Frequency-focused actuators for active vibrational energy control systems

• US 5,754,662 A
• Filed: 11/30/1994
• Issued: 05/19/1998
• Est. Priority Date: 11/30/1994
• Status: Expired due to Term

• Current Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Original Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Inventors: Jolly, Mark R., Southward, Steve C., Norris, Mark A., Swanson, Douglas A., Rossetti, Dino J.
• Primary Examiner(s): Kuntz, Curtis
• Assistant Examiner(s): Mei, Xu
• Application Number:
  US08/347,521
• Time in Patent Office: 1,266 Days
• Field of Search: 381/71, 381/94
• US Class Current: 381/71.4
• CPC Class Codes: G10K 11/17823 Reference signals, e.g. ambient acoustic environment
• CPC Class Codes: G10K 11/17825 Error signals
• CPC Class Codes: G10K 11/17854 the filter being an adaptive filter
• CPC Class Codes: G10K 11/17857 Geometric disposition, e.g. placement of microphones
• CPC Class Codes: G10K 11/17881 the reference signal being an acoustic signal, e.g. recorded with a microphone
• CPC Class Codes: G10K 2210/128 Vehicles
• CPC Class Codes: G10K 2210/3027 Feedforward
• CPC Class Codes: G10K 2210/3028 Filtering, e.g. Kalman filters or special analogue or digital filters
• CPC Class Codes: G10K 2210/3046 Multiple acoustic inputs, multiple acoustic outputs
• CPC Class Codes: G10K 2210/509 Hybrid, i.e. combining different technologies, e.g. passive and active
• CPC Class Codes: G10K 2210/51 Improving tonal quality, e.g. mimicking sports cars
• CPC Class Codes: G10K 2210/512 Wide band, e.g. non-recurring signals

Abstract

Actuators for active vibrational energy control systems which are frequency focused. The high-frequency cancellation function is decoupled from the low-frequency cancellation function to enable the size, force, number and placement of the actuators to be optimized. A hybrid system employing structural actuators to cancel low-frequency vibrations and speakers to cancel higher-frequency vibrations is also taught.

Claims

1. An active vibration control system for controlling vibrational energy within an enclosure such as an aircraft cabin, an automobile passenger compartment, and the like, said system being capable of a broadened control and comprising:

a) reference sensor means for monitoring a disturbance to be controlled, said disturbance having various spectral frequencies contained therein, said reference sensor means producing a reference signal which corresponds to said disturbance;

b) first frequency-focused structural actuator means for producing a low-frequency vibrational control signal reducing at least a first portion of said disturbance by interfering with some of said various spectral frequencies;

c) second frequency-focused acoustic actuator means within said enclosure for producing a higher-frequency acoustic control signal canceling at least a second portion of said disturbance by interfering with other of said various spectral frequencies;

d) an adaptive controller including adaptive filter means for processing said reference signal and producing at least two actuator command signals, one each to said first frequency-focused structural actuator means and said second frequency-focused acoustic actuator means, which are of appropriate frequency and magnitude to activate a respective said actuator means;

e) error sensor means for sensing a residual signal resulting from combining said low-frequency vibrational control signal and said higher-frequency acoustic control signals with said disturbance, and

f) circuitry means for feeding said residual signal back to said adaptive filter means to make adjustments in said at least two actuator command signals.

2. The active vibration control system of claim 1 wherein said passenger compartment has K acoustic modes and said system further comprises M first frequency-focused structural actuator means where M≧

K.

3. The active vibration control system of claim 2 wherein said system includes L error sensor means within said compartment and N second-frequency focused acoustic actuators, where N≧

L/2.

4. The active vibration control system of claim 1 further comprising means to frequency focus said reference signal prior to feeding it to said adaptive controller.

5. The active vibration control system of claim 4 wherein said means to frequency focus said reference signal comprises a filter selected from the group consisting of a low pass filter, a high pass filter, and a band pass filter.

6. The active vibration control system of claim 1 wherein said first frequency-focused structural actuator means comprise at least one inertial shaker and said second frequency-focused acoustic actuator means comprise at least one speaker.

7. The active vibration control system of claim 1 wherein said error sensor means comprise one or more spaced microphones within said enclosure.

8. The active vibration control system of claim 1 wherein said error sensor means comprise one or more spaced frequency focused accelerometers attached to structural portions of said enclosure.

9. The active vibration control system of claim 1 wherein said enclosure is an aircraft cabin of a turboprop aircraft.

10. The active vibrational control system of claim 9 wherein said first frequency-focused structural actuator means is a counter-vibration producing element and is attached to said enclosure and is focused to a frequency corresponding to a primary blade passage frequency 4P and said second frequency-focused acoustic actuator means is a speaker and is focused to a frequency corresponding to a second or higher harmonic of said blade pass frequency.

11. The active vibration control system of claim 1 wherein said enclosure is a cabin of a helicopter.

12. The active vibration control system of claim 11 wherein said first frequency-focused structural actuator means comprises at least one structural actuator positioned beneath one or more seats within said cabin and said second frequency-focused acoustic actuator means comprises a plurality of speakers positioned in a vicinity of a passenger'"'"'s head.

13. The active vibration control system of claim 12 wherein said plurality of speakers are mounted upon headrest means within said cabin.

14. The active vibration control system of claim 1 wherein said first frequency-focused structural actuator means interfere with some of said various spectral frequencies which are directly coupled to structural vibration of said enclosure and said second frequency-focused acoustic actuator means interfere with other of said various spectral frequencies which are uncoupled to said structural vibration of said enclosure.

15. An active control system for controlling vibrational energy within an enclosure such as an aircraft cabin, an automobile passenger compartment, and the like, said system comprising:

a) reference sensor means for monitoring a disturbance to be controlled , said disturbance having various spectral frequencies contained therein, said reference sensor means producing a reference signal which corresponds to said disturbance;

b) first frequency-focused structural actuator means for producing a first cancelling signal reducing at least a first portion of said disturbance by interfering with some of said various spectral frequencies which are directly coupled to structural vibration of said enclosure;

c) second frequency-focused acoustic actuator means for producing a second cancellation signal canceling at least a second portion of said disturbance by interfering with other of said various spectral frequencies which are uncoupled to structural vibration of said enclosure;

d) an adaptive controller including adaptive filter means for processing said reference signal and producing at least two actuator command signals, one each to said first frequency-focused structural actuator means and second frequency-focused acoustic actuator means, which are of appropriate frequency and magnitude to activate a respective said actuator means;

e) error sensor means for sensing a residual signal resulting from combining said first cancellation signal and said second cancellation signal with said disturbance, and

f) circuitry means for feeding said residual signal back to said adaptive filter means to make adjustments in said at least two actuator command signals.

16. An active control system for controlling a disturbance generated by and aircraft engine various spectral frequencies including an N1 frequency range and a higher N2 frequency range emerging within an enclosure such as an aircraft cabin, said system comprising:

a) reference sensor means for monitoring said disturbance to be controlled and producing a reference signal which corresponds to said disturbance;

b) first frequency-focused structural actuator means for producing a first cancelling signal within said N1 frequency range reducing at least a first portion of said disturbance by interfering with some of said various spectral frequencies that are within said N1 frequency range;

c) second frequency-focused structural actuator means for producing a second cancelling signal within said N2 frequency range reducing at least a second portion of said disturbance by interfering with some of said various spectral frequencies that are within said N2 frequency range;

d) an adaptive controller including adaptive filter means for processing said reference signal and producing at least two actuator command signals, one each to said first frequency-focused structural actuator means and said second frequency-focused structural actuator means, which are of appropriate frequency and magnitude to activate a respective said actuator means;

e) error sensor means for sensing a residual signal resulting from combining said first cancellation signal, said second cancellation signal, and said disturbance, and

f) circuitry means for feeding said residual signal back to said adaptive filter means to make adaptations in said at least two actuator command signals.

17. An active control system of claim 16 wherein said first frequency-focused structural actuator means is tuned to a low end of said N1 frequency range and said second frequency-focused structural actuator means is tuned to a low end of said N2 frequency range.

18. An active vibration control system for controlling vibrational energy within an enclosure such as an aircraft cabin, an automobile passenger compartment, and the like, said system being capable of a broadened control and comprising:

a) reference sensor means for monitoring a disturbance to be controlled, said disturbance having various spectral frequencies contained therein, said reference sensor means producing a reference signal which corresponds to said disturbance;

b) frequency-focused structural actuator means for producing a vibrational control signal within a first frequency range reducing at least a first portion of said disturbance by interfering with some of said various spectral frequencies;

c) frequency-focused acoustic actuator means within said enclosure for producing an acoustic control signal within a second frequency range canceling at least a second portion of said disturbance by interfering with other of said various spectral frequencies;

d) a controller including adaptive filter means for processing said reference signal and producing at least two actuator command signals, one each to said frequency-focused structural actuator means and said frequency-focused acoustic actuator means, which are of appropriate frequency and magnitude to activate a respective said actuator means;

e) error sensor means for sensing a residual signal resulting from combining said vibrational control signal and said acoustic control signals with said disturbance, and

f) circuitry means for feeding said residual signal back to said adaptive filter means to make adjustments in said at least two actuator command signals.