Real-Time Execution of a High Fidelity Aero-Thermodynamic Turbofan Engine Simulation

Author(s):  
Igor Fuksman ◽  
Steven Sirica

In the past, a typical way of executing simulations in a real-time environment had been to use transfer function models, state-variable models, or reduced-order aero-thermodynamic models. These models are typically not as accurate as the conventional full-fidelity aero-thermodynamic simulations used as a basis for the generation of real-time models. Also, there is a cost associated with the creation and maintenance of these derived real-time models. The ultimate goal is to use the high fidelity aero-thermodynamic simulation as the real-time model. However, execution of the high fidelity aero-thermodynamic simulation in a real-time environment is a challenging objective since accuracy of the simulation cannot be sacrificed to optimize execution speed, yet execution speed still has to be limited by some means to fit into real-time constraint. This paper discusses the methodology used to resolve this challenge, thereby enabling use of a contemporary turbofan engine high fidelity aero-thermodynamic simulation in real-time environments. This publication reflects the work that was initially presented at the ASME Turbo Expo 2011 (Fuksman and Sirica, 2011, “Real-Time Execution of a High Fidelity Aero-Thermodynamic Turbofan Engine Simulation,” ASME Turbo Expo, Jun. 6-10, Vancouver, Canada, Paper No. GT2011-46661).

Author(s):  
Igor Fuksman ◽  
Steven Sirica

In the past, a typical way of executing simulations in the real-time environment had been to use transfer function models, state-variable models or reduced-order aero-thermodynamic models. These models are typically not as accurate as the conventional full-fidelity aero-thermodynamic simulations used as basis for generation of the real-time models. Also, there is a cost associated with creation and maintenance of these derived real-time models. The ultimate goal is to use the high fidelity aero-thermodynamic simulation as the real-time model. However, execution of the high fidelity aero-thermodynamic simulation in a real-time environment is a challenging objective since accuracy of the simulation cannot be sacrificed to optimize execution speed, yet execution speed still has to be limited by some means to fit into real-time constraint. This paper discusses the methodology used to resolve this challenge, thereby enabling use of a contemporary turbofan engine high fidelity aero-thermodynamic simulation in the real-time environments.


Author(s):  
Igor Fuksman ◽  
Steven Sirica

Simulating the thermodynamics of a multi-spool turbofan engine during engine start can present challenges to the conventional high fidelity aero-thermodynamic simulation. The conventional high fidelity aero-thermodynamic simulation uses an iterative solver technique to preserve flow continuity and conservation of energy based on component maps and subsystem characteristics. Traditionally, operation of such simulations have been limited to regions from self-sustaining idle to maximum power, where component and subsystem representation has been well defined and engine operating pressures are sufficient to ensure one-directional flow. However, simulating transient operation which initiates from engine “off” condition followed by starter engagement and fuel introduction, presents a new set of challenges. These include the modeling of the engine “off” state itself, as well as two aspects of the starting process particular to a multi-spool turbofan: the modeling of the flow passing through the entire core stream even though only the high pressure shaft is rotating, and the modeling of the flow split into the bypass stream when the fan is not rotating. This paper discusses the modeling techniques that have been developed to overcome these challenges in order to ensure the smooth operation starting with engine off and continuing through the regions of starter engagement, fuel addition, and starter disengagement leading to normal engine operating regime.


Author(s):  
Naveed U. Rahman ◽  
James F. Whidborne

This paper presents a transient three-spool turbofan engine simulation model that uses a combination of intercomponent volume and iterative techniques. The engine model runs in real time and has been implemented in MATLAB/SIMULINK environment. The main advantage of this hybrid approach is that it preserves the accuracy of the iterative method while maintaining the simplicity of the intercomponent volume method. The iterative approach is applied at each engine subsystem to solve algebraic thermodynamic equations for exit enthalpy, entropy, and temperature, whereas the intercomponent volume method is used to calculate pressures derivatives and hence pressures at corresponding engine stations. This allows the engine state vector to be updated at each pass through the engine calculations. This technique was applied as a test case on the Rolls Royce Trent 500 three-spool turbofan engine, and the results were compared with an iterative method. As the engine state vector is updated during each cycle, the model lends itself for easy integration into nonlinear aircraft simulations, real-time engine diagnostics/prognostics, and jet engine control applications.


2021 ◽  
Vol 157 ◽  
pp. 107720
Author(s):  
Christina Insam ◽  
Arian Kist ◽  
Henri Schwalm ◽  
Daniel J. Rixen
Keyword(s):  

1997 ◽  
Vol 31 (3) ◽  
pp. 45-51
Author(s):  
Jianmin Hou ◽  
Xuandong Li ◽  
Xiaocong Fan ◽  
Guoliang Zheng
Keyword(s):  

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