The baseline engine control requirements were generated from previous control design experience. The control requirements for the 680-B1 (next generation engine) were then generated from a top down analysis of mission (weapon system), aircraft, and engine requirements. The performance, operability, and engine component life parameters were then varied to determine the trade-offs with each other. It was clearly demonstrated that the control logic can perform trade-offs in these parameters through the choices made throughout the logic design procedure. (Author)
Performance, Life, and Operability Trade-Offs in VCE (Variable Cycle Engine) Control Logic Design
1981
154 pages
Report
No indication
English
Jet & Gas Turbine Engines , Aircraft , Variable cycle engines , Turbines , Control systems , Logic devices , Trade off analysis , Aircraft engines , Mechanical engineering , Control , Requirements , Performance(Engineering) , Operation , Missions , Simulation , Test methods , Engine components , Turbojet engines , Optimization , Steady state , Life expectancy
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