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Engine Presentation 1: Pratt & Whitney PW-100 series 1 pt Answer the following questions about the engine: 1. Give two examples of aircraft in which this engine is used. 2. What is the general type of engine? (Turboprop, turboshaft, turbojet, turbofan) 3. Describe the inlet using any of the following features that are present: 1. Bellmouth, divergent, or convergent shape 2. Variable or fixed geometry 3. Variable inlet guide vanes (VIGV) 4. Inertial (particle) separator 5. Bypass ratio 6. Bypass vanes 7. Mixed or unmixed bypass/exhaust flow 4. Describe the compressor using any of the following features that are present: 1. Style of compressor(s) (centrifugal, axial, blisk) 2. Number of compressor stages and on which shaft they are located 3. Are shafts co-rotating or counter-rotating? 4. Variable stator vanes 5. Variable bleed valve (VBV) system 5. Describe the combustor using any of the following features that are present: 1. Can, cannular, annular, or reverse flow configuration 2. Single-annular, dual-annular, or twin-annular-premixing-swirler injectors 6. Describe the turbine using any of the following features that are present: 1. Number of spools and turbine stages 2. Turbine exit guide vanes 3. Turbine blade cooling methods 7. Describe the exhaust section and thrust reversers using any of the following features that are present: 1. Exhaust duct shape (convergent, divergent) 2. Fixed or variable geometry exhaust duct 3. Mixed or unmixed exhaust and bypass airflow 4. Type and location of thrust reverser 5. Noise reduction components