# US 5,702,230 A · Actively controlled acoustic treatment panel

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- Number: US 5,702,230 A
- Document ID: US5702230A
- Status: Granted
- Kind: A
- Application number: 08/603,850
- Filed: 1996-01-29
- Granted: 1997-12-30
- Earliest claimed: 1996-01-29
- Assignees: General Electric Company
- Inventors: Robert E. Kraft; Asif A. Syed
- Web page: https://patentgrep.com/patent/US5702230A

## CPC

- F02C 7/045: having provisions for noise suppression
- F01D 25/04: Antivibration arrangements
- F02K 1/827: {Sound absorbing structures or liners}
- G10K 11/1785: {Methods, e.g. algorithms; Devices (G10K11/1781, G10K11/1783 take precedence)}
- G10K 11/17857: {Geometric disposition, e.g. placement of microphones}
- G10K 11/17861: {using additional means for damping sound, e.g. using sound absorbing panels}
- G10K 11/17873: {using a reference signal without an error signal, e.g. pure feedforward}
- B64D 2033/0206: {comprising noise reduction means, e.g. acoustic liners}
- B64D 2033/0286: {for turbofan engines}
- F05D 2260/96: Preventing, counteracting or reducing vibration or noise
- G10K 2210/107: Combustion, e.g. burner noise control of jet engines
- G10K 2210/109: Compressors, e.g. fans
- G10K 2210/1281: Aircraft, e.g. spacecraft, airplane or helicopter
- G10K 2210/3046: Multiple acoustic inputs, multiple acoustic outputs
- G10K 2210/3224: Passive absorbers
- G10K 2210/3227: Resonators
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F02K: JET-PROPULSION PLANTS (features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C7/00, F02C9/00)
- G10K: SOUND-PRODUCING DEVICES; METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING, NOISE OR OTHER ACOUSTIC WAVES IN GENERAL; ACOUSTICS NOT OTHERWISE PROVIDED FOR
- B64D: EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

An actively controlled acoustic treatment panel for suppressing noise in a gas turbine engine nacelle including a backsheet formed by a planar matrix of adjacent individually controllable elements, where each of the controllable elements has a transducer and a honeycomb cell enclosing the transducer. A facesheet is also bonded to the controllable elements. A plurality of sensors are positioned within the acoustic treatment panel for sensing acoustic pressure of the noise propagated against the facesheet. A driver is provided for electrically driving each of the transducers to effect displacement thereof in a direction substantially perpendicular to the facesheet. Circuitry is also operatively connected to the pressure sensors and the driver for controlling velocity magnitude and phase of the transducers during displacement, wherein a resulting acoustic impedance at the facesheet achieves a desired acoustic impedance boundary condition at the nacelle. The transducer is further made up of an inner lamination layer, an outer lamination layer, and a piezoelectric membrane positioned between the inner and outer lamination layers, wherein a plurality of aligned openings are provided in the inner and outer lamination layers so that the piezoelectric membrane can be displaced either toward or away from the facesheet.

## Claims

### Claim 1

An actively controlled acoustic treatment panel for suppressing noise in a gas turbine engine nacelle, comprising:
(a) a piezoelectric membrane;
(b) a plurality of interconnected honeycomb members having a first end positioned adjacent a radially inner surface of said piezoelectric membrane and a second end spaced from said first end to form a cavity between said piezoelectric membrane and said second honeycomb member end, wherein a circumferential matrix of adjacent individually controllable elements is formed within the boundary of each honeycomb member;
(c) a facesheet bonded to said second end of said interconnected honeycomb members;
(d) a plurality of sensors positioned within said acoustic treatment panel for sensing acoustic pressure of said noise propagated against said facesheet;
(e) means for electrically driving each of said individually controllable elements to effect displacement in a direction substantially perpendicular to said facesheet; and
(f) means operatively connected to said pressure sensors and said driving means for controlling velocity magnitude and phase of said individually controllable elements during displacement, wherein a resulting acoustic impedance at said facesheet achieves a desired acoustic impedance boundary condition at said nacelle.

### Claim 2 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein each said honeycomb member is substantially hexagonal.

### Claim 3 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, further comprising a rigid backplate positioned adjacent a radially outer surface of said piezoelectric membrane.

### Claim 4 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, further comprising means for acquiring and processing spectral data from said pressure sensors.

### Claim 5 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said interconnected honeycomb members and said facesheet are assembled into a continuous ring and mounted circumferentially around said nacelle.

### Claim 6 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, further comprising:
(a) a first lamination layer positioned adjacent said inner radial surface of said piezoelectric membrane; and
(b) a second lamination layer positioned adjacent an outer radial surface of said piezoelectric membrane;
wherein a plurality of aligned openings are provided in said first and second lamination layers so that said piezoelectric membrane can be displaced either toward or away from said facesheet.

### Claim 7 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said acoustic impedance includes positive resistance and negative reactance.

### Claim 8 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said acoustic impedance includes negative resistance.

### Claim 9 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said acoustic impedance is substantially constant circumferentially across said treatment panel.

### Claim 10 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said acoustic impedance is varied circumferentially across said treatment panel.

### Claim 11 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said acoustic impedance is provided adaptively across said treatment panel in response to locally sensed pressure fields by said sensors.

### Claim 12 (depends on 1)

The actively controlled acoustic treatment panel of claim 1, wherein said treatment panel is able to suppress said noise in a frequency range of approximately 800 to approximately 8,000 Hertz.