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Gas turbine engine comprising a nacelle compartment plenum for bleed air flow delivery system
Gas turbine engine comprising a nacelle compartment plenum for bleed air flow delivery system
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机译:包括用于引气流输送系统的机舱室增压室的燃气涡轮发动机
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摘要
A gas turbine engine (10) is provided with a nacelle (100) having a hollow inner space (120). The inner space (120) is utilized as a plenum for directing air from an inlet (116) to an outlet (104) at the upstream end (99) of the nacelle (100) to allow control of an effective lip width of the nacelle (100) under certain flight conditions.
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