Study of design method for the zero-stage compressor in an expendable gas turbine engine

被引：0
|
作者：
The 31st Research Institute, CASIC, Beijing 100074, China [1 ]
不详 [2 ]
机构：
来源：
Hangkong Dongli Xuebao | 2006年 / 6卷 / 1098-1102期
关键词：
Computational fluid dynamics - Gas turbines - Propulsion;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Analyzing the evolvement from TRI60-2 engine to TRI60-20 engine developed by France MicroTurbo Inc, the technical characteristic and design method of adding zero-stage compressor were researched. Taking obtaining the compressor's structure and characteristics as the primary concern, the process of adding zero-stage compressor was discussed, and using CFD software validated by test data the flow field was numerically simulated in full three dimensions and analyzed through computation. The result indicates that the method of adding zero-stage compressor discussed in this paper is basically successful.
引用
收藏
相关论文
共 50 条
  • [1] A Comprehensive Solution of the Problems of Ensuring the Strength of Gas Turbine Engine Compressor at the Design Stage
    Vedeneev, V. V.
    Kolotnikov, M. E.
    Mossakovskii, P. A.
    Kostyreva, L. A.
    Abdukhakimov, F. A.
    Makarov, P., V
    Pyhalov, A. A.
    Dudaev, M. A.
    2017 INTERNATIONAL CONFERENCE ON AEROSPACE TECHNOLOGY, COMMUNICATIONS AND ENERGY SYSTEMS (ATCES 2017), 2018, 302
  • [2] APPROXIMATION METHOD OF THE GAS TURBINE ENGINE COMPRESSOR CHARACTERISTICS
    Avdeev, Sergey
    Tkachenko, Andrey
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2C, 2021,
  • [3] DESIGN OF HIGHLY LOADED TURBINE STAGE FOR SMALL GAS TURBINE ENGINE
    Rajeevalochanam, Prathapanayaka
    Sunkara, S. N. Agnimitra
    Mayandi, Balamurugan
    Banda, Bala Venkata Ganesh
    Chappati, Veera Sesha Kumar
    Kumar, Kishor
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2C, 2016,
  • [4] Preliminary design optimization of a gas turbine multi-stage compressor
    Tahsini A.M.
    Tahsini, Amir Mahdi, 1600, Gas Turbine Society of Japan (11): : 50 - 55
  • [5] Expanding the choke margin of a mixed flow compressor stage for a micro gas turbine engine
    van Eck, Hano
    van der Spuy, Sybrand J.
    Gannon, Anthony J.
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2024, 41 (01) : 91 - 101
  • [6] The Design and Optimization of Additively Manufactured Radial Compressor of a Miniature Gas Turbine Engine
    Ergin, Cagdas C.
    Verstraete, Tom
    Saracoglu, Bayindir H.
    JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2024, 146 (07):
  • [7] Upgrading the Compressor Stage of the CAT250TJ Micro Gas Turbine Engine
    Hano van Eck
    Sybrand Johannes van der Spuy
    Aerotecnica Missili & Spazio, 2025, 104 (2): : 91 - 104
  • [8] CHARACTERIZING COMPRESSOR ROTOR UNCLAMP IN A GAS TURBINE ENGINE
    Alban, Cory
    Tolstykh, Masha
    Hilty, Devin
    Bollman, Andrew
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 4, PTS A AND B, 2012, : 1083 - 1087
  • [9] Failure Analysis of a Compressor Blade of Gas Turbine Engine
    Biswas, Swati
    Ganeshachar, M. D.
    Kumar, Jivan
    Kumar, V. N. Satish
    STRUCTURAL INTEGRITY, 2014, 86 : 933 - 939
  • [10] Fracture of a Compressor Stator Blade in a Gas Turbine Engine
    Neidel, A.
    Matijasevic-Lux, B.
    PRAKTISCHE METALLOGRAPHIE-PRACTICAL METALLOGRAPHY, 2013, 50 (01): : 43 - 49
12345