Results 11 to 20 of about 16,739 (234)

Active Jet Noise Control of Turbofan Engine Based on Explicit Model Predictive Control

open access: yesApplied Sciences, 2022
The active jet noise control received significant attention due to the little influence it has on the engine performance. The active jet noise control is a multivariable problem because it needs to achieve the simultaneous closed-loop control of jet ...
Runmin Ji, Xianghua Huang, Xiaochun Zhao
doaj   +1 more source

Research of Comprehensive Modeling of Two-Dimensional Vector Nozzle/Actuator Load/Turbofan Engine

open access: yesIEEE Access, 2023
To investigate the effect of the dynamic deflection process of a two-dimensional vector nozzle on its actuator load and engine performance, a comprehensive modeling method of two-dimensional vector nozzle/actuator load/turbofan engine is proposed ...
Yuan Wang   +3 more
doaj   +1 more source

Transient Analysis and Safety Assessment of Turbofan Engine Structures during Bird Ingestion

open access: yesInternational Journal of Aerospace Engineering, 2020
The high bypass ratio turbofan engine’s load-carrying structure transient response during bird ingestion was analyzed in accordance with the engine bird ingestion certification regulations, the principles of structural safety assessment were represented,
Gang Luo   +4 more
doaj   +1 more source

A Linearization Model of Turbofan Engine for Intelligent Analysis Towards Industrial Internet of Things

open access: yesIEEE Access, 2019
Big data processing technologies, e.g., multi-sensor data fusion and cloud computing are being widely used in research, development, manufacturing, health monitoring and maintenance of aero-engines, driven by the ever-rapid development of intelligent ...
Linfeng Gou   +5 more
doaj   +1 more source

Energy Optimization Analysis of Turbofan Engine for More-Electric Civil Aircraft

open access: yesIEEE Access, 2020
The civil aviation industry is moving into the more-electric environment where the civil aircraft uses electricity to meet the multiple energy demands of the associated aircraft subsystems.
Yuanchao Yang, Hao Li, Chen Yu
doaj   +1 more source

Design Considerations of Low Bypass Ratio Mixed Flow Turbofan Engines with Large Power Extraction

open access: yesFluids, 2022
The possibility of extracting large amounts of electrical power from turbofan engines is becoming increasingly desirable from an aircraft perspective. The power consumption of a future fighter aircraft is expected to be much higher than today’s fighter ...
Daniel Rosell, Tomas Grönstedt
doaj   +1 more source

Performance Estimation and Fault Diagnosis Based on Levenberg–Marquardt Algorithm for a Turbofan Engine

open access: yesEnergies, 2018
Establishing the schemes of accurate and computationally efficient performance estimation and fault diagnosis for turbofan engines has become a new research focus and challenges.
Junjie Lu, Feng Lu, Jinquan Huang
doaj   +1 more source

Improved Thrust Performance Optimization Method for UAVs Based on the Adaptive Margin Control Approach

open access: yesMathematics, 2023
This study proposes a strategy for improving the thrust performance of fixed-wing UAV turbine engines from the perspective of aircraft/engine integration.
Yeguang Wang, Honglin Liu, Kai Liu
doaj   +1 more source

PD-14 – is it so good?

open access: yesАвіаційно-космічна техніка та технологія, 2022
The introductory part of the article provides information about the features of the modern Russian aircraft and engine designations, about the disappearance of the world famous brands such as "Tu", "Yak", "PS", "NK" and others.
Vadym Nerubasskyi
doaj   +1 more source

MODELING OF THRUST AND SPECIFIC FUEL CONSUMPTION FOR A TURBOFAN ENGINE VIA GMDH-TYPE NEURAL NETWORKS [PDF]

open access: yesمجله مدل سازی در مهندسی, 2012
In this paper, Group Method of Data Handling (GMDH)-type neural networks based on Genetic Algorithm, as an effective means to model the complex and nonlinear system, used for the modeling of turbofan engine.
مسیح Sharifi   +2 more
doaj   +1 more source

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