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TF30: Pratt and Whitney Mixed Flow Turbofan Engine: TF30: Pratt and Whitney Mixed Flow Turbofan Engine The TF30−P−414 engine is a mixed−flow, dual spool afterburning low−bypass turbofan designed and manufactured by Pratt and Whitney Aircraft of WestPalm Beach, Florida. The engine incorporates a nine−stage low pressure compressor including a three−stage fan driven by a three−stage low pressure turbine; and a 7−stage axial flow high−pressure compressor driven by a single−stage high−pressure turbine.
Theory of Mixing: Theory of Jet Propulsion: Jet Enough Work Performance Analysis of Mixed Turbofan Engine: Performance Analysis of Mixed Turbofan Engine P M V Subbarao Professor Mechanical Engineering Department Synthesize new Layout for better fuel Economy. The powerpoints for Jet Engine Propulsion are below. Please click on these to download.
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Details of F110-GE 400: Details of F110-GE 400 The F110−GE−400 engine is a mixed−flow, dual spool afterburning low−bypass turbofan designed and manufactured by General Electric Aircraft Engines in Lynn, Massachusetts. The engine is of modular construction, consisting of six engine modules, and an accessories gearbox. The engine incorporates a 3−stage fan driven by a two−stage low pressure turbine; and a 9−stage axial flow high−pressure compressor driven by a single−stage high−pressure turbine. To moderate engine performance at various power levels the engine features a variable geometry system. The combustor is a through flow annular type.
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The hinged flap cam−linked exhaust nozzle is hydraulically actuated. The engine−mounted accessory gearbox provides the necessary extracted power needed to drive the accessories. The engine control system regulates speeds, temperature levels and fuel flow for afterburning and non−afterburning operation.
The lubrication and ignition system are self−contained on the engine.Development was initiated April 1984 and engine was placed in service in late 1986. /duck-hunt-2-202-full-for-mac/.