Active noise and vibration control system

• US 5,802,184 A
• Filed: 08/15/1996
• Issued: 09/01/1998
• Est. Priority Date: 08/15/1996
• Status: Expired due to Term

• Current Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Original Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Inventors: Heath, Michael C.
• Primary Examiner(s): CHIN, VIVIAN C
• Application Number:
  US08/698,544
• Time in Patent Office: 747 Days
• Field of Search: 381/71, 381/94, 381/86, 381/73.1, 381/120, 381/96, 381/71.1, 381/71.2, 381/71.8, 381/71.13, 381/94.1, 381/71.11, 330/10
• US Class Current: 381/71.4
• CPC Class Codes: F16F 15/002 characterised by the control method or circuitry control of mechanical oscillations per se G05D19/00
• CPC Class Codes: F16F 15/02 Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems F16F15/005 takes precedence ; layered products B32B; suppression of vibration in ships B63; relieving load on bearings, using magnetic means F16C39/06
• CPC Class Codes: F16F 7/1011 by electromagnetic means
• CPC Class Codes: G10K 11/17855 for improving speed or power requirements
• CPC Class Codes: G10K 11/17879 using both a reference signal and an error signal
• CPC Class Codes: G10K 11/17881 the reference signal being an acoustic signal, e.g. recorded with a microphone
• 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 2210/106 Boxes, i.e. active box covering a noise source; Enclosures
• CPC Class Codes: G10K 2210/1281 Aircraft, e.g. spacecraft, airplane or helicopter
• CPC Class Codes: G10K 2210/1282 Automobiles
• CPC Class Codes: G10K 2210/1291 Anti-Vibration-Control, e.g. reducing vibrations in panels or beams
• CPC Class Codes: G10K 2210/3026 Feedback
• CPC Class Codes: G10K 2210/3027 Feedforward
• CPC Class Codes: H03F 3/217 Class D power amplifiers; Switching amplifiers

Abstract

Vibrational energy in a first frequency range within a vehicle or the like is controlled by an active vibration control system which includes a sensor, controller, driver, actuator and actuator power dissipation reduction circuit. The controller provides a control signal to a Class-D power amplifier operating at a second higher frequency to generate an output signal to the actuator in the frequency range of the noise/vibration to be controlled resulting in a force output from the actuator controlling vibration and/or noise in a passenger compartment of the vehicle. The actuator power dissipation reduction circuit reduces high frequency energy transients with in-series inductors to prevent heat inducing eddy currents in the actuator without additional current flow in the power amplifier.

Claims

1. A control system for controlling vibrational energy in a first frequency range to a vehicle from a vibrational energy source, comprising:

a) a sensor for monitoring said vibrational energy to be controlled;

b) a vibrational energy control circuit responsive to said sensor having a first output pole and a second output pole for providing a drive signal between said first output pole and said second output pole which contains high frequency energy transients at frequencies outside said first frequency range and at least one frequency component in said first frequency range;

c) an actuator electrically connected to said first output pole and said second output pole and responsive to said at least one frequency component in said first frequency range of said drive signal for generating forces to control said vibrational energy;

d) an actuator power dissipation reduction circuit electrically connected between said vibrational energy control circuit and said actuator for preferentially reducing an amplitude of said high frequency energy transients in said drive signal to reduce power dissipation in said actuator from said high frequency energy transients, said actuator power dissipation reduction circuit including a first inductor serially electrically connecting said first output pole to said actuator and a second inductor serially electrically connecting said second output pole to said active vibration control actuator; and

wherein said vibrational energy control circuit generates current and substantially all of said current from said vibrational energy control circuit is provided to said actuator.

2. A control system as in claim 1 wherein said actuator comprises an active vibration control actuator.

3. A control system as in claim 2 wherein said active vibration control actuator includes an iron core.

4. A control system as in claim 3 wherein said vibrational energy control circuit includes a power-amplifier.

5. A control system as in claim 4 wherein said power-amplifier comprises a Class-D power amplifier.

6. A control system as in claim 4 wherein said power-amplifier comprises a pulse width modulated power amplifier.

7. A control system as in claim 6 wherein said pulse width modulated power amplifier generates alternating current and substantially all of said alternating current from said pulse width modulated power amplifier is provided to said active vibration control actuator.