Search
Now showing items 1-7 of 7
Approximate Nonlinear Modeling and Feedback Linearization Control for Aeroengines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper aims to develop an applicable nonlinear control technique for aeroengines. An approximate nonlinear model is presented and a rational identification procedure is given. Exact input-output ...
Multiobjective Robust Regulating and Protecting Control for Aeroengines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The multiobjective regulating and protecting control method presented here will enable improved control of multiloop switching control of an aeroengine. The approach is based on switching control ...
Experimental Study on Fault Caused by Partial Arc Steam Forces and Its Economic Solution
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: It is noticed in a few steam turbines that there are a pad temperature rise of more than 10°C and a radial journal movement of more than 50 μm in the bearings adjacent to control ...
Early Fault Detection of Hot Components in Gas Turbines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The working environment of hot components is the most adverse of all gas turbine components. Malfunction of hot components is often followed by catastrophic consequences. Early fault detection plays a significant role in ...
Establishment of Nonlinear Dynamic Model for Prediction of Rotordynamic Instability of Steam Turbine Rotor-Bearing System Caused by Partial Admission
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A nonlinear dynamic model is developed for a rotor-bearing system with radial steam force due to partial admission, taking into account the prediction of subsynchronous instability of a steam ...
A Novel Degree of Observability Used for Measurement Selections in Gas Path Diagnostics
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A novel method for measurement selections of gas path diagnostics has been developed. This method is based on the singular value decomposition of the observability matrix of linear systems, ...
Ignition Characteristics of a Liquid-Kerosene-Fueled Scramjet during Air Throttling Combined with a Gas Generator
Publisher: American Society of Civil Engineers
Abstract: The ignition characteristics of a flush wall, liquid-kerosene-fueled scramjet combustor are tested in a directly connected ground test rig. The total temperature and Mach number of the vitiated airflow at the exit of the ...