Fatigue Resistance of Aircraft Propeller Blades.

被引:0
|
作者
Stepnov, M.N.
Seregin, A.S.
Leonova, O.V.
Sukhorosov, Yu.L.
Kulikov, E.I.
Dunaev, E.V.
机构
来源
Problemy Prochnosti | 1977年 / 05期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
Results of fatigue tests of various types of blades, processed statistically, are presented. Equations are selected permitting description of the blade fatigue curve. Relations are shown characterizing variations of mean square deviations of logarithms of the number of cycles depending on the test basis.
引用
收藏
页码:36 / 39
相关论文
共 50 条
  • [41] METHOD FOR DESIGNING LONG TURBINE BLADES.
    Gogolev, I.G.
    Kuz'michev, R.V.
    1600, (20):
  • [42] Finishing Machining of Hydraulic Turbine Blades.
    Sokolova, L.S.
    Energomashinostroenie, 1979, (12): : 25 - 27
  • [43] New Real-Time Structural Health Monitoring Microsystem for Aircraft Propeller Blades
    Escriba, Christophe
    Fourniols, Jean-Yves
    Lastapis, Mathieu
    Boizard, Jean-Louis
    Auriol, Guillaume
    Andrieu, Stephane
    IEEE AEROSPACE AND ELECTRONIC SYSTEMS MAGAZINE, 2012, 27 (02) : 29 - 41
  • [44] INVERSE DESIGN OF INTERNALLY COOLED TURBINE BLADES.
    Kennon, S.R.
    Dulikravich, G.S.
    Journal of Engineering for Gas Turbines and Power, 1985, 107 (01) : 123 - 126
  • [45] The gilded chain: A tale of the King's Blades.
    Cassada, J
    LIBRARY JOURNAL, 1998, 123 (17) : 103 - 103
  • [46] SPARK EROSION MACHINE FINISHES TURBINE BLADES.
    Anon
    Aircraft Engineering and Aerospace Technology, 1985, 57 (09): : 16 - 17
  • [47] CNC LASERS CUT OUT SAW BLADES.
    Winship, John T.
    American machinist, 1984, 128 (05): : 92 - 94
  • [48] DETERMINING USEFUL LIFE OF STEAM TURBINE BLADES.
    Sokolov, V.S.
    Kunavin, S.A.
    Lebedeva, A.I.
    Soviet energy technology, 1987, (05): : 55 - 60
  • [49] PRETWIST AND SHEAR FLEXIBILITY IN THE VIBRATIONS OF TURBINE BLADES.
    Krenk, S.
    Gunneskov, O.
    1600, (52):
  • [50] COMPARISON OF DESIGN TECHNIQUES FOR PUMPS WITH SKEWED BLADES.
    Treaster, A.L.
    Smith, F.E.
    Journal of Propulsion and Power, 1985, 1 (01): : 39 - 44