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31. 发明公开

KR1020100024927A 연료 펌프 无效
标题翻译：燃油泵
公开(公告)号：KR1020100024927A
公开(公告)日：2010-03-08
申请号：KR1020097025190
申请日：2008-05-15
申请人： 콘티넨탈 오토모티브 게엠베하
发明人： 피셔,마티아스 , 슈미트,크리스토프
IPC分类号： F02M37/04
CPC分类号： F02M37/048 , F02M37/08 , F04D5/002 , F04D29/026 , F04D29/046 , F04D29/2227 , F05D2300/12 , F05D2300/43 , F05D2300/611 , F05D2300/70
摘要： A fuel pump for delivering fuel has a housing part (8) made from a coated material. An insert (10) made from an electrically non-conductive material, such as for example phenolic resin, is pressed into the housing part (8). The insert (10) which is produced from phenolic resin can be pressed into the housing part (8) before a surface treatment of the housing part (8), since phenolic resin is not electrically conductive. As a result, the fuel pump can be produced particularly inexpensively.
摘要翻译：用于输送燃料的燃料泵具有由涂覆材料制成的壳体部分（8）。由不导电材料（例如酚醛树脂）制成的插入件（10）被压入壳体部分（8）中。由于酚醛树脂不导电，所以由酚醛树脂制成的插入件（10）可以在壳体部件（8）的表面处理之前压入壳体部分（8）。结果，可以特别廉价地生产燃料泵。

32. 发明公开

KR1020090057120A 작동 환경에서의 사용을 위해 계장화된 부품 有权
标题翻译：用于操作环境的仪表组件
公开(公告)号：KR1020090057120A
公开(公告)日：2009-06-03
申请号：KR1020097007678
申请日：2007-07-24
申请人： 지멘스 에너지, 인코포레이티드
发明人： 밋첼,데이비드,제이. , 쿨카르니,안앤드,에이. , 서브라마니안,라메쉬 , 로쉬,에드워드,알.
IPC分类号： F01D17/02 , G08C17/02 , F01D5/12 , C04B35/00
CPC分类号： C23C28/321 , B33Y70/00 , C23C28/3215 , C23C28/34 , C23C28/341 , C23C28/345 , C23C28/3455 , F01D5/288 , F01D17/02 , F01D21/003 , F01D21/10 , F05D2230/90 , F05D2300/611 , F23R3/007 , G01D3/08 , H04Q9/00 , H04Q2209/40 , H04Q2209/50 , Y02T50/673
摘要： An instrumented component (18, 19) for use in various operating environments such as the hot gas path section of a combustion turbine engine (10). The component (18, 19) may have a substrate, a sensor (50, 204, 210) connected with the substrate for sensing a condition of the component (18, 19) within the casing during operation of the combustion turbine (10) and a connector (52, 202) attached to the substrate and in communication with the sensor (50, 204, 210) for routing a data signal from the sensor (50, 204, 210) to a termination location (53). The component (18, 19) may include a wireless telemetry device (54, 202) in communication with the connector (52, 202) for wirelessly transmitting the data signal outside the casing. A transceiver (56) may be located outside the casing for receiving the data signal and transmitting it to a processing module (30) for developing information with respect to a condition of the component (18, 19) or a coating (26) deposited on the component (18, 19).
摘要翻译：一种用于各种操作环境（例如燃气涡轮发动机（10）的热气路径部分））的仪表部件（18,19）。组件（18,19）可以具有衬底，与衬底连接的传感器（50,204,210），用于在燃气轮机（10）的操作期间感测壳体内的部件（18,19）的状态，以及连接器（52,202），其连接到所述基板并与所述传感器（50,204,210）通信，用于将数据信号从所述传感器（50,204,210）路由到终止位置（53）。组件（18,19）可以包括与连接器（52,202）通信的无线遥测设备（54,202），用于在壳体外部无线地传输数据信号。收发器（56）可以位于外壳外部，用于接收数据信号并将其发送到处理模块（30），用于相对于组件（18,19）或沉积在其上的涂层（26）的状态显影信息组件（18,19）。

33. 发明公开

KR1020090057076A 터보 차저 无效
标题翻译：涡轮增压器
公开(公告)号：KR1020090057076A
公开(公告)日：2009-06-03
申请号：KR1020097006450
申请日：2007-10-01
申请人： 도후지 덴키 가부시키가이샤 , 미츠비시 쥬고교 가부시키가이샤
发明人： 하시모토시게오 , 하마구치노보루 , 진나이야스아키
IPC分类号： F02B37/22 , F02B39/00 , F01D17/16 , F01D25/24
CPC分类号： F01D17/165 , F01D25/005 , F02B37/24 , F02C6/12 , F05D2220/40 , F05D2230/313 , F05D2230/90 , F05D2300/121 , F05D2300/132 , F05D2300/171 , F05D2300/611
摘要： A turbocharger with a long service life, capable of inexpensively and accurately performing nozzle vane angle synchronous control by using inexpensive and highly wear resistant components in a link mechanism for driving the nozzle vane rotation mechanism of a variable nozzle mechanism. Pins are fixedly arranged in a ring plate rotatably supported on the turbocharger, and the pins set the angle of the nozzle vanes for controlling the amount of exhaust gas for rotating the turbine rotor. A hard coating having a thickness of approximately 2 mum and formed by physical vapor deposition of Al, Cr, Si, and N on an austenitic stainless steel as the base metal is formed on the pins.
摘要翻译：一种使用寿命长的涡轮增压器，其能够通过在用于驱动可变喷嘴机构的喷嘴叶片旋转机构的连杆机构中使用廉价且高度耐磨的部件来廉价和精确地执行喷嘴叶片角同步控制。引脚固定地布置在可旋转地支撑在涡轮增压器上的环板中，并且销设置喷嘴叶片的角度以控制用于旋转涡轮机转子的排气量。在作为母材的奥氏体不锈钢上形成厚度约2μm，通过物理气相沉积Al，Cr，Si和N形成的硬涂层。

34. 发明授权

KR100894519B1 물체의 코팅 방법 有权
标题翻译：涂装物件的方法
公开(公告)号：KR100894519B1
公开(公告)日：2009-04-22
申请号：KR1020047009116
申请日：2002-12-17
申请人： 라이볼트 게엠베하
发明人： 헤펙카우젠,요세프 , 슐테,프랭크
IPC分类号： C04B41/83 , B05D7/24 , B05D1/16
CPC分类号： C23C28/322 , C23C28/00 , C25D11/18 , F04D19/04 , F04D29/023 , F05D2300/21 , F05D2300/43 , F05D2300/512 , F05D2300/611
摘要： 본 발명은 밸브 금속 또는 그들의 합금으로 이루어지고, 상기 금속으로 구성된 얇은 배리어층과, 그 위에 마련된, 표면이 플루오로폴리머로 코팅되어 있는 산화물 세라믹층을 갖는 물체의 상기 코팅의 방법으로서, 상기 플루오로폴리머를 용액 상태로 진공 함침에 의해 상기 산화물 세라믹층의 캐필러리 시스템에 도입하고, 상기 용액의 비습윤 부분을 제거하고 건조하는 것을 특징으로 한다.
밸브 금속, 플루오로폴리머

35. 发明公开

KR1020070114241A 퇴적물의 제거 방법 有权
标题翻译：去除沉积物的方法
公开(公告)号：KR1020070114241A
公开(公告)日：2007-11-30
申请号：KR1020070049713
申请日：2007-05-22
申请人： 롤스-로이스 피엘씨
发明人： 개리이안머레이 , 로이드제임스리차드아이유안 , 버틀러토마스
IPC分类号： F01D5/00 , B23P6/00 , C23C4/18 , F02C7/00
CPC分类号： F01D25/002 , B08B3/024 , B08B3/04 , B08B5/02 , B23P6/002 , B23P2700/06 , B24C3/327 , B24C7/0007 , F05D2230/90 , F05D2260/202 , F05D2260/607 , F05D2300/611
摘要： A method of removing deposits is provided to eliminate the necessity of accurately jetting liquid toward a specific hole by using a component as a mask for injecting the liquid jet through a cooling hole. A method of removing deposits(30) from a passage(16) extended through a component(44) includes a step of immersing the passage into a liquid(101), and a step of injecting a liquid jet at the speed sufficient for moving at least a portion of the deposits toward the passage from a source(32) in a liquid bath. The deposit is formed sequentially with a coating(28) provided on a first surface of the component.
摘要翻译：提供了一种去除沉积物的方法，以消除通过使用组分作为用于通过冷却孔注射液体射流的掩模来将液体精确地喷射到特定孔的必要性。从延伸穿过部件（44）的通道（16）去除沉积物（30）的方法包括将通道浸入液体（101）中的步骤，以及以足以在至少一部分沉积物朝向从液体槽中的源（32）通过的沉积物。沉积物依次形成在组件的第一表面上设置的涂层（28）。

36. 发明公开

KR1020070098751A 기계 구성 요소 및 가공 방법 无效
标题翻译：机器组件和制作方法
公开(公告)号：KR1020070098751A
公开(公告)日：2007-10-05
申请号：KR1020070032370
申请日：2007-04-02
申请人： 제너럴 일렉트릭 캄파니
发明人： 펭간지앙 , 다마치오폴에스 , 샤에퍼존씨
IPC分类号： C23C28/00 , C23C4/10
CPC分类号： F01D5/288 , C23C4/073 , C23C4/11 , C23C4/129 , C23C4/18 , C23C30/00 , F05D2230/311 , F05D2300/611 , Y10T428/12493 , Y10T428/12611 , Y10T428/12944 , Y10T428/31678
摘要： A machine component and a fabricating method thereof are provided to increase wear resistance and reliability and to decrease an operation-stopped time period of a turbine system and maintenance cost. A machine component includes a TBC(Thermal Blocking Coating) system(110). The TBC system comprises at least one TBC layer(112) and at least one top coating layer(120). The TBC layer is formed on a substrate surface area(108) and formed with at least one TBC material of nickel-chromium-aluminum-yttrium formation including silicon, hafnium, and 10 weight% of cobalt or less. The top coating layer is formed on the TBC layer. The TBC layer includes 5.0~30.00 weight% of chromium, 5.00~20.00 weight% of aluminum, 0.01~5.00 weight% of yttrium, 0.5~4.00 weight% of silicon, 0.20~2.00 weight% of hafnium, 0.00~5.00 weight% of cobalt, and nickel.
摘要翻译：提供了一种机器部件及其制造方法，以增加耐磨性和可靠性，并减少涡轮机系统的运转停止时间和维护成本。机器组件包括TBC（热封层）系统（110）。 TBC系统包括至少一个TBC层（112）和至少一个顶部涂层（120）。 TBC层形成在衬底表面区域（108）上并形成有至少一种包含硅，铪和10重量％钴或更少的镍 - 铬 - 铝 - 钇形成的TBC材料。顶层涂层形成在TBC层上。 TBC层含有5.0〜30.00重量％的铬，5.00〜20.00重量％的铝，0.01〜5.00重量％的钇，0.5〜4.00重量％的硅，0.20〜2.00重量％的铪，0.00〜5.00重量％钴和镍。

37. 发明公开

KR1020070078685A 기막 냉각 방법 및 구멍 제조 无效
标题翻译：薄膜冷却方法和孔制造
公开(公告)号：KR1020070078685A
公开(公告)日：2007-08-01
申请号：KR1020060064901
申请日：2006-07-11
申请人： 유나이티드 테크놀로지스 코포레이션
发明人： 루작블레케제이. , 코치에릭엘.
IPC分类号： F01D5/18 , F01D5/14 , B22D7/00
CPC分类号： F01D5/186 , B22C9/103 , F02C7/185 , F05D2230/12 , F05D2230/13 , F05D2230/21 , F05D2230/211 , F05D2230/90 , F05D2240/121 , F05D2240/303 , F05D2260/204 , F05D2300/611 , Y02T50/676
摘要： A film cooling method and a hole manufacturing method are provided to improve the film cooling efficiency by limiting a heating of a second airflow when the second airflow passes between an inlet and an outlet. A method for manufacturing cooled parts includes the steps of: forming a plurality of feeding passages(54); forming a plenum(55) communicating with at least one of the feeding passages and having a plurality of posts; forming outlet passages(57) through the posts(66) and communicating with at least one of the feeding passages; and casting a core assembly, and breaking and removing the core assembly such that the feeding passages are left at a first portion of the core assembly and at least a portion of the plenum surrounding the posts are left at a second portion of the core assembly.
摘要翻译：提供薄膜冷却方法和孔制造方法，以通过在第二气流在入口和出口之间通过时限制第二气流的加热来提高薄膜冷却效率。制造冷却部件的方法包括以下步骤：形成多个供给通道（54）; 形成与所述供给通道中的至少一个连通并具有多个柱的增压室（55）通过所述柱（66）形成出口通道（57）并与至少一个所述进给通道连通; 并且铸造芯组件，以及断开和移除所述芯组件，使得所述馈送通道留在所述芯组件的第一部分处，并且围绕所述柱的所述增压室的至少一部分留在所述芯组件的第二部分。

38. 发明公开

KR1020070077056A ＣＭＡＳ 저항성 열차폐 피막 无效
标题翻译： CMAS耐热热障涂层
公开(公告)号：KR1020070077056A
公开(公告)日：2007-07-25
申请号：KR1020060132326
申请日：2006-12-22
申请人： 유나이티드 테크놀로지스 코포레이션
发明人： 프레링머빈 , 슈리히팅캐빈더블유. , 맬러니마이클제이. , 리톤데이비드에이. , 스메길존지. , 스노우데이비드비.
IPC分类号： C23C4/10
CPC分类号： C04B35/50 , C04B2235/3224 , C23C26/00 , C23C28/042 , C23C28/048 , C23C28/321 , C23C28/3215 , C23C28/345 , C23C28/3455 , C23C28/36 , C23C28/42 , F01D5/288 , F05D2230/90 , F05D2300/15 , F05D2300/211 , F05D2300/2285 , F05D2300/611 , Y02T50/67
摘要： A thermal barrier coating which can be applied to a turbine engine component, and in which a yttria-stabilized zirconia layer and a molten silicate resistant layer are alternately deposited, a method for forming the thermal barrier coating, and a turbine engine component having the thermal barrier coating are provided. A thermal barrier coating system(18) comprises: a first yttria-stabilized zirconia layer(10); a first molten silicate resistant material layer(20) deposited onto the first yttria-stabilized zirconia layer; a second yttria-stabilized zirconia layer(22) deposited onto the first molten silicate resistant material layer; and a second molten silicate resistant material layer(24) deposited onto the second yttria-stabilized material layer. The thermal barrier coating system further comprises at least one additional yttria-stabilized zirconia layer and at least one additional molten silicate resistant material layer. The molten silicate resistant material comprises at least one oxide of a material selected from the group consisting of lanthanum, cerium, praseodymium, neodymium, promethium, samarium, europium, gadolinium, terbium, dysprosium, holmium, erbium, thulium, ytterbium, lutetium, scandium, indium, zirconium, hafnium, and titanium. The molten silicate resistant material comprises a gadolinia-stabilized zirconia. The gadolinia-stabilized zirconia consists of 25 to 99.9 wt.% of gadolinia and the balance of zirconia.
摘要翻译：可应用于涡轮发动机部件并且其中交替沉积氧化钇稳定的氧化锆层和熔融硅酸盐抗蚀层的热障涂层，形成该热障涂层的方法和具有该热障涂层的涡轮发动机部件提供阻隔涂层。热障涂层系统（18）包括：第一氧化钇稳定的氧化锆层（10）; 沉积在第一氧化钇稳定的氧化锆层上的第一熔融硅酸盐材料层（20）沉积在第一熔融硅酸盐材料层上的第二氧化钇稳定的氧化锆层（22）; 和沉积到第二氧化钇稳定的材料层上的第二熔融硅酸盐抵抗材料层（24）。热障涂层系统还包括至少一个额外的氧化钇稳定的氧化锆层和至少一个附加的耐熔融硅酸盐材料层。所述耐熔融硅酸盐材料包括选自镧，铈，镨，钕，ium，钐，铕，钆，铽，镝，镝，钬，铒，ium，镱，镥，钪，钪中的至少一种材料，铟，锆，铪和钛。熔融硅酸盐材料包括氧化钆稳定的氧化锆。氧化钆稳定的氧化锆由25至99.9重量％的氧化钆和余量的氧化锆组成。

39. 发明公开

KR1020060056229A 보호성 코팅 无效
标题翻译：保护涂料
公开(公告)号：KR1020060056229A
公开(公告)日：2006-05-24
申请号：KR1020050087455
申请日：2005-09-20
申请人： 유나이티드 테크놀로지스 코포레이션
发明人： 이튼해리이. , 브하티아타니아 , 선엘렌와이. , 로튼토마스에이치.
IPC分类号： C23C14/22
CPC分类号： C04B41/009 , C04B41/5024 , C04B41/85 , C04B2111/00405 , C23C4/11 , C23C4/18 , C23C30/00 , F01D5/288 , F05D2230/90 , F05D2300/611 , C04B41/4527 , C04B35/565 , C04B35/584 , C04B35/806 , C04B35/597
摘要： 본 명세서에서 보호성 코팅이 설명된다. 이러한 코팅들의 실시예들은 대체로 내부에 특정 평형 상만을 포함하며, 코팅이 증착된 기판의 CTE와 대체로 동일한 CTE를 갖는다. 소정의 코팅은 코팅 내의 소정 상 또는 미세구조를 생성하기 위한 코팅 도포의 제어 및/또는 코팅된 기판의 열처리에 의해 얻어질 수 있다.
보호성 코팅, 평형 상, 기판, 열처리, 코팅된 기판

40. 发明公开

KR1020060039922A 코팅 有权
标题翻译：涂层
公开(公告)号：KR1020060039922A
公开(公告)日：2006-05-09
申请号：KR1020067001418
申请日：2004-07-12
申请人： 에드워즈 리미티드
发明人： 오코로어포임마뉴엘우조마
IPC分类号： C25D11/02 , F04D7/00
CPC分类号： F04D19/046 , F04D19/044 , F04D29/023 , F05D2230/31 , F05D2230/90 , F05D2260/95 , F05D2300/10 , F05D2300/21 , F05D2300/611 , Y10T428/12611 , Y10T428/30
摘要： A method of forming a coating on a plastics component (14) of a vacuum pump comprises the steps of applying a metallic layer (20) to the component and forming the coating (30, 32, 34) from the metallic layer by subjecting the metallic layer to electrolytic plasma oxidation.
摘要翻译：在真空泵的塑料部件（14）上形成涂层的方法包括以下步骤：将金属层（20）施加到部件上，并通过使金属层（20,32）从金属层形成涂层（30,32,34）层到电解质等离子体氧化。

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