CN114059066A - 一种用于提高基于铂铝粘结层的热障涂层寿命的方法 - Google Patents

一种用于提高基于铂铝粘结层的热障涂层寿命的方法 Download PDF

Info

Publication number
CN114059066A
CN114059066A CN202110894538.1A CN202110894538A CN114059066A CN 114059066 A CN114059066 A CN 114059066A CN 202110894538 A CN202110894538 A CN 202110894538A CN 114059066 A CN114059066 A CN 114059066A
Authority
CN
China
Prior art keywords
platinum
coating
aluminum
tgo
thermal barrier
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
CN202110894538.1A
Other languages
English (en)
Inventor
于昊君
宫骏
李运通
李伟
孙超
姜肃猛
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.)
Institute of Metal Research of CAS
Original Assignee
Institute of Metal Research of CAS
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 Institute of Metal Research of CAS filed Critical Institute of Metal Research of CAS
Priority to CN202110894538.1A priority Critical patent/CN114059066A/zh
Publication of CN114059066A publication Critical patent/CN114059066A/zh
Pending legal-status Critical Current

Links

Images

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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/34Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates
    • C23C28/345Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer
    • C23C28/3455Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one inorganic non-metallic material layer, e.g. metal carbide, nitride, boride, silicide layer and their mixtures, enamels, phosphates and sulphates with at least one oxide layer with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer
    • 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
    • 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/08Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
    • C23C8/10Oxidising
    • C23C8/12Oxidising using elemental oxygen or ozone

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Inorganic Chemistry (AREA)
  • Ceramic Engineering (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)

Abstract

本发明公开了一种用于提高基于铂铝粘结层的热障涂层寿命的方法,属于高温防护涂层技术领域。本发明通过预氧化的方法,预先在铂铝涂层表面制备一层TGO氧化膜,作为TBC涂层的底层粘结层。铂铝涂层粘结层主要依靠表面生成氧化膜TGO来与TBCs热障涂层顶层YSZ粘结,TGO氧化膜的厚度增加由于O与Al原子扩散速率的原因呈现抛物线型生长模式,当TGO厚度增加产生的应力集中导致TGO本身开裂脱落,会导致TBC涂层失效。由于低压预氧化工艺可以预先在铂铝粘结层表面生成一层致密氧化膜TGO,减缓TGO的生长速度,因此可以改善TBCs热障涂层的寿命。

Description

一种用于提高基于铂铝粘结层的热障涂层寿命的方法
技术领域
本发明涉及高温防护涂层技术领域,具体涉及一种用于提高基于铂铝粘结层的热障涂层寿命的方法。
背景技术
作为一种具有良好抗氧化、抗热腐蚀性能的铂改性铝化物涂层,已被广泛应用于航空发动机、燃气轮机叶片等耐热部件的防护,它既可以单独使用,也可以作为粘接层(bond coat)与表面陶瓷层(如Y2O3稳定ZrO2)一起构成热障涂层(TBCs,即thermal barriercoatings)体系,来提高部件的抗高温氧化、抗热腐蚀性能,延长部件的服役寿命。相关应用的文献如:①中国发明专利,Pt+Si改性的β-NiAl热障涂层极其制备方法,申请号201210078703.7;②中国发明专利,用于隔热涂层的经铂改性的NiCoCrAlY结合涂层,申请号20061016095.5;③中国发明专利,一种防护涂层,申请号200410003852.2。
对于高温合金及高温防护涂层部件而言,其抗氧化性能主要依靠:(1)一层致密并且生长缓慢的Al2O3膜(TGO),阻止元素的内外扩散;以及(2)氧化钇稳定氧化锆陶瓷涂层来降低粘结层表面的温度。但是由于Al2O3膜和陶瓷涂层很脆,粘结层涂层在使用过程当中Al2O3膜(TGO)厚度增加导致的应力集中很容易导致Al2O3膜和陶瓷涂层脱落,因此如能抑制Al2O3膜(TGO)的生长则可以提高TBCs涂层的使用寿命。
发明内容
为了进一步提高铂铝粘结层在TBCs中的服役时间,本发明提供一种用于提高基于铂铝粘结层的热障涂层寿命的方法,该方法采用低压氧化的手段在铂铝涂层表面生成一层致密的氧化铝薄膜,延缓铂铝涂层在高温氧化中TGO的生长速度,该方法提高了TBCs涂层的使用寿命。
为实现上述目的,本发明所采用的技术方案如下:
一种用于提高基于铂铝粘结层的热障涂层寿命的方法,该方法首先在基体表面制备铂铝涂层,然后采用低压预氧化工艺在铂铝涂层表面形成一层致密TGO获得铂铝粘结层,最后在所述TGO上面制备YSZ氧化钇改性氧化锆涂层。
所述基体为CMSX-4、DD419、Rene5或DD5合金。
所述铂铝涂层化学成分为:Pt为10-40wt%,Al为20-40wt%,Ni为30-40wt%;所述铂铝涂层中β-(Ni,Pt)Al为主相。
所述铂铝涂层厚度为20~60μm。
所述低压预氧化工艺是指采用氧气对基体上的铂铝涂层进行处理,其中:处理压力为1×10-2~1×103Pa,处理温度为900~1080℃,处理时间为3~8h,通入浓度≥99.99%纯氧,通入纯氧流量为1~300ml/min。所述低压预氧化工艺中,在真空条件下加热,达到处理温度900℃-1080℃后通入氧气,保温结束后停止通入气体,在真空条件下炉冷到100℃以下取样。
所述铂铝涂层采用低压预氧化工艺处理后,铂铝涂层表面生成一层TGO氧化膜(主要为α-Al2O3膜),TGO氧化膜厚度为0.5~4μm。生成TGO氧化膜的表面粗糙度为Ra=0.5~1.6。
所述YSZ氧化钇改性氧化锆涂层的厚度为80~250μm。
本发明的优点和有益效果如下:
1、本发明通过低压预氧化处理在铂铝涂层表面预先生成一层很薄的致密的Al2O3膜(TGO),进而可以抑制Al2O3膜中O和Al的互扩散,降低生长速率,延长TBCs热障涂层服役时间。
2、铂铝涂层主要依靠表面生成氧化膜TGO与TBCs热障涂层顶层YSZ粘结,TGO氧化膜的厚度增加由于O与Al原子扩散速率的原因呈现抛物线型生长模式,当TGO厚度增加产生的应力集中导致TGO本身开裂脱落,会导致TBC涂层失效。本发明采用低压预氧化工艺可以预先在铂铝涂层表面生成一层致密氧化膜TGO(主要为α-Al2O3膜),通过消耗一部分β-(Ni,Pt)Al相在表面形成致密的氧化铝薄膜,减缓TGO的生长速度,因此可以提高TBCs热障涂层的寿命。
3、单纯的铂铝涂层在进行高温氧化时,氧化膜中多数为致密性较差的θ-Al2O3,而进行预氧化后,铂铝粘结层表面生成一层致密的α-Al2O3,可减缓涂层进一步的氧化,降低氧化速率。因此预氧化可以有效的提高的铂铝粘结层TBCs的寿命。
附图说明
图1为30μm铂铝涂层的表面形貌。
图2为30μm铂铝涂层的截面形貌。
图3为30μm铂铝涂层在1000℃预氧化后的表面形貌。
图4为30μm铂铝涂层在1000℃预氧化后的截面形貌。
图5为1000℃预氧化的TBCs试样(30μm铂铝涂层)在1100℃进行450h热循环后的截面形貌。
图6为1000℃预氧化的TBCs试样(30μm铂铝涂层)在1100℃下经过2200次热冲击后的截面形貌。
图7为30μm铂铝涂层在900℃预氧化后的表面形貌。
图8为900℃预氧化的TBCs试样(30μm铂铝涂层)在1100℃进行450h热循环后的截面形貌。
图9为900℃预氧化的TBCs试样(30μm铂铝涂层)在1100℃下经过2200次热冲击后的截面形貌。
图10为无预氧化、900℃预氧化以及1000℃预氧化的TBCs试样(30μm铂铝涂层)在1100℃恒温氧化净增重曲线。
图11为无预氧化、900℃预氧化以及1000℃预氧化的TBCs试样(30μm铂铝涂层)热冲击和热循环实验的试样表面状态。
具体实施方式
为了进一步理解本发明,以下结合实例对本发明进行描述,但实例仅为对本发明的特点和优点做进一步阐述,而不是对本发明权利要求的限制。
本发明提供一种用于提高基于铂铝粘结层的热障涂层寿命的方法,具体过程如下:
(1)在基体上制备铝铂涂层:
制备的铂铝涂层一般是先电镀铂再进行热处理,热处理温度一般为1000℃-1100℃,热处理时间一般为1-3小时;热处理后采用化学气相沉积的方法沉积铝,沉积过程中(渗铝)温度为900℃-1100℃,时间3-6小时。
(2)低压预氧化处理:
将带有铂铝涂层的试样在真空条件下加热到900℃-1080℃,在该温度下进行保温3-8小时,并通入氧气,在涂层表面生成致密的氧化膜;保温结束后在真空条件下炉冷到100℃以下取样。
氧化过程是采用管式炉在真空条件下加热和冷却,一般真空度为1.5×10-1Pa,在负压条件下发生氧化,生成致密的氧化铝薄膜。
(3)在TGO氧化膜表面沉积厚度为80~250μm的YSZ氧化钇改性氧化锆涂层。
实施例1:
基材采用定向凝固镍基高温合金DD5。
其化学成分如下(质量百分比):Co:7.5%,Cr:7%,W:5%,Mo:1.5%,Al:6.2%,Ta:6.5%,Re:3%,Ni:余量。将直径为13mm的DD5高温合金棒用线切割加工成厚2毫米的圆片,在圆片的上方正中间位置切Φ3mm的圆孔,以方便电镀和气相沉积的过程中悬挂。
利用电镀制备铂层,再采用CVD引入铝离子,制备的铂铝涂层为30μm,表面和截面形貌如图1和图2所示。该铂铝涂层外层1/3处Pt含量为10~40wt%,Ni含量为30-40wt%,Al含量为20-40wt%。
将制备好铂铝涂层的合金试样放入管式炉中,通入氩气对炉膛进行洗气;
洗气结束后,进行抽真空,当炉内达到压强为1.5×10-1Pa时,开始以10-15℃/min速度加热到1000℃;
到温后,通入流量为35ml/min的99.99%纯氧,并在1000℃保温5h进行氧化,此时炉内压强在25Pa左右;
氧化结束后,停止通入氧气,在真空条件下进行炉冷,当温度下降到100℃以下取样。
对样品进行检测发现涂层表面为致密的α-Al2O3,形貌如图3所示,氧化膜的厚度为1.2微米,如图4所示。
在预氧化后的铂铝粘结层上制备YSZ氧化钇改性氧化锆并进行了恒温氧化实验、热循环实验和热冲击实验。1100℃恒温氧化得到的试样净增重曲线如图10所示,相对于铂铝涂层,1000℃预氧化后的试样增重最小。1100℃热循环450小时后的实验截面如图5所示。1100℃的热冲击2200次的试样截面如图6所示。热循环和热冲击实验的试样情况如图11所示,根据图可知,添加预氧化工艺后涂层在经过长时间的热循环和热冲击时具有较好的结合力,。
实施例2:
基体采用DD5高温合金,将直径为13毫米的高温合金棒用线切割加工成厚2毫米的圆片,在圆片的上方正中间位置切Φ3mm的圆孔,以方便电镀和气相沉积的过程当中悬挂。
利用电镀和化学气相沉积的方法制备30μm铂铝涂层,表面和截面如图1和图2所示;
在管式炉中利用氩气对炉膛进行洗气处理,洗气结束后,进行抽真空,当炉内达到压强为1.5×10-1Pa时,开始以10-15℃/min速度加热到900℃;
到温后,通入流量为35ml/min的99.99%纯氧,并在900℃保温5h进行氧化,此时炉内压强在15Pa左右;
氧化结束后停止通入氧气,在真空条件下进行炉冷,当温度下降到100℃以下取样。预氧化后的表面形貌图如图7所示,涂层表面形成了致密的氧化铝薄膜。
在预氧化后的铂铝粘结层上制备YSZ氧化钇改性氧化锆并进行了恒温氧化实验、热循环实验和热冲击实验。1100℃恒温氧化得到的试样净增重曲线如图10所示,相对于铂铝涂层,具有较小的增重。1100℃热循环450小时后的试样截面如图8所示。1100℃热冲击2200次的试样截面如图9所示。热循环和热冲击试样表面状况如图11所示,根据图可知,添加预氧化工艺后涂层在经过长时间的热循环和热冲击时具有较好的结合力。

Claims (9)

1.一种用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:该方法首先在基体表面制备铂铝涂层,然后采用低压预氧化工艺在铂铝涂层表面形成一层致密TGO获得铂铝粘结层,最后在所述TGO上面制备YSZ氧化钇改性氧化锆涂层。
2.根据权利要求1所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述基体为CMSX-4、DD419、Rene5或DD5合金。
3.根据权利要求1所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述铂铝涂层化学成分为:Pt为10-40wt%,Al为20-40wt%,Ni为30-40wt%;所述涂层中β-(Ni,Pt)Al为主相。
4.根据权利要求1所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述铂铝涂层厚度为20~60μm。
5.根据权利要求1所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述低压预氧化工艺是指采用氧气对基体上的铂铝涂层进行处理,其中:处理压力为1×10-2~1×103Pa,处理温度为900~1080℃,处理时间为3~8h,通入浓度≥99.99%纯氧,通入纯氧流量为1~300ml/min。
6.根据权利要求5所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述低压预氧化工艺中,在真空条件下加热,达到处理温度900℃-1080℃后通入氧气,保温结束后停止通入气体,在真空条件下炉冷到100℃以下取样。
7.根据权利要求5所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述铂铝涂层采用低压预氧化工艺处理后,铂铝涂层表面生成一层TGO氧化膜,TGO氧化膜厚度为0.5~4μm。
8.根据权利要求5或7所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述TGO氧化膜为α-Al2O3,生成TGO氧化膜的表面粗糙度为Ra 0.5~1.6。
9.根据权利要求1所述的用于提高基于铂铝粘结层的热障涂层寿命的方法,其特征在于:所述YSZ氧化钇改性氧化锆涂层的厚度为80~250μm。
CN202110894538.1A 2021-08-05 2021-08-05 一种用于提高基于铂铝粘结层的热障涂层寿命的方法 Pending CN114059066A (zh)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202110894538.1A CN114059066A (zh) 2021-08-05 2021-08-05 一种用于提高基于铂铝粘结层的热障涂层寿命的方法

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202110894538.1A CN114059066A (zh) 2021-08-05 2021-08-05 一种用于提高基于铂铝粘结层的热障涂层寿命的方法

Publications (1)

Publication Number Publication Date
CN114059066A true CN114059066A (zh) 2022-02-18

Family

ID=80233494

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202110894538.1A Pending CN114059066A (zh) 2021-08-05 2021-08-05 一种用于提高基于铂铝粘结层的热障涂层寿命的方法

Country Status (1)

Country Link
CN (1) CN114059066A (zh)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030203221A1 (en) * 2001-07-06 2003-10-30 Irene Spitsberg Method for improving the TBC life of a single phase platinum aluminide bond coat by preoxidation heat treatment
CN102615914A (zh) * 2012-03-23 2012-08-01 上海大学 Pt改性的热障涂层及其制备方法
CN109930102A (zh) * 2019-04-25 2019-06-25 清华大学无锡应用技术研究院 一种新型热障涂层制备工艺
CN110172703A (zh) * 2019-05-27 2019-08-27 昆明理工大学 一种提高镍基合金上高温涂层寿命的方法

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20030203221A1 (en) * 2001-07-06 2003-10-30 Irene Spitsberg Method for improving the TBC life of a single phase platinum aluminide bond coat by preoxidation heat treatment
CN102615914A (zh) * 2012-03-23 2012-08-01 上海大学 Pt改性的热障涂层及其制备方法
CN109930102A (zh) * 2019-04-25 2019-06-25 清华大学无锡应用技术研究院 一种新型热障涂层制备工艺
CN110172703A (zh) * 2019-05-27 2019-08-27 昆明理工大学 一种提高镍基合金上高温涂层寿命的方法

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
宋鹏等: "铂铝涂层高温氧化的影响因素研究", 《稀有金属材料与工程》 *

Similar Documents

Publication Publication Date Title
EP1995350B1 (en) High temperature component with thermal barrier coating
EP1640477B2 (en) High temperature component with thermal barrier coating and gas turbine using the same
CA2525320C (en) High-temperature coatings with pt metal modifed .gamma.-ni+.gamma.'-ni3a1 alloy compositions
JP2006083469A (ja) 保護層を被着するための方法
CA2576004A1 (en) Oxidation-resistant coating and formation method thereof, thermal barrier coating, heat-resistant member, and gas turbine
US20130202913A1 (en) Ni-BASED SUPERALLOY COMPONENT HAVING HEAT-RESISTANT BOND COAT LAYER FORMED THEREIN
CN113584419B (zh) 用于TiAl合金表面的热障涂层及其制备方法
JP5905336B2 (ja) 発電用ガスタービン翼、発電用ガスタービン
JP7174811B2 (ja) 高温部材
JPH0251978B2 (zh)
EP1908857A2 (en) Method for forming a thermal barrier coating
US20190047253A1 (en) Adhesion promoter layer for joining a high-temperature protection layer to a substrate, and method for producing same
CN114231906A (zh) 一种船用燃气轮机高压涡轮叶片的热障涂层及其制备方法
EP0985745B1 (en) Bond coat for a thermal barrier coating system
US20080292873A1 (en) Method for Providing a Thermal Barrier Coating and Substrate Having Such Coating
CN110396623B (zh) 一种适用于单晶镍基高温合金叶片的高温防护涂层材料
US20090258165A1 (en) Platinum-modified cathodic arc coating
CN110306216B (zh) 一种活性元素Re改性β-(Ni,Pt)-Al涂层及其制备工艺
CN115198271B (zh) 一种高热匹配性热障涂层及其制备方法与应用
CN114059066A (zh) 一种用于提高基于铂铝粘结层的热障涂层寿命的方法
CN113005417B (zh) 一种航空发动机涡轮动叶片及提高其寿命的方法与应用
JPS61174385A (ja) セラミツク被覆耐熱部材及びその製造方法
CN111621735A (zh) 一种dd5单晶表面金属涂层阻扩散层制备方法
Pint et al. The performance of Pt-modified alumina-forming coatings and model alloys
Xu et al. Thermal cycling of EB-PVD/NiCoCrAlYHf thermal barrier coatings

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20220218

RJ01 Rejection of invention patent application after publication