Acoustic panel having a variable acoustic characteristic
View Patent ↗An acoustic panel includes a reflective layer, at least one alveolar structure, and an acoustically resistive structure forming an aerodynamic surface of an aircraft on the surface of which at least one acoustic wave propagates along an axis of propagation ( 24 ), whereby at least one of the characteristics of the acoustic panel influences the impedance of the panel that varies along the axis of propagation of the at least one acoustic wave, characterized in that it includes at least one first zone A with a constant acoustic impedance that is juxtaposed along the axis of propagation of the at least one acoustic wave at a zone C at which at least one characteristic of the acoustic panel that influences the impedance gradually varies along the axis of propagation of the at least one acoustic wave, whereby the characteristic has a value without sudden variations from one zone to the next.
1. An aircraft nacelle that comprises:
a duct that extends from an air intake to a rear outlet, said duct being coated by an acoustic panel that comprises a reflective layer ( 28 );
at least one alveolar structure ( 30 ); and
an acoustically resistive structure ( 32 ) that forms an aerodynamic surface of said duct on the surface of which at least on, acoustic wave propagates along an axis of propagation ( 24 ),
wherein at least one of the characteristics of the acoustic panel influences the impedance of said panel that varies along the axis of propagation ( 24 ) of said at least one acoustic wave, and
wherein at least one of the characteristics of the acoustic panel influencing the impedance is constant in a zone A disposed at the level of the air intake and has a value V 1 , is constant in a zone C disposed at the level of the outlet and has a value V 2 and varies within a zone B that separates the zones A and C passing continuously from the value V 1 to the value V 2 .
2. The aircraft nacelle according to claim 1 , wherein all of the characteristics of the acoustic panel that influence the impedance are essentially constant in a plane that is perpendicular to the axis of propagation ( 24 ).
3. The aircraft nacelle according to claim 1 , wherein the characteristic of the acoustic panel that varies is the open surface ratio.
4. The aircraft nacelle according to claim 1 , wherein the panel comprises two characteristics that vary simultaneously: the resistance to a flow at zero speed RO and a non-linearity factor NLF.