Active combustion control (ACC) has been proved to be an effective method for the
suppression of pressure oscillation in aero engine combustion chambers, which will …

Abstract A Cyber–Physical System (CPS) comprises physical as well as software
subsystems. Simulation-based approaches are typically used to support design and …

The fuel system is one of the most important and complex parts of aircraft, being tasked with
suppling the correct quantity of fuel to the aircraft engine during all operative conditions, from …

A thermal model of bistable permanent magnet actuator (BPMA) was established and
verified using multiphysics methodology. By treating the nonsimplified energy consumption …

Aiming at the adverse effects of strong nonlinearity and high uncertainty existing in the gas
path performance deterioration assessment of turbofan engines, in contrast to previously …

Turboshaft gas turbine engine is one of the main components in most marine vehicle
propulsion systems. The most important part of the turboshaft engines, which has direct …

Fuel flow rate is the most important and most used control parameter for aero engines and it
is assured by a device called the fuel control unit (FCU). To investigate factors that …

The quantitative analysis of the uncertainty influence on thermodynamic parameters and
performance parameters is usually difficult to achieve due to the strong nonlinear working …

In the hardware-in-the-loop (HIL) simulation of the fuel control unit (FCU) for aero-engines,
the back pressure has a great impact on the metered fuel, thus influencing the confidence of …

The correct operation of a gas turbine engine depends on the accurate and stable
performance of fuel control system and its components such as fuel control unit. Fuel control …