Aircraft with two engines having by-pass air inlet openings and bleed air outlets as well as engine for an aircraft

摘要

The invention relates to an aircraft (1) having at least one first and one second engine (3a, 3b), each engine comprising a main air inlet opening, a by-pass air inlet opening (15a) and a bleed air outlet (18a, 18b), said main air inlet opening being provided with an inlet barrier filter for filtering a main air stream through said main air inlet opening into the engine (3a, 3b), said by-pass air inlet opening (15a) being provided with a by-pass door (15) that is operable by an associated operating element (17) to enable a by-pass air stream through said by-pass air inlet opening into the engine (3a, 3b), and said bleed air outlet (18a, 18b) being provided for creating an outgoing bleed air stream (18c, 18d) going out of the engine in operation, at least one associated operating element (17) being controllable by an outgoing bleed air stream (18c, 18d).