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DESIGN OF A GAS TURBINE BASED AIR START UNIT FOR LARGER AIRCRAFT ENGINE

机译：用于较大飞机发动机的燃气轮机的空气启动单元设计

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A novel Air Start Unit powered by gas turbine engine is developed. The feature of this unit is that it can start various aircraft engines, including the hundred thousand pound thrust class engine like GE90, with different air flow rate in a compact design. This paper introduces the complete design and development of large centrifugal compressor, digital engine control system, testing of gas turbine system.

机译：开发出由燃气轮机供电的新型空气启动单元。本机的特征是它可以启动各种飞机发动机，包括GE90等十万英镑的推力级发动机，具有紧凑的设计中的不同空气流速。本文介绍了大型离心式压缩机，数字发动机控制系统，燃气轮机系统测试的完整设计和开发。

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《ASME Turbo Expo》|2004年||共7页
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Li-Chieh Hsu; Wu-Chi Ho; Chien-Ching Hsueh;
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中图分类 TK47-53;
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1. Joint Prediction of Aircraft Gas Turbine Engine Axial Flow Compressor Off-Design Performance and Surge Line Based on the Expanded Method of Generalized Functions [J] . A. B. Mikhailova, D. A. Akhmedzyanov, Yu. M. Akhmetov, Russian Aeronautics . 2014,第3期

机译：基于广义函数展开法的飞机燃气轮机轴流压气机偏离设计性能和喘振线的联合预测
2. Provision of the Required Lifetime and Strength Reliability of Gas Turbine Units Developed on the Aircraft Engines Basis [J] . Yu. A. Nozhnitskii, B. S. Blinnik, N. G. Bychkov, Thermal engineering . 2005,第11期

机译：提供基于飞机发动机开发的燃气轮机所需的使用寿命和强度可靠性
3. Seventy-Five Years at the Head of Scientific and Technical Progress in the Field of Aircraft Engines and Gas Turbine Units [J] . V. A. Skibin, V. I. Solonin, G. K. Vedeshkin Thermal engineering . 2005,第11期

机译：七十五年来担任航空发动机和燃气涡轮机领域的科学技术进步负责人
4. DESIGN OF A GAS TURBINE BASED AIR START UNIT FOR LARGER AIRCRAFT ENGINE [C] . Li-Chieh Hsu, Wu-Chi Ho, Chien-Ching Hsueh American Society of Mechanical Engineers(ASME) Turbo Expo vol.4; 20040614-17; Vienna(AT) . 2004

机译：基于燃气轮机的大型飞机发动机起步单元设计
5. Simultaneous multi-design point approach to gas turbine on-design cycle analysis for aircraft engines. [D] . Schutte, Jeffrey Scott. 2009

机译：飞机发动机燃气轮机设计周期分析的同时多设计点方法。
6. Non-volatile particle emissions from aircraft turbine engines at ground-idle induce oxidative stress in bronchial cells [O] . Hulda R. Jonsdottir, Mathilde Delaval, Zaira Leni, 2019

机译：飞机怠速时飞机涡轮发动机的非挥发性颗粒物排放会在支气管细胞中引起氧化应激
7. Advanced Gas Turbine Concept, Design and Evaluation Methodology. Preliminary Design of Highly Loaded Low Pressure Gas Turbine of Aircraft Engine [O] . Leonid Romanenko, Leonid Moroz, Petr Pagur, 2008

机译：先进的燃气轮机概念，设计和评估方法。高负荷低压燃气轮机的初步设计
8. Starting of Aircraft Gas Turbine Engines [R] . Alabin, M. A., Kats, B. M., Litvinov, Y. A. 1972

机译：启动飞机燃气涡轮发动机

DESIGN OF A GAS TURBINE BASED AIR START UNIT FOR LARGER AIRCRAFT ENGINE

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