COOLING OF GAS TURBINES BLADES.

被引：0
|
作者：
Mukherjee, D.K.
机构：
来源：
| 1600年 / 64期
关键词：
D O I：
暂无
中图分类号：
TK [能源与动力工程];
学科分类号：
0807 ;
摘要：
Due to the high inlet temperature of gas turbines, the blades in the first rows have to be cooled. Using appropriate methods of cooling. Brown Boveri have succeeded in achieving a high cooling efficiency. Sophisticated computer programs are used in the design of blades and to predict the useful life of blading. Exhaustive experimental studies have confirmed the suitability of the method of calculation.
引用
收藏
相关论文
共 50 条
  • [21] FORGING OF BLADES FOR GAS-TURBINES
    WRIGHT, DC
    SMITH, DJ
    MATERIALS SCIENCE AND TECHNOLOGY, 1986, 2 (07) : 742 - 747
  • [22] Hydraulic Characteristics of the Cooling System for Channel-type Rotor Blades.
    Arsen'ev, L.V.
    Makarov, V.N.
    Mitryaev, I.B.
    Vorob'ev, V.A.
    Kovalev, A.N.
    Energomashinostroenie, 1984, (04): : 6 - 8
  • [23] VIBRATING BEAM DAMPERS FOR REDUCING VIBRATIONS IN GAS TURBINE BLADES.
    Jones, D.I.G.
    Nashif, A.D.
    Stargardter, H.
    1600, (97 Ser A):
  • [24] Control of Fir-Tree Roots of Gas Turbine Blades.
    Kudevitskii, Ya.V.
    Lekhtman, A.P.
    Energomashinostroenie, 1972, (08): : 28 - 30
  • [25] The pigment of potamogeton blades.
    Prat, S
    BIOCHEMISCHE ZEITSCHRIFT, 1924, 152 : 495 - 497
  • [26] TESTING ENGINE BLADES.
    Schatz, David
    Robotics World, 1987, 5 (11): : 24 - 26
  • [27] EVALUATION OF A NEW CORROSION RESISTANT ALLOY FOR GAS TURBINE BLADES.
    Just, Ch.
    Huber, R
    Bauer, R.
    Marine Geology, 1979, 3
  • [28] BEHAVIOR OF THERMAL BARRIER COATINGS FOR ADVANCED GAS TURBINE BLADES.
    Chang, George C.
    Phucharoen, W.
    Miller, Robert A.
    1600, (30):
  • [29] The Cardinal's Blades.
    Cassada, Jackie
    LIBRARY JOURNAL, 2010, 135 (15) : 65 - 65
  • [30] CONSISTENT CUTTING OF TURBINE BLADES.
    Anon
    Foundry Trade Journal, 1987, 162 (3348):
12345