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AIRCRAFT ENGINE ASSEMBLY COMPRISING A PYLON LEADING EDGE INCORPORATED WITH AN ANNULAR ROW OF UNFAIRED AFTER-GUIDE VANES
AIRCRAFT ENGINE ASSEMBLY COMPRISING A PYLON LEADING EDGE INCORPORATED WITH AN ANNULAR ROW OF UNFAIRED AFTER-GUIDE VANES
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机译:飞机发动机总成,其主塔缘与未导向的后导翼环行结合
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摘要
To reduce the overall mass of an engine assembly for aircraft, this assembly comprises a part of the fuselage of an aircraft, a turbomachine comprising an unfaired propeller, together with an annular row of unfaired after-guide vanes located aft of the propeller and rotationally fixed in relation to a longitudinal axis of the turbomachine, and a mounting pylon. At least part of the leading edge of the pylon is incorporated within the annular row between two after-guide vanes.
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