CN203236064U - Reamer for machining sandwich structure of titanium alloy and aluminum alloy - Google Patents
Reamer for machining sandwich structure of titanium alloy and aluminum alloy Download PDFInfo
- Publication number
- CN203236064U CN203236064U CN 201320127336 CN201320127336U CN203236064U CN 203236064 U CN203236064 U CN 203236064U CN 201320127336 CN201320127336 CN 201320127336 CN 201320127336 U CN201320127336 U CN 201320127336U CN 203236064 U CN203236064 U CN 203236064U
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- Prior art keywords
- reamer
- aluminum alloy
- angle
- machining
- titanium alloy
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- Expired - Fee Related
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 22
- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 17
- 238000003754 machining Methods 0.000 title claims abstract description 14
- 239000011229 interlayer Substances 0.000 claims description 12
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
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- Milling, Broaching, Filing, Reaming, And Others (AREA)
Abstract
The utility mode provides a reamer for machining a sandwich structure of titanium alloy and aluminum alloy. The reamer for machining the sandwich structure of titanium alloy and aluminum alloy comprises a reamer front guide, a reamer edge part, a reamer rear guide and a reamer handle part, wherein the front angle of a cutting edge on the reamer edge part is 3-5 degrees, the rear angle of the cutting edge is 13-15 degrees, the helical angle is 3-5 degrees, and the angle of the cross section of a chip pocket of the reamer is 85-90 degrees. The reamer for machining the sandwich structure of titanium alloy and aluminum alloy promotes machining quality and efficiency of reaming of assembly holes in the sandwich structure of titanium alloy and aluminum alloy and avoids scratches in the machining process of aluminum alloy holes.
Description
Technical field
The utility model relates to a kind of reamer, is used for the fraising processing of titanium alloy and aluminum alloy interlayer structure.
Background technology
Titanium alloy and aluminum alloy interlayer structure are used in the aeroplane structure design more and more widely, but because machining titanium alloy and aluminum alloy interlayer structure reamer main structure parameters design are unreasonable, caused existing machining titanium alloy and aluminum alloy interlayer structure in the fraising process, often to produce easily the phenomenon that aluminum alloy surface scratches.It is in particular in: the numerical value of anterior angle and helical angle is 0 °, so that cutting edge is not sharp, produces easily the bits knurl; The angle of cutter chip pocket cross section is too little, and its numerical value is 80 °, causes easily chip space not enough.The problems referred to above have finally had a strong impact on precision and the efficient of aircraft assembling processing, and are difficult to satisfy the requirement of aircraft assembling processing.
The utility model content
The purpose of this utility model provides the reamer of a kind of machining titanium alloy and aluminum alloy interlayer structure, has improved quality and the efficient of titanium alloy and aluminum alloy interlayer Standard hole fraising processing, has avoided the scuffing of aluminium alloy hole work in-process.
The technical solution of the utility model: the reamer of a kind of machining titanium alloy and aluminum alloy interlayer structure, guide and the reamer shank after comprising the front guiding of reamer, reamer blade, reamer, cutting edge anterior angle on the reamer blade is 3 °～5 °, the cutting edge relief angle is 13 °～15 °, helical angle is 3 °～5 °, and the angle of reamer chip pocket cross section is 85 °～90 °.
The beneficial effects of the utility model: the utility model is by the main structure parameters redesign to machining titanium alloy and aluminum alloy interlayer structure reamer, the cutting edge anterior angle that is about to reamer strengthens, make 3 °～5 °, reamer cutting edge helical angle is strengthened, make 3 °～5 °, and the angle of reamer chip pocket cross section strengthened, make 85 °～90 °, so that the fraising processing effect of reamer is better, being difficult for producing the aluminium alloy hole scratches, thereby improved quality and the efficient of titanium alloy and the fraising processing of aluminum alloy interlayer Standard hole, avoided the scuffing of aluminium alloy hole work in-process.
Description of drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is the A-A cutaway view of Fig. 1.
The specific embodiment
As depicted in figs. 1 and 2, the machining titanium alloy take the cutting edge diameter as 10mm and aluminum alloy interlayer structure reamer are example, and it comprises before the reamer guiding 3 and reamer shank 4 behind guiding 1, reamer blade 2, the reamer.Wherein, the diameter of guiding 1 before the reamer is made 9.9mm, the cutting edge diameter is made 10mm, cutting edge length is made 15mm, guiding 3 diameters behind the reamer are made 13mm, the cutting edge anterior angle 6 on the reamer blade 2 is made 3 °～5 °, the cutting edge relief angle is made 13 °～15 °, cutting edge helical angle 5 is made 3 °～5 °, the angle 6 of reamer chip pocket cross section is made 85 °～90 °.
Claims (1)
1. the reamer of a machining titanium alloy and aluminum alloy interlayer structure, guide (3) and reamer shank (4) after comprising the front guiding of reamer (1), reamer blade (2), reamer, it is characterized in that: the cutting edge anterior angle (6) on the reamer blade (2) is 3 °～5 °, the cutting edge relief angle is 13 °～15 °, helical angle (5) is 3 °～5 °, and the angle (6) of reamer chip pocket cross section is 85 °～90 °.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320127336 CN203236064U (en) | 2013-03-20 | 2013-03-20 | Reamer for machining sandwich structure of titanium alloy and aluminum alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320127336 CN203236064U (en) | 2013-03-20 | 2013-03-20 | Reamer for machining sandwich structure of titanium alloy and aluminum alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203236064U true CN203236064U (en) | 2013-10-16 |
Family
ID=49313397
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320127336 Expired - Fee Related CN203236064U (en) | 2013-03-20 | 2013-03-20 | Reamer for machining sandwich structure of titanium alloy and aluminum alloy |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203236064U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103612067A (en) * | 2013-11-14 | 2014-03-05 | 沈阳飞机工业（集团）有限公司 | High-precision reaming method for aluminium alloy and multi-layer titanium-alloy-interlayer semi-closed structure |
| CN104668663A (en) * | 2015-01-21 | 2015-06-03 | 杭州福朗机电科技有限公司 | Reamer for machining coupler bolt hole |
| CN105642972A (en) * | 2016-04-12 | 2016-06-08 | 山东大学 | Drilling-reaming-dimpling integrated cutting tool |
| CN106001771A (en) * | 2016-06-17 | 2016-10-12 | 哈尔滨汽轮机厂有限责任公司 | Screw pin hole reamer and method for machining screw pin hole of exhaust cylinder of gas turbine by means of screw pin hole reamer |
| CN106925841A (en) * | 2017-04-27 | 2017-07-07 | 沈阳飞机工业（集团）有限公司 | One kind is for processing intersection point 1 before abdomeinal fin bearing:The taper reamer of 20 tapered holes |
| CN108971638A (en) * | 2018-08-15 | 2018-12-11 | 国营芜湖机械厂 | A kind of coaxial pair of bushing original position repair apparatus and its application method |
| CN114472985A (en) * | 2021-12-03 | 2022-05-13 | 中航沈飞民用飞机有限责任公司 | Large-size high-precision stepped reaming cutter with front and rear guide |
-
2013
- 2013-03-20 CN CN 201320127336 patent/CN203236064U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103612067A (en) * | 2013-11-14 | 2014-03-05 | 沈阳飞机工业（集团）有限公司 | High-precision reaming method for aluminium alloy and multi-layer titanium-alloy-interlayer semi-closed structure |
| CN103612067B (en) * | 2013-11-14 | 2016-04-20 | 沈阳飞机工业（集团）有限公司 | Aluminium alloy and laminated titanium-alloy interlayer semi-closed structure high accuracy ream processing method |
| CN104668663A (en) * | 2015-01-21 | 2015-06-03 | 杭州福朗机电科技有限公司 | Reamer for machining coupler bolt hole |
| CN105642972A (en) * | 2016-04-12 | 2016-06-08 | 山东大学 | Drilling-reaming-dimpling integrated cutting tool |
| CN106001771A (en) * | 2016-06-17 | 2016-10-12 | 哈尔滨汽轮机厂有限责任公司 | Screw pin hole reamer and method for machining screw pin hole of exhaust cylinder of gas turbine by means of screw pin hole reamer |
| CN106925841A (en) * | 2017-04-27 | 2017-07-07 | 沈阳飞机工业（集团）有限公司 | One kind is for processing intersection point 1 before abdomeinal fin bearing:The taper reamer of 20 tapered holes |
| CN106925841B (en) * | 2017-04-27 | 2018-12-21 | 沈阳飞机工业（集团）有限公司 | It is a kind of for processing the taper reamer of intersection point 1:20 tapered hole before abdomeinal fin support |
| CN108971638A (en) * | 2018-08-15 | 2018-12-11 | 国营芜湖机械厂 | A kind of coaxial pair of bushing original position repair apparatus and its application method |
| CN114472985A (en) * | 2021-12-03 | 2022-05-13 | 中航沈飞民用飞机有限责任公司 | Large-size high-precision stepped reaming cutter with front and rear guide |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131016 Termination date: 20160320 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |