Active noise control using an array of plate radiators and acoustic resonators

• US 5,590,849 A
• Filed: 12/19/1994
• Issued: 01/07/1997
• Est. Priority Date: 12/19/1994
• Status: Expired due to Term

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Pla, Frederic G.
• Primary Examiner(s): Barefoot, Galen L.
• Application Number:
  US08/359,162
• Time in Patent Office: 750 Days
• Field of Search: 244/1 N, 244/53 R, 415/119, 415/118, 181/206, 181/20, 381/71, 381/152, 381/64, 340/388.1, 340/388.3
• US Class Current: 244/1.00N
• CPC Class Codes: F02C 7/04 Air intakes for gas-turbine plants or jet-propulsion plants
• CPC Class Codes: F02K 1/00 Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto rocket nozzles F02K9/97
• CPC Class Codes: F05D 2260/962 by means of "anti-noise"
• CPC Class Codes: G10K 11/1785 Methods, e.g. algorithms; Devices G10K11/1781, G10K11/1783 take precedence
• CPC Class Codes: G10K 11/17857 Geometric disposition, e.g. placement of microphones
• CPC Class Codes: G10K 11/17883 the reference signal being derived from a machine operating condition, e.g. engine RPM or vehicle speed
• CPC Class Codes: G10K 2210/109 Compressors, e.g. fans
• CPC Class Codes: G10K 2210/1161 NMR or MRI
• CPC Class Codes: G10K 2210/121 Rotating machines, e.g. engines, turbines, motors; Periodic or quasi-periodic signals in general
• CPC Class Codes: G10K 2210/1281 Aircraft, e.g. spacecraft, airplane or helicopter
• CPC Class Codes: G10K 2210/3046 Multiple acoustic inputs, multiple acoustic outputs
• CPC Class Codes: G10K 2210/3212 Actuator details, e.g. composition or microstructure
• CPC Class Codes: G10K 2210/511 Narrow band, e.g. implementations for single frequency cancellation

Abstract

An active noise control subassembly array for reducing noise caused by a source (such as an aircraft engine). A pair of subassemblies each has a piezoceramic-driven noise radiating panel to generate a panel noise canceling at least some of the source noise. A front plate is spaced apart from the panel and has a sound exit port. A first pair of spaced-apart side walls each generally abuts the panel and the front plate so as to generally enclose a front cavity to define a resonator. A back plate is spaced apart from the panel by a second pair of side walls. The pair of subassemblies are spaced apart to create a space between their adjacent side walls. A third subassembly is similar to the pair of subassemblies but may have a different resonant frequency and is positioned such that the back plates of the subassembly pair serve as the front plate of the third subassembly with the space between the subassembly pair serving as the sound exit port of the third subassembly.

Claims

1. An active noise control subassembly array for reducing source noise caused by a source independent of said array, said array comprising:

a) a pair of active noise control subassemblies each including;

1) a piezoceramic-driven noise radiating panel bendably vibratable to generate a panel noise canceling at least a portion of the source noise and having a panel resonating frequency;

2) a front plate spaced apart from said panel, disposed generally between said source noise and said panel, and having a sound exit port;

3) a first pair of spaced-apart side walls each generally abutting said panel and said front plate so as to generally enclose a front cavity to define a resonator having a resonator resonating frequency;

4) a back plate spaced apart from said panel with said panel disposed generally between said source noise and said back plate; and

5) a second pair of spaced-apart side walls each generally abutting said panel and said back plate so as to generally enclose a back cavity, wherein said pair of subassemblies are spaced apart to create a space between adjacent side walls of said pair of subassemblies; and

b) a third active noise control subassembly including;

1) a piezoceramic-driven noise radiating sheet bendably vibratable to generate a sheet noise canceling at least a portion of the source noise and having a sheet resonating frequency, said sheet spaced apart from said back plates of said pair of subassemblies; and

2) a third pair of spaced-apart side walls each generally abutting said sheet and a corresponding back plate of said pair of subassemblies so as to generally enclose a foreground cavity to define a resonator having a resonator resonating frequency and with said space defining a sound exit port.

2. The array of claim 1, wherein said third subassembly also includes a background plate spaced apart from said sheet and further includes a fourth pair of spaced-apart side walls each generally abutting said sheet and said background plate so as to generally enclose a background cavity.

3. The array of claim 1, wherein said resonator resonating frequency of one of said pair of subassemblies is equal to generally said panel resonating frequency of said one of said pair of subassemblies and wherein said resonator resonating frequency of the other of said pair of subassemblies is equal to generally said panel resonating frequency of said other of said pair of subassemblies.

4. The array of claim 3, wherein said resonator resonating frequency of said one of said pair of subassemblies is generally equal to said resonator resonating frequency of said other of said pair of subassemblies.

5. The array of claim 4, wherein said resonator resonating frequency of said third subassembly is equal to generally said panel resonating frequency of said third subassembly.

6. The array of claim 5, wherein said resonator resonating frequency of said third subassembly is different from said resonator resonating frequency of said one of said pair of subassemblies.

7. The array of claim 6, wherein said source is an aircraft engine having a fan and wherein said front plates of said pair of subassemblies are portions of an inner wall of a fan nacelle.

8. The array of claim 7, wherein said discrete tonal noise includes first and second dominant frequencies, wherein said resonator resonating frequency of said one of said pair of subassemblies is equal to generally said first dominant frequency, and wherein said resonator resonating frequency of said third subassembly is equal to generally said second dominant frequency.

9. The array of claim 8, wherein said fan rotates about an engine centerline, wherein said pair of subassemblies is disposed generally on a first circle which has a first radius and which is coaxially aligned with said centerline, wherein said third subassembly is disposed generally on a second circle which has a second radius and which is coaxially aligned with said centerline, and wherein said second radius is longer than said first radius.

10. The array of claim 9, wherein said third subassembly also includes a background plate spaced apart from said sheet and further includes a fourth pair of spaced-apart side walls generally abutting said sheet and said background plate so as to generally enclose a background cavity.