Abstract:
PURPOSE: A method for forming a thermal barrier coating on hot-gas-path components of a gas turbine is provided to do a thermal barrier coating without stopping the gas turbine. CONSTITUTION: A method of the thermal barrier coating layer during the operation of the gas turbine comprises: a step of adding the organic compound which contain in the fuel the silicon under the first condition; and a step of adding the organic compound which contain in the fuel the silicon under the second condition. A base layer and a porous layer include silicon dioxide which becomes with the reaction of the organic compound and fuel gas. The thickness of the base layer 1 ~ 5 μm The porosity of the porous layer 60%, and the thickness more than 5 μm.
Abstract:
PURPOSE: A thermal element scale removal method of a heat exchanger for a flue gas desulfurization system is provided to dip scale into a caustic soda solution and easily wash the scale through cleaning water of high pressure and high temperature, thereby improving heat exchange efficiency of the flue gas desulfurization system. CONSTITUTION: Plural thermal elements are laminated within a case. In an upper part of the thermal element, boiler fuel gas flows in. In a lower part, fuel gas of an absorbing tower flows in. The thermal element where scales are piled is dipped into a caustic soda solution of a constant temperature. The thermal element is washed through cleaning water of high temperature and high pressure.
Abstract:
A single hot isostatic pressing-heat treating process of Ni-based superalloy components for gas turbines, which effectively removes fine defects of the components and optimizes material properties of the components simultaneously at high temperature and high pressure, a single hot isostatic pressing-heat treating process having improved properties as compared with an existing simple heat treatment process in the manufacturing process of an alloy material, and components for gas turbines of which fine defects are removed and properties are optimized by the single hot isostatic pressing-heat treating process are provided. In manufacture of Ni-based superalloy components for gas turbines, a method of manufacturing Ni-based superalloy components for gas turbines by a single hot isostatic pressing-heat treating process is characterized in that a hot isostatic pressing process and a heat treating process are simultaneously performed en bloc on a Ni-based superalloy under high temperature and pressure conditions by using a hot isostatic press. The high temperature condition is applied to each step of the hot isostatic pressing process and the heat treating process simultaneously performed en bloc on the Ni-based superalloy. The high temperature condition is maintained at 1210 to 1250 deg.C for 1 to 3 hours in the first step, and the high temperature condition is maintained at 1000 to 1200 deg.C for 1 to 3 hours in the second step. The high pressure condition is 1000 to 1500 atmospheric pressures.
Abstract:
본 발명은 복합 화력 발전소나 항공기 등에서 사용되는 가스터빈의 부품 소재인 니켈계 초합금 부품의 재생공정의 일환으로, HF 가스를 이용하여 재생품의 표면이나 미세균열 상에 존재하는 산화물을 제거하는 가스터빈용 니켈계 초합금 부품의 건식세정방법에 관한 것으로, 더욱 상세하게는 폴리테트라플루오로에틸렌 (Polytetrafluoroethylene: PTFE or 테플론) 분말을 휘발성 유체와 섞어 균열 표면에 도포하므로써, PTFE 분말이 미세균열 내로 삽입되게 하여, 미세균열 깊숙한 곳에서 PTFE 분말의 열분해로 발생한 C 2 F 4 와 수소의 반응으로 발생된 HF 가스를 이용할 수 있는 니켈계 초합금 부품의 건식세정 방법에 관한 것이다.
Abstract:
본 발명은 열 차폐 코팅의 수명을 향상시키고자 금속 중간 결합층에 치밀하고 견고한 고온 내산화성이 높은 알루미늄 산화물층을 얻기 위한 열처리 공정에 관한 것이다. 본 발명에 의한 열처리 공정은 기존의 열 차폐 코팅 공정과 모두 동일하지만 단지 공정 중간단계에서 모재에 금속 중간결합층을 코팅한 후 예산화처리를 하는 것만 다르다. 예산화처리는 중간 결합층까지만 코팅한 시편을 대기 중에서 1050℃에서 최대 50시간까지 열처리를 통해 금속 중간결합 코팅층 위에 치밀하고 견고한 알루미늄 산화층을 얻는 것을 목적으로 한다. 상기 방법으로 처리된 열 차폐 코팅의 시편을 1100℃ 공기 중에서 반복산화 시험한 결과 아주 우수한 내산화 특성을 보였으며, 열충격 특성 또한 우수하였다.
Abstract:
PURPOSE: A powder composition for simultaneously coating aluminum and chromium on metal surface and a method for coating the same are provided to obtain pack cementation of aluminum and chromium by freely controlling a composition of aluminum and chromium oxide, and supply economical mixed powder by using oxide powder instead of alloy powder. CONSTITUTION: A powder composition for simultaneously coating aluminum and chromium on metal surface is a mixed powder comprising an aluminum powder, a chromium oxide powder producing chromium by reacting with the aluminum powder, an activator powder activating chromium produced by the reaction and the remaining aluminum, and a filler for preventing condensation thereof. A method for simultaneously coating aluminum and chromium on metal surface comprises the process of putting the mixed powder into a heat resistant container, coating the container with metal, and simultaneously coating chromium and aluminum on the metal by sealing the container or heating the container under the inert gas or hydrogen environment at a temperature of 800 to 1200 deg.C for 1 to 30 hours.