Post-combustion emissions control in aero-gas turbine engines

Low Emission Combustion Technology for Stationary Gas Turbine Engines

The need to control exhaust emissions from stationary power sources is dictated by environmental regulations that limit the amount of smoke (particulates), sulfur dioxide, carbon monoxide, hydrocarbons, and oxides of nitrogen or NOx that can be exhausted into the atmosphere. In areas where atmospheric pollution is a serious concern, as in the Los Angeles basin, very low emission levels are dema...

Distributed Control Systems for Aero Gas Turbine Engines: A wicked problem for systems engineering?

Present day jet engines are controlled and monitored by a series of hydraulic, fueldraulic, electrical and pneumatic sub-systems known as the Full Authority Digital Engine Controller (FADEC). At the heart of the FADEC lies a centralised Electronic Engine Controller (EEC) responsible for control and safety of the wider engine system. It has long been postulated that a distributed EEC would contr...

Investigation and Modeling of Combustion instabilities in Aero Engines

Combustion instability results from a coupling between acoustic and heat release fluctuations. From the analysis of published works by various research teams including ONERA, this paper describes the coupling lines involved, the model used to describe it and the methods developed to predict the thermo-acoustic risks. The application is focused on the liquid-fueled aero engine specificities. Rec...

Understanding and Control of Combustion Dynamics in Gas Turbine

Verifiable Control System Development for Gas Turbine Engines

A control software verification framework for gas turbine engines is developed. A stability proof is presented for gain scheduled closed-loop engine system based on global linearization and linear matrix inequality (LMI) techniques. Using convex optimization tools, a single quadratic Lyapunov function is computed for multiple linearizations near equilibrium points of the closed-loop system. Wit...