PROCESS FOR REMOVING ADHERENT OXIDE PARTICLES FROM AN ALUMINIZED SURFACE
    1.
    发明申请
    PROCESS FOR REMOVING ADHERENT OXIDE PARTICLES FROM AN ALUMINIZED SURFACE 审中-公开
    从氧化表面去除附着的氧化物颗粒的方法

    公开(公告)号:US20050127039A1

    公开(公告)日:2005-06-16

    申请号:US10707465

    申请日:2003-12-16

    摘要: A process for removing particles that become adherently sintered to an aluminized surface during an aluminiding process. The method is particularly suited for the removal of adherent particles that form as a result of oxidation of a metallic powder used as an aluminum source during slurry aluminiding processes, wherein the adherent particles become attached by sintering to the aluminized surface. The process includes contacting the aluminized surface with an aqueous caustic hydroxide solution until the particles are removed therefrom.

    摘要翻译: 一种在铝化过程中除去附着烧结到镀铝表面的颗粒的方法。 该方法特别适用于去除由浆料铝化过程中用作铝源的金属粉末的氧化形成的附着颗粒,其中粘合颗粒通过烧结附着在镀铝表面上。 该方法包括使镀铝表面与苛性氢氧化钠水溶液接触,直至从中除去颗粒。

    BETA-PHASE NICKEL ALUMINIDE OVERLAY COATING AND PROCESS THEREFOR
    2.
    发明申请
    BETA-PHASE NICKEL ALUMINIDE OVERLAY COATING AND PROCESS THEREFOR 审中-公开
    BETA相镍合金镀层及其工艺

    公开(公告)号:US20050019491A1

    公开(公告)日:2005-01-27

    申请号:US10711584

    申请日:2004-09-27

    摘要: A beta-phase nickel aluminide (NiAl) overlay coating (24) and method for modifying the grain structure of the coating (24) to improve its oxidation resistance. The coating (24) is deposited by a method that produces a grain structure characterized by grain boundaries (44) exposed at the outer coating surface (36). The grain boundaries (44) may also contain precipitates (40) as a result of the alloyed chemistry of the coating (24). During or after deposition, the overlay coating (24) is caused to form new grain boundaries (34) that, though open to the outer surface (36) of the coating (24), are free of precipitates or contain fewer precipitates (40) than the as-deposited grain boundaries (44). New grain boundaries (34) are preferably produced by causing the overlay coating (24) to recrystallize during coating deposition or after deposition as a result of a surface treatment followed by heat treatment.

    摘要翻译: β相镍铝化合物(NiAl)覆盖层(24)以及用于改变涂层(24)的晶粒结构以提高其抗氧化性的方法。 通过产生以在外涂层表面(36)处暴露的晶界(44)为特征的晶粒结构的方法沉积涂层(24)。 作为涂层(24)的合金化学的结果,晶界(44)也可以含有沉淀物(40)。 在沉积期间或之后,使覆盖涂层(24)形成新的晶粒边界(34),其尽管向涂层(24)的外表面(36)开口,但没有沉淀物或含有较少的沉淀物(40) 比沉积的晶界(44)。 优选通过在涂布沉积期间或沉积后的覆盖涂层(24)进行再结晶,然后进行热处理后的表面处理,来制造新的晶界(34)。

    CERAMIC CORROSION RESISTANT COATING FOR OXIDATION RESISTANCE
    3.
    发明申请
    CERAMIC CORROSION RESISTANT COATING FOR OXIDATION RESISTANCE 审中-公开
    陶瓷耐腐蚀涂层耐氧化

    公开(公告)号:US20100279018A1

    公开(公告)日:2010-11-04

    申请号:US12839142

    申请日:2010-07-19

    IPC分类号: B05D3/02

    摘要: A coating system and a method for forming the coating system, the method including coating a surface of a gas turbine engine turbine component having a metallic surface that is outside the combustion gas stream and exposed to cooling air during operation of the engine. A gel-forming solution including a ceramic metal oxide precursor is provided. The gel-forming solution is heated to a first preselected temperature for a first preselected time to form a gel. The gel is then deposited on the metallic surface. Thereafter the gel is fired at a second preselected temperature above the first preselected temperature to form a ceramic corrosion resistant coating comprising a ceramic metal oxide is selected from the group consisting of zirconia, hafnia and combinations thereof. The ceramic corrosion resistant coating having a thickness of up to about 127 microns and remaining adherent at temperatures greater than about 1000° F.

    摘要翻译: 一种涂覆系统和一种形成涂层系统的方法,所述方法包括在发动机操作期间涂覆具有在燃烧气流外部的金属表面并暴露于冷却空气的燃气涡轮发动机涡轮机部件的表面。 提供了包含陶瓷金属氧化物前体的凝胶形成溶液。 将凝胶形成溶液加热至第一预选温度第一预选时间以形成凝胶。 然后将凝胶沉积在金属表面上。 此后,凝胶在高于第一预选温度的第二预选温度下烧制以形成陶瓷耐腐蚀涂层,其包含选自氧化锆,铪及其组合的陶瓷金属氧化物。 陶瓷耐腐蚀涂层的厚度高达约127微米,并在大于约1000°F的温度下保持粘附。

    DIFFUSION COATING PROCESS
    4.
    发明申请
    DIFFUSION COATING PROCESS 有权
    扩散涂布工艺

    公开(公告)号:US20050095358A1

    公开(公告)日:2005-05-05

    申请号:US10605858

    申请日:2003-10-31

    IPC分类号: C23C10/30 B05D3/02

    CPC分类号: C23C10/30

    摘要: A process capable of depositing a diffusion coating of uniform thickness on localized surface regions of a component. The process makes use of an adhesive mixture containing a binding agent that is consumed as part of the deposition process so as not to negatively affect the quality and uniformity of the resulting coating. The process entails mixing a particulate donor material containing a coating element, a dissolved activator, and a particulate filler to form an adhesive mixture having a formable, malleable consistency. The adhesive mixture is applied to a surface of the component, and the component is heated to a temperature sufficient to vaporize and react the activator with the coating element of the donor material, thereby forming a reactive vapor of the coating element. The reactive vapor reacts at the surface of the component to form a diffusion coating containing the coating element.

    摘要翻译: 一种能够在组件的局部表面区域上沉积均匀厚度的扩散涂层的方法。 该方法使用含有作为沉积工艺的一部分消耗的粘合剂的粘合剂混合物,以便不会不利地影响所得涂层的质量和均匀性。 该方法需要混合含有涂层元素,溶解的活化剂和颗粒填料的颗粒供体材料,以形成具有可成形的可延展稠度的粘合剂混合物。 将粘合剂混合物施加到部件的表面上,并且将组分加热至足以蒸发并使活化剂与施主材料的涂层元件反应的温度,从而形成涂层元件的反应蒸气。 反应蒸汽在组分的表面处反应形成包含涂层元素的扩散涂层。

    CERAMIC CORROSION RESISTANT COATING FOR OXIDATION RESISTANCE
    6.
    发明申请
    CERAMIC CORROSION RESISTANT COATING FOR OXIDATION RESISTANCE 审中-公开
    陶瓷耐腐蚀涂层耐氧化

    公开(公告)号:US20090239061A1

    公开(公告)日:2009-09-24

    申请号:US11557693

    申请日:2006-11-08

    摘要: A coating system and a method for forming the coating system, the method including coating a surface of a gas turbine engine turbine component having a metallic surface that is outside the combustion gas stream and exposed to cooling air during operation of the engine. A gel-forming solution including a ceramic metal oxide precursor is provided. The gel-forming solution is heated to a first preselected temperature for a first preselected time to form a gel. The gel is then deposited on the metallic surface. Thereafter the gel is fired at a second preselected temperature above the first preselected temperature to form a ceramic corrosion resistant coating comprising a ceramic metal oxide is selected from the group consisting of zirconia, hafnia and combinations thereof. The ceramic corrosion resistant coating having a thickness of up to about 127 microns and remaining adherent at temperatures greater than about 1000° F.

    摘要翻译: 一种涂覆系统和一种形成涂层系统的方法,所述方法包括在发动机操作期间涂覆具有在燃烧气流外部的金属表面并暴露于冷却空气的燃气涡轮发动机涡轮机部件的表面。 提供了包含陶瓷金属氧化物前体的凝胶形成溶液。 将凝胶形成溶液加热至第一预选温度第一预选时间以形成凝胶。 然后将凝胶沉积在金属表面上。 此后,凝胶在高于第一预选温度的第二预选温度下烧制以形成陶瓷耐腐蚀涂层,其包含选自氧化锆,铪及其组合的陶瓷金属氧化物。 陶瓷耐腐蚀涂层的厚度高达约127微米,并在大于约1000°F的温度下保持粘附。

    Turbine component other than airfoil having ceramic corrosion resistant coating and methods for making same
    7.
    发明申请
    Turbine component other than airfoil having ceramic corrosion resistant coating and methods for making same 有权
    除了具有陶瓷耐腐蚀涂层的翼型以外的涡轮部件及其制造方法

    公开(公告)号:US20060222884A1

    公开(公告)日:2006-10-05

    申请号:US11094351

    申请日:2005-03-31

    IPC分类号: B32B19/00 B32B9/00

    摘要: An article comprising a turbine component other than an airfoil having a metal substrate and a ceramic corrosion resistant coating overlaying the metal substrate. This coating has a thickness up to about 5 mils (127 microns) and comprises a ceramic metal oxide selected from the group consisting of zirconia, hafnia and mixtures thereof. This coating can be formed by a method comprising the following steps: (a) providing a turbine component other than an airfoil comprising the metal substrate; (b) providing a gel-forming solution comprising a ceramic metal oxide precursor; (c) heating the gel-forming solution to a first preselected temperature for a first preselected time to form a gel; (d) depositing the gel on the metal substrate; and (e) firing the gel at a second preselected temperature above the first preselected temperature to form the ceramic corrosion resistant coating comprising the ceramic metal oxide. This coating can also be formed by alternative methods wherein a ceramic composition comprising the ceramic metal oxide is deposited by physical vapor deposition on the metal substrate to provide a strain-tolerant columnar structure, or is thermal sprayed on the metal substrate.

    摘要翻译: 一种制品,其包括除了具有金属基底的翼型以外的涡轮机部件和覆盖所述金属基底的陶瓷耐腐蚀涂层。 该涂层具有高达约5密耳(127微米)的厚度,并且包含选自氧化锆,铪和其混合物的陶瓷金属氧化物。 该涂层可以通过包括以下步骤的方法形成:(a)提供除了包括金属基底的翼型之外的涡轮机部件; (b)提供包含陶瓷金属氧化物前体的凝胶形成溶液; (c)将凝胶形成溶液加热至第一预选温度,以第一预选时间形成凝胶; (d)将凝胶沉积在金属基底上; 和(e)在高于第一预选温度的第二预选温度下烧制凝胶以形成包含陶瓷金属氧化物的陶瓷耐腐蚀涂层。 该涂层也可以通过替代方法形成,其中通过物理气相沉积将包含陶瓷金属氧化物的陶瓷组合物沉积在金属基底上以提供耐应变柱状结构,或者热喷涂在金属基底上。

    BETA-PHASE NICKEL ALUMINIDE OVERLAY COATINGS AND PROCESS THEREFOR
    8.
    发明申请
    BETA-PHASE NICKEL ALUMINIDE OVERLAY COATINGS AND PROCESS THEREFOR 有权
    BETA相镍合金镀层及其工艺

    公开(公告)号:US20060182892A9

    公开(公告)日:2006-08-17

    申请号:US10248056

    申请日:2002-12-13

    摘要: A beta-phase nickel aluminide (NiAl) overlay coating (24) and method for modifying the grain structure of the coating (24) to improve its oxidation resistance. The coating (24) is deposited by a method that produces a grain structure characterized by grain boundaries (44) exposed at the outer coating surface (36). The grain boundaries (44) may also contain precipitates (40) as a result of the alloyed chemistry of the coating (24). During or after deposition, the overlay coating (24) is caused to form new grain boundaries (34) that, though open to the outer surface (36) of the coating (24), are free of precipitates or contain fewer precipitates (40) than the as-deposited grain boundaries (44). New grain boundaries (34) are preferably produced by causing the overlay coating (24) to recrystallize during coating deposition or after deposition as a result of a surface treatment followed by heat treatment.

    摘要翻译: β相镍铝化合物(NiAl)覆盖层(24)以及用于改变涂层(24)的晶粒结构以提高其抗氧化性的方法。 通过产生以在外涂层表面(36)处暴露的晶界(44)为特征的晶粒结构的方法沉积涂层(24)。 由于涂层(24)的合金化学,晶界(44)也可含有沉淀物(40)。 在沉积期间或之后,使覆盖涂层(24)形成新的晶粒边界(34),其尽管向涂层(24)的外表面(36)开口,但没有沉淀物或含有较少的沉淀物(40) 比沉积的晶界(44)。 优选通过在涂布沉积期间或沉积后的覆盖涂层(24)进行再结晶,然后进行热处理后的表面处理,来制造新的晶界(34)。

    Method of selective region vapor phase aluminizing
    10.
    发明申请
    Method of selective region vapor phase aluminizing 有权
    选择性区域气相镀铝的方法

    公开(公告)号:US20050084706A1

    公开(公告)日:2005-04-21

    申请号:US10685637

    申请日:2003-10-15

    摘要: The present invention is process for forming diffusion aluminide coatings on an uncoated surface of a substrate, without interdiffusing a sufficient amount of aluminum into a coating layer to adversely affect the coating growth potential and mechanical properties of said coating layer. A metal substrate is provided comprising an external surface and an internal passage therein defined by an internal surface, at least a portion of the external surface of the substrate being coated with a coating layer selected from the group consisting of β-NiAl-base, MCrAlX, a line-of-sight diffusion aluminide, a non-line-of-sight diffusion aluminide, a pack diffusion aluminide, and a slurry diffusion aluminide on said substrate. The external surface of the substrate is cleaned. The metal substrate is subjected to a aluminum vapor phase deposition process performed using a fluorine-containing activator selected from the group consisting of AlF3, CrF3, NH4F, and combinations thereof, at a rate in the range of about 0.036 mols of fluorine per ft3/hr of transport gas to about 0.18 mols of fluorine per ft3/hr of transport gas, at a temperature in the range of about 1350° F. (730° C.) to about 1925° F. (1050° C.), using a transport gas selected from the group consisting of argon, nitrogen, hydrogen, and combinations thereof, the transport gas being provided at a flow rate in the range of about 20 ft3/hr to about 120 ft3/hr for a period of time in the range of about 2 hours to about 10 hours. The substrate is then cooled. The present invention is also a superalloy article coated with a diffusion aluminide layer using the diffusion aluminide coating process of the present invention.

    摘要翻译: 本发明是在基材的未涂覆表面上形成扩散铝化物涂层的方法,而不会将足够量的铝相互扩散到涂层中,从而不利地影响涂层生长电位和所述涂层的机械性能。 提供了一种金属基底,其包括由内表面限定的外表面和内部通道,所述基底的外表面的至少一部分被涂覆有选自β-NiAl基,MCrAlX ,视线扩散铝化物,非视线扩散铝化物,包层扩散铝化物和在所述衬底上的浆料扩散铝化物。 清洁基板的外表面。 对金属基板进行铝蒸气相沉积工艺,该方法使用选自AlF 3 N 3,CrF 3 N,NH 4的含氟活化剂 F和它们的组合,以约0.036摩尔氟/ ft 3 /小时的运输气体至约0.18摩尔氟/ ft 3的范围内的速率, 在约1350°F(730℃)至约1925°F(1050℃)的温度范围内使用选自以下的输送气体: 氩气,氮气,氢气及其组合,输送气体的流速为约20ft 3 / hr至约120ft 3 / hr 一段时间在约2小时至约10小时的范围内。 然后将衬底冷却。 本发明也是使用本发明的扩散铝化物涂覆方法涂覆有扩散铝化物层的超级合金制品。