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21. 发明公开

KR1020080012193A 복합 사이클 발전 장치에 대한 압축기 오염의 영향을추산하는 방법 및 시스템 无效
标题翻译：压缩机排放对组合循环电厂的影响的方法与系统
公开(公告)号：KR1020080012193A
公开(公告)日：2008-02-11
申请号：KR1020070076256
申请日：2007-07-30
申请人： 제너럴 일렉트릭 캄파니
发明人： 장얀다 , 페츠틀페테르 , 페텍요세프
IPC分类号： F02C7/057 , F02C7/05 , F02C7/00
CPC分类号： F04D27/02 , Y02E20/16
摘要： A method and a system for estimating compressor fouling impact to combined cycle power plants are provided to optimize an off-line compressor cleaning process of a gas turbine in the combined cycle power plants. A method for estimating compressor fouling impact to combined cycle power plants, includes a step of measuring the present performance of a combined cycle power block(100), a step of standardizing the present performance of the combined cycle power block to one or more reference condition, a step of measuring a reference performance of a gas turbine(105) of the combined cycle power block, a step of determining estimated performance of the combined cycle power block, a step of calculating impact to the performance of the combined cycle power block by the compressor fouling in the gas turbine, and a step of calculating recoverable impact to the fuel consumption of the combined cycle power block on the basis of the recoverable impact to the performance of the combined cycle power block.
摘要翻译：提供了一种用于估计对联合循环发电厂的压缩机污染冲击的方法和系统，以优化联合循环发电厂中的燃气轮机的离线压缩机清洁过程。一种用于估计对联合循环发电厂的压缩机污染影响的方法，包括测量组合循环功率块（100）的当前性能的步骤，将组合循环功率块的当前性能标准化为一个或多个参考条件测量组合循环功率块的燃气轮机（105）的参考性能的步骤，确定组合循环功率块的性能的步骤，计算对联合循环功率块的性能的影响的步骤燃气轮机中的压缩机结垢，以及基于对组合循环功率块的性能的可恢复影响来计算对组合循环功率块的燃料消耗的可恢复影响的步骤。

22. 发明公开

KR1020070040320A 터빈 엔진의 입구 캡을 수리하는 방법 无效
标题翻译：涡轮发动机入口修理方法
公开(公告)号：KR1020070040320A
公开(公告)日：2007-04-16
申请号：KR1020060098838
申请日：2006-10-11
申请人： 유나이티드 테크놀로지스 코포레이션
发明人： 홀랜드브라이언케네스
IPC分类号： F02C7/04 , F02C7/057 , F02C7/05 , F02C7/00
CPC分类号： B29C73/10 , F01D5/005 , F02C7/04 , F05D2230/80 , F05D2300/603 , Y02T50/672
摘要： 터빈 엔진의 손상된 입구 캡을 수리하는 방법은 제1 내 부식층에 내재하여 위치된 구조 섬유층의 손상된 부분을 제거하는 단계를 포함한다. 구조 교체층은 구조 섬유층의 제거된 부분을 대체하기 위해 입구 캡에 적용되고, 제2 내 부식층은 제2 내 부식층이 구조 섬유층 위쪽에 위치되도록 입구 캡에 적용된다.
터빈 엔진, 입구 캡, 제1 내 부식층, 구조 섬유층, 구조 교체층

23. 发明公开

KR1020070026003A 가스 터빈 공기 공급원을 위한 먼지 분리기 无效
标题翻译：用于气体涡轮空气供应的DIRT分离器
公开(公告)号：KR1020070026003A
公开(公告)日：2007-03-08
申请号：KR1020060074449
申请日：2006-08-08
申请人： 유나이티드 테크놀로지스 코포레이션
发明人： 실버맨리차드 , 백위쓰배리 , 오닐리사 , 피에트라즈키에비츠에드워드에프.
IPC分类号： F02C7/05 , F01D25/08 , F02C7/052
CPC分类号： F01D11/24 , F01D9/065 , F05D2260/607 , Y02T50/675
摘要： A dirt separator for a gas turbine air supply is provided to prevent a cooling channel from being clogged by dirt, by removing the large amount of dirt found in a radially outer air flow before air reaches a cooling chamber. A gas turbine engine(120) comprises a housing(140) covering a stationary vane(22) and a rotating rotor; a turbine section including the stationary vane and the rotating rotor, wherein at least one of the stationary vane and the rotating rotor is provided with a radially outer cooling air flow from the position adjacent to a radially outer position in the housing; and a dirt separator(130) arranged in a flow path(26) of the radially outer cooling air flow. The dirt separator operates to remove impurities from the radially outer cooling air flow, and air moving downstream of the dirt separator and at least one of the stationary vane and the rotating rotor carries less impurities.
摘要翻译：提供了一种用于燃气轮机空气供应的污垢分离器，以防止在空气到达冷却室之前，通过去除在径向外部气流中发现的大量污垢来防止冷却通道被灰尘堵塞。燃气涡轮发动机（120）包括覆盖静止叶片（22）和旋转转子的壳体（140）包括固定叶片和旋转转子的涡轮机部分，其中固定叶片和旋转转子中的至少一个设置有从邻近壳体中的径向外部位置的位置的径向外部冷却空气流; 以及布置在所述径向外部冷却空气流的流动路径（26）中的污垢分离器（130）。污垢分离器用于从径向外部冷却空气流中除去杂质，并且在污垢分离器的下游移动的空气和固定叶片和旋转转子中的至少一个承载较少的杂质。

24. 发明授权

KR102015513B1 복합발전설비의 부생가스 열량조절장치 有权
公开(公告)号：KR102015513B1
公开(公告)日：2019-08-28
申请号：KR1020170180041
申请日：2017-12-26
申请人： 주식회사 포스코
发明人： 백두현 , 박성환 , 성두만 , 최성근 , 오염근
IPC分类号： F02C7/14 , F01D25/12 , F01K23/10 , F02C7/05

25. 发明公开

KR1020170130236A 선박용 가스 터빈 흡기 계통을 위한 바이 패스 장치 및 방법 无效
标题翻译：用于船舶燃气轮机进气系统的旁路装置和方法
公开(公告)号：KR1020170130236A
公开(公告)日：2017-11-28
申请号：KR1020160061075
申请日：2016-05-18
申请人： (주)성신엔스텍
发明人： 권대훈 , 강경식 , 김영목
IPC分类号： F02C7/05 , F02C7/055 , F02C7/052 , F02C6/20 , B63H21/16
摘要： 본발명은선박용가스터빈을위한것으로서, 특히도입덕트, 프론트세퍼레이터, 필터유닛, 리어세퍼레이터그리고배출덕트사이에각각바이패스부를구비한후 문제가발생한부품만을바이패스하여가스터빈의손상을감소할수 있는선박용가스터빈흡기계통을위한바이패스장치및 방법이다.
摘要翻译：本发明是一种用于船用燃气轮机，具有与所述出口管旁路，可以减少对燃气轮机的损坏之间发生的旁通部后，特别是导入管，所述前隔板，过滤器单元，后分离器和只有各个部件是一个问题以及用于船舶的燃气轮机进气系统的旁路设备和方法。

26. 发明公开

KR1020130054727A 가스터빈의 연소공기와 냉각공기의 유입시스템 无效
标题翻译：气体涡轮机燃烧和冷却空气的流动系统
公开(公告)号：KR1020130054727A
公开(公告)日：2013-05-27
申请号：KR1020110120293
申请日：2011-11-17
申请人： 현대중공업 주식회사
发明人： 이상면
IPC分类号： F02C7/05 , F02C7/18 , F02C7/055
摘要： PURPOSE: An intake system of combustion air and cooling air of a gas turbine is provided to obtain an intake system for supplying combustion air and cooling air to various gas turbines. CONSTITUTION: An intake system of combustion air and cooling air of a gas turbine(13) comprises a combustion air pipe(12), a combustion air pipe(12), a cooling air pipe(20), a demister(10), and an extension pipe(16). The combustion air pipe supplies the combustion air to the gas turbine. The cooling air pipe and the combustion air pipe make the cooling air flow into the gas turbine. The dimester is formed on a combustion cooling air inlet pipe(11). The extension pipe is connected to a first stage of the cooling air pipe and lift upwardly by bending the pipe.
摘要翻译：目的：提供燃气轮机的燃烧空气和冷却空气的进气系统，以获得用于向各种燃气轮机供应燃烧空气和冷却空气的进气系统。构成：燃气轮机（13）的燃烧空气和冷却空气的进气系统包括燃烧空气管（12），燃烧空气管（12），冷却空气管（20），除雾器（10）和延伸管（16）。燃烧空气管将燃烧空气供给燃气轮机。冷却空气管和燃烧空气管使得冷却空气流入燃气轮机。二聚体形成在燃烧冷却空气入口管（11）上。延伸管连接到冷却空气管的第一级，并通过弯曲管向上提升。

27. 发明公开

KR1020120092513A 터빈 유입 에어 시스템 및 가스 터빈 엔진의 필터 내로의 에어의 흐름에서 소액적의 흡입을 제한하는 방법 无效
标题翻译：涡轮进气系统
公开(公告)号：KR1020120092513A
公开(公告)日：2012-08-21
申请号：KR1020120012951
申请日：2012-02-08
申请人： 비에이치에이 알테어, 엘엘씨
发明人： 자리에에티엔느르네
IPC分类号： F02C7/05 , F02C7/055
CPC分类号： F02C7/052 , F01D25/32 , F02C7/05
摘要： PURPOSE: An inflow air system of a turbine and a method for preventing small droplets from flowing into a filter are provided to improve the efficiency and lifespan of a filter by removing large droplets and reducing the small droplets. CONSTITUTION: An inflow air system(100) of a turbine comprises a small droplet coalescer(230), a moisture remover(220), and a filter(210). The moisture remover is placed around the small droplet coalescer. The filter is placed at lower parts of the small droplet coalescer and moisture remover. The small droplet coalescer comprises a plurality of telltales(250). The plurality of telltales comprises synthetic or glass filaments.
摘要翻译：目的：提供涡轮机的流入空气系统和防止小液滴流入过滤器的方法，以通过去除大液滴并减少小液滴来提高过滤器的效率和寿命。构成：涡轮机的流入空气系统（100）包括小液滴聚结器（230），除湿器（220）和过滤器（210）。除湿器放置在小液滴聚结器周围。过滤器放置在小液滴聚结器和除湿器的下部。小液滴聚结器包括多个指示物（250）。多个指示物包括合成纤维或玻璃丝。

28. 发明公开

KR1020110130624A 가스터빈의 에어 인테이크 필터 고정장치 有权
标题翻译：用于固定气体涡轮机空气过滤器的装置
公开(公告)号：KR1020110130624A
公开(公告)日：2011-12-06
申请号：KR1020100050039
申请日：2010-05-28
申请人： 주식회사 한성더스트킹
发明人： 최경채
IPC分类号： F02C7/05 , F02C7/055 , F02C7/20
摘要： PURPOSE: A fixing device for an air intake filter of a gas turbine is provided to secure smooth operation of a gas turbine even if a rubber packing of an air intake filter is damaged because the fragments are filtered through a basket type filter fixing bracket. CONSTITUTION: A fixing device for an air intake filter of a gas turbine comprises conical and cylindrical mesh nets(42,44) which are connected to each other and located inside an air intake filter(20), a fixing member(50) having a cylindrical structure composed of a vertical fixing part(52) and a horizontal fixing part(54), a fixing plate(32) with a male thread rod(33), and a compression support plate(35) which is tightened with the male thread rod and a nut(34) to press the front side of a cylindrical filter(24) of the air intake filter.
摘要翻译：目的：提供一种用于燃气轮机的进气过滤器的固定装置，用于确保燃气轮机的平稳运行，即使进气过滤器的橡胶垫片因为通过筐式过滤器固定支架过滤而被损坏。构成：用于燃气轮机的进气过滤器的固定装置包括彼此连接并位于进气过滤器（20）内部的锥形和圆柱形网状网（42,44），固定构件（50）具有由垂直固定部分（52）和水平固定部分（54）组成的圆柱形结构，具有外螺纹杆（33）的固定板（32）和压紧支承板（35）杆和螺母（34）以按压进气过滤器的圆柱形过滤器（24）的前侧。

29. 发明授权

KR100705866B1 가스 터빈 액체 연료로부터의 알칼리 금속 오염물의제거방법 및 이를 위한 장치 失效
标题翻译：从燃气涡轮机液体燃料中去除碱金属污染的方法和装置
公开(公告)号：KR100705866B1
公开(公告)日：2007-04-09
申请号：KR1020010080116
申请日：2001-12-17
申请人： 제너럴 일렉트릭 캄파니
发明人： 화이트헤드알란 , 파리크비노드쿠마 , 샤피로앤드류필립
IPC分类号： F02C7/05
CPC分类号： C10G31/09 , C10G33/06 , C10G53/02
摘要： 본 발명은 연료 공급원; 가스 터빈에 연료를 공급하는 수단(12, 14, 26); 상기 연료 공급원의 다운스트림이면서 가스 터빈의 업스트림에 설치되는, 액체 연료로부터 고형 미립자를 제거하기 위한 예비여과기(20); 및 상기 예비여과기의 다운스트림이면서 가스 터빈의 업스트림에 설치되는, 액체 연료로부터 알칼리 금속을 함유하는 물을 분리하기 위한 응집기(22)를 포함하는, 가스 터빈(18)의 연소기(16)에 공급되는 액체 연료로부터 알칼리 금속 오염물을 연속적으로 제거하기 위한 시스템에 관한 것이다.

30. 发明公开

KR1020050008195A 가스터빈의 오일 피드 파이프 내부 이물질 제거방법 无效
标题翻译：通过研磨设备消除尺寸从气体涡轮机油管中移除外部事项的方法
公开(公告)号：KR1020050008195A
公开(公告)日：2005-01-21
申请号：KR1020030048050
申请日：2003-07-14
申请人： 두산중공업 주식회사
发明人： 김대중
IPC分类号： F02C7/05
摘要： PURPOSE: A method for removing foreign matters from an oil feed pipe of a gas turbine is provided to improve the quality of the product, and to cut down manufacturing cost by preventing generation of foreign matters inside the oil feed pipe and eliminating scale completely. CONSTITUTION: To manufacture an oil feed pipe(20) formed in an inlet casing of a gas turbine, the oil feed pipe is manufactured through the casting process. Chrome sand(22) is charged in the oil feed pipe before the heat treatment of the processed oil feed pipe, and both sides of the oil feed pipe are sealed by using clay(24). The oil feed pipe is processed with the heat when combined with the inlet casing of the gas turbine. Chrome sand is removed from the oil feed pipe, and scale is removed from the oil feed pipe by using a grinding apparatus.
摘要翻译：目的：提供一种从燃气轮机的供油管中除去异物的方法，以提高产品的质量，并且通过防止在进料管内产生异物并完全消除水垢来降低制造成本。构成：为了制造形成在燃气轮机的入口壳体上的给油管（20），通过铸造工序制造给油管。在加工油供给管的热处理之前，将铬砂（22）装入供油管中，并且通过使用粘土（24）密封供油管的两侧。当与燃气轮机的入口壳结合时，供油管被加热。铬砂从进油管中取出，并通过使用研磨装置从供油管中除去氧化皮。

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