JPS62176663A - Production of blade - Google Patents
Production of bladeInfo
- Publication number
- JPS62176663A JPS62176663A JP1854986A JP1854986A JPS62176663A JP S62176663 A JPS62176663 A JP S62176663A JP 1854986 A JP1854986 A JP 1854986A JP 1854986 A JP1854986 A JP 1854986A JP S62176663 A JPS62176663 A JP S62176663A
- Authority
- JP
- Japan
- Prior art keywords
- blade
- aluminum
- ingot
- reinforced metal
- erosion
- 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
- 238000004519 manufacturing process Methods 0.000 title claims description 4
- 229910052751 metal Inorganic materials 0.000 claims abstract description 21
- 239000002184 metal Substances 0.000 claims abstract description 21
- 229910000838 Al alloy Inorganic materials 0.000 claims abstract description 12
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 12
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 12
- 239000000835 fiber Substances 0.000 claims abstract description 10
- 239000011159 matrix material Substances 0.000 claims abstract description 8
- 239000012783 reinforcing fiber Substances 0.000 claims abstract description 7
- 239000000919 ceramic Substances 0.000 claims abstract description 4
- 238000000034 method Methods 0.000 claims description 6
- 238000005520 cutting process Methods 0.000 claims description 2
- 230000003628 erosive effect Effects 0.000 abstract description 22
- 239000000463 material Substances 0.000 abstract description 9
- 238000005266 casting Methods 0.000 abstract 2
- 238000003754 machining Methods 0.000 abstract 2
- 239000000155 melt Substances 0.000 abstract 1
- HBMJWWWQQXIZIP-UHFFFAOYSA-N silicon carbide Chemical compound [Si+]#[C-] HBMJWWWQQXIZIP-UHFFFAOYSA-N 0.000 description 3
- 229910010271 silicon carbide Inorganic materials 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 239000011248 coating agent Substances 0.000 description 2
- 238000000576 coating method Methods 0.000 description 2
- 239000000428 dust Substances 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000002265 prevention Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000003384 imaging method Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 238000005470 impregnation Methods 0.000 description 1
- 239000010985 leather Substances 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 238000010998 test method Methods 0.000 description 1
- 230000004580 weight loss Effects 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明は軸流ファンのブレードやブロアのブＬ／−トー
１．トタストエロージョンや、液滴エロージョンなどの
エロージョン損傷が問題になっているアルミニウム製ブ
レードの製造方法に関する０
また、エロージョン防止という観点から各種ポンプイン
ペラーやプロペラにも応用することもできる。DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to blades of axial fans and blowers L/-toe 1. 0 Regarding the manufacturing method of aluminum blades where erosion damage such as torsion erosion and droplet erosion is a problem.In addition, it can also be applied to various pump impellers and propellers from the viewpoint of erosion prevention.
従来、軸流ファンやブロアなどのブレードの材料として
は１軽量化の目的からアルミニウムやアルミニウム合金
が用いられてきた。Conventionally, aluminum and aluminum alloys have been used as materials for blades of axial fans, blowers, etc. for the purpose of reducing weight.
従来のアルミニウムやアルミニウム合金によるブレード
では流体中に含まれるダストや液滴によシブレード端面
部にエロージョン奮起こ丁ことが多かった。また、この
ようなエロージョンを防止するためにブレード表面にゴ
ムや硬質の有機系樹脂ｔライニングあるいはコーティン
グする対策がとられてき友が、これらのエロージョン防
止対策７行なっても、ライニング材やコーティング皮膜
が簡単に剥ａＴることか多く１満足できる耐エロージョ
ン性ケ保つことが難しかった。Conventional blades made of aluminum or aluminum alloys often suffer from erosion at the end of the blade due to dust and droplets contained in the fluid. In addition, measures have been taken to prevent such erosion by lining or coating the blade surface with rubber or hard organic resin, but even if these 7 erosion prevention measures are taken, the lining material and coating film will still be damaged. It was difficult to maintain satisfactory erosion resistance because it often peeled off easily.
エロージョン損傷が問題になるブレードの前端部に、炭
化ケイ素やアルミナなどのセラミックスウィスカあるい
は短繊維ケ強化繊維とし、アルミニウムあるいはアルミ
ニウム合金とマトリックスとし皮繊維強化金属上位置さ
せるために。At the front end of the blade where erosion damage is a problem, ceramic whiskers or short fibers such as silicon carbide or alumina are used as reinforcing fibers, and aluminum or aluminum alloy is used as a matrix and the skin fiber reinforced metal is placed on top.
先ず鋳型内に強化繊維のブリフォームヶ配置し之後溶湯
ｒ注入して得られるインゴット５ケ削成してブレードの
前端部に上記繊維強化金属が位＃するようにした。First, a preform of reinforcing fibers was placed in a mold, and then molten metal was poured into the resulting ingots. Five ingots were shaved so that the fiber-reinforced metal was placed at the front end of the blade.
繊維強化金属と母材本体とが一体的に生成されるのでブ
レードの耐エロージヨン性が従来材に比べ大幅に同上す
ることはもちろん、軽量でしかも繊維強化金属の剥離、
脱落等の不具合が全く生じない。Since the fiber-reinforced metal and the base material body are integrally produced, the erosion resistance of the blade is significantly higher than that of conventional materials, and it is also lightweight, and the fiber-reinforced metal does not peel off easily.
No problems such as falling off occur.
繊維強化金属ケブレードの一面あるいは全面に適用する
方法としては、第１図に示すように。The method of applying it to one or the entire surface of the fiber-reinforced metal Keblade is as shown in Figure 1.
鋳型１の中に部分的に炭化ケイ素、アルミナ等のセラミ
ックスウィスカあるいは短繊維等の強化繊維のプリフォ
ーム２ケ配置Ｔる。In a mold 1, two preforms made of ceramic whiskers such as silicon carbide or alumina or reinforcing fibers such as short fibers are partially arranged.
なお、プリフォームはマトリックスとなる金属ケ含浸で
きるようにした強化繊維の多孔質体である。その状態で
アルミニウムまたはアルミニウム合金の溶湯３ケ鋳型１
内に流し込んでインゴツト５ケ作る。Note that the preform is a porous body of reinforcing fibers that can be impregnated with a metal serving as a matrix. In that state, 3 molds of molten aluminum or aluminum alloy 1
Pour it inside to make 5 ingots.
従って１強化繊維のプリフォーム２には、アルミニウム
またはアルミニウム合金がマトリックスとなって含浸さ
れ、この繊維強化金属部と。Therefore, the preform 2 of 1 reinforcing fiber is impregnated with aluminum or aluminum alloy as a matrix, and this fiber-reinforced metal part.
プリフォーム２を配置していない部分のアルミニウムま
たはアルミニウム合金部が一体的に形成されたインゴッ
ト５が作られる。An ingot 5 is produced in which the aluminum or aluminum alloy portion of the portion where the preform 2 is not placed is integrally formed.
次にこのインゴツト５ｉ第１図に点線で示すブレード４
の形状に削成して仕上げる。即ち。Next, this ingot 5i is
Finish by cutting into the shape. That is.
ダストや液滴によってエロージョン損傷じゃすいブレー
ド４の前端部４ａに繊維強化金属が配置されるようにイ
ンゴット５ケ削成して、同インゴット５ケブレード４形
状に仕上げる。Five ingots are ground so that the fiber-reinforced metal is disposed at the front end 4a of the blade 4, which is damaged by erosion due to dust or droplets, and the five ingots are finished in the shape of the blade 4.
上記方法により炭化ケイ素つィスカ會強化繊維、（体積
含有率１５％）とし、 Ａ６０６１（アルミニウム合金
）ケマトリックスとした繊維強化金属ケ溶湯加圧含浸法
により製作し１次の条件でアルミニウム合金と繊維強化
金属とについて磁歪式エロージョン試験ゲ夫施し九〇
振動数： ６５００ｆ５０Ｈｚ
撮 幅：９０μｍ
試験時間：３０分
エロージョン試験前後の重量減量を第２図に示すが第２
図によると、繊維強化金属は母材のアルミニウム合金Ａ
６０６１と比べ、約１５倍程度の耐エロージョン性ケ示
した。Silicon carbide reinforced fibers (volume content 15%) were made using the above method, and fiber-reinforced metal fibers made of A6061 (aluminum alloy) were produced by molten metal pressure impregnation method under the following conditions. Magnetostrictive erosion test on reinforced metals 90 Vibration frequency: 6500f50Hz Imaging width: 90μm Test time: 30 minutes The weight loss before and after the erosion test is shown in Figure 2.
According to the figure, the fiber reinforced metal is the base material aluminum alloy A.
Compared to 6061, it exhibited about 15 times the erosion resistance.
尚１本試験法は通常キャビテーションエロージョンの評
価に用いるものであるが、液滴などによるエロージョン
評価にも有効である。また。This test method is usually used to evaluate cavitation erosion, but it is also effective in evaluating erosion caused by droplets. Also.
材料の耐エロージヨン性は硬度が増す程良好になること
から１本繊維強化金属（ブリネル硬さ１２５）の耐エロ
ージヨン性はマトリックスのアルミニウム合金Ａ６０６
１（ブリネル硬さ７７）よりも大幅に優れていることが
わかった。The erosion resistance of a material improves as its hardness increases, so the erosion resistance of a single fiber-reinforced metal (Brinell hardness 125) is higher than that of the matrix aluminum alloy A606.
1 (Brinell hardness 77).
ブレードの二ローション損傷が問題となる前端部に配置
てれる繊維強化金属と、それ以外のブレード材とが接着
等によらず一体的に形成されるので、剥離、脱落等の心
配が全くなく、シかも軽量化が損なわれない。又、ブレ
ードの耐エロージヨン性は大巾に改善され、ブレードの
長寿命化ケ達成することができるなど５本発明は産業の
発達に寄与するところが大きい。Since the fiber-reinforced metal placed at the front end of the blade, where damage would be a problem, and the other blade materials are integrally formed without adhesion, there is no need to worry about peeling or falling off. However, the weight reduction is not impaired. In addition, the erosion resistance of the blade is greatly improved, and the life of the blade can be extended.5 The present invention greatly contributes to the development of industry.
第１図は１本発明方法に係るブレードの製造方法の一実
施例ゲ示す断面図で、第２図は、アルミニウム合金Ａ６
０６１と、これｔマトリックスとし皮繊維強化金属との
エロージョン試験結果ケ示す比較図である。
１・・・ｍＷ、２・・・プレフォーム、３・・・溶湯、
４・・・フｖ−１”＋ ４ ａ・・・ブレードの
前端部、５・・・インゴット０
第１閃
易２閃FIG. 1 is a cross-sectional view showing an embodiment of the method for manufacturing a blade according to the method of the present invention, and FIG.
061 and a t-matrix leather fiber-reinforced metal, this is a comparison diagram showing the results of an erosion test. 1... mW, 2... preform, 3... molten metal,
4... Fu v-1"+ 4 a... Front end of the blade, 5... Ingot 0 1st flash 2 flash
Claims (1)
成る強化繊維のプリフォームを配置し、同鋳型内にアル
ミニウム又はアルミニウム合金の溶湯を注入して一部に
アルミニウム又はアルミニウム合金をマトリックスとす
る繊維強化金属を含むインゴットを作製した後、同イン
ゴットの繊維強化金属部がブレードの前端部に位置する
ように前記インゴットからブレードを削成することを特
徴とするブレードの製造方法。Fiber-reinforced metal in which a reinforcing fiber preform made of ceramic whiskers or short fibers is placed in a part of the mold, and molten aluminum or aluminum alloy is injected into the mold, so that part of the mold has aluminum or aluminum alloy as a matrix. A method for manufacturing a blade, comprising: producing an ingot containing the ingot, and then cutting a blade from the ingot so that the fiber-reinforced metal part of the ingot is located at the front end of the blade.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1854986A JPS62176663A (en) | 1986-01-30 | 1986-01-30 | Production of blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1854986A JPS62176663A (en) | 1986-01-30 | 1986-01-30 | Production of blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS62176663A true JPS62176663A (en) | 1987-08-03 |
Family
ID=11974711
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1854986A Pending JPS62176663A (en) | 1986-01-30 | 1986-01-30 | Production of blade |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62176663A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12013448B2 (en) | 2018-09-25 | 2024-06-18 | Suzhou Gyz Electronic Technology Co., Ltd. | Base with electronic component and voice coil motor |
-
1986
- 1986-01-30 JP JP1854986A patent/JPS62176663A/en active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12013448B2 (en) | 2018-09-25 | 2024-06-18 | Suzhou Gyz Electronic Technology Co., Ltd. | Base with electronic component and voice coil motor |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| HU208270B (en) | Lose-pattern, pressure precision casting method | |
| CN107470592A (en) | One kind covers sand cooling iron construction and its manufacture craft | |
| BR9204096A (en) | PROCESS OF OBTAINING COMPOSITE CUISINES | |
| JPS62176663A (en) | Production of blade | |
| Sequeira et al. | Effect of section thickness and microstructure on the mechanical properties of high pressure die cast magnesium alloy AZ 91 D | |
| US4427742A (en) | Core or core part for use in the lost wax casting process | |
| TW330866B (en) | Casting method for composite parts with non-uniform distribution of reinforcing materials | |
| JPH04224198A (en) | Production of mmc preform | |
| JPH0489155A (en) | Manufacture of precise casting having complex part | |
| JPH0433745A (en) | Manufacture of precise casting product having composite part | |
| JP2000271728A (en) | Production of composite stock with non-pressurize impregnating permeation method | |
| JPH07313635A (en) | Golf club head and its manufacture | |
| JP2000202613A (en) | Manufacture of cylinder block | |
| JP2002316238A (en) | Mold structure | |
| JP2002282998A (en) | Mold structure | |
| JP2000152575A (en) | Squirrel-cage rotor and its manufacture | |
| JPH08325655A (en) | Production of aluminum casting | |
| JP2002316253A (en) | Method for tilting-casting metal-ceramics composite material | |
| SU778926A1 (en) | Method of surface alloying of castings | |
| JPH10288079A (en) | Cylinder block and its casting method | |
| Shi | Research and Application on the Immersing Shakeout for Steel Castings | |
| JPS5852501B2 (en) | Manufacturing method for resin-coated zinc alloy castings | |
| JPS59213961A (en) | Rotor of rotary fluid pump | |
| JP2002224815A (en) | Fiber-reinforced metallic cylinder liner, and manufacturing method of fiber-reinforced metallic cylinder liner and cylinder block | |
| Scredon | Next Generation Superalloy is Cast into Blade by GE |