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Improving the Efficiency of Gas Turbines During Off-Design Operation by Adjusting the Turbine and Compressor Blade Stagger Angles

机译：通过调节涡轮机和压缩机叶片错开角度在非设计过程中提高燃气轮机的效率

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1. Improving the Efficiency of Gas Turbines During Off-Design Operation by Adjusting the Turbine and Compressor Blade Stagger Angles [J] . Schobeiri MT Journal of Applied Mechanical Engineering . 2018,第1期

机译：通过调整涡轮机和压气机叶片的错开角度来提高燃气轮机的非设计运行效率
2. Analytical study of articulating turbine rotor blade concept for improved off-design performance of gas turbine engines [J] . Murugan Muthuvel Senthil, Ghoshal Anindya, Xu Fei, Journal of Engineering for Gas Turbines and Power . 2017,第10期

机译：铰接式涡轮转子叶片概念的分析研究，以改善燃气涡轮发动机的非设计性能
3. Improving Gas Turbine Efficiency using Optical Pyrometry: MEASURING INDIVIDUAL BLADE TEMPERATURES OF GAS TURBINES CAN IMPROVE OVERALL PLANT EFFICIENCY [J] . D. C. Amory, R. A. Hovan Turbomachinery International . 2004,第1期

机译：使用光学高温法提高燃气轮机效率：测量燃气涡轮机的单个叶片温度可以提高工厂的整体效率
4. Impact of Turbine Blade Stagger Angle Adjustment On the Efficiency and Performance of Gas Turbines During Off-Design and Dynamic Operation [C] . Meinhard T. Schobeiri ASME turbo expo: turbomachinery technical conference and exposition . 2018

机译：涡轮叶片错位角调整对非设计和动态运行期间燃气轮机效率和性能的影响
5. Development of an Ultra-High Efficiency Gas Turbine Engine (UHEGT) with Stator Internal Combustion: Design, Off-Design, and Nonlinear Dynamic Operation [D] . Ghoreyshi, Seyed Mostafa 2018

机译：具有定子内燃的超高效燃气涡轮发动机（UHEGT）的开发：设计，非设计和非线性动态运行
6. Full-Scale Fatigue Testing of a Wind Turbine Blade in Flapwise Direction and Examining the Effect of Crack Propagation on the Blade Performance [O] . Othman Al-Khudairi, Homayoun Hadavinia, Christian Little, 2017

机译：风力涡轮机叶片沿翼展方向的全尺寸疲劳测试并研究裂纹扩展对叶片性能的影响
7. Post-operation state and extension of service life of compressor blades of the gas-turbine power plant GTE-45-3 [O] . Y. P. Tarasenko, O. B. Berdnik, I. N. Tsareva 2014

机译：燃气涡轮发电厂GTE-45-3的压缩机叶片使用寿命的操作后状态和延长
8. Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed IV : effect of increasing blade speed on velocity diagrams of turbine for engine operation at constant rotative speed [R] . Davison, Elmer H, English, Robert E 1952

机译：适用于具有高压缩机压力比和低压缩机叶尖速度的涡轮喷气发动机的涡轮机的研究IV：在恒定转速下增加叶片速度对涡轮机速度图的影响

Improving the Efficiency of Gas Turbines During Off-Design Operation by Adjusting the Turbine and Compressor Blade Stagger Angles

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