CN209632188U - A kind of dedicated form cutter of aerospace - Google Patents

A kind of dedicated form cutter of aerospace Download PDF

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Publication number
CN209632188U
CN209632188U CN201920392327.6U CN201920392327U CN209632188U CN 209632188 U CN209632188 U CN 209632188U CN 201920392327 U CN201920392327 U CN 201920392327U CN 209632188 U CN209632188 U CN 209632188U
Authority
CN
China
Prior art keywords
milling cutter
external disk
saw blade
keyhole
milling
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.)
Expired - Fee Related
Application number
CN201920392327.6U
Other languages
Chinese (zh)
Inventor
成锋娜
张玉言
李娟�
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 Forestry University
Original Assignee
Nanjing Forestry University
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
Application filed by Nanjing Forestry University filed Critical Nanjing Forestry University
Priority to CN201920392327.6U priority Critical patent/CN209632188U/en
Application granted granted Critical
Publication of CN209632188U publication Critical patent/CN209632188U/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 dedicated form cutters of aerospace, including milling cutter external disk, milling cutter inner disc is provided on the inside of the milling cutter external disk, the outer surface of the milling cutter inner disc is provided with guiding set, milling cutter inner hole is offered on the inside of the milling cutter inner disc, milling cutter saw blade is provided on the outside of the milling cutter external disk, the surface inserting of the milling cutter external disk has heat dissipating ring, the second bolt is provided at the heat dissipating ring and the link position of milling cutter external disk, the surface of the milling cutter saw blade is fixedly connected with limit convex, the inside of the limit convex offers the first keyhole, the inside of the milling cutter external disk corresponds to and offers limiting slot at the position of milling cutter saw blade, the second keyhole is offered on the outside of the limiting slot, the first bolt is provided at the position of corresponding second keyhole in the outside of the milling cutter external disk;By the assembly type saw blade of setting, can when saw blade is damaged timely dismounting and change, so that it is guaranteed that metal saw has optimal milling effect.

Description

A kind of dedicated form cutter of aerospace
Technical field
The utility model belongs to milling cutter technology, and in particular to a kind of dedicated form cutter of aerospace.
Background technique
Milling cutter is for Milling Process, the rotary cutter with one or more cutters tooth.When work each cutter tooth successively between Cut the surplus of workpiece with having a rest.Milling cutter is mainly used for processing plane, step, groove, forming surface and cutting workpiece on milling machine Deng having more cutter tooth for processing deep trouth and cutting workpiece, on circumference.In order to reduce friction when milling, metal saw There are cotter mill cutter, fish-tail cutter, T-slot milling cutter and various form cutters etc., is widely used in adding for aerospace parts Work.
The saw blade and cutterhead of existing metal saw are integral structures, once a certain saw blade is impaired to be individually replaced, And being changed without influences milling effect, is inconvenient;And the saw blade due to milling cutter and metal high-speed friction can generate largely Heat can not quickly scatter and disappear in air, be easy heated the problem of excessively causing to be lost, reducing service life, thus we It is proposed a kind of dedicated form cutter of aerospace.
Utility model content
The purpose of this utility model is to provide a kind of dedicated form cutters of aerospace, to solve above-mentioned background technique The saw blade and cutterhead of the existing metal saw of middle proposition are integral structures, once a certain saw blade is impaired to be individually replaced, And being changed without influences milling effect, is inconvenient;And the saw blade due to milling cutter and metal high-speed friction can generate largely Heat can not quickly scatter and disappear in air, be easy heated the problem of excessively causing to be lost, reducing service life.
To achieve the above object, the utility model provides the following technical solutions: a kind of dedicated form cutter of aerospace, Including milling cutter external disk, milling cutter inner disc is provided on the inside of the milling cutter external disk, the outer surface of the milling cutter inner disc, which is provided with, leads Draw set, milling cutter inner hole is offered on the inside of the milling cutter inner disc, milling cutter saw blade, the milling are provided on the outside of the milling cutter external disk The surface inserting of knife external disk has heat dissipating ring, is provided with the second bolt at the heat dissipating ring and the link position of milling cutter external disk, described The surface of milling cutter saw blade is fixedly connected with limit convex, and the inside of the limit convex offers the first keyhole, the milling cutter external disk Limiting slot is offered at the position of the corresponding milling cutter saw blade in inside, the second keyhole, the milling cutter are offered on the outside of the limiting slot The first bolt is provided at the position of corresponding second keyhole in the outside of external disk.
Preferably, the guiding set is the circular ring structure that one end radius is greater than the other end, the guiding set and milling cutter inner disc By being welded and fixed.
Preferably, the heat dissipating ring is fixed with milling cutter external disk by the second bolt.
Preferably, the milling cutter saw blade is inserted after engaging limit with limiting slot by limit convex with milling cutter external disk by the first bolt Enter the second keyhole to be fixed with the first keyhole.
Preferably, the milling cutter saw blade is an integral structure with limit convex.
Compared with prior art, the utility model has the beneficial effects that
1, in the utility model, by the assembly type saw blade of setting, can when saw blade is damaged timely dismounting and change, thus Ensure that metal saw has optimal milling effect.
2, in the utility model, by the way that the heat dissipating ring on the inside of saw blade is arranged in, the heat production of saw blade high-speed friction can be made fast Speed passes to heat dissipating ring, to scatter and disappear in air, increases the service life of metal saw.
3, in the utility model, by the guiding set of setting, milling cutter inner hole can be kept quickly right when metal saw is installed Quasi- shaft is fixed, and is facilitated and is carried out metal saw installation.
Detailed description of the invention
Fig. 1 is the overlooking surface structural schematic diagram of the utility model;
Fig. 2 is the fixed schematic cross-sectional view of saw blade of the utility model;
Fig. 3 is that the guiding of the utility model covers overall structure diagram;
In figure: 1, heat dissipating ring;2, the first bolt;3, milling cutter inner disc;4, milling cutter saw blade;5, milling cutter external disk;6, the second bolt; 7, milling cutter inner hole;8, guiding set;9, the first keyhole;10, limit convex;11, limiting slot;12, the second keyhole.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model provides a kind of technical solution: a kind of dedicated form cutter of aerospace, packet Milling cutter external disk 5 is included, the inside of milling cutter external disk 5 is provided with milling cutter inner disc 3, and the outer surface of milling cutter inner disc 3 is provided with guiding set 8, The inside of milling cutter inner disc 3 offers milling cutter inner hole 7, and the outside of milling cutter external disk 5 is provided with milling cutter saw blade 4, the surface of milling cutter external disk 5 It is inlaid with heat dissipating ring 1, the second bolt 6 is provided at heat dissipating ring 1 and the link position of milling cutter external disk 5, the surface of milling cutter saw blade 4 is solid Surely it is connected with limit convex 10, the inside of limit convex 10 offers the first keyhole 9, and the inside of milling cutter external disk 5 corresponds to milling cutter saw blade 4 Limiting slot 11 is offered at position, the outside of limiting slot 11 offers the second keyhole 12, corresponding second bolt in the outside of milling cutter external disk 5 The first bolt 2 is provided at the position in hole 12.
In order to be tightly combined guiding set 8 with milling cutter inner disc 3, in the present embodiment, it is preferred that guiding set 8 is one end radius Greater than the circular ring structure of the other end, guiding set 8 is with milling cutter inner disc 3 by being welded and fixed.
In order to make heat dissipating ring 1 facilitate installation, in the present embodiment, it is preferred that heat dissipating ring 1 and milling cutter external disk 5 pass through the second spiral shell Bolt 6 is fixed.
In order to make 4 easy disassembly of milling cutter saw blade, in the present embodiment, it is preferred that milling cutter saw blade 4 and milling cutter external disk 5 pass through limit Position convex 10 is fixed by the first bolt 2 the second keyhole 12 of insertion with the first keyhole 9 after engaging limit with limiting slot 11.
In order to be tightly combined milling cutter saw blade 4 with limit convex 10, in the present embodiment, it is preferred that milling cutter saw blade 4 and limit convex 10 are an integral structure.
The working principle and process for using of the utility model: the big one end of guiding 8 radiuses of set is directed at shaft and is moved to shaft Dynamic to be fixed up to shaft sticks into inside milling cutter inner hole 7, then shaft drives milling cutter inner disc 3, milling cutter external disk 5 and milling cutter saw blade 4 high-speed rotations contact aerospace close to milling cutter saw blade 4 with milling cutter saw blade 4 with part and carry out polishing milling angle, in milling angle In bruting process, the heat that the friction of milling cutter saw blade 4 generates can quickly pass to heat dissipating ring 1 nearby and is dissipated in by heat dissipating ring 1 In air, and after milling cutter saw blade 4 accidentally abrasion, the first bolt 2 can be made to be detached from the first keyhole 9 and the second keyhole 12, then Make impaired milling cutter saw blade 4 be detached from disassembly from the limiting slot 11 inside milling cutter external disk 5 to be replaced.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art, It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.

Claims (5)

1. a kind of dedicated form cutter of aerospace, including milling cutter external disk (5), it is characterised in that: the milling cutter external disk (5) Inside is provided with milling cutter inner disc (3), and the outer surface of the milling cutter inner disc (3) is provided with guiding set (8), the milling cutter inner disc (3) it offers milling cutter inner hole (7), is provided with milling cutter saw blade (4) on the outside of the milling cutter external disk (5), outside the milling cutter on the inside of The surface inserting of disk (5) has heat dissipating ring (1), is provided with the second spiral shell at the link position of the heat dissipating ring (1) and milling cutter external disk (5) The surface of bolt (6), the milling cutter saw blade (4) is fixedly connected with limit convex (10), and the inside of the limit convex (10) offers One keyhole (9), the inside of the milling cutter external disk (5) correspond to and offer limiting slot (11), the limit at the positions of milling cutter saw blade (4) It is offered the second keyhole (12) on the outside of position slot (11), the position in the outside corresponding second keyhole (12) of the milling cutter external disk (5) Place is provided with the first bolt (2).
2. a kind of dedicated form cutter of aerospace according to claim 1, it is characterised in that: the guiding covers (8) It is greater than the circular ring structure of the other end for one end radius, the guiding set (8) is with milling cutter inner disc (3) by being welded and fixed.
3. a kind of dedicated form cutter of aerospace according to claim 1, it is characterised in that: the heat dissipating ring (1) It is fixed with milling cutter external disk (5) by the second bolt (6).
4. a kind of dedicated form cutter of aerospace according to claim 1, it is characterised in that: the milling cutter saw blade (4) engaged by limit convex (10) with limiting slot (11) with milling cutter external disk (5) and be inserted into the second keyhole by the first bolt (2) after limiting (12) it is fixed with the first keyhole (9).
5. a kind of dedicated form cutter of aerospace according to claim 1, it is characterised in that: the milling cutter saw blade (4) it is an integral structure with limit convex (10).
CN201920392327.6U 2019-03-26 2019-03-26 A kind of dedicated form cutter of aerospace Expired - Fee Related CN209632188U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201920392327.6U CN209632188U (en) 2019-03-26 2019-03-26 A kind of dedicated form cutter of aerospace

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201920392327.6U CN209632188U (en) 2019-03-26 2019-03-26 A kind of dedicated form cutter of aerospace

Publications (1)

Publication Number Publication Date
CN209632188U true CN209632188U (en) 2019-11-15

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201920392327.6U Expired - Fee Related CN209632188U (en) 2019-03-26 2019-03-26 A kind of dedicated form cutter of aerospace

Country Status (1)

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CN (1) CN209632188U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111644851A (en) * 2020-06-15 2020-09-11 天津市威达数控机械有限公司 Combined chamfering saw device
CN111957641A (en) * 2020-08-12 2020-11-20 黄华贵 Agricultural machine belt cleaning device

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111644851A (en) * 2020-06-15 2020-09-11 天津市威达数控机械有限公司 Combined chamfering saw device
CN111644851B (en) * 2020-06-15 2022-02-11 天津市威达数控机械有限公司 Combined chamfering saw device
CN111957641A (en) * 2020-08-12 2020-11-20 黄华贵 Agricultural machine belt cleaning device

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

Granted publication date: 20191115

Termination date: 20200326