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1. 发明授权

US06884461B2 Turbine nozzle with heat rejection coats 失效
标题翻译：涡轮喷嘴采用排热外套
公开(公告)号：US06884461B2
公开(公告)日：2005-04-26
申请号：US10325000
申请日：2002-12-20
申请人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
发明人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
IPC分类号： C23C10/20 , C23C26/00 , C23C28/00 , F01D5/28 , B05D1/38 , B05D3/04 , B05D7/14
CPC分类号： C23C26/00 , C23C10/20 , C23C28/00 , F01D5/288 , F05D2230/90 , F05D2300/611 , Y02T50/67
摘要： A method for applying a coating system that is applied to a surface of a component, such as a turbine nozzle, for preventing or at least substantially preventing interdiffusion between the component surface and a protective thermal layer applied to the component surface when the thermal layer is exposed to elevated temperatures. The method includes applying a carrier layer containing aluminum to the component surface. Next, the layer is heated to a first predetermined temperature for a first predetermined period of time in the substantial absence of oxygen to bond the aluminum with the component surface, the heat dissolving the carrier portion of the aluminum layer. The remaining portion of the aluminum layer is then heated to a second predetermined temperature for a second predetermined period of time to form an oxidized aluminum layer. Finally, at least one protective thermal layer is applied over the oxidized aluminum layer.
摘要翻译：一种施加涂覆系统的方法，所述涂覆系统施加到诸如涡轮喷嘴的部件的表面，用于当热层为...时防止或至少基本上防止组件表面和施加到部件表面的保护热层之间的相互扩散暴露在高温下。该方法包括在组件表面上涂覆含有铝的载体层。接下来，在实质上不存在氧的情况下将层加热到第一预定温度第一预定时间段，以将铝与组分表面结合，使铝层的载体部分溶解。然后将铝层的剩余部分加热至第二预定温度持续第二预定时间段以形成氧化铝层。最后，在氧化铝层上施加至少一个保护热层。

2. 发明授权

US07094446B2 Method for applying a coating system including a heat rejection layer to a substrate surface of a component 有权
标题翻译：将包括排热层的涂层系统施加到部件的基板表面的方法
公开(公告)号：US07094446B2
公开(公告)日：2006-08-22
申请号：US10941448
申请日：2004-09-15
申请人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
发明人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
IPC分类号： B05D1/38 , B05D3/02 , B05D7/14
CPC分类号： B32B15/04
摘要： A method for applying a coating system that is applied to a surface of a component for preventing or at least substantially preventing interdiffusion between the component surface and a protective thermal layer applied to the component surface when the thermal layer is exposed to elevated temperatures. The method includes applying a carrier layer containing aluminum to the component surface. Next, the layer is heated to a first predetermined temperature for a first predetermined period of time in the substantial absence of oxygen to bond the aluminum with the component surface, the heat dissolving the carrier portion of the aluminum layer. The remaining portion of the aluminum layer is then heated to a second predetermined temperature for a second predetermined period of time to form an oxidized aluminum layer. Finally, at least one protective thermal layer is applied over the oxidized aluminum layer.
摘要翻译：一种施加涂覆系统的方法，其用于防止或至少基本上防止在热层暴露于高温下时组分表面和施加到部件表面的保护热层之间的相互扩散。该方法包括在组件表面上涂覆含有铝的载体层。接下来，在实质上不存在氧的情况下将层加热到第一预定温度第一预定时间段，以将铝与组分表面结合，使铝层的载体部分溶解。然后将铝层的剩余部分加热至第二预定温度持续第二预定时间段以形成氧化铝层。最后，在氧化铝层上施加至少一个保护热层。

3. 发明授权

US06884515B2 Afterburner seals with heat rejection coats 有权
标题翻译：后燃器密封带排热外套
公开(公告)号：US06884515B2
公开(公告)日：2005-04-26
申请号：US10324550
申请日：2002-12-20
申请人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
发明人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
IPC分类号： B05D3/02 , B32B9/00 , B32B15/04 , F03B3/12
CPC分类号： B32B15/04
摘要： A method for applying a coating system that is applied to a surface of a component for preventing or at least substantially preventing interdiffision between the component surface and a protective thermal layer applied to the component surface when the thermal layer is exposed to elevated temperatures. The method includes applying a carrier layer containing aluminum to the component surface. Next, the layer is heated to a first predetermined temperature for a first predetermined period of time in the substantial absence of oxygen to bond the aluminum with the component surface, the heat dissolving the carrier portion of the aluminum layer. The remaining portion of the aluminum layer is then heated to a second predetermined temperature for a second predetermined period of time to form an oxidized aluminum layer. Finally, at least one protective thermal layer is applied over the oxidized aluminum layer.
摘要翻译：一种施加涂层系统的方法，其用于防止或至少基本上防止当热层暴露于升高的温度时，组件表面和施加到部件表面的保护热层之间的相互偏移。该方法包括在组件表面上涂覆含有铝的载体层。接下来，在实质上不存在氧的情况下将层加热到第一预定温度第一预定时间段，以将铝与组分表面结合，使铝层的载体部分溶解。然后将铝层的剩余部分加热至第二预定温度持续第二预定时间段以形成氧化铝层。最后，在氧化铝层上施加至少一个保护热层。

4. 发明授权

US06884460B2 Combustion liner with heat rejection coats 失效
标题翻译：带排气外套的燃烧衬套
公开(公告)号：US06884460B2
公开(公告)日：2005-04-26
申请号：US10324704
申请日：2002-12-20
申请人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
发明人： John Frederick Ackerman , Paul Arszman , Andrew J. Skoog
IPC分类号： C23C4/18 , C23C10/60 , C23C26/00 , C23C28/00 , F01D5/28 , B05D1/38 , B05D3/04 , B05D7/14
CPC分类号： C23C28/00 , C23C4/18 , C23C10/60 , C23C26/00 , F01D5/288 , F05D2230/90 , F05D2300/611 , Y02T50/67
摘要： A method for applying a coating system that is applied to a surface of a component for preventing or at least substantially preventing interdiffusion between the component surface and a protective thermal layer applied to the component surface when the thermal layer is exposed to elevated temperatures. The method includes applying a carrier layer containing aluminum to the component surface. Next, the layer is heated to a first predetermined temperature for a first predetermined period of time in the substantial absence of oxygen to bond the aluminum with the component surface, the heat dissolving the carrier portion of the aluminum layer. The remaining portion of the aluminum layer is then heated to a second predetermined temperature for a second predetermined period of time to form an oxidized aluminum layer. Finally, at least one protective thermal layer is applied over the oxidized aluminum layer.
摘要翻译：一种施加涂覆系统的方法，其用于防止或至少基本上防止在热层暴露于高温下时组分表面和施加到部件表面的保护热层之间的相互扩散。该方法包括在组件表面上涂覆含有铝的载体层。接下来，在实质上不存在氧的情况下将层加热到第一预定温度第一预定时间段，以将铝与组分表面结合，使铝层的载体部分溶解。然后将铝层的剩余部分加热至第二预定温度持续第二预定时间段以形成氧化铝层。最后，在氧化铝层上施加至少一个保护热层。

5. 发明授权

US08039113B2 Environmental barrier coatings providing CMAS mitigation capability for ceramic substrate components 有权
标题翻译：环保屏障涂层为陶瓷衬底部件提供CMAS缓解能力
公开(公告)号：US08039113B2
公开(公告)日：2011-10-18
申请号：US12340138
申请日：2008-12-19
申请人： Glen Harold Kirby , Brett Allen Boutwell , John Frederick Ackerman
发明人： Glen Harold Kirby , Brett Allen Boutwell , John Frederick Ackerman
IPC分类号： B32B9/04
CPC分类号： C04B41/009 , C04B41/52 , C04B41/89 , C23C28/042 , Y10T428/12611 , Y10T428/31667 , C04B41/5096 , C04B41/5071 , C04B41/522 , C04B41/5031 , C04B41/5053 , C04B41/5024 , C04B41/5066 , C04B41/5046 , C04B41/5032 , C04B41/5027 , C04B41/524 , C04B41/5042 , C04B41/5044 , C04B35/10 , C04B35/00 , C04B35/14 , C04B35/18 , C04B35/185 , C04B35/565 , C04B35/584 , C04B35/806 , C04B35/803
摘要： Environmental barrier coating having CMAS mitigation capability for oxide components. In one embodiment, the barrier coating includes an outer layer selected from AeAl2O19, AeHfO3, AeZrO3, ZnAl2O4, MgAl2O4, Ln4Al2O9, Lna4Ga2O9, Ln3Al5O12, Ln3Ga5O12, and Ga2O3.
摘要翻译：环氧屏障涂层具有氧化物组分的CMAS缓解能力。在一个实施方案中，阻挡涂层包括选自AeAl2O19，AeHfO3，AeZrO3，ZnAl2O4，MgAl2O4，Ln4Al2O9，Lna4Ga2O9，Ln3Al5O12，Ln3Ga5O12和Ga2O3的外层。

6. 发明授权

US07208230B2 Optical reflector for reducing radiation heat transfer to hot engine parts 有权
标题翻译：用于减少辐射热量传递到热机部件的光学反射器
公开(公告)号：US07208230B2
公开(公告)日：2007-04-24
申请号：US10651420
申请日：2003-08-29
申请人： John Frederick Ackerman , Paul Vincent Arszman , Bangalore Aswatha Nagaraj , Nicole Justis
发明人： John Frederick Ackerman , Paul Vincent Arszman , Bangalore Aswatha Nagaraj , Nicole Justis
IPC分类号： B32B15/00 , B32B15/04
CPC分类号： F23M5/00 , C23C28/322 , C23C28/345 , C23C28/3455 , C23C30/00 , F01D5/288 , F05D2230/314 , F05D2230/90 , F05D2300/504 , F05D2300/611 , F23M2900/05004 , F23R3/007 , Y02T50/67 , Y02T50/672 , Y02T50/673 , Y10T428/12
摘要： A high temperature gas turbine component for use in the gas flow path that comprises a specular optical reflector coating system. A thin specular optical reflector coating system is applied to the gas flow path of the component, that is, the surface of the component that forms a boundary for hot combustion gases. The component typically includes a thermal barrier coating overlying the high temperature metallic component that permits the component to operate at elevated temperatures. The thermal barrier coating must be polished in order to provide a surface that can suitably reflect the radiation into the gas flow path. The thin reflector coating system comprises a thin high temperature and corrosion resistant refractory stabilizing layer, which is applied over a thin reflective metal layer, which is applied over a thin high temperature and corrosion resistant refractory sealing layer. The coating system is applied over the polished thermal barrier coating by a process that can adequately adhere the reflector to the polished surface without increasing the roughness of the surface. The coating system reflects radiation back into the hot gas flow path or into the atmosphere. The reflected radiation is not focused onto any other hardware component. The design of the component is such that the radiation is returned to the gas flow path or sent to the atmosphere rather than absorbed into a component that only serves to increase the temperature of such a component.
摘要翻译：一种用于气体流路的高温燃气轮机部件，包括镜面光反射涂层系统。将薄镜面光反射涂层系统应用于部件的气体流动路径，即构成热燃气体边界的部件的表面。该部件通常包括覆盖高温金属部件的热障涂层，其允许部件在升高的温度下操作。必须抛光热障涂层，以便提供可以适当地将辐射反射到气体流动路径中的表面。薄反射器涂层系统包括薄的耐高温和耐腐蚀的耐火稳定层，其被涂覆在薄的反射金属层上，其被涂覆在薄的耐高温和耐腐蚀的耐火密封层上。涂层系统通过可以将反射器充分地粘附到抛光表面而不增加表面粗糙度的方法施加在抛光的热障涂层上。涂层系统将辐射反射回热气流路径或大气中。反射的辐射没有集中在任何其他硬件组件上。部件的设计使得辐射返回到气体流动路径或送到大气中，而不是被吸收到仅用于增加这种部件的温度的部件中。

7. 发明授权

US5693368A Low temperature chemical vapor deposition method for cleaning substrate and depositing protective coating 失效
标题翻译：低温化学气相沉积方法，用于清洁基材和沉积保护涂层
公开(公告)号：US5693368A
公开(公告)日：1997-12-02
申请号：US715052
申请日：1996-09-17
申请人： John Frederick Ackerman , William Randolph Stowell , George Albert Coffinberry , John Herbert Wood , Adrian Maurice Beltran
发明人： John Frederick Ackerman , William Randolph Stowell , George Albert Coffinberry , John Herbert Wood , Adrian Maurice Beltran
IPC分类号： C23C10/08 , C23C16/02 , C23C16/20 , C23C16/12
CPC分类号： C23C16/0236 , C23C10/08 , C23C16/20
摘要： A method is disclosed to deposit aluminum coatings on high temperature superalloys for corrosion, oxidation, and erosion protection using low temperature chemical vapor deposition and an organometallic halide precursor, specifically an aluminum alkyl halide. The process is adapted to protective coatings for turbine parts having internal passages. Due to the lower temperatures used during chemical vapor deposition, a broad range of substrate materials can be utilized. The precursor vapors clean the substrate surfaces by removing native oxides while simultaneously depositing aluminum.
摘要翻译：公开了一种将低温化学气相沉积和有机金属卤化物前体，特别是烷基铝卤化物的铝涂层沉积在高温超级合金上用于腐蚀，氧化和侵蚀保护的方法。该方法适用于具有内部通道的涡轮部件的保护涂层。由于在化学气相沉积期间使用的较低温度，可以使用宽范围的基底材料。前体蒸汽通过去除天然氧化物同时沉积铝来清洁基材表面。

8. 发明授权

US08806849B2 System and method of operating a power generation system with an alternative working fluid 有权
标题翻译：用替代工作流体操作发电系统的系统和方法
公开(公告)号：US08806849B2
公开(公告)日：2014-08-19
申请号：US12182837
申请日：2008-07-30
申请人： John Frederick Ackerman , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
发明人： John Frederick Ackerman , Matthew Timothy Franer , Randy Lee Lewis , David Allen Bell , Morris Dee Argyle , Brian Francis Towler
IPC分类号： F02C3/34 , F02C6/00 , F02C6/18
CPC分类号： F02C3/34
摘要： A method of operating a turbine engine system and a turbine engine system are provided. The method comprises supplying a flow of oxygen to a combustion chamber defined within a plurality of turbines coupled serially together within the turbine engine system, supplying a flow of hydrocarbonaccous fuel to the combustion chambers of each of the plurality of turbines in the turbine engine system, and supplying a working fluid to an inlet of a first turbine engine coupled within the turbine engine system, wherein the working fluid is substantially nitrogen-free and wherein each of the turbines coupled within the turbine engine system is operable with the resulting fuel-oxygen-working fluid mixture.
摘要翻译：提供了一种操作涡轮发动机系统和涡轮发动机系统的方法。该方法包括向在涡轮发动机系统内串联连接的多个涡轮机内限定的燃烧室供应氧气流，向涡轮发动机系统中的多个涡轮机的每一个的燃烧室供应烃类燃料流，以及将工作流体供应到耦合在所述涡轮发动机系统内的第一涡轮发动机的入口，其中所述工作流体基本上是无氮的，并且其中联接在所述涡轮发动机系统内的所述涡轮机中的每一个可利用所得到的燃料 - 工作流体混合物。

9. 发明申请

US20100291302A1 ARTICLE PROTECTED BY A THERMAL BARRIER COATING HAVING A GROUP 2 OR 3/GROUP 5 STABILIZATION-COMPOSITION-ENRICHED SURFACE 审中-公开
标题翻译：具有2组或3组/ 5组稳定表面的热障涂层保护的物品
公开(公告)号：US20100291302A1
公开(公告)日：2010-11-18
申请号：US11684981
申请日：2007-03-12
申请人： John Frederick Ackerman , Venkat Subramanian Venkataramani , Irene T. Spitsberg , Brett Allen Rohrer Boutwell , Ramgopal Darolia
发明人： John Frederick Ackerman , Venkat Subramanian Venkataramani , Irene T. Spitsberg , Brett Allen Rohrer Boutwell , Ramgopal Darolia
IPC分类号： B05D3/10
CPC分类号： C23C28/3215 , C23C28/321 , C23C28/325 , C23C28/345 , C23C28/3455
摘要： A protected article is prepared by providing the article, depositing a bond coat onto an exposed surface of the article, and producing a thermal barrier coating on an exposed surface of the bond coat. The step of producing the thermal barrier coating includes the steps of depositing a primary ceramic coating onto an exposed surface of the bond coat, and depositing a stabilization composition onto an exposed surface of the primary ceramic coating. The stabilization composition includes a first element selected from Group 2 or Group 3 of the periodic table, and a second element selected from Group 5 of the periodic table. The atomic ratio of the amount of the first element to the amount of the second element is at least 1.3, more preferably at least 1:1.
摘要翻译：通过提供制品来制备受保护制品，将粘合涂层沉积在制品的暴露表面上，并在粘合涂层的暴露表面上产生热障涂层。生产热障涂层的步骤包括以下步骤：将初级陶瓷涂层沉积在粘合涂层的暴露表面上，并将稳定化组合物沉积到初级陶瓷涂层的暴露表面上。稳定化组合物包括选自元素周期表第2族或第3族的第一元素和选自元素周期表第5族的第二元素。第一元素的量与第二元素的量的原子比为至少1.3，更优选至少1:1。

10. 发明授权

US07360997B2 Vibration damper coating 有权
标题翻译：振动阻尼涂层
公开(公告)号：US07360997B2
公开(公告)日：2008-04-22
申请号：US11244938
申请日：2005-10-06
申请人： William Kent Wagner , John Frederick Ackerman , Kenneth Lee Johnson
发明人： William Kent Wagner , John Frederick Ackerman , Kenneth Lee Johnson
IPC分类号： F03B3/12 , F03B3/00
CPC分类号： F01D5/16 , F01D5/34 , F04D29/023 , F04D29/668 , F05D2230/90 , F05D2300/43 , F05D2300/501 , F05D2300/603 , F05D2300/615 , Y10S416/50
摘要： A coated fan rotor blade and method for coating a fan rotor blade. The coated fan rotor blade includes a fan rotor blade; and a coating disposed on said fan rotor blade. The coating comprises a binder; and a filler made up of a plurality of particles. The filler material is incorporated into the binder material, and the particles in the filler interact to produce vibrational damping. In particular, the coating includes small, dense, flattened particles or plates that are incorporated into a thin layer of visco-elastic material, such as rubber, silicone, fluoro-elastomer, or urethane and bonded to the surface of the rotor blade to provide damping of high frequency excitation.
摘要翻译：一种涂覆的风扇转子叶片和用于涂覆风扇转子叶片的方法。涂覆风扇转子叶片包括风扇转子叶片; 以及设置在所述风扇转子叶片上的涂层。涂层包括粘合剂; 以及由多个颗粒构成的填料。填充材料被结合到粘合剂材料中，并且填料中的颗粒相互作用以产生振动阻尼。特别地，涂层包括小的，致密的，扁平的颗粒或板，其结合到薄的粘弹性材料层中，例如橡胶，硅树脂，氟弹性体或氨基甲酸酯并且结合到转子叶片的表面，以提供阻尼高频励磁。

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