Method and apparatus for actively adjusting and controlling a resonant mass-spring system

• US 5,456,341 A
• Filed: 04/23/1993
• Issued: 10/10/1995
• Est. Priority Date: 04/23/1993
• Status: Expired due to Term

• Current Assignee: Moog Incorporated
• Original Assignee: Moog Incorporated
• Inventors: Rey, Gonzalo J., Garnjost, Kenneth D., Rauch, Christopher A.
• Primary Examiner(s): Butler, Douglas C.
• Application Number:
  US08/052,474
• Time in Patent Office: 900 Days
• Field of Search: 188/378, 188/379, 188/380, 188/382, 188/267, 248/550, 267/136, 267/140.14, 267/140.15, 280/707, 244/17.27, 244/17.11, 244/158 R, 416/500
• US Class Current: 188/378
• CPC Class Codes: B60G 17/018 characterised by the use of a specific signal treatment or control method
• CPC Class Codes: B60G 2202/25 Dynamic damper
• CPC Class Codes: B60G 2202/413 Hydraulic actuator
• CPC Class Codes: B60G 2202/422 Linear motor
• CPC Class Codes: B60G 2400/102 vertical
• CPC Class Codes: B60G 2400/206 Body oscillation speed; Body vibration frequency
• CPC Class Codes: B60G 2400/25 Stroke; Height; Displacement
• CPC Class Codes: B60G 2400/60 Load
• CPC Class Codes: B60G 2400/91 Frequency
• CPC Class Codes: B60G 2600/182 Active control means
• 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 15/03 using magnetic or electromagnetic means F16F9/53, F16F15/005 take precedence
• CPC Class Codes: F16F 7/1005 characterised by active control of the mass

Abstract

An actively-controlled resonant-type force generator (20) is adapted to be attached to a structure (21), and includes a mass (23) mounted for movement relative to the structure and a plurality of springs (22, 24) operatively arranged between the mass and the structure. A servoactuator (26) is arranged to controllably excite the mass-spring system. The actual force (F_a) transmitted from the mass to the structure is compared with a commanded force (F_c) to produce a force error signal (F_e). The actuator is caused to produce a velocity as a function of the error signal. The gain of the closed force loop is selected so that the resonance of the mass-spring system has an effective damping ratio (ζ) greater than about 0.5, and preferably about 0.7. Thus, the mass-spring system will not be substantially resonantly excited by vibrations of the structure near its resonant frequency (ω_n).

Claims

1. A vibratory inertial force generator including an actively-controlled mass-spring system arranged to be resonantly excited so as to exert a vibratory reaction force on a structure, said system having a mass mounted for movement relative to said structure and having a spring arranged between said mass and structure, wherein the improvement comprises:

an externally-powered servoactuator mounted on one of said mass and structure and arranged to modulate said vibratory reaction force transmitted from said mass to said structure as a function of the acceleration of said mass so as to controllably modify the resonant frequency of said system.

2. A vibratory inertial force generator as set forth in claim 1 wherein said servoactuator is connected mechanically in series with said mass and said spring.

3. A vibratory inertial force generator as set forth in claim 2 wherein said servoactuator is arranged between said structure and said spring.

4. A vibratory inertial force generator as set forth in claim 1 wherein said servoactuator is hydraulically powered.

5. A vibratory inertial force generator as set forth in claim 1 wherein said spring is formed by the compliance of a fluid contained in a piston-cylinder assembly.

6. A vibratory inertial force generator as set forth in claim 1, and further comprising:

command means for generating an oscillatory force command signal;

transducer means arranged to generate a feedback signal proportional to the acceleration of said mass;

means for producing an error signal proportional to the difference between said command signal and said feed back signal; and

control means for modulating said servoactuator as a function of said error signal to cause said system resonant frequency to equal that of the oscillatory force command signal, and to further excite the mass-spring system at its modified resonant frequency so that the reaction force exerted on said structure will be essentially equal to the commanded oscillatory force.

7. A vibratory inertial force generator as set forth in claim 6 wherein said structure is a helicopter having a rotor, and wherein the frequency of said oscillatory force command signal is a function of the rotational speed of said rotor.

8. A vibratory inertial force generator as set forth in claim 6 wherein said force command signal is a function of the vibratory velocity of at least one point in said structure affected by the force transmitted from said mass.

9. A vibratory inertial force generator as set forth in claim 8 wherein the vibrations at said one point are substantially cancelled.

10. A vibratory inertial force generator as set forth in claim 6 wherein said control means is arranged to cause said actuator to produce a velocity as a function of said error signal such that said mass-spring system will not be substantially resonantly excited by vibrations of said structure near the resonant frequency.

11. A vibratory inertial force generator as set forth in claim 10 wherein the gain of the closed loop so formed is selected so that the resonance of said mass and each spring of said system has an effective damping ratio greater than about 0.5.

12. A vibratory inertial force generator as set forth in claim 6 wherein said transducer means includes an accelerometer mounted on said mass for sensing the spatial acceleration of said mass.

13. A vibratory inertial force generator as set forth in claim 1 wherein said system is configured as an active resonant absorber mounted on a vibrating structure, and further comprising:

transducer means operatively arranged to sense the acceleration of said mass; and

control means responsive to the output signal from said transducer means and operatively arranged to modulate said servoactuator so as to continuously modify the resonant frequency of said mass-spring system to equal the frequency of the vibrating structure;

whereby the mass-spring system will be resonantly excited by the structural vibration and the resulting reaction force on said structure, acting to damp said structural vibration, will be maximized.

14. A vibratory inertial force generator as set forth in claim 13 wherein said control mass will cause the servoactuator displacement to be proportional to said sinusoidal acceleration of said mass minus a frequency-squared correction function;

whereby the servoactuator modulation amplitude is zero when the structural vibration frequency is equal to the unmodified resonant frequency, and is continuously adjusted as a function of the incremental change of the structural vibration frequency from the unmodified system resonant frequency.

15. The method of controlling an active resonant inertial force generator having a movable mass coupled through at least one spring to a structure, comprising the steps of:

mounting an externally-powered servoactuator on one of said mass and structure so as to be capable of modulating the vibratory reaction force transmitted between said mass and structure;

commanding a desired vibratory force, at a desired frequency, to be exerted on said structure by said generator;

modulating said servoactuator so as to excite the mass-spring system and to continuously adjust the natural frequency of the mass-spring system so as to generate a vibratory reaction force acting on said structure at said commanded frequency;

measuring said vibratory reaction force; and

controlling the modulation of said servoactuator to minimize the difference between said commanded force and said measured vibratory reaction force.

16. The method as set forth in claim 15 wherein said vibratory force is measured as a function of the acceleration of said mass.

17. The method as set forth in claim 16 wherein the steps previously set forth form an acceleration feedback servoloop, and wherein the gain of said servoloop is adjusted so that the effective damping ratio of the resonant mass-spring system, when excited by structural vibrations, is at least 0.5.

18. In an actively-controlled mass-spring system having a resonantly-vibrating mass adapted to exert a vibratory reaction force on a vibrating structure at a mounting point in response to an electrical command signal, the improvement which comprises:

an externally-powered servoactuator operatively arranged to act on one of said mass and structure;

means for providing an electrical command signal reflecting a desired force; and

control means responsive to said command signal for modulating said servoactuator so as to cause the resonant frequency of said system to continuously approximate the frequency of said command signal and to resonantly excite the mass-spring system such that the reaction force exerted on said structure is substantially equal to the electrically-commanded force.

19. The improvement as set forth in claim 18 wherein said servoactuator is controlled as a function of the vibratory acceleration of said mass.

20. The improvement as set forth in claim 18 wherein said system includes a mass acceleration feedback control loop closed around said servoactuator and said control means, and wherein the gain of said feedback loop is adjusted such that the response of the mass-spring system to structural vibrations exhibits a damping ratio greater than about 0.5.

21. A vibratory inertial force generator including an actively-controlled mass-spring system arranged to be resonantly excited so as to exert a vibratory reaction force on a structure, said system having a mass mounted for movement relative to said structure and having a spring arranged between said mass and structure, wherein the improvement comprises:

an externally-powered servoactuator mounted on one of said mass and structure and arranged to modulate said vibratory reaction force transmitted from said mass to said structure as a function of the acceleration of said mass so as to controllably modify the resonant frequency of said system;

command means for generating an oscillatory force command signal;

transducer means arranged to generate a feedback signal proportional to the force transmitted from said mass to said structure; and

means for producing an error signal proportional to the difference between said command signal and said feedback signal.

22. A vibratory inertial force generator including an actively-controlled mass-spring system arranged to be resonantly excited so as to exert a vibratory reaction force on a structure, said system having a mass mounted for movement relative to said structure and having a spring arranged between said mass and structure, wherein the improvement comprises:

an externally-powered servoactuator mounted on one of said mass and structure and arranged to modulate said vibratory reaction force transmitted from said mass to said structure as a function of the acceleration of said mass so as to controllably modify the resonant frequency of said system;

command means for generating an oscillatory force command signal;

transducer means arranged to generate a feedback signal proportional to the acceleration of said mass;

means for producing an error signal proportional to the difference between said command signal and said feedback signal; and

control means for modulating said servoactuator as a function of said error signal to cause said system resonant frequency to equal that of the oscillatory force command signal, and to further excite the mass-spring system at its modified resonant frequency so that the reaction force exerted on said structure will be essentially equal to the commanded oscillory force.