LOW NOISE AEROENGINE INLET SYSTEM

摘要

An aeroengine is provided with a splitter apparatus (46,48,50,52) disposed in a section (44) of ain inlet duct (24). The splitter apparatus can be actuated from a stowed position to a deployed position to allow splitter(s) to selectively move from out of the inlet flow to a position extending into the inlet duct (24) to divide the inlet flow into multiple passages.