed disk 6 separate from fixed slot 3, thus take off fixed block 4 and tool bit 5 that renews with fixed block 4 and tool bit 5, then, fix threaded rod 9 again, fix fixed disk 6, make the joint piece 7 on the fixed disk 6 insert fixed slot 3 and support fixed block 4;
when the threaded rod 9 is fixed, the latch A12 on the operation block 10 at one end of the threaded rod 9 extrudes and pushes the elastic gasket 16, so that the elastic gasket 16 and the latch B15 on the lantern ring 14 are enabled to slide relatively due to the elastic force of the elastic gasket 16, the elastic gasket 16 deforms, and the latch A12 and the latch B15 slide relatively with the elastic gasket 16, but when the threaded rod is rotated in the opposite direction, the latch A12 and the latch B15 are clamped with the elastic gasket 16, so that the threaded rod 9 is limited from rotating in the opposite direction, and the threaded rod is prevented from loosening, but the strength of the elastic gasket 16 is limited, and the elastic gasket 16 can be damaged by applying a large force manually, so that the threaded rod 9 is dismounted.
It will be apparent to those skilled in the art that various changes and modifications may be made without departing from the spirit and scope of the invention. Thus, if such modifications and variations of the present invention fall within the scope of the claims of the present invention and their equivalents, the present invention is also intended to include such modifications and variations.
Claims (5)
1. The utility model provides a processing aviation aluminium cylinder face highlight milling cutter, includes dead lever (1), its characterized in that: the utility model discloses a welding fixture, including dead lever (1), the outside upper portion of dead lever (1) is seted up threadedly, the lower extreme of dead lever (1) is fixed with installation piece (2), a plurality of fixed slots (3) have been seted up to the bottom surface outside of installation piece (2), the inboard sliding connection of fixed slot (3) has fixed block (4), the welding groove has been seted up to the one end of fixed block (4), the inboard in welding groove is fixed with tool bit (5), the below of installation piece (2) is equipped with fixed disk (6), the top surface external fixation of fixed disk (6) has a plurality of joint pieces (7), the outside of joint piece (7) cooperates with the inboard joint of fixed slot (3).
2. The milling cutter for machining the high gloss cylindrical surface of aviation aluminum according to claim 1, wherein the mounting block (2) is provided with a thread groove (8) at the middle of the outer side, and the inner side of the thread groove (8) is connected with a threaded rod (9) in a threaded manner.
3. The milling cutter for machining the high gloss cylindrical aluminum surface of the aviation according to claim 2, wherein the lower end of the threaded rod (9) is fixed with an operating block (10), the bottom surface of the operating block (10) is provided with a straight groove (11), the top surface of the operating block (10) is provided with a plurality of latch teeth A (12), and the latch teeth A (12) are in a triangular structure.
4. The milling cutter for machining the high gloss cylindrical surface of aviation aluminum according to claim 3, wherein the fixed disk (6) is provided with a through groove (13) inside, the bottom surface of the fixed disk (6) is fixed with a lantern ring (14), and the bottom surface of the lantern ring (14) is provided with a latch B (15).
5. The milling cutter for machining the cylindrical surface of aviation aluminum as claimed in claim 4, wherein an elastic gasket (16) is arranged between the collar (14) and the operating block (10), and two sides of the elastic gasket (16) are in sliding contact with the outer sides of the latch B (15) and the latch A (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221254217.1U CN218080619U (en) | 2022-05-24 | 2022-05-24 | Highlight milling cutter for machining aviation aluminum cylindrical surface |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221254217.1U CN218080619U (en) | 2022-05-24 | 2022-05-24 | Highlight milling cutter for machining aviation aluminum cylindrical surface |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218080619U true CN218080619U (en) | 2022-12-20 |
Family
ID=84461777
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221254217.1U Active CN218080619U (en) | 2022-05-24 | 2022-05-24 | Highlight milling cutter for machining aviation aluminum cylindrical surface |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218080619U (en) |
-
2022
- 2022-05-24 CN CN202221254217.1U patent/CN218080619U/en active Active
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