Modeling of Start Up From Engine Off Conditions Using High Fidelity Turbofan Engine SimulationsSource: Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005::page 51201DOI: 10.1115/1.4031474Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Engine models are widely used to simulate the engine behavior at steady state and transient operating conditions over the full flight envelope. Within the engine development process such simulations are used to support component design, evaluate engine performance, operability and test data, as well as to develop and optimize the engine controls. Recent developments have raised interest in the modeling of startup processes of turbofan engines in order to support the definition of sufficient engine control laws. This implies that simulations are started at a condition where the engine shafts are static and temperatures and pressures are equal to ambient. During startup the engine can only be operated transiently through the subsubidle region (near zero speed) using a starter torque. The activity presented here was targeted to support the development of industrialstandard highfidelity turbofan engine models capable of simulating startup, shutdown or windmilling operation. Within the three previously mentioned cases starting from an engineoff condition, ground start from zerospeed is the most challenging in terms of physical and numerical modeling. For this reason, this paper concentrates on that case only. Zero mass flow and speed at the beginning of the simulation impose a set of special problems that do not exist in standard simulations: the modeling of a static engineoff condition, the modeling of static friction, and the modeling of reverse flows. The requirement to support an existing industrial model development process also made it necessary to apply the same quality of physical modeling to startup simulations as would be the case for aboveidle engine simulations. The physical effects present during engine start are discussed and modeling solutions are presented. Finally, results of a dry crank simulation are presented and discussed, illustrating that the expected effects are present and that the simulation is capable of predicting the correct trends.
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| contributor author | Bretschneider, Stefan | |
| contributor author | Reed, John | |
| date accessioned | 2017-05-09T01:28:19Z | |
| date available | 2017-05-09T01:28:19Z | |
| date issued | 2016 | |
| identifier issn | 1528-8919 | |
| identifier other | gtp_138_05_051201.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/161052 | |
| description abstract | Engine models are widely used to simulate the engine behavior at steady state and transient operating conditions over the full flight envelope. Within the engine development process such simulations are used to support component design, evaluate engine performance, operability and test data, as well as to develop and optimize the engine controls. Recent developments have raised interest in the modeling of startup processes of turbofan engines in order to support the definition of sufficient engine control laws. This implies that simulations are started at a condition where the engine shafts are static and temperatures and pressures are equal to ambient. During startup the engine can only be operated transiently through the subsubidle region (near zero speed) using a starter torque. The activity presented here was targeted to support the development of industrialstandard highfidelity turbofan engine models capable of simulating startup, shutdown or windmilling operation. Within the three previously mentioned cases starting from an engineoff condition, ground start from zerospeed is the most challenging in terms of physical and numerical modeling. For this reason, this paper concentrates on that case only. Zero mass flow and speed at the beginning of the simulation impose a set of special problems that do not exist in standard simulations: the modeling of a static engineoff condition, the modeling of static friction, and the modeling of reverse flows. The requirement to support an existing industrial model development process also made it necessary to apply the same quality of physical modeling to startup simulations as would be the case for aboveidle engine simulations. The physical effects present during engine start are discussed and modeling solutions are presented. Finally, results of a dry crank simulation are presented and discussed, illustrating that the expected effects are present and that the simulation is capable of predicting the correct trends. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Modeling of Start Up From Engine Off Conditions Using High Fidelity Turbofan Engine Simulations | |
| type | Journal Paper | |
| journal volume | 138 | |
| journal issue | 5 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.4031474 | |
| journal fristpage | 51201 | |
| journal lastpage | 51201 | |
| identifier eissn | 0742-4795 | |
| tree | Journal of Engineering for Gas Turbines and Power:;2016:;volume( 138 ):;issue: 005 | |
| contenttype | Fulltext |