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High-fidelity simulation of turbofan engine. ; Verification and improvement of model's dynamical characteristics in linear operating range. Turbofan engine no koseito simulation. ; Senkei sado han'i ni okeru model dotokusei no kensho to seido kojo ni tsuite

Abstract

This paper describes providing pulse inputs to a fuel supply in trial operation of a turbofan engine, measurement of its response, and calculation of the frequency characteristics and time constants to acquire dynamic characteristics of the engine on the ground. The resultant engine characteristics were compared with the model characteristics of numerically analyzing a mathematical simulation model, and corrected to develop a high-accuracy simulation model. An element model and a dynamics model were prepared in detail on the main engine components, such as fans, a compressor, a combustor, and a turbine, along a flow diagram from the air intake opening to the exhaust nozzle. The pulses were inputted into the fuel supply by opening and closing an electromagnetic valve. Closing of the illustrated electromagnetic valve for about 0.7 second caused a difference (of phase and trend) in both characteristics of high and low frequencies as a result of pulse-like change in the flow rate. To correct the model characteristics, the combustion delay tie was set to 0.02 second upon considering the combustion delay time relative to the heat capacity of the combustor. Improvement in the model was verified as the phase characteristics was approximated to the engine characteristics. 13 refs.,  More>>
Authors:
Yamane, H; Kagiyama, S [1] 
  1. Defence Agency, Tokyo (Japan)
Publication Date:
Sep 25, 1993
Product Type:
Journal Article
Reference Number:
NEDO-93-913276; EDB-94-036661
Resource Relation:
Journal Name: Nippon Kikai Gakkai Ronbunshu. B Hen (Transactions of the Japan Society of Mechanical Engineers. Part B); (Japan); Journal Volume: 59:565
Subject:
33 ADVANCED PROPULSION SYSTEMS; 99 GENERAL AND MISCELLANEOUS//MATHEMATICS, COMPUTING, AND INFORMATION SCIENCE; FLUID FLOW; AXIAL SYMMETRY; PULSE COMBUSTION; FREQUENCY ANALYSIS; TIME DEPENDENCE; TURBOFAN ENGINES; SIMULATION; BLOWERS; COMBUSTORS; FUEL FEEDING SYSTEMS; GAS TURBINES; MATHEMATICAL MODELS; THERMODYNAMICS; CHEMICAL REACTIONS; COMBUSTION; ENGINES; EQUIPMENT; FUEL SYSTEMS; HEAT ENGINES; INTERNAL COMBUSTION ENGINES; MACHINERY; OXIDATION; SYMMETRY; THERMOCHEMICAL PROCESSES; TURBINES; TURBOMACHINERY; 330100* - Internal Combustion Engines; 990200 - Mathematics & Computers
OSTI ID:
5500708
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
Journal ID: ISSN 0387-5016; CODEN: NKGBDD
Submitting Site:
NEDO
Size:
Pages: 306-313
Announcement Date:
Mar 15, 1994

Citation Formats

Yamane, H, and Kagiyama, S. High-fidelity simulation of turbofan engine. ; Verification and improvement of model's dynamical characteristics in linear operating range. Turbofan engine no koseito simulation. ; Senkei sado han'i ni okeru model dotokusei no kensho to seido kojo ni tsuite. Japan: N. p., 1993. Web.
Yamane, H, & Kagiyama, S. High-fidelity simulation of turbofan engine. ; Verification and improvement of model's dynamical characteristics in linear operating range. Turbofan engine no koseito simulation. ; Senkei sado han'i ni okeru model dotokusei no kensho to seido kojo ni tsuite. Japan.
Yamane, H, and Kagiyama, S. 1993. "High-fidelity simulation of turbofan engine. ; Verification and improvement of model's dynamical characteristics in linear operating range. Turbofan engine no koseito simulation. ; Senkei sado han'i ni okeru model dotokusei no kensho to seido kojo ni tsuite." Japan.
@misc{etde_5500708,
title = {High-fidelity simulation of turbofan engine. ; Verification and improvement of model's dynamical characteristics in linear operating range. Turbofan engine no koseito simulation. ; Senkei sado han'i ni okeru model dotokusei no kensho to seido kojo ni tsuite}
author = {Yamane, H, and Kagiyama, S}
abstractNote = {This paper describes providing pulse inputs to a fuel supply in trial operation of a turbofan engine, measurement of its response, and calculation of the frequency characteristics and time constants to acquire dynamic characteristics of the engine on the ground. The resultant engine characteristics were compared with the model characteristics of numerically analyzing a mathematical simulation model, and corrected to develop a high-accuracy simulation model. An element model and a dynamics model were prepared in detail on the main engine components, such as fans, a compressor, a combustor, and a turbine, along a flow diagram from the air intake opening to the exhaust nozzle. The pulses were inputted into the fuel supply by opening and closing an electromagnetic valve. Closing of the illustrated electromagnetic valve for about 0.7 second caused a difference (of phase and trend) in both characteristics of high and low frequencies as a result of pulse-like change in the flow rate. To correct the model characteristics, the combustion delay tie was set to 0.02 second upon considering the combustion delay time relative to the heat capacity of the combustor. Improvement in the model was verified as the phase characteristics was approximated to the engine characteristics. 13 refs., 17 figs., 2 tabs.}
journal = []
volume = {59:565}
journal type = {AC}
place = {Japan}
year = {1993}
month = {Sep}
}