Device for reducing noise from jet-pylon interactions on jet engines
An engine and hanger technology, which is applied to jet power units, exhaust ports of power units, drag reduction, etc., and can solve the problems of not solving noise problems, not solving problems
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[0031] refer to figure 1 , figure 1 Shown is an engine 1 of the twin-flow or bypass turbojet type, from which there emerges a main or hot flow 2 and a secondary or bypass flow, also called cold flow 3 . The hot flow leaves the engine 1 at the primary exhaust pipe 4 , while the cold flow exits at the secondary exhaust pipe 5 . The engine 1 is connected via a supporting pylon 7 to the wing 6 of an aircraft (not shown). The pylon 7 is generally flat in shape, having an upper surface connected to the aircraft, shown here as two sides generally perpendicular and parallel to each other, and a lower or bottom surface. rectifier 20, in Figure 5 As can be seen in , a connection is formed between the side of the pylon 7 and the top of the main exhaust duct 4 to ensure a clean aerodynamic flow at the junction between these two elements. The pylon 7 extends longitudinally, ie in the direction of air flow around the engine, downstream of the exit faces of the exhaust pipes 4 and 5 of ...
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