JPS62694A - Coated blade - Google Patents

Coated blade

Info

Publication number
JPS62694A
JPS62694A JP60137985A JP13798585A JPS62694A JP S62694 A JPS62694 A JP S62694A JP 60137985 A JP60137985 A JP 60137985A JP 13798585 A JP13798585 A JP 13798585A JP S62694 A JPS62694 A JP S62694A
Authority
JP
Japan
Prior art keywords
layer
coating
erosion
corrosion
layers
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
Application number
JP60137985A
Other languages
Japanese (ja)
Inventor
Masakatsu Fukuda
福田 正勝
Tatsuo Morimoto
森本 立男
Hiroshi Notomi
納富 啓
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP60137985A priority Critical patent/JPS62694A/en
Publication of JPS62694A publication Critical patent/JPS62694A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To improve corrosion and erosion resistance by applying anti-corrosion coating to the first layer of the surface of an aluminum or aluminum alloy-made moving blade used in an exhaust gas ventilator, etc., and anti-erosion coating to its outer-most layer. CONSTITUTION:A 0.2mm-thick plasma flame coating of TiO2 powders is applied as anti-corrosion coating to the surface of an aluminum alloy blade 1 after surface preparation, and then, as anti-erosion coating, a 0.2mm-thick plasma flame coating of TiO2 powders blended with powders containing 20% Cr2O3 is applied to the third, fourth, and fifth layer with a TiO2-Cr2O3 ratio of 60:40, 40: and 20:80 respectively, and to the sixth layer with a 0.2mm-thick plasma flame coating of Cr2O3 to. Consequently, a coating layer 2 consisting of six layers is formed on the metal surface. The sixth layer on the outermost surface is effective for erosion resistance and the first layer for corrosion resistance, and the coatings between said two layers gradually change in proportion of the materials, to prevent peeling between the layers.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 本発明は耐食耐エロージョン翼に関し、特にボイラなど
の排ガス通風機、例えば誘引通風機や脱硫通風機などの
動翼に関する。
DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a corrosion-resistant and erosion-resistant blade, and particularly to a rotor blade of an exhaust gas fan such as a boiler, such as an induced draft fan or a desulfurization fan.

〔従来の技術〕[Conventional technology]

例えば、ボイラの排脱装置の一部に設置される脱硫通風
機は強酸性の排ガスによる腐食や、ダストやミストによ
るエロージョンに耐えることが要求される。とのような
条件を兼備するものとしてN1基合金があげられるが、
これらは高価であるとともに大型化した場合の製作技術
、例えば鍛造性や鋳造性において、不具合点が多く、ま
た、表面処理技術としても耐食性、耐エロージョン性を
兼備し念ものはない。
For example, a desulfurization ventilator installed in a part of a boiler exhaust system is required to withstand corrosion caused by strongly acidic exhaust gas and erosion caused by dust and mist. N1-based alloys can be cited as ones that meet the above conditions.
These are expensive and have many defects in manufacturing techniques such as forgeability and castability when enlarged, and there is no surface treatment technique that can provide both corrosion resistance and erosion resistance.

まえ、安価な金属材料の表面に塗装あるいは溶射によシ
コーティングを施すことも試みられてhるが、現状では
耐食性と耐エロージョン性を兼備したコーティング材料
はない。
Previously, attempts have been made to apply coatings by painting or thermal spraying to the surfaces of inexpensive metal materials, but at present there is no coating material that has both corrosion resistance and erosion resistance.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

本発明は上述の従来法において解決できなかった点を解
決し、安価な材料で耐食性と耐二は−ジョン性を兼備し
た被覆層を有する軽量な動翼を提供しようとするもので
ある。
The present invention solves the problems that could not be solved by the above-mentioned conventional methods, and aims to provide a lightweight rotor blade having a coating layer that has both corrosion resistance and corrosion resistance using an inexpensive material.

〔問題点を解決するための手段〕[Means for solving problems]

本発明は耐食性の優れたコーテイング材と、耐エロージ
ョン性の優れたコーテイング材を、アルミニウムまたは
アルミニウム合金面から段階的に混合割合を変化させて
溶射し、アルミニウムまたはアルミニウム合金°表面側
で耐食性コーティング材100%、  コーテイング膜
表面で耐エロージョン性コーテイング材100%、その
中間では両者の混合割合を徐々に変化させて多層盛りす
ることKよシ、耐食性と耐エロージョン性を兼備し九コ
ーティング層を形成させることによって、上記目的を達
成するものである。
In the present invention, a coating material with excellent corrosion resistance and a coating material with excellent erosion resistance are thermally sprayed from the aluminum or aluminum alloy surface in a stepwise varying mixing ratio. 100% erosion-resistant coating material on the surface of the coating film, and in the middle, gradually changing the mixing ratio of the two to form a multilayer coating that combines corrosion resistance and erosion resistance. By doing so, the above objective is achieved.

すなわち本発明はアルミニウムまたはアルミニウム合金
よりなる翼基材に接して耐食性材料が、最外周面に耐エ
ロージョン性材料が位置し、それらの中間においては前
記両材料のうち、外周面になるに従って順次耐エロージ
ョン性材料の混合比を増加して成る材料で多層に被覆し
て成る被覆翼である。
That is, in the present invention, a corrosion-resistant material is located in contact with a wing base material made of aluminum or an aluminum alloy, and an erosion-resistant material is located on the outermost surface, and between them, out of the above-mentioned materials, the corrosion-resistant material is located in order toward the outer peripheral surface. This is a coated blade made of a multi-layer coating made of a material with an increased mixing ratio of erodible materials.

本発明被覆属の與作例の一例を示すと、金属型具の表面
に例えば6層盛りする場合、翼面に第1層として耐食性
コーテイング材をコーティングし、第2層目は耐食コー
テイング材80チト耐二ローシヨン性コーテイング材2
0%の混合材を、同様に第3層は60チ:4層%、第4
層は40%:60%、第5層は80%:20%とし、最
終の第6層は耐工p−ジョン性コーチインク材100%
をコーティングし、耐食、耐エロージョン性翼を形成す
ることKよって本発明の目的とする被覆翼が得られる。
To give an example of the coating of the present invention, when applying six layers on the surface of a metal mold, for example, the blade surface is coated with a corrosion-resistant coating material as the first layer, and the second layer is coated with 80 layers of corrosion-resistant coating material. Double lotion resistant coating material 2
0% mixed material, similarly the third layer is 60chi:4 layer%, the fourth layer
The layers are 40%:60%, the 5th layer is 80%:20%, and the final 6th layer is 100% engineering-resistant p-joon coach ink material.
A coated blade, which is the object of the present invention, can be obtained by coating it to form a corrosion-resistant and erosion-resistant blade.

耐食性材料としては、’f’io、、  52チ00−
28チNo −17チC!r−3チS1  よりなるト
リバロイr−aoo (米国キャボト社製)などが使用
される。
As a corrosion-resistant material, 'f'io,, 52chi00-
28 Chi No -17 Chi C! Tribaloy r-aoo (manufactured by Cabot Co., Ltd., USA) made of r-3chi S1 is used.

耐エロージョン性材料としてはOr、O□wa+a。Or, O□wa+a are examples of erosion-resistant materials.

などが使用できる。etc. can be used.

コーテイング膜の製作には任意のコーティング法が採用
できるが、溶射法コーティング材のうち、耐エロージョ
ン性の良好なものはセラミックス系材料が多いため、溶
射によるコーティングが有利である。
Any coating method can be used to produce the coating film, but among thermal spray coating materials, many ceramic materials have good erosion resistance, so thermal spray coating is advantageous.

〔実施例〕〔Example〕

本発明を軸流式通風機用具に適用した場合を、第1図、
第2図に示す。第1図は軸流式通風機用具に本発明を適
用した場合の断面図、第2図は第1図のム部の拡大図で
ある。
Figure 1 shows the case where the present invention is applied to an axial flow fan tool.
Shown in Figure 2. FIG. 1 is a sectional view when the present invention is applied to an axial flow fan tool, and FIG. 2 is an enlarged view of the arm portion of FIG. 1.

ブラストや脱脂などの下地処理を施したアルミニウム合
金製翼10表百に先ず耐食性コーティングとしてT10
.粉末をα2m厚さにプラズマ溶射し、次1c ’i’
10.粉末に耐エロージョン性コーティングとしてOr
、O,を20%均一に混合した粉末を溶射、第3層とし
てはTie、 :Or、 O@=60:40、第4層T
ie、: Or、0. = 40 : 60 、第5層
’I’10゜: Or、0. =20 : 80、第6
層にはor、o、をそれぞれ(L2mm厚さプラズマ溶
射した。金属表面には以上のように6層のコーティング
層2が形成され、耐エロージョン性に関しては表層の第
 46層が、耐食性に関しては第1層目が効果を発揮し
、それぞれの中間層もそれぞれ耐食性及び耐エロージョ
ン性を有するとともに1両コーテイング材が徐々に割合
変化をしているため、一般に多層盛りした増合のように
材質特性の変化による眉間剥離などが防止できる。なお
、耐食性としてはトリバロイ、耐エロージョン性はwa
+oo も有効である。
Aluminum alloy blades that have undergone surface treatment such as blasting and degreasing are first coated with T10 as a corrosion-resistant coating.
.. Plasma spray the powder to α2m thickness, then 1c 'i'
10. Or as an erosion-resistant coating on powder
The third layer is Tie, :Or, O@=60:40, and the fourth layer is T.
ie, : Or, 0. = 40: 60, 5th layer 'I' 10°: Or, 0. =20: 80, 6th
The layers were plasma sprayed with or and o, respectively (L2 mm thick). Six coating layers 2 were formed on the metal surface as described above, and the 46th layer of the surface layer was for erosion resistance, and the 46th layer was for corrosion resistance. The first layer is effective, and each intermediate layer also has corrosion resistance and erosion resistance, and the ratio of the coating material changes gradually, so the material properties are generally the same as in a multi-layered compound. It is possible to prevent peeling between the eyebrows due to changes in
+oo is also valid.

〔発明の効果〕〔Effect of the invention〕

アルミニウムまたはアルミニウム合金型具の表面の第1
層に耐食コーティングを施し、最外層に耐エロージョン
性コーティングを施し、その中間層では段階的に両者の
割合を変化させることで、耐食性と耐エロージョン性を
兼備した通風機用具を得ることができる。
The first surface of the aluminum or aluminum alloy mold tool
By applying a corrosion-resistant coating to the layer, applying an erosion-resistant coating to the outermost layer, and changing the ratio of the two in stages in the intermediate layer, it is possible to obtain a ventilator tool that has both corrosion resistance and erosion resistance.

なお、中間層は割合を段階的に変えるため、各層間での
特性変化が小さく、従来の多層盛りコーティングl1i
XK見られたような層間剥離は防止できる。
In addition, since the ratio of the intermediate layer is changed stepwise, the change in characteristics between each layer is small, and it is different from the conventional multilayer coating l1i.
It is possible to prevent delamination as seen in XK.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は軸流式通風機用具に本発明のコーティングを施
した横断面図、第2図は第1図ム部の拡大で多層コーテ
ィングの6層盛りの例を示す0 徨代理人  内 1)  明 復代理人  萩 原 亮 − 復代理人  安 西 篤 夫
Figure 1 is a cross-sectional view of an axial flow fan tool coated with the coating of the present invention, and Figure 2 is an enlarged view of the part in Figure 1, showing an example of six layers of multilayer coating. ) Meifuku agent Ryo Hagiwara − Sub-agent Atsuo Anzai

Claims (1)

【特許請求の範囲】[Claims] アルミニウムまたはアルミニウム合金よりなる翼基材に
接して耐食性材料が、最外周面に耐エロージョン性材料
が位置し、それらの中間においては前記両材料のうち、
外周面になるに従って順次耐エロージョン性材料の混合
比を増加して成る材料で多層に被覆して成る被覆翼。
A corrosion-resistant material is located in contact with the wing base material made of aluminum or aluminum alloy, and an erosion-resistant material is located on the outermost peripheral surface, and between them, among the two materials,
A coated blade that is coated in multiple layers with a material in which the mixing ratio of erosion-resistant materials is gradually increased toward the outer peripheral surface.
JP60137985A 1985-06-26 1985-06-26 Coated blade Pending JPS62694A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP60137985A JPS62694A (en) 1985-06-26 1985-06-26 Coated blade

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP60137985A JPS62694A (en) 1985-06-26 1985-06-26 Coated blade

Publications (1)

Publication Number Publication Date
JPS62694A true JPS62694A (en) 1987-01-06

Family

ID=15211360

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60137985A Pending JPS62694A (en) 1985-06-26 1985-06-26 Coated blade

Country Status (1)

Country Link
JP (1) JPS62694A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5209645A (en) * 1988-05-06 1993-05-11 Hitachi, Ltd. Ceramics-coated heat resisting alloy member
CN101639080A (en) * 2008-07-31 2010-02-03 通用电气公司 Compressor blade leading edge shim and related method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53139211A (en) * 1977-05-12 1978-12-05 Mitsubishi Heavy Ind Ltd Manufacturing of light alloy blade
JPS5791398A (en) * 1980-11-28 1982-06-07 Mitsubishi Heavy Ind Ltd Corrosion-resisting and errosion-resisting blade
JPS5820996A (en) * 1981-07-31 1983-02-07 Mitsubishi Heavy Ind Ltd Corrosion-and erosion-resisting blade

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS53139211A (en) * 1977-05-12 1978-12-05 Mitsubishi Heavy Ind Ltd Manufacturing of light alloy blade
JPS5791398A (en) * 1980-11-28 1982-06-07 Mitsubishi Heavy Ind Ltd Corrosion-resisting and errosion-resisting blade
JPS5820996A (en) * 1981-07-31 1983-02-07 Mitsubishi Heavy Ind Ltd Corrosion-and erosion-resisting blade

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5209645A (en) * 1988-05-06 1993-05-11 Hitachi, Ltd. Ceramics-coated heat resisting alloy member
CN101639080A (en) * 2008-07-31 2010-02-03 通用电气公司 Compressor blade leading edge shim and related method

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