AIRCRAFT WITH AN ENGINE HAVING A BY-PASS AIR INLET OPENING AND A BLEED AIR OUTLET

摘要

An aircraft having at least one first and one second engine, each engine comprising a main air inlet opening, a by-pass air inlet opening and a bleed air outlet, 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, said by-pass air inlet opening being provided with a by-pass door that is operable by an associated operating element to enable a by-pass air stream through said by-pass air inlet opening into the engine, and said bleed air outlet being provided for creating an outgoing bleed air stream going out of the engine in operation, at least one associated operating element being controllable by an outgoing bleed air stream.

主权项

1. An aircraft having at least one first and one second engine, each engine comprising a main air inlet opening, a by-pass air inlet opening and a bleed air outlet, 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, said by-pass air inlet opening being provided with a by-pass door that is operable by an associated operating element to enable a by-pass air stream through said by-pass air inlet opening into the engine, and said bleed air outlet being provided for creating an outgoing bleed air stream going out of the engine in operation, characterized in that the associated operating element of the at least one first engine is connected to the bleed air outlet of the at least one second engine and controllable by the outgoing bleed air stream that goes out of the at least one second engine in operation, and the associated operating element of the at least one second engine is connected to the bleed air outlet of the at least one first engine and controllable by the outgoing bleed air stream that goes out of the at least one first engine in operation.