The invention discloses a helicopter ducted
tail rotor
noise reduction lining for low-frequency line spectrum
noise suppression, and belongs to the technical field of helicopter ducted
tail rotor
noise reduction. Ducted
tail rotor noise belongs to multi-line spectrum
harmonic noise, and
noise energy is reduced along with increase of frequency, that is, the
noise energy is concentrated in first two-order
harmonic waves. And on the other hand, the ducted
tail rotor is low in rotating speed and small in blade number, so that the noise frequency is low. The micro-perforated plate composite folding back cavity is used as the sound absorption unit, and two sound absorption
resonance frequencies of the sound absorption unit coincide with the first two orders of
harmonic noise of the
tail rotor through
parameter design, so that the thickness of the whole sound absorption unit is reduced, and meanwhile, the low-frequency multi-line-spectrum
noise reduction performance is achieved; the weight cost is reduced, and the
tail rotor noise is effectively restrained.