Thermophysical properties of ceramic materials of molds and cores for casting the heat-resistant alloy-based blades of gas-turbine engines

被引:4
|
作者
Loshchinin Y.V. [1 ]
Folomeikin Y.I. [1 ]
Rykova T.P. [1 ]
Marakhovsky P.S. [1 ]
Pakhomkin S.I. [1 ]
机构
[1] All-Russian Scientific Research Institute of Aviation Materials (VIAM), Moscow
来源
Inorganic Materials: Applied Research | 1600年 / Maik Nauka Publishing / Springer SBM卷 / 05期
关键词
adiabatic calorimeter; differential scanning calorimetry; methods of laser flash; specific heat capacity; temperature coefficient of linear expansion; thermal conductivity; thermal diffusivity;
D O I
10.1134/S2075113314040303
中图分类号
学科分类号
摘要
The thermal diffusivity, thermal conductivity, temperature coefficient of linear expansion (TCLE), and specific heat capacity of ceramic materials of shell molds and cores for casting parts of heatresistant nickel-based alloys for gas-turbine engines (GTEs) are measured in a temperature range from 20 to 1500°C by the use of methods of laser flash, relative dilatometer with a pusher, and differential scanning calorimetry (DSC). The effect of the sample thickness, various process coatings, and environment is investigated. The composition and temperature dependences of thermal diffusivity and heat expansion are considered. © 2014 Pleiades Publishing, Ltd.
引用
收藏
页码:407 / 412
页数:5
相关论文
共 21 条
  • [1] THERMAL-STABILITY OF HEAT-RESISTANT MATERIALS FOR GAS-TURBINE BLADES
    GETSOV, LB
    MALYGIN, AF
    REVYAKINA, NN
    BALANDIN, IM
    THERMAL ENGINEERING, 1974, 21 (03) : 32 - 35
  • [2] Evaluation of the Endurance Limit of Cooled Blades of Gas-Turbine Engines Made of Heat-Resistant Nickel Alloy
    Kvasnytska, Yu. H.
    Ivaskevych, L. M.
    Balitskii, A. I.
    Mialnitsa, H. P.
    Kvasnytska, K. H.
    MATERIALS SCIENCE, 2023, 59 (03) : 340 - 346
  • [3] Evaluation of the Endurance Limit of Cooled Blades of Gas-Turbine Engines Made of Heat-Resistant Nickel Alloy
    Yu. H. Kvasnytska
    L. M. Ivaskevych
    A. I. Balitskii
    H. P. Mialnitsa
    K. H. Kvasnytska
    Materials Science, 2023, 59 : 340 - 346
  • [4] CONTEMPORARY HEAT-RESISTANT AND CAST ALLOYS FOR GAS-TURBINE BLADES
    OREKHOV, NG
    GLEZER, GM
    KULESHOVA, EA
    TOLORAIYA, VN
    METAL SCIENCE AND HEAT TREATMENT, 1993, 35 (7-8) : 413 - 417
  • [5] Novel approach to investment casting of heat-resistant steel turbine blades for aircraft engines
    Huang, Pei-Hsing
    Shih, Leonard Kuo-Liang
    Lin, Hung-Mao
    Chu, Che-I
    Chou, Chuen-Shii
    INTERNATIONAL JOURNAL OF ADVANCED MANUFACTURING TECHNOLOGY, 2019, 104 (5-8): : 2911 - 2923
  • [6] Novel approach to investment casting of heat-resistant steel turbine blades for aircraft engines
    Pei-Hsing Huang
    Leonard Kuo-Liang Shih
    Hung-Mao Lin
    Che-I Chu
    Chuen-Shii Chou
    The International Journal of Advanced Manufacturing Technology, 2019, 104 : 2911 - 2923
  • [7] Laser Surface Strengthening of Heat-Resistant Titanium Alloy for Gas Turbine Engines
    Girzhon, V. V.
    Smolyakov, O., V
    Ovchinnikov, O., V
    Zavgorodny, O., V
    METALLOPHYSICS AND ADVANCED TECHNOLOGIES, 2022, 44 (03) : 383 - 391
  • [8] Modeling the structure formation during hot deforming the billets of the parts of gas-turbine engines made of heat-resistant nickel alloy
    Burlakov I.A.
    Valitov V.A.
    Ganeev A.A.
    Zabel’yan D.M.
    Morozov S.V.
    Sukhorukov R.Y.
    Utyashev F.Z.
    Journal of Machinery Manufacture and Reliability, 2016, 45 (5) : 469 - 475
  • [9] Heat Resistant Coatings for Titan Alloy-based Parts of a Gas Turbine Engine
    Urbahs, A.
    Savkovs, K.
    Kurjanovics, I.
    Zujevs, V.
    TRANSPORT MEANS 2011, 2011, : 225 - 228
  • [10] INFLUENCE OF COATING ON THE PROPERTIES OF HEAT-RESISTANT GAS-TURBINE ALLOYS .2. MICROSTRUCTURES
    SACHOVA, E
    HOUGARDY, HP
    MATERIALWISSENSCHAFT UND WERKSTOFFTECHNIK, 1988, 19 (10) : 329 - 335