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1. 发明授权

US06863925B1 Method for vapor phase aluminiding including a modifying element 失效
标题翻译：包括改性元素的气相铝化方法
公开(公告)号：US06863925B1
公开(公告)日：2005-03-08
申请号：US09670189
申请日：2000-09-26
申请人： Gary Eugene Wheat , Terri Kay Brown , Roger Dale Wustman , Joseph David Rigney
发明人： Gary Eugene Wheat , Terri Kay Brown , Roger Dale Wustman , Joseph David Rigney
IPC分类号： C23C10/02 , C23C10/06 , C23C16/08 , C23C28/00
CPC分类号： C23C10/02 , C23C10/14 , C23C16/08 , C23C28/021 , C23C28/028 , C23C28/321 , C23C28/325 , C23C28/345 , C23C28/3455 , Y02T50/67
摘要： An article is coasted by preparing a coating source having an aluminum halide, a fluoride or an iodide of a modifying element as a source of the modifying element, and a carrier gas. The modifying element is zirconium, hafnium, and yttrium, or combinations thereof. The coating source is contacted to the article, and the coating source and the article are heated to a coating temperature of at least about 1850° F. for a period of time sufficient to permit aluminum and the modifying element to coat onto the surface of the article. The preferred fluorides of modifying elements are zirconium tetrafluoride and hafnium tetrafluoride.
摘要翻译：通过制备具有改性元素的卤化铝，氟化物或碘化物作为改性元素的来源的涂料源和载气来制备物品。改性元素是锆，铪和钇，或其组合。将涂料源与制品接触，并将涂料源和制品加热至至少约1850°F的涂布温度一段足以允许铝和改性元素涂覆在表面上的时间文章。改性元素的优选氟化物是四氟化锆和四氟化铪。

2. 发明授权

US06434876B1 Method of applying a particle-embedded coating to a substrate 有权
标题翻译：将颗粒包埋的涂层施加到基底的方法
公开(公告)号：US06434876B1
公开(公告)日：2002-08-20
申请号：US09670187
申请日：2000-09-26
申请人： Gary Eugene Wheat , Terri Kay Brown , Roger Dale Wustman
发明人： Gary Eugene Wheat , Terri Kay Brown , Roger Dale Wustman
IPC分类号： B05D136
CPC分类号： C23C26/00 , C23C10/52 , Y02T50/67
摘要： A turbine blade is coated by first applying a particle-entrapped tip coating to the tip of the airfoil. An aluminum-containing coating is thereafter applied to the airfoil, including to the tip of the airfoil overlying the particle-entrapped tip coating. The aluminum-containing coating is applied by providing a source of aluminum contacting the airfoil that deposits aluminum onto the airfoil at a coating temperature, and heating the airfoil to the coating temperature so that the aluminum-containing coating is deposited onto the airfoil, and so that the aluminum-containing coating and the particle-entrapped tip coating are diffused into the turbine blade substrate. The step of applying the aluminum-containing coating occurs without substantial prior interdiffusing of the particle-entrapped tip coating with the tip of the airfoil as a separate step.
摘要翻译：通过首先将颗粒捕获的尖端涂层施加到翼型的尖端来涂覆涡轮叶片。然后将含铝涂层施加到翼型件，包括覆盖颗粒捕获的尖端涂层的翼型的末端。通过在涂覆温度下提供与铝箔接触而将铝沉积在翼型上的铝源，通过提供含铝涂层，并将翼型加热到涂层温度，使含铝涂层沉积在翼型上，等等含铝涂层和颗粒捕获的尖端涂层扩散到涡轮叶片基板中。作为单独的步骤，施加含铝涂层的步骤发生在与翼型件的尖端之间的颗粒捕获的尖端涂层没有实质的先前相互扩散的情况下。

3. 发明授权

US06339879B1 Method of sizing and forming a cooling hole in a gas turbine engine component 失效
标题翻译：在燃气轮机发动机部件中调整和形成冷却孔的方法
公开(公告)号：US06339879B1
公开(公告)日：2002-01-22
申请号：US09684987
申请日：2000-08-29
申请人： Gary Eugene Wheat , Terri Kay Brown , Thomas Phillip Schumacher
发明人： Gary Eugene Wheat , Terri Kay Brown , Thomas Phillip Schumacher
IPC分类号： B21D5378
CPC分类号： B21D53/78 , B23P2700/06 , C23C10/02 , Y10T29/49336 , Y10T29/49341 , Y10T29/49343
摘要： A method for accurately sizing and forming the cooling holes of an air-cooled gas turbine engine component on which a protective diffusion coating will be deposited. The method generally entails drilling a hole in a surface region of a substrate, and then measuring the thickness of any recast surface region surrounding the hole and created as a result of a portion of the surface region having melted and then resolidified. The thickness of the additive layer of the diffusion coating that will deposit on a corresponding recast surface region of the component is then predicted based on an inverse relationship determined to exist with the thickness of the recast surface region formed during drilling of the cooling hole. An appropriately-oversized hole can then be formed in the component so that, after depositing the diffusion coating on the component, the additive layer grows sufficiently within the hole to yield a cooling hole approximately having the required final diameter.
摘要翻译：一种用于精确地确定和形成将要沉积保护性扩散涂层的空气冷却燃气涡轮发动机部件的冷却孔的方法。该方法通常需要在基板的表面区域中钻孔，然后测量由孔的周围的任何重铸表面区域的厚度，并且由于表面区域的一部分已经熔化然后重新固化而产生。然后基于与冷却孔的钻孔期间形成的重铸表面区域的厚度确定的反比关系来预测将沉积在部件的相应重铸表面区域上的扩散涂层的添加层的厚度。然后可以在部件中形成适当大小的孔，使得在将扩散涂层沉积在部件上之后，添加剂层在孔内充分生长以产生大致具有所需最终直径的冷却孔。

4. 发明授权

US07056555B2 Method for coating an internal surface of an article with an aluminum-containing coating 失效
标题翻译：用含铝涂层涂覆制品的内表面的方法
公开(公告)号：US07056555B2
公开(公告)日：2006-06-06
申请号：US10318761
申请日：2002-12-13
申请人： Steven Earl Bauer , Gary Eugene Wheat , Matthew David Saylor , Jeffrey Allan Pfaendtner , Atul Natwerlal Shah
发明人： Steven Earl Bauer , Gary Eugene Wheat , Matthew David Saylor , Jeffrey Allan Pfaendtner , Atul Natwerlal Shah
IPC分类号： B05D7/22 , B05D3/02 , B05D3/12
CPC分类号： C23C10/28 , C23C10/18 , Y02T50/67
摘要： An article having an internal passage therein and an internal article surface is coated by providing a coating slurry that is a mixture of a deposition source including a source of aluminum, a halide activator, and a flowable carrier comprising a flowable compound selected from the group consisting of a flowable organic compound and a flowable inorganic compound. There is no oxide dispersant in the coating slurry. The coating slurry is introduced into the internal passage and dried to remove at least a portion of the carrier therefrom and leave a dried coating material. The article surface in gaseous communication with the dried coating material is heated to form an aluminum-containing coating bonded to the article surface. Any residual dried coating material is removed by blowing compressed air through the internal passage.
摘要翻译：通过提供作为包括铝源，卤化物活化剂和可流动载体的沉积源的混合物的涂料浆料涂覆其中具有内部通道的物品和内部物品表面，所述沉积源包括可流动化合物，所述可流动化合物选自的可流动有机化合物和可流动的无机化合物。涂层浆料中没有氧化物分散剂。将涂料浆料引入内部通道中并干燥以从其中除去至少一部分载体，并留下干燥的涂料。与干燥的涂料材料气相连的制品表面被加热以形成结合到制品表面的含铝涂层。通过内部通道吹入压缩空气来除去任何残留的干燥涂层材料。

5. 发明授权

US07918024B2 Methods and apparatus for manufacturing components 失效
标题翻译：组件制造方法和装置
公开(公告)号：US07918024B2
公开(公告)日：2011-04-05
申请号：US11336002
申请日：2006-01-20
申请人： Frank Delano Mooney, Jr. , Gary Eugene Wheat , Timothy Riggs , Kenneth Ray Hill, Jr. , Ronald Dale Edwards
发明人： Frank Delano Mooney, Jr. , Gary Eugene Wheat , Timothy Riggs , Kenneth Ray Hill, Jr. , Ronald Dale Edwards
IPC分类号： B21K25/00 , B23Q7/00 , B25B27/14 , B25B1/24
CPC分类号： B23Q3/18 , B23Q3/063 , Y10T29/4932 , Y10T29/49321 , Y10T29/49323 , Y10T29/49998 , Y10T29/53961
摘要： A method for manufacturing a turbine nozzle assembly using a fixture includes providing a first position of the fixture, positioning at least one datum of the turbine nozzle assembly adjacent at least one datum location point on the fixture when the fixture is in the first position, coupling the turbine nozzle assembly to the fixture when the fixture is in the first position, rotating the fixture from the first position into a second position that facilitates manufacturing the turbine nozzle assembly, and performing a manufacturing process on the turbine nozzle assembly when the fixture is in the second position.
摘要翻译：用于制造使用夹具的涡轮喷嘴组件的方法包括提供固定装置的第一位置，当固定装置处于第一位置时，将至少一个基准面定位在涡轮喷嘴组件的至少一个基准点位置上，当所述固定装置处于所述第一位置时，所述涡轮喷嘴组件到所述固定装置，将所述固定装置从所述第一位置旋转到便于制造所述涡轮喷嘴组件的第二位置，以及当所述固定装置处于所述装置时，在所述涡轮喷嘴组件上执行制造过程第二个位置。

6. 发明授权

US06367687B1 Method for preparing a plate rim for brazing 失效
标题翻译：制备钎焊板边缘的方法
公开(公告)号：US06367687B1
公开(公告)日：2002-04-09
申请号：US09836038
申请日：2001-04-17
申请人： Jim Dean Reeves , Gary Eugene Wheat , Nicholas Charles Palmer , Robert Eugene McCracken
发明人： Jim Dean Reeves , Gary Eugene Wheat , Nicholas Charles Palmer , Robert Eugene McCracken
IPC分类号： B23K3102
CPC分类号： F01D5/20 , B23K1/20 , B23K1/206 , B23K35/38 , B23K2101/001 , C21D3/00 , C23G5/00 , F05D2260/202 , Y02P10/212
摘要： A method is provided for treating cooperating, juxtaposed substantially uncoated alloy substrate surfaces in preparation for brazing, for example an inner wall of the radially outer open end of a turbine engine blading member with the rim of an end plate or tip cap. The method includes treating at least one of the cooperating surfaces with a reducing gas comprising halogen gas for a time and at a temperature, for example 1-6 hours at 1650-1950° F., sufficient to remove any surface debris, for example oxides, and to deplete the alloy substrate surface of the total of elements selected from Al and Ti to a level of less than about 1 weight %. Depletion is to a depth in the surface which avoids intergranular attack of the substrate alloy surface. For example, the depth is no greater than about 0.0015″. Then the cooperating surfaces are brazed together.
摘要翻译：提供了一种用于处理协同并置的基本上未涂覆的合金基底表面以准备钎焊的方法，例如涡轮发动机叶片构件的径向外开口端的内壁，其具有端板或端盖的边缘。该方法包括用包含卤素气体的还原气体处理至少一个配合表面一段时间，并在例如1650-1950°F的温度例如1-6小时，足以除去任何表面碎屑，例如氧化物并且将从Al和Ti中选出的总量的合金基材表面消耗至小于约1重量％的水平。消耗是表面的深度，避免了基体合金表面的晶间侵蚀。例如，深度不大于约0.0015“。然后将配合表面钎焊在一起。

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