JPH0372706B2 - - Google Patents

Info

Publication number
JPH0372706B2
JPH0372706B2 JP57137165A JP13716582A JPH0372706B2 JP H0372706 B2 JPH0372706 B2 JP H0372706B2 JP 57137165 A JP57137165 A JP 57137165A JP 13716582 A JP13716582 A JP 13716582A JP H0372706 B2 JPH0372706 B2 JP H0372706B2
Authority
JP
Japan
Prior art keywords
coating
hafnium
nicocraly
superalloy
yttrium
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 - Lifetime
Application number
JP57137165A
Other languages
Japanese (ja)
Other versions
JPS5837146A (en
Inventor
Sukotsuto Dejuaru Deuitsudo
Kumaa Guputa Deinetsushu
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPS5837146A publication Critical patent/JPS5837146A/en
Publication of JPH0372706B2 publication Critical patent/JPH0372706B2/ja
Granted legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C30/00Coating with metallic material characterised only by the composition of the metallic material, i.e. not characterised by the coating process
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/058Alloys based on nickel or cobalt based on nickel with chromium without Mo and W
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C4/00Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
    • C23C4/04Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
    • C23C4/06Metallic material
    • C23C4/073Metallic material containing MCrAl or MCrAlY alloys, where M is nickel, cobalt or iron, with or without non-metal elements
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B29/00Single crystals or homogeneous polycrystalline material with defined structure characterised by the material or by their shape
    • C30B29/10Inorganic compounds or compositions
    • C30B29/52Alloys
    • CCHEMISTRY; METALLURGY
    • C30CRYSTAL GROWTH
    • C30BSINGLE-CRYSTAL GROWTH; UNIDIRECTIONAL SOLIDIFICATION OF EUTECTIC MATERIAL OR UNIDIRECTIONAL DEMIXING OF EUTECTOID MATERIAL; REFINING BY ZONE-MELTING OF MATERIAL; PRODUCTION OF A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; SINGLE CRYSTALS OR HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; AFTER-TREATMENT OF SINGLE CRYSTALS OR A HOMOGENEOUS POLYCRYSTALLINE MATERIAL WITH DEFINED STRUCTURE; APPARATUS THEREFOR
    • C30B33/00After-treatment of single crystals or homogeneous polycrystalline material with defined structure

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Organic Chemistry (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Mechanical Engineering (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Inorganic Chemistry (AREA)
  • Coating By Spraying Or Casting (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Physical Vapour Deposition (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

[産業上の利用分野] 本発明は、超合金基質にNiCrAlY又は
NiCoCrAlY被覆を形成する方法に係る。 [従来の技術] 超合金基質を、NiCrAlY被覆又はNiCoCrAlY
被覆により保護する機能は、基質の表面に薄いア
ルミナの層が形成されることにより得られる。酸
化及び高温腐食に抵抗するのはかかるアルミナ層
である。アルミナの密着性を向上させ且その剥離
傾向を低減すべく、被覆に対しイツトリウムの如
き酸素活性元素が添加される。 超合金の開発の初期段階に於ては、超合金はい
わゆる等軸晶にて使用され、被覆されずに、ある
いは被覆される場合にも、アルミナイド被覆の如
き簡単な被覆が施された状態で使用されていた。
超合金に対する性能の条件が厳しくなるにつれ
て、超合金それ自体の改善及び被覆の改善が行な
われた。 超合金それ自体の改善の分野に於ては、超合金
が結晶組織学的に一方向に配向された細長い結晶
粒として凝固せしめられる、いわゆる一方向凝固
法の開発によつて、著しい改善がなされた。この
ことは本願出願人と同一の譲受人に譲渡された米
国特許第3260505号に記載されている。 またほぼこれと同時に、被覆の改善の分野に於
ては、NiCrAlY又はNiCoCrAlYの如きMCrAlY
型の被覆が開発された。この被覆は従来より使用
されていたアルミナイド被覆よりも保護性能に優
れたものである。米国特許第3542530号、同第
3676085号、同第3754903号、同第3928026号は
MCrAlY被覆に関するものである。 一方向凝固法は有望なものではあるが、横方向
に延性に関して重大な問題が発生した。一方向に
配向された細長い結晶粒の間の粒界は、結晶粒の
配向軸線に垂直な方向に於て極めて弱いことが発
見された。この問題は、同じく本願出願人と同一
の譲受人に譲渡された米国特許第3711337号に記
載されている如く、合金に対し少量(0.5〜2%)
のハフニウムを添加することによつて解決され
た。 ハフニウムを添加することによつて上記の強度
に於ける方向性の問題を改善された一方向凝固物
品の開発と、MCrAlY被覆の開発とは、同一の
実験室に於てほぼ同時に行なわれたもので、当然
これらは組合せて使用された。従つて、熱的にも
強度的にも厳しく要求が課せられる用途、特に第
一段のタービンブレードに於ては、当然の如く、
ハフニウムを添加され一方向凝固された基質に
MCrAlY被覆を施すことが行われた。 [発明が解決しようとする課題] しかし、ハフニウムを含有し一方向凝固された
柱状晶基質に対し、MCrAlY被覆を施す場合に、
MCrAlY被覆の組成を最適化すべく、そのイツ
トリウム含有量を重量で約0.5%又は0.7%以上と
すると、被覆と基質の界面に好ましからざる低融
点の相(イツトリウムとハフニウムとに基く相)
が発生することが解つた。 本発明は、一方向凝固された柱状晶基質の如く
ハフニウムを含むことが強度特性の改善上望まれ
る基質に、イツトリウムが被覆の密着性と対剥離
性の改善上重要な要素をなしているMCrAlY被
覆を施さんとする場合に生ずることが明らかとな
つた上記の問題に着目し、この問題を解決するこ
とによつて、ハフニウムを含む超合金基質に上記
の低融点相を生ずることなくMCrAlY被覆を施
すことができ、これによつてハフニウムを添加す
ることにより超合金基質自体の強度特性の改善を
充分に計り且その表面にイツトリウムを最適含有
量にて含むことにより密着性と対剥離性に於いて
充分改善されたMCrAlY被覆を施し、基質それ
自身の強度特性に於て優れ且高温強度に優れた被
覆が高い密着性と耐剥離性をもつて施された超合
金物品を得る方法を提供することを課題としてい
る。 [課題を解決するための手段] かかる課題は、本発明によれば、Hfを0.5〜2
%含む超合金の基質上に、Crを10〜35%、Alを
8〜20%、Yを1.1〜3%含み、残部が実質的に
Niよりなる被覆、又はCrを10〜35%、Alを8〜
20%、Coを30%以下、Yを1.1〜3%含み、残部
が実質的にNiよりなる被覆を、プラズマスプレ
ー法によつて施すことにより被覆された超合金物
品を得る方法によつて達成される。 [作用] 上記の如くハフニウムを含む超合金基質上に上
記の如き組成のMCrAlY型被覆を特にプラズマ
スプレー法により施すときには、プラズマスプレ
ーによつて被覆材が基質の表面に噴付けられる
際、基質の表面に近い部分にあるハフニウムは、
プラズマによつて与えられる高温の下に、被覆材
中に酸化イツトリウム及び酸化アルミニウムとし
て存在する酸素によつて酸化され、酸化ハフニウ
ムになる。ハフニウムは一旦酸化されると安定
し、有害な融点の低い相を形成することはない。
こうしてハフニウムを、それがイツトリウムと反
応して低融点の相を形成する前に酸化させておく
ことにより、低融点相の発生を回避してイツトリ
ウムを含む超合金基質上にMCrAlY型の被覆を
形成することができる。 [実施例] 本発明によれば、NiCoCrAlY被覆内のイツト
リウムの量を従来技術に於ける量以上に増大し、
被覆の密着性及び対剥離性に於いてより有効な効
果を得ることができる。下記の表1は本発明に適
用できる被覆の組成範囲を示している。
[Industrial Application Field] The present invention provides superalloy matrix with NiCrAlY or
The present invention relates to a method of forming a NiCoCrAlY coating. [Prior art] A superalloy substrate is coated with NiCrAlY or NiCoCrAlY.
The protective function of the coating is obtained by the formation of a thin layer of alumina on the surface of the substrate. It is such an alumina layer that resists oxidation and hot corrosion. Oxygen active elements such as yttrium are added to the coating to improve the adhesion of the alumina and reduce its tendency to peel. In the early stages of superalloy development, superalloys were used in so-called equiaxed crystals, either uncoated or, if coated, with a simple coating such as an aluminide coating. It was used.
As performance requirements for superalloys have become more stringent, improvements have been made to the superalloys themselves and to their coatings. In the field of improving superalloys themselves, significant improvements have been made with the development of the so-called unidirectional solidification process, in which superalloys are solidified as elongated grains oriented in one direction crystallographically. Ta. This is described in commonly assigned US Pat. No. 3,260,505. Also, at about the same time, in the field of coating improvement, MCrAlY such as NiCrAlY or NiCoCrAlY
A mold coating was developed. This coating provides better protection than the previously used aluminide coating. U.S. Patent No. 3,542,530;
No. 3676085, No. 3754903, No. 3928026 are
It concerns MCrAlY coating. Although the unidirectional solidification method is promising, significant problems have arisen with regard to ductility in the transverse direction. It has been discovered that grain boundaries between unidirectionally oriented elongated grains are extremely weak in the direction perpendicular to the grain orientation axis. This problem can be solved in small amounts (0.5-2%) in alloys, as described in U.S. Pat. No. 3,711,337, also assigned to the same assignee.
was solved by adding hafnium. The development of the directionally solidified article, which improved the above-mentioned problem of directionality in strength by adding hafnium, and the development of the MCrAlY coating were carried out at almost the same time in the same laboratory. Of course, these were used in combination. Therefore, it is natural that in applications where strict demands are placed on both thermal and strength requirements, especially for first stage turbine blades,
Directly solidified substrate with added hafnium
An MCrAlY coating was applied. [Problem to be solved by the invention] However, when applying MCrAlY coating to a unidirectionally solidified columnar crystal matrix containing hafnium,
In order to optimize the composition of the MCrAlY coating, if its yttrium content is greater than about 0.5% or 0.7% by weight, undesirable low-melting phases (phases based on yttrium and hafnium) at the interface between the coating and the substrate
It was found that this occurs. The present invention uses MCrAlY, which is an important element for improving the adhesion and peeling resistance of coatings, for substrates such as unidirectionally solidified columnar crystal substrates in which hafnium is desired for improving strength properties. By focusing on the above-mentioned problem that has been found to occur when attempting to apply a coating, and by solving this problem, it is possible to coat a superalloy containing hafnium without forming the above-mentioned low melting point phase. By adding hafnium, the strength characteristics of the superalloy matrix itself can be sufficiently improved, and by containing yttrium in an optimal amount on the surface, the adhesion and peeling resistance can be improved. Provided is a method for obtaining a superalloy article coated with a sufficiently improved MCrAlY coating, which has excellent strength properties of the substrate itself and has excellent high temperature strength, and has high adhesion and peeling resistance. The challenge is to do so. [Means for solving the problem] According to the present invention, this problem can be solved by reducing Hf from 0.5 to 2
% containing 10 to 35% Cr, 8 to 20% Al, 1.1 to 3% Y, with the balance being substantially
Coating made of Ni or 10-35% Cr and 8-8% Al
Achieved by a method of obtaining a coated superalloy article by applying a coating containing 20% Co, 30% or less Co, 1.1 to 3% Y, and the remainder substantially Ni, by a plasma spray method. be done. [Function] When a MCrAlY type coating having the above composition is applied to a hafnium-containing superalloy substrate by a plasma spray method, when the coating material is sprayed onto the surface of the substrate by plasma spray, the surface of the substrate is Hafnium near the surface is
Under the high temperatures provided by the plasma, it is oxidized to hafnium oxide by the oxygen present in the coating as yttrium oxide and aluminum oxide. Once hafnium is oxidized, it is stable and does not form harmful low-melting phases.
The hafnium is thus oxidized before it reacts with yttrium to form a low-melting phase, thereby avoiding the formation of a low-melting phase and forming a MCrAlY-type coating on the yttrium-containing superalloy substrate. can do. [Example] According to the present invention, the amount of yttrium in the NiCoCrAlY coating is increased over the amount in the prior art,
More effective effects can be obtained in terms of adhesion and peeling resistance of the coating. Table 1 below shows the composition range of coatings applicable to the present invention.

【表】 かかる組成によれば被覆の耐酸化性が向上す
る。尚、かかる組成は、イツリウムの含有量が高
いことを除けば、米国特許第3928026号に記載さ
れたNiCoCrAlY被覆組成と同様である。かかる
被覆組成物はニツケル基超合金を保護するのに好
適なものである。当技術分野に於ては、ある状況
の下ではNiCoCrAlY被覆に他の元素を添加する
ことが有効であることが知られている。例えば米
国特許第4034142号には、MCrAlY被覆にケイ素
を添加することが提案されており、また米国特許
第3918139号には、NiCoCrAlY被覆にプラチナ
及びこれと同様の貴金属を添加することが提案さ
れている。本発明は上述の如き米国特許に記載さ
れた修正されたNiCoCrAlY被覆にも適用され得
るものである。また本発明に従つて使用される被
覆に於て、イツトリウムの含有量が高いことによ
り得られる有益な効果に関し大きく悪影響を与え
ることなく、その特性を改善をすべく、タンタル
(0〜10%)がイツトリウム含有量の高い
NiCoCrAlY被覆に添加されてよいことが解つて
いる。 添付の図面は、NiCoCrAlY被覆材料及びケイ
素を添加することにより修正されたNiCoCrAlY
+Si被覆材料の酸化寿命に対するイツトリウム含
有量の影響を示している。NiCoCrAlY被覆材料
の公称組成は重量で22%Co、18%Cr、12.5%Al、
種々の量のY、残部Niであり、ケイ素を含有す
るNiCoCrAlY被覆の公称組成は重量で22%Co、
18%Cr、12.5%Al、1.5%Si、種々の量のY、残
部Niであつた。試験は1149℃の最高温度にて運
転された繰返しバーナ装置内にて行なわれた。尚
被覆寿命の測定結果は被覆の厚さの相違を反映す
るよう補正された。 添付の図面により、イツトリウムの含有量を増
大させれば被覆の寿命が大幅に増大することが解
る。例えばNiCoCrAlY被覆については、イツト
リウムの含有量を1%より2%に増大することに
より、被覆の寿命が約825時間より約1290時間に
まで50%以上増大することが解る。 かかる被覆材料がハフニウムを含有する基質に
対しプラズマスプレー法により着装された。この
場合、被覆と基質の界面の近傍に於ける基質中の
ハフニウムは、被覆材中に酸化イツトリウム及び
酸化アルミニウムとして存在する酸素により酸化
されて安定な酸化ハフニウムになり、有害の融点
の低い相は形成されないことが確認された。
[Table] Such a composition improves the oxidation resistance of the coating. Note that this composition is similar to the NiCoCrAlY coating composition described in US Pat. No. 3,928,026, except for the higher ythurium content. Such coating compositions are suitable for protecting nickel-based superalloys. It is known in the art that under certain circumstances it is useful to add other elements to the NiCoCrAlY coating. For example, U.S. Pat. No. 4,034,142 proposes adding silicon to MCrAlY coatings, and U.S. Pat. No. 3,918,139 proposes adding platinum and similar noble metals to NiCoCrAlY coatings. There is. The present invention may also be applied to the modified NiCoCrAlY coatings described in the above-mentioned US patents. In addition, tantalum (0-10%) is added to the coating used according to the invention in order to improve its properties without significantly adversely affecting the beneficial effects obtained by the high yttrium content. has a high yztrium content
It has been found that it may be added to NiCoCrAlY coatings. The attached drawings show NiCoCrAlY coating material and NiCoCrAlY modified by adding silicon.
It shows the influence of yttrium content on the oxidation life of +Si coating materials. The nominal composition of the NiCoCrAlY coating material is 22% Co, 18% Cr, 12.5% Al by weight,
The nominal composition of the NiCoCrAlY coating with varying amounts of Y, balance Ni, and silicon is 22% Co, by weight.
It consisted of 18% Cr, 12.5% Al, 1.5% Si, various amounts of Y, and the balance Ni. The test was conducted in a cyclic burner unit operated at a maximum temperature of 1149°C. The coating life measurements were corrected to reflect differences in coating thickness. It can be seen from the accompanying figures that increasing the yttrium content significantly increases the lifetime of the coating. For example, for the NiCoCrAlY coating, it can be seen that increasing the yttrium content from 1% to 2% increases the lifetime of the coating by more than 50%, from about 825 hours to about 1290 hours. Such a coating material was applied to a hafnium-containing substrate by plasma spraying. In this case, the hafnium in the substrate near the interface between the coating and the substrate is oxidized to stable hafnium oxide by the oxygen present in the coating as yttrium oxide and aluminum oxide, and the harmful low melting point phase is It was confirmed that no formation occurred.

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

添付の図面はNiCoCrAlYとそれにSiを加えた
二つの被覆についてイツトリウム含有量の関数と
して被覆の寿命を示すグラフである。
The accompanying drawing is a graph showing coating life as a function of yttrium content for two coatings: NiCoCrAlY and Si plus Si.

Claims (1)

【特許請求の範囲】 1 Hfを0.5〜2%含む超合金の基質上に、Crを
10〜35%、Alを8〜20%、Yを1.1〜3%含み、
残部が実質的にNiよりなる被覆を、プラズマス
プレー法によつて施すことにより被覆された超合
金物品を得る方法。 2 Hfを0.5〜2%含む超合金の基質上に、Crを
10〜35%、Alを8〜20%、Coを30%以下、Yを
1.1〜3%含み、残部が実質的にNiよりなる被覆
を、プラズマスプレー法によつて施すことにより
被覆された超合金物品を得る方法。
[Claims] 1. Cr is applied on a superalloy matrix containing 0.5 to 2% Hf.
Contains 10-35%, Al 8-20%, Y 1.1-3%,
A method of obtaining a coated superalloy article by applying a coating with the balance essentially consisting of Ni by a plasma spray method. 2 Cr was applied onto a superalloy substrate containing 0.5 to 2% Hf.
10-35%, Al 8-20%, Co 30% or less, Y
1. A method for obtaining a coated superalloy article by applying a coating containing 1.1 to 3% Ni, the remainder consisting essentially of Ni, by a plasma spray method.
JP57137165A 1981-08-05 1982-08-05 Coating composition Granted JPS5837146A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US28995381A 1981-08-05 1981-08-05
US289953 2002-11-06

Publications (2)

Publication Number Publication Date
JPS5837146A JPS5837146A (en) 1983-03-04
JPH0372706B2 true JPH0372706B2 (en) 1991-11-19

Family

ID=23113894

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57137165A Granted JPS5837146A (en) 1981-08-05 1982-08-05 Coating composition

Country Status (6)

Country Link
JP (1) JPS5837146A (en)
CA (1) CA1209827A (en)
DE (1) DE3229285A1 (en)
FR (1) FR2511043B1 (en)
GB (1) GB2103656B (en)
IL (1) IL66443A (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4743514A (en) * 1983-06-29 1988-05-10 Allied-Signal Inc. Oxidation resistant protective coating system for gas turbine components, and process for preparation of coated components
US4677035A (en) * 1984-12-06 1987-06-30 Avco Corp. High strength nickel base single crystal alloys
DE3612568A1 (en) * 1986-04-15 1987-10-29 Bbc Brown Boveri & Cie HIGH TEMPERATURE PROTECTIVE LAYER
EP0486489B1 (en) * 1989-08-10 1994-11-02 Siemens Aktiengesellschaft High-temperature-resistant, corrosion-resistant coating, in particular for components of gas turbines
US5401307A (en) * 1990-08-10 1995-03-28 Siemens Aktiengesellschaft High temperature-resistant corrosion protection coating on a component, in particular a gas turbine component
US5582635A (en) * 1990-08-10 1996-12-10 Siemens Aktiengesellschaft High temperature-resistant corrosion protection coating for a component in particular a gas turbine component
JP2003147464A (en) 2001-11-02 2003-05-21 Tocalo Co Ltd Member with high-temperature strength
DE102005053531A1 (en) * 2005-11-08 2007-05-10 Man Turbo Ag Heat-insulating protective layer for a component within the hot gas region of a gas turbine
US7754342B2 (en) * 2005-12-19 2010-07-13 General Electric Company Strain tolerant corrosion protecting coating and spray method of application
GB2443283A (en) * 2006-10-26 2008-04-30 Gen Electric Rub coating for gas turbine engine compressors
US7879459B2 (en) * 2007-06-27 2011-02-01 United Technologies Corporation Metallic alloy composition and protective coating
EP2366674A4 (en) 2008-12-16 2013-08-14 Asahi Glass Co Ltd Filmed metal member for float glass manufacturing equipment and float glass manufacturing method

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5029436A (en) * 1973-04-02 1975-03-25
JPS5231911A (en) * 1975-08-22 1977-03-10 Gen Electric Porous sealing material for use against high temperatures
JPS55161041A (en) * 1979-05-29 1980-12-15 Howmet Turbine Components Covering material

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL136758C (en) * 1963-10-21 1900-01-01
US3494709A (en) * 1965-05-27 1970-02-10 United Aircraft Corp Single crystal metallic part
US3542530A (en) * 1968-05-23 1970-11-24 United Aircraft Corp Nickel or cobalt base with a coating containing iron chromium and aluminum
US3711337A (en) * 1970-12-16 1973-01-16 United Aircraft Corp Columnar-grained nickel-base superalloy castings
US3676085A (en) * 1971-02-18 1972-07-11 United Aircraft Corp Cobalt base coating for the superalloys
US3928026A (en) * 1974-05-13 1975-12-23 United Technologies Corp High temperature nicocraly coatings
US3918139A (en) * 1974-07-10 1975-11-11 United Technologies Corp MCrAlY type coating alloy
FR2315387A1 (en) * 1975-06-23 1977-01-21 Cabot Corp Nickel alloy contg. chromium, aluminium and yttrium - with high thermal shock resistance, and useful for coating nickel or cobalt base superalloys
DE2528241A1 (en) * 1975-06-25 1977-01-13 Cabot Corp Nickel alloy contg. chromium, aluminium and yttrium - with high thermal shock resistance, and useful for coating nickel or cobalt base superalloys
US4029477A (en) * 1975-10-29 1977-06-14 General Electric Company Coated Ni-Cr base dispersion-modified alloy article
US4034142A (en) * 1975-12-31 1977-07-05 United Technologies Corporation Superalloy base having a coating containing silicon for corrosion/oxidation protection
US4116723A (en) * 1976-11-17 1978-09-26 United Technologies Corporation Heat treated superalloy single crystal article and process
US4101713A (en) * 1977-01-14 1978-07-18 General Electric Company Flame spray oxidation and corrosion resistant superalloys

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5029436A (en) * 1973-04-02 1975-03-25
JPS5231911A (en) * 1975-08-22 1977-03-10 Gen Electric Porous sealing material for use against high temperatures
JPS55161041A (en) * 1979-05-29 1980-12-15 Howmet Turbine Components Covering material

Also Published As

Publication number Publication date
IL66443A0 (en) 1982-12-31
GB2103656A (en) 1983-02-23
IL66443A (en) 1985-11-29
DE3229285C2 (en) 1988-11-24
JPS5837146A (en) 1983-03-04
CA1209827A (en) 1986-08-19
FR2511043B1 (en) 1987-05-22
FR2511043A1 (en) 1983-02-11
DE3229285A1 (en) 1983-03-24
GB2103656B (en) 1985-06-26

Similar Documents

Publication Publication Date Title
US4615865A (en) Overlay coatings with high yttrium contents
US4034142A (en) Superalloy base having a coating containing silicon for corrosion/oxidation protection
US4086391A (en) Alumina forming coatings containing hafnium for high temperature applications
JP3001161B2 (en) Aluminum coating for super alloy
CA1212020A (en) Minor element additions to single crystals for improved oxidation resistance
JP3370676B2 (en) Protective layer for protecting members against corrosion, oxidation and thermal overload, and method of manufacturing the same
US4419416A (en) Overlay coatings for superalloys
US4758480A (en) Substrate tailored coatings
US5238752A (en) Thermal barrier coating system with intermetallic overlay bond coat
JP2773050B2 (en) Heat-resistant and corrosion-resistant protective coating layer
USRE32121E (en) Overlay coatings for superalloys
US4117179A (en) Oxidation corrosion resistant superalloys and coatings
US7357958B2 (en) Methods for depositing gamma-prime nickel aluminide coatings
JPS61136649A (en) High strength nickel monocrystralline alloy
JPS5873761A (en) Powder composition for metal coating formation having high heat resistance
JP2002167636A (en) Low density oxidation resistant superalloy material capable of thermal barrier coating retention without bond coat
JPH0372706B2 (en)
JP3881489B2 (en) Superalloy turbine part repair method and superalloy turbine part
US4973445A (en) High-temperature protective coating
JPS6039173A (en) High temperature protecting layer
US6620524B2 (en) Nickel aluminide coating and coating systems formed therewith
US4909984A (en) High temperature protective coating
JP2003055753A (en) METHOD FOR DEPOSITING MCrAlY BOND COATING ONTO SURFACE OF ARTICLE
NO148114B (en) THERMALLALLY PROTECTED CONSTRUCTION OF A SUPER alloy.
US4237193A (en) Oxidation corrosion resistant superalloys and coatings