公开(公告)号：US6090191A

公开(公告)日：2000-07-18

申请号：US407947

申请日：1999-09-29

申请人： Aza Fedorovna Atlanova ,  Galina Andreevna Babaeva ,  Evgeny Alexeevich Belov ,  Dina Ivanovna Dubovik ,  Jury Alexandrovich Pestov ,  Margarita Evgenievna Judina ,  Leonid Vasilievich Cherkasov ,  Vadim Iliich Semenov ,  Felix Jurievich Chelkis ,  Alexandr Mikhailovich Kashkarov ,  Konstantin Pavlovich Khaplanov

发明人： Aza Fedorovna Atlanova ,  Galina Andreevna Babaeva ,  Evgeny Alexeevich Belov ,  Dina Ivanovna Dubovik ,  Jury Alexandrovich Pestov ,  Margarita Evgenievna Judina ,  Leonid Vasilievich Cherkasov ,  Vadim Iliich Semenov ,  Felix Jurievich Chelkis ,  Alexandr Mikhailovich Kashkarov ,  Konstantin Pavlovich Khaplanov

IPC分类号： F16L58/04 ,  C22C29/12 ,  C23C4/06 ,  C23C30/00 ,  C09K5/00

CPC分类号： C23C30/00 ,  C22C29/12 ,  C23C4/06

摘要： The invention relates to the field of producing the means for protecting the alloys on the nickel base against the influence of corrosive media, and more particularly concerns the metal-ceramic coatings used for protecting the flow parts of the turbines of turbopump liquid-propellant rocket engines (LRE). The composition for producing the metal-ceramic coating consists of nickel and of oxides of barium, boron, aluminum, cerium and zirconium at the following percentage of components by mass: nickel--36-58, barium oxide--16-19, boron oxide--7-13, aluminum oxide--6-9, cerium oxide--14-19, zirconium oxide--1-2. The coating is produced of a slip, that is applied to the pieces by dipping, spraying or flooding. The slip layers are dried in the flow of hot air. The coating is fired in a furnace in the inert gas medium, argon for example, at a temperature of 1000-1100.degree. C. during 0.5-1 hour. The use of the composition for producing a metal-ceramic coating for the pieces and units of complicated shape made of nickel alloys with a layer of nickel secures their serviceability and reliability at a cyclic action of a high-temperature flow of oxidizing generator gas containing the particles of AMg6 alloy at the temperature of up to 900.degree. C.

摘要翻译： 本发明涉及生产用于保护镍基底上的合金抵抗腐蚀性介质的影响的装置的领域，更具体地涉及用于保护涡轮泵液体推进剂火箭发动机涡轮机的流动部分的金属 - 陶瓷涂层 （LRE）。 用于制备金属 - 陶瓷涂层的组合物由以下组成的以下百分比的镍和钡，硼，铝，铈和锆的氧化物组成：镍-36-58，氧化钡-16-19，氧化硼 - 7-13，氧化铝-6-9，氧化铈-14-19，氧化锆-1-2。 涂层由滑块制成，通过浸渍，喷涂或浸渍施加到碎片上。 滑层在热空气流中干燥。 将涂层在惰性气体介质中的炉中，例如氩气，在1000-1100℃的温度下在0.5-1小时内焙烧。 使用由具有镍层的镍合金制成的复杂形状的元件和单元的金属陶瓷涂层的组合物在包含氧化发生器气体的高温流动的循环作用下确保其使用性和可靠性 AMg6合金颗粒在高​​达900℃的温度下