Redundant active vibration and noise control systems and methods

• US 10,393,216 B2
• Filed: 12/12/2014
• Issued: 08/27/2019
• Est. Priority Date: 12/13/2013
• Status: Active Grant

• Current Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Original Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Inventors: Swanson, Douglas A.
• Primary Examiner(s): Lo, Kenneth M
• Assistant Examiner(s): Huntley, Michael J
• Application Number:
  US15/303,632
• Publication Number:
  US 20170067530A1
• Time in Patent Office: 1,719 Days
• CPC Class Codes: B06B 1/16 operating with systems involving rotary unbalanced masses
• CPC Class Codes: B64C 2027/004 using actuators, e.g. active systems
• CPC Class Codes: B64C 27/001 Vibration damping devices
• CPC Class Codes: F16F 15/002 characterised by the control method or circuitry control of mechanical oscillations per se G05D19/00
• CPC Class Codes: G05B 15/02 electric

Abstract

Redundant active vibration and noise control systems and methods are provided, which include safety-critical systems and methods. In one embodiment, a safety-critical active vibration control system (SCAVCS) is provided, which includes a plurality of digital buses, a force generator, at least one sensor and at least one system parameter. The at least one force generator is in electronic communication with at least two digital buses. The force generator includes a pair of unbalanced masses, at least one motor, at least one microprocessor, at least one speed sensor, at least one accelerometer, and at least one power input. The at least one sensor is in electronic communication with each of the digital buses and with each of the microprocessors. The at least one system parameter is in electronic communication with each of the digital buses and each of the microprocessors.

Claims

1. An active vibration control system (AVCS), the system comprising:

at least two digital bus communication lines;

a plurality of sensors in electronic communication with each of the at least two digital bus communications lines;

at least two circular force generators (CFG), each of the at least two CFGs having at least one motor, at least two imbalance masses and at least two microprocessors therein, wherein each of the at least two microprocessors of each CFG is in electronic communication with each of the at least two digital bus communication lines and each of the at least two microprocessors of each CFG are in electronic communication with each of the plurality of sensors and the microprocessors of all the other CFGs, wherein the at least two CFGS are in a distributed architecture;

wherein at least a first microprocessor within each CFG is configured to process redundant information communicated from the at least two digital bus communication lines and the other microprocessors with the same CFG, and each of the microprocessors within each CFG monitor each of the other microprocessors within the same CFG for errors, faults, or failures in vibration control; and

wherein any one of the microprocessors in each CFG is configured to control the at least one motor thereby producing a force that substantially cancels an unwanted vibration force detected by the plurality of sensors.

2. The AVCS of claim 1, wherein the redundant information includes electronic signals indicative of vibration information, system parameters, additional inputs, information regarding the rotation of imbalance masses, or forces generated by each of the at least two CFGs.

3. The AVCS of claim 2, wherein the vibration information is obtained using one or more sensors and wherein the information regarding the rotation of imbalance masses is obtained using an accelerometer.

4. The AVCS of claim 3, wherein the sensors include accelerometers, microphones, strain gauges, inertial motion systems, temperature sensors, force sensors, or motion detectors.

5. The AVCS of claim 2, wherein the additional inputs include information regarding a type of cargo, a center of gravity, or a responsiveness of an unwanted vibration force.

6. The AVCS of claim 2, wherein the system parameters include any one of a true airspeed, an altitude, an angle of attack, an engine speed, a rotor azimuth, a rotor speed, weather conditions, or landing conditions.

7. The AVCS of claim 1, wherein the system is devoid of a centralized controller disposed outside of each of the at least two CFGs.

8. The AVCS of claim 1, wherein the system includes at least two controllers in electronic communication with at least some of the CFGs using at least one of the digital bus communication lines.

9. The AVCS of claim 8, wherein the redundant information includes a force control command signal generated by at least two controllers, wherein the at least two microprocessors are configured to provide local control of the CFG while receiving input commands from one of the at least two controllers.

10. The AVCS of claim 1, further comprising at least two motors disposed within each CFG, wherein each of the at least two microprocessors is configured to drive a respective motor.

11. The AVCS of claim 1, wherein the at least one of the at least two CFGs is configured to process the redundant information via at least one of the at least two plurality of microprocessors.

12. The AVCS of claim 11, further comprising more than two CFGs, and wherein at least one microprocessor residing within each of the CFGs is configured to monitor some or all of the microprocessors within the other CFGs for errors, faults, or failures of the system or components thereof.

13. The AVCS of claim 1, wherein the at least one CFG comprises at least two motors, where each motor is controllable by either a first microprocessor or a second microprocessor.

14. A method of providing a redundant active vibration control system (AVCS), the method comprising:

providing at least two of digital bus communication lines;

providing a plurality of sensors, wherein each of the plurality of sensors is in electronic communication with each of the at least two digital bus communications lines;

electronically connecting each of at least two circular force generators (CFG) to each of the digital bus communication lines for facilitating electronic communication therewith, wherein each of the at least two CFGs has at least one motor, at least two imbalance masses and at least two microprocessors therein, wherein each of the at least two microprocessors within each CFG is configured to receive and send communications from and to each of the at least two digital bus communications lines;

processing redundant information electronically communicated from each of the at least two digital bus communication lines in one of the at least two microprocessors within each CFG;

processing the same microprocessor receiving redundant information from each of the at least two digital bus communication lines redundant information communicated from the other microprocessors within the same CFG to the one microprocessor;

monitoring each of the at least two microprocessors, wherein each of the at least two microprocessors in each CFG monitor the other microprocessors within the same CFG for errors, faults, or failures in vibration control;

generating a force that substantially cancels an unwanted noise or vibration force detected by the plurality of sensors, wherein at least one of the microprocessors in each of the CFGs controls the at least one motor that generates the force.

15. The method of claim 14, wherein electronically communicating redundant information includes sending electronic signals indicative of vibration information, system parameters, additional inputs, or information regarding the rotation of an imbalance masses.

16. The method of claim 14, further comprising electronically connecting at least one controller to each of the at least two digital bus communication lines for instructing at least one of the microprocessors within each CFG.

17. The method of claim 14, wherein each CFG comprises at least two motors, and where each motor is controllable by either a first microprocessor or a second microprocessor.