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High-Temperature and High-Speed Gas Turbine Pump Electro-Hydraulic Energy System for Aircraft

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High Speed Pneumatic Theory and Technology Volume II

Abstract

This chapter covers the electro-hydraulic servo control technology and its practical progress of aircraft gas turbine pump; the design theory and technology of the core components of gas power energy, such as steering gear system, gas generator, and gas turbine, etc.; starting characteristics of missile gas turbine motor pump with electro-hydraulic energy combination; basic characteristics and design technology of missile electro-hydraulic energy system; the power matching design method of steering gear system; and the design theory of electro-hydraulic energy system for high-temperature and high-speed gas turbine pump of aircraft is described in detail.

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Authors and Affiliations

  1. School of Mechanical Engineering, Tongji University, Shanghai, China

    Yaobao Yin

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  1. Yaobao Yin
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Correspondence to Yaobao Yin .

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Yin, Y. (2020). High-Temperature and High-Speed Gas Turbine Pump Electro-Hydraulic Energy System for Aircraft. In: High Speed Pneumatic Theory and Technology Volume II. Springer, Singapore. https://doi.org/10.1007/978-981-15-2202-4_9

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