Method of forming a diffusion aluminide-hafnide coating
    1.
    发明授权
    Method of forming a diffusion aluminide-hafnide coating 失效
    形成扩散铝化物 - 海滨涂层的方法

    公开(公告)号:US06332931B1

    公开(公告)日:2001-12-25

    申请号:US09474550

    申请日:1999-12-29

    IPC分类号: C23C800

    CPC分类号: C23C10/14

    摘要: A process for forming a diffusion aluminide-hafnide coating on an article, such as a component for a gas turbine engine. The process is a vapor phase process that generally entails placing the article in a coating chamber containing a halide activator and at least one donor material. The donor material collectively consists essentially of at least 0.5 weight percent hafnium and at least 20 weight percent aluminum with the balance being chromium and/or cobalt.

    摘要翻译: 一种用于在诸如燃气涡轮发动机的部件的物品上形成扩散铝化物 - 海菲尔德涂层的方法。 该方法是气相方法,其通常需要将物品置于含有卤化物活化剂和至少一种供体材料的涂料室中。 供体材料基本上由至少0.5重量%的铪和至少20重量%的铝组成,余量为铬和/或钴。

    Diffusion aluminide bond coat for a thermal barrier coating system and method therefor
    2.
    发明授权
    Diffusion aluminide bond coat for a thermal barrier coating system and method therefor 失效
    用于热障涂层体系的扩散铝化物粘合涂层及其方法

    公开(公告)号:US06168874A

    公开(公告)日:2001-01-02

    申请号:US09016975

    申请日:1998-02-02

    IPC分类号: B32B900

    摘要: A thermal barrier coating system and a method for forming the coating system on a component designed for use in a hostile thermal environment, such as superalloy turbine, combustor and augmentor components of a gas turbine engine. The coating system includes a diffusion aluminide bond coat whose oxide growth rate is significantly reduced to improve the spallation resistance of a thermal barrier layer by forming the bond coat to include a dispersion of aluminum, chromium, nickel, cobalt and/or platinum group metal oxides. The oxides preferably constitute about 5 to about 20 volume percent of the bond coat. A preferred method of forming the bond coat is to initiate a diffusion aluminizing process in the absence of oxygen to deposit a base layer of diffusion aluminide, and then intermittently introduce an oxygen-containing gas into the diffusion aluminizing process to form within the bond coat the desired dispersion of oxides. Thereafter, a ceramic layer is deposited on the bond coat to form a thermal barrier coating.

    摘要翻译: 一种热障涂层系统和一种在设计用于恶劣热环境的部件上形成涂层系统的方法,例如燃气涡轮发动机的超级合金涡轮机,燃烧器和增压器部件。 涂层体系包括扩散铝化物粘合涂层,其氧化物生长速率显着降低,以通过形成粘合涂层来改善热障层的抗剥落性,包括铝,铬,镍,钴和/或铂族金属氧化物的分散体 。 氧化物优选构成约5至约20体积%的粘合涂层。 形成粘合涂层的优选方法是在不存在氧的情况下开始扩散镀铝工艺以沉积扩散铝化物的基底层,然后间歇地将含氧气体引入扩散镀铝工艺中以在粘合涂层内形成 所需的氧化物分散体。 此后,在接合涂层上沉积陶瓷层以形成热障涂层。

    Process for recycling vapor phase aluminiding donor alloy
    3.
    发明授权
    Process for recycling vapor phase aluminiding donor alloy 失效
    回收汽相铝化合物合金的方法

    公开(公告)号:US06306458B1

    公开(公告)日:2001-10-23

    申请号:US09474548

    申请日:1999-12-29

    IPC分类号: B32B3500

    CPC分类号: C23C8/06

    摘要: A process for reclaiming aluminum alloy donor from a vapor phase deposition process used to form a diffusion aluminide coating on a component, such as the high-temperature superalloy components of gas turbine engines. The process generally entails recycling a particulate aluminum alloy donor material that, as a result of having been used as the donor material for depositing a diffusion aluminide coating on an article by vapor phase deposition, particles of the donor material comprise an aluminum alloy core encased in an aluminum-depleted shell. The process generally entails tumbling the donor material in a manner that removes the aluminum-depleted shell, followed by sieving the donor material to remove shell fragments and undersized particles.

    摘要翻译: 用于从气相沉积工艺回收铝合金供体的方法,用于在诸如燃气涡轮发动机的高温超合金部件的组分上形成扩散铝化物涂层。 该方法通常需要循环使用颗粒状铝合金供体材料,该材料由于已被用作通过气相沉积在制品上沉积扩散铝化物涂层的供体材料的结果,供体材料的颗粒包含铝合金芯 一个铝耗尽的壳。 该方法通常需要以去除贫铝壳的方式翻转供体材料,然后筛选供体材料以除去壳碎片和尺寸过小的颗粒。

    Method of forming a diffusion aluminide coating
    6.
    发明授权
    Method of forming a diffusion aluminide coating 有权
    形成扩散铝化物涂层的方法

    公开(公告)号:US06440496B1

    公开(公告)日:2002-08-27

    申请号:US09487103

    申请日:2000-01-19

    IPC分类号: C23C1606

    摘要: A thermal barrier coating system and a method for forming the coating system on a component designed for use in a hostile thermal environment, such as superalloy turbine, combustor and augmentor components of a gas turbine engine. The coating system includes a diffusion aluminide bond coat whose oxide growth rate is significantly reduced to improve the spallation resistance of a thermal barrier layer by forming the bond coat to include a dispersion of aluminum, chromium, nickel, cobalt and/or platinum group metal oxides. The oxides preferably constitute about 5 to about 20 volume percent of the bond coat. A preferred method of forming the bond coat is to initiate a diffusion aluminizing process in the absence of oxygen to deposit a base layer of diffusion aluminide, and then intermittently introduce an oxygen-containing gas into the diffusion aluminizing process to form within the bond coat the desired dispersion of oxides. Thereafter, a ceramic layer is deposited on the bond coat to form a thermal barrier coating.

    摘要翻译: 一种热障涂层系统和一种在设计用于恶劣热环境的部件上形成涂层系统的方法,例如燃气涡轮发动机的超级合金涡轮机,燃烧器和增压器部件。 涂层体系包括扩散铝化物粘合涂层,其氧化物生长速率显着降低,以通过形成粘合涂层来改善热障层的抗剥落性,包括铝,铬,镍,钴和/或铂族金属氧化物的分散体 。 氧化物优选构成约5至约20体积%的粘合涂层。 形成粘合涂层的优选方法是在不存在氧的情况下开始扩散镀铝工艺以沉积扩散铝化物的基底层,然后间歇地将含氧气体引入扩散镀铝工艺以在粘合涂层内形成 所需的氧化物分散体。 此后,在接合涂层上沉积陶瓷层以形成热障涂层。

    Apparatus for masking turbine components during vapor phase diffusion coating
    7.
    发明授权
    Apparatus for masking turbine components during vapor phase diffusion coating 有权
    用于在气相扩散涂层期间遮蔽涡轮机部件的装置

    公开(公告)号:US06224673B1

    公开(公告)日:2001-05-01

    申请号:US09372106

    申请日:1999-08-11

    IPC分类号: C23C1600

    摘要: Apparatus and method to improve vapor phase diffusion coating of articles. The apparatus provides a barrier to segregate the portion of the article requiring coating from the portion of the article not requiring coating. The fixture is reusable, being unaffected by the coating gases. The fixture reduces the exposure of the coating gases with the portion of the article not requiring coating. By use of an optional seal, the portion of the article not requiring coating can be isolated from the coating gases.

    摘要翻译: 改善制品气相扩散涂层的装置和方法。 该装置提供了隔离物,从而使需要涂层的制品的部分从不需要涂覆的部分分离。 夹具可重复使用,不受涂层气体的影响。 固定装置可减少涂层气体与不需要涂层的物品部分的接触。 通过使用可选的密封件,不需要涂覆的制品的部分可以与涂覆气体隔离。

    Method of controlling thickness and aluminum content of a diffusion aluminide coating
    8.
    发明授权
    Method of controlling thickness and aluminum content of a diffusion aluminide coating 失效
    控制扩散铝化物涂层的厚度和铝含量的方法

    公开(公告)号:US06334907B1

    公开(公告)日:2002-01-01

    申请号:US09417468

    申请日:1999-10-13

    IPC分类号: C23C800

    CPC分类号: C23C16/12 C23C10/08

    摘要: A process for forming a diffusion aluminide coating on a substrate, such as a component for a gas turbine engine. The process generally entails placing the substrate in a suitable coating chamber, flowing an inert or reducing gas into and through the coating chamber, and then aluminizing the substrate using an aluminizing technique with a substantially constant aluminum activity, such as a vapor phase deposition process. During the aluminizing process, the amount of unreacted aluminum within the coating chamber is controlled by altering the flow rate of the gas through the coating chamber so that a portion of the unreacted aluminum is swept from the coating chamber by the gas. The amount of unreacted aluminum swept from the coating chamber is regulated by metering the gas flow rate in order to control the aluminizing rate and aluminum content of the resulting aluminide coating.

    摘要翻译: 在基底上形成扩散铝化物涂层的方法,例如用于燃气涡轮发动机的部件。 该方法通常需要将基底放置在合适的涂布室中,使惰性或还原性气体流入涂层室并通过涂层室,然后使用具有基本上恒定的铝活性的镀铝技术(例如气相沉积工艺)使基底镀铝。 在镀铝过程中,通过改变通过涂覆室的气体的流速来控制涂覆室内的未反应铝的量,使得一部分未反应的铝被气体从涂覆室扫过。 通过计量气体流速来调节从涂覆室扫过的未反应铝的量,以便控制所得铝化物涂层的镀铝速率和铝含量。

    Vapor phase diffusion aluminide process
    9.
    发明授权
    Vapor phase diffusion aluminide process 有权
    气相扩散铝化物工艺

    公开(公告)号:US06326057B1

    公开(公告)日:2001-12-04

    申请号:US09474549

    申请日:1999-12-29

    IPC分类号: C23C1600

    摘要: A process for forming a diffusion aluminide coating on an article, such as a component for a gas turbine engine. The process is a vapor phase process that generally entails placing the article in a coating chamber containing an aluminum donor material, without any halide carrier or inert filler present. The aluminum donor material consists essentially of about 20 to about 70 weight percent aluminum, with the balance being chromium or cobalt. While the article is held out of contact with the donor material, coating is initiated in an inert or reducing atmosphere by heating the article and the donor material to vaporize the aluminum constituent of the donor material, which then condenses on the surface of the article and diffuses into the surface to form a diffusion aluminide coating on the article.

    摘要翻译: 用于在诸如燃气涡轮发动机的部件的物品上形成扩散铝化物涂层的方法。 该方法是气相法,其通常需要将物品置于包含铝供体材料的涂层室中,而不存在任何卤化物载体或惰性填料。 铝供体材料基本上由约20至约70重量%的铝组成,余量为铬或钴。 虽然制品与供体材料不接触,但是通过加热制品和供体材料来在惰性或还原性气氛中引发涂层,以蒸发供体材料的铝组分,然后将其冷凝在制品的表面上, 扩散到表面以在制品上形成扩散的铝化物涂层。

    Method for fabricating a hollow component for a rocket engine
    10.
    发明授权
    Method for fabricating a hollow component for a rocket engine 失效
    制造火箭发动机中空部件的方法

    公开(公告)号:US5075966A

    公开(公告)日:1991-12-31

    申请号:US577241

    申请日:1990-09-04

    摘要: A method for making an engine component with a hollow interior includes the steps of: selectively patterning a principal substrate surface; forming a slurry including a selected amount of a binder material, a selected amount of a solvent and a selected amount of a filter material; inserting the slurry into the substrate surface pattern; evaporating the solvent to solidify the slurry; depositing a close-out layer of material over the patterned substrate surface and over the solidifed slurry; and without removing the close-out layer, removing the solidified slurry to provide a structure with a hollow interior.

    摘要翻译: 用于制造具有中空内部的发动机部件的方法包括以下步骤:选择性地图案化主基板表面; 形成包含选定量的粘合剂材料,选定量的溶剂和选定量的过滤材料的浆料; 将浆料插入基材表面图案中; 蒸发溶剂以固化浆料; 在图案化的衬底表面上和固化的浆料上沉积封闭层材料; 并且不去除封闭层,除去固化的浆料以提供具有中空内部的结构。