Gradient complex protective coatings for single-crystal turbine blades of high-heat gas turbine engines

被引：0
|
作者：
V. P. Kuznetsov
V. P. Lesnikov
S. A. Muboyadzhyan
O. V. Repina
机构：
[1] Ural State Technical University — Ural Polytechnic Institute (UGTU-UPI),
[2] TUBOMET Company,undefined
[3] All-Russia Institute for Aircraft Materials (VIAM),undefined
来源：
Metal Science and Heat Treatment | 2007年 / 49卷
关键词：
Turbine Blade; Diffusion Zone; Aluminide Coating; External Zone; Complex Coating;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Complex diffusion-condensation protective coatings characterized by gradient distribution of alloying elements over the thickness due to formation of a diffusion barrier layer on the surface of blades followed by deposition of condensation alloyed layers based on the Ni-Co-Cr-Al-Y system and an external layer based on a NiAl alloyed β-phase and a ZrO2: Y2O3 ceramics are presented. A complex gradient coating possessing unique protective properties at t = 1100–1200°C for single-crystal blades from alloy ZhS36VI for advanced gas turbine engines with gas temperature of 1550°C at the inlet to the turbine is described.
引用
收藏
页码：253 / 259
页数：6
相关论文
共 50 条
  • [41] Insight into the sensitivities of freckles in the directional solidification of single-crystal turbine blades
    Ren, Neng
    Li, Jun
    Panwisawas, Chinnapat
    Xia, Mingxu
    Dong, Hongbiao
    Li, Jianguo
    [J]. JOURNAL OF MANUFACTURING PROCESSES, 2022, 77 : 219 - 228
  • [42] Stray grain formation in the seed region of single-crystal turbine blades
    Yang, XL
    Lee, PD
    D'Souza, N
    [J]. JOM, 2005, 57 (05) : 40 - 44
  • [43] Stray grain formation in the seed region of single-crystal turbine blades
    X. L. Yang
    P. D. Lee
    N. D’Souza
    [J]. JOM, 2005, 57 : 40 - 44
  • [44] Ion-Plasma Protective Coatings for Gas-Turbine Engine Blades
    Kablov, E. N.
    Muboyadzhyan, S. A.
    Budinovskii, S. A.
    Lutsenko, A. N.
    [J]. RUSSIAN METALLURGY, 2007, (05): : 364 - 372
  • [45] HEAT AND EROSION-RESISTANT NANOSTRUCTURED COATINGS FOR GAS TURBINE ENGINES
    Urbahs, Aleksandrs
    Savkovs, Konstantins
    Urbaha, Margarita
    Carjova, Kristine
    [J]. AVIATION, 2013, 17 (04) : 137 - 144
  • [46] Corrosion-Resistant High-Temperature Alloys for Large Single-Crystal Turbine Blades
    V. N. Toloraiya
    N. G. Orekhov
    B. S. Lomberg
    [J]. Metal Science and Heat Treatment, 2003, 45 : 32 - 34
  • [47] Corrosion-resistant high-temperature alloys for large single-crystal turbine blades
    Toloraiya, VN
    Orekhov, NG
    Lomberg, BS
    [J]. METAL SCIENCE AND HEAT TREATMENT, 2003, 45 (1-2) : 32 - 34
  • [48] HIGH-TEMPERATURE COATINGS FOR GAS-TURBINE BLADES - A REVIEW
    SIVAKUMAR, R
    MORDIKE, BL
    [J]. SURFACE & COATINGS TECHNOLOGY, 1989, 37 (02): : 139 - 160
  • [49] Improvement of Hydrogen-Resistant Gas Turbine Engine Blades: Single-Crystal Superalloy Manufacturing Technology
    Balitskii, Alexander I.
    Kvasnytska, Yulia H.
    Ivaskevych, Ljubomyr M.
    Kvasnytska, Katrine H.
    Balitskii, Olexiy A.
    Miskiewicz, Radoslaw M.
    Noha, Volodymyr O.
    Parkhomchuk, Zhanna V.
    Veis, Valentyn I.
    Dowejko, Jakub Maciej
    [J]. MATERIALS, 2024, 17 (17)
  • [50] THERMOCYCLIC- AND STATIC-FAILURE CRITERIA FOR SINGLE-CRYSTAL SUPERALLOYS OF GAS-TURBINE BLADES
    Getsov, Leonid B.
    Semenov, Artem S.
    Tikhomirova, Elena A.
    Rybnikov, Alexander I.
    [J]. MATERIALI IN TEHNOLOGIJE, 2014, 48 (02): : 255 - 260
12345