Systems and Methodologies for Achieving Acoustic Cancellation in Synthetic Jet Ejectors
A system is provided for producing synthetic jets. The system comprises a first synthetic jet ejector equipped with a first diaphragm which operates at a first frequency f 1 , and a second synthetic jet ejector equipped with a second diaphragm which operates at a second frequency f 2 . The first and second synthetic jet ejectors are positioned with respect to each other such that the sound intensity of at least one of the first and second synthetic jet ejectors is reduced through destructive interference, wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 20≦φ≦60.
1 . A system for producing synthetic jets, comprising:
a synthetic jet ejector comprising a first diaphragm which operates at a first frequency f 1 ; and
an acoustical speaker comprising a second diaphragm which operates at a second frequency f 2 ;
wherein the acoustical speaker is adapted to reduce the sound intensity of the synthetic jet ejector through destructive interference.
2 . The system of claim 1 , wherein f 1 and f 2 are the same frequency.
3 . The system of claim 2 , wherein f 1 and f 2 have the same amplitude.
4 . The system of claim 3 , wherein f 1 and f 2 are out-of-phase.
5 . The system of claim 3 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 20≦φ≦60.
6 . The system of claim 3 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 30≦φ≦50.
7 . The system of claim 3 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 35≦φ≦45.
8 . A method for reducing the sound intensity of a synthetic jet ejector, comprising:
providing a synthetic jet ejector comprising a first diaphragm;
providing an acoustical speaker comprising a second diaphragm;
operating the synthetic jet ejector such that the first diaphragm vibrates at a first frequency f 1 ; and
operating the acoustical speaker such that the second diaphragm vibrates at a second frequency f 2 ;
wherein the acoustical speaker is positioned with respect to the synthetic jet ejector such that the sound intensity of the synthetic jet ejector is reduced through destructive interference between the first and second frequencies.
9 . The method of claim 8 , wherein f 1 and f 2 are the same frequency.
10 . The method of claim 9 , wherein f 1 and f 2 have the same amplitude.
11 . The method of claim 10 , wherein f 1 and f 2 are out-of-phase.
12 . The method of claim 10 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 20≦φ≦60.
13 . The method of claim 10 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 30≦φ≦50.
14 . The method of claim 10 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 35≦φ≦45.
15 . A system for producing synthetic jets, comprising:
a first synthetic jet ejector equipped with a first diaphragm which operates at a first frequency f 1 ; and
a second synthetic jet ejector equipped with a second diaphragm which operates at a second frequency f 2 ;
wherein the first and second synthetic jet ejectors are positioned with respect to each other such that reduce the sound intensity of the synthetic jet ejector through destructive interference, wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 20≦φ≦60.
16 . The system of claim 15 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 30≦φ≦50.
17 . The system of claim 15 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 35≦φ≦45.
18 . A method for producing synthetic jets, comprising:
providing a first synthetic jet ejector equipped with a first diaphragm which operates at a first frequency f 1 , and a second synthetic jet ejector equipped with a second diaphragm which operates at a second frequency f 2 ; and
positioning the first and second synthetic jet ejectors with respect to each other such that the sound intensity of the synthetic jet ejectors is reduced through destructive interference, wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 20≦φ≦60.
19 . The method of claim 18 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 30≦φ≦50.
19 . The method of claim 18 , wherein f 1 and f 2 are out-of-phase by φ degrees, and wherein 35≦φ≦45.
20 . A method for reducing the acoustical footprint of a synthetic jet ejector having a synthetic jet actuator, comprising:
determining the velocity output of the synthetic jet ejector;
determining a transform G(z) which operates on the input to the synthetic jet actuator to produce the velocity output;
calculating an inverse transform G′(z) corresponding to G(z);
verifying G′(z) by reproducing the actuator input from the velocity output; and
using G′(z) to determine an input for the synthetic jet actuator which will reduce the acoustical footprint of the synthetic jet ejector.
21 . The method of claim 20 , wherein the actuator input is sinusoidal.
22 . The method of claim 20 , wherein reducing the acoustical footprint of the synthetic jet actuator involves reducing the tonality of the synthetic jet actuator.