An air intake unit (3) for an engine of an aircraft (1); the intake unit (3) has: a tubular housing (4); a first inlet opening (7) which is obtained through an outer wall (6) of the tubular housing (4) and through which external air can be taken in; an air filter (8) which engages the first inlet opening (7); a second inlet opening (9) which is obtained through the outer wall (6) of the tubular housing (4) and through which external air can be taken in; a shutter device (10) which is coupled to the second inlet opening (9) and is movable between a closed position, in which it closes the second inlet opening (9), and an open position, in which it sets the passage through the second inlet opening (9) free; and an actuator (11), which moves the shutter device (10).
AIR INTAKE UNIT FOR AN ENGINE OF AN AIRCRAFT
LUFTEINLASSEINHEIT FÜR EINEN MOTOR EINES FLUGZEUGES
UNITÉ D'ADMISSION D'AIR POUR UN MOTEUR D'AÉRONEF
2019-09-11
Patent
Electronic Resource
English