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首页> 外文期刊>Tehnika >Plazma i plamene prevlake Ni4.5Al za kompresore turbinskih motora mlaznih aviona
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Plazma i plamene prevlake Ni4.5Al za kompresore turbinskih motora mlaznih aviona

机译:用于喷气涡轮发动机压缩机的Ni4.5Al等离子和火焰涂层

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摘要

U ovom radu prikazani su rezultati razvoja ispitivanja i primene plazma i plamene prevlake Ni4.5Al. Plazma prevlaka se dobija raspršivanjem kompozitnog plazma praha u plazmi argona i vodonika i stopljene čestice praha se zakale iz tečne faze, te je stoga tvrdoća plazma prevlake visoka. Prikazani su rezultati mikrostrukturnih i strukturnih ispitivanja kao i mehaničkih. Prazma prevlake Ni4.5Al čvrsto se vezuju za osnovni materijal, dok je plazmena prevlaka, dobijena u kiseonično acetilenskom plamenu, kontrolisane poroznosti podložna abraziji, te obezbeđuje kontrolisane zazore među spregnutim delovima motora. Stoga se ove prevlake primenjuju za nanošenje na gasne zaptivke kompresora turbinskih motora mlaznih aviona.%Results of development, investigation and application of composite plasma and flame sprayed coatings of Ni4.5Al are presented. The plasma sprayed coatings are obtained from composite plasma powder Ni4.5Al and sprayed in plasma of mixed gases argon and hydrogen. The particles of plasma powder are melted in plasma and ultrarapidly quenched from liquid to solid state. Therefore the plasma coatings of special properties for extence a high hardnes are obtained. The microstructure and the structure and the mechanical properties are presented. The bonding coating of plasma sprayed Ni4.5Al has a high bonding strength with the basic material. This coating has a low porosity about 2% and therefore has a good anticorosity resistance. The flame sprayed coating of Ni4.5Al is the working coating and has a controled high porosity about 40%. This coating is abrodable and provides controled clearence between mating parts of engine. Therefore they are applied on the gas seal of compresors of jet engine.
机译:本文介绍了等离子和Ni4.5Al火焰涂层的测试和应用开发的结果。通过在氩气和氢等离子体中喷射复合等离子体粉末来获得等离子体涂层,并且将熔融粉末颗粒从液相中淬灭,因此等离子体涂层的硬度高。给出了微观结构和结构测试以及机械测试的结果。 Ni4.5Al涂层结合牢固地结合到基础材料上,而在氧气-乙炔火焰中获得的等离子涂层则受到控制的孔隙磨损,并在相连的发动机部件之间提供受控的间隙。因此,这些涂层被用于喷气飞机的涡轮发动机的压缩机的气密封。%给出了Ni4.5Al复合等离子和火焰喷涂涂层的开发,研究和应用的结果。等离子喷涂涂层是从复合等离子粉末Ni4.5Al获得的,并喷涂在混合气体氩气和氢气的等离子体中。等离子粉末的颗粒在等离子中融化,并从液态快速转变为固态。因此,获得了具有延伸高硬度的特殊性能的等离子涂层。介绍了显微组织,结构和力学性能。等离子喷涂Ni4.5Al的结合层与基础材料的结合强度高。该涂层具有约2%的低孔隙率,因此具有良好的抗腐蚀性。 Ni4.5Al的火焰喷涂涂层是工作涂层,并具有约40%的受控高孔隙率。该涂层是可磨蚀的,并在发动机配合部分之间提供受控的间隙。因此,它们被应用于喷气发动机压缩机的气密封。

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