Distributed active vibration control systems and rotary wing aircraft with suppressed vibrations

• US 8,639,399 B2
• Filed: 12/21/2011
• Issued: 01/28/2014
• Est. Priority Date: 10/25/2007
• Status: Active Grant

• Current Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Original Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Inventors: Jolly, Mark R., Badre-Alam, Askari, Altieri, Russell E., Meyers, Andrew D.
• Primary Examiner(s): Nguyen, Kim T
• Application Number:
  US13/333,196
• Publication Number:
  US 20120158217A1
• Time in Patent Office: 769 Days
• Field of Search: 701/3, 701/29.2, 701/29.3, 701/31.4, 701/31, 701/5, 701/32.7, 700/66, 700/279, 700/280
• US Class Current: 701/3
• CPC Class Codes: B64C 2027/004 using actuators, e.g. active systems
• CPC Class Codes: B64C 2027/005 using suspended masses
• 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: F16F 15/223 Use of systems involving rotary unbalanced masses where the phase-angle of masses mounted on counter-rotating shafts can be varied generation of mechanical vibrations per se with such systems B06B1/166
• CPC Class Codes: Y10T 29/49009 Dynamoelectric machine

Abstract

A method and system is disclosed for controlling problematic vibrations in an aircraft having. The method and system have the ability to cancel problematic rotary wing helicopter vibrations using independent active force generator power and with distributed communications therebetween.

Claims

1. An aircraft, said aircraft comprised of a nonrotating vehicle structure, said nonrotating vehicle structure including a plurality of distributed active vibration control system sites, with said aircraft including:

at least a first distributed active vibration circular force generator, said first distributed active vibration circular force generator fixed to said nonrotating vehicle structure at a first distributed active vibration control system site,

at least a second distributed active vibration circular force generator, said second distributed active vibration circular force generator fixed to said nonrotating vehicle structure at a second distributed active vibration control system site,

a plurality of electrical power distribution lines, said electrical power distribution lines connecting said circular force generators with a power source,

a distributed circular force generator data communications network, said distributed circular force generator data communications network linking together at least said first distributed active vibration circular force generator and at least said second distributed active vibration circular force generator, with at least said first distributed active vibration circular force generator and at least said second distributed active vibration circular force generator communicating circular force generator vibration control data through said distributed force generator data communications network independently of said electrical power distribution lines, with said first distributed active vibration circular force generator and said second distributed active vibration circular force generator outputting circular forces into said nonrotating vehicle structure to minimize a plurality of troublesome vibrations.

2. An aircraft as claimed in claim 1, including a master system controller, said master system controller connected to said distributed force generator data communications network wherein said master system controller provides a plurality of authority commands to at least said first distributed active vibration circular force generator and said second distributed active vibration circular force generator with said first distributed active vibration circular force generator and said second distributed active vibration circular force generator executing a plurality of subordinate local circular force generator operation commands.

3. An aircraft as claimed in claim 1, including a migrating master system control authority, said migrating master system control authority movable between at least said first distributed active vibration circular force generator and said second distributed active vibration circular force generator, with the migrating master system control authority providing a plurality of authority commands to at least said first distributed active vibration circular force generator and said second distributed active vibration circular force generator to execute a plurality of subordinate local force generator operation commands.

4. An aircraft as claimed in claim 1, including a distributed master system control authority, said distributed master system control authority distributed among at least said first distributed active vibration circular force generator and said second distributed active vibration circular force generator with the distributed master system control authority providing a plurality of authority commands to at least said first distributed active vibration circular force generator and said second distributed active vibration circular force generator to execute a plurality of subordinate local force generator operation commands.

5. An aircraft as claimed in claim 1, including at least a first distributed networked accelerometer, said at least first distributed networked accelerometer having an accelerometer network link with said distributed force generator data communications network.

6. An aircraft as claimed in claim 1, wherein said first distributed active vibration circular force generator executes a plurality of local circular force generator operation rotating motor commands, and said second distributed active vibration circular force generator executes a plurality of local force generator operation rotating motor commands.

7. An aircraft as claimed in claim 1, wherein said troublesome vibrations are created by an aircraft rotating machine and said first distributed active vibration control system site is distal from said aircraft rotating machine, and said second distributed active vibration control system site is distal from said aircraft rotating machine.

8. A method of making a vibration control system for suppressing troublesome vibrations in a structure with at least one rotating machine creating troublesome vibrations, said method comprising:

providing at least a first distributed active vibration circular force generator, said first distributed active vibration circular force generator including a first distributed electronic control system,

fixing said first distributed active vibration circular force generator to said structure at a first distributed active vibration control system site,

providing at least a second distributed active vibration circular force generator, said second distributed active vibration circular force generator including a second distributed electronic control system,

fixing said second distributed active vibration circular force generator to said structure at a second distributed active vibration control system site,

connecting said at least first and second circular force generators with a plurality of electrical power distribution lines to a power source,

providing a distributed force generator data communications network, said distributed force generator data communications network linking together said at least first and second distributed electronic control systems,

communicating force generator vibration control data through said distributed force generator data communications network independently of said electrical power distribution lines to generate circular forces to minimize said troublesome vibrations.

9. A method as claimed in claim 8, wherein said first distributed active vibration control system site is distal from said at least one rotating machine.

10. A method as claimed in claim 9, wherein said second distributed active vibration control system site is distal from said at least one rotating machine.

11. A method as claimed in claim 9, wherein said first distributed active vibration circular force generator includes a first containment chamber containing said first distributed electronic control system and a second containment chamber containing at least a first electromagnetically driven rotating mass.

12. A method as claimed in claim 11, wherein said second containment chamber contains a second corotating electromagnetically driven rotating mass.

13. A vehicle vibration control system for suppressing troublesome vehicle vibrations in a vehicle structure connected with at least one rotating machine creating troublesome vibrations in said vehicle structure, said vehicle vibration control system including:

at least a first distributed active vibration circular force generator, said first distributed active vibration circular force generator including a first distributed electronic control system and a first rotating mass, said first distributed active vibration circular force generator for fixing to said vehicle structure at a first distributed active vibration control system site,

at least a second distributed active vibration circular force generator, said second distributed active vibration circular force generator including a second distributed electronic control system and a second rotating mass, said second distributed active vibration circular force generator for fixing to said vehicle structure at a second distributed active vibration control system site,

a plurality of electrical power distribution lines, said electrical power distribution lines for connecting said first distributed active vibration circular force generator and said second distributed active vibration circular force generator with a power source,

a distributed force generator data communications network, said distributed force generator data communications network for linking together said at least first and second distributed electronic control systems wherein said distributed electronic control systems communicate circular force generator vibration control data through said distributed force generator data communications network independently of said electrical power distribution lines to minimize said troublesome vibrations.

14. A system as claimed in claim 13 wherein said first distributed active vibration circular force generator includes a first containment chamber containing said first distributed electronic control system and a second containment chamber containing said first rotating mass.

15. A system as claimed in claim 14 wherein said second containment chamber contains a second corotating electromagnetically driven rotating mass.

16. A method of suppressing a plurality of vibrations, said method comprising:

providing a structure, providing at least a first distributed active vibration electromagnetic force generator, said first distributed active vibration electromagnetic force generator including a first distributed electronic control system and at least a first electromagnetically driven mass,

fixing said first distributed active vibration electromagnetic force generator to said structure at a first distributed active vibration control system site,

providing at least a second distributed active vibration electromagnetic force generator, said second distributed active vibration electromagnetic force generator including a second distributed electronic control system and at least a second electromagnetically driven mass,

fixing said second distributed active vibration electromagnetic force generator to said structure at a second distributed active vibration control system site,

connecting said at least first electromagnetic force generator and said at least second electromagnetic force generator to a power source to provide an electromagnetic source of power,

providing a distributed force generator data communications network, said distributed force generator data communications network linking together said at least first distributed electronic control system and said at least second distributed electronic control system,

communicating force generator vibration control data through said distributed force generator data communications network independently of said electromagnetic source of power to minimize said vibrations.

17. A method as claimed in claim 16, wherein said first distributed active vibration electromagnetic force generator at least first electromagnetically driven mass is comprised of a sprung mass resonant actuator force generator having a natural resonant frequency.

18. A method as claimed in claim 16, wherein said first distributed active vibration electromagnetic force generator at least first electromagnetically driven mass is comprised of a linear motor electromagnetically driven sprung mass.

19. A method as claimed in claim 16, wherein said first distributed active vibration electromagnetic force generator at least first electromagnetically driven mass is comprised of a first rotating mass.

20. A method as claimed in claim 19, wherein said first distributed active vibration electromagnetic force generator includes a second corotating electromagnetically driven rotating mass.