Research on the Transient Characteristics of a Three-Stream Adaptive Cycle Engine

Author:

Yu Qiuxia12,Hu Jun1,Wang Weili2,Gu Bin2

Affiliation:

1. College of Energy and Power, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

2. AECC Sichuan Gas Turbine Establishment, Chengdu 610500, China

Abstract

Based on the transient-performance calculation model of a dual-spool mixed-flow turbofan engine, this article improves the dynamic algorithm of geometric adjustment mechanisms and establishes a transient-performance calculation model suitable for a three-stream adaptive cycle engine (three-stream ACE). Using this model, the transient characteristics of a three-stream ACE were analyzed. The results indicate that the delay in the area of the fan nozzle significantly reduces the surge margin of the front fan during deceleration, while the delay in the angle of the front-fan and aft-fan guide vanes significantly reduces the surge margin of the front fan during acceleration, therefore becoming a limitation of the transient performance of the engine. At the same time, to meet the demand for equal-thrust mode switching, this article also proposes a mode-switching control scheme that solves the problem of engine state oscillation during the mode-conversion process and achieves a smooth conversion with thrust fluctuations within 1%. The research results of this article can guide the optimization design of three-stream ACE transition-state control laws and the design of control system architecture, which has important engineering significance.

Funder

National Science and Technology Major Project

Publisher

MDPI AG

Subject

Energy (miscellaneous),Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment,Electrical and Electronic Engineering,Control and Optimization,Engineering (miscellaneous),Building and Construction

Reference40 articles.

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4. GE Aviation (2021, May 13). Testing on GE’s First XA100 Adaptive Cycle Engine Concludes, Proves out Transformational Capabilities. Available online: https://blog.geaviation.com/technology.

5. Patel, H.R. (2016). Parametric Cycle Analysis of Adaptive Cycle Engine. [Master’s Thesis, The University of Texas at Arlington].

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