Adaptive tuned vibration absorber, system utilizing same and method of controlling vibration therewith

• US 5,954,169 A
• Filed: 10/24/1997
• Issued: 09/21/1999
• Est. Priority Date: 10/24/1997
• Status: Expired due to Fees

• Current Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Original Assignee: Lord Corporation (Parker-Hannifin Corporation)
• Inventors: Jensen, William S.
• Primary Examiner(s): Butler, Douglas C.
• Application Number:
  US08/957,718
• Time in Patent Office: 697 Days
• Field of Search: 244/54, 244/17.27, 244/129.1, 244/1 N, 244/17.11, 188/378, 188/379, 188/380, 381/71.1, 381/71.2, 381/71.4, 180/300, 180/312, 248/559, 248/550, 248/636, 248/562, 248/638, 415/119, 267/136, 267/140.15, 267/140.14, 702/195, 416/500, 364/528.15, 52/167.1, 52/167.3
• US Class Current: 188/378
• 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 7/1005 characterised by active control of the mass
• CPC Class Codes: F16F 7/116 on metal springs

Abstract

A flex-plate tuned vibration absorber (35) including a tuned mass (43) flexibly suspended by one or more flex plates (58). In one aspect the tunable vibration absorber (TVA) (35) is adaptive in that the position of the mass is adaptively moveable with respect to its initial position, thereby effectuating a change in the TVA'"'"'s resonant frequency. In one embodiment, the tuned mass (43) moves along a rigid frame (53). In another, movement of the mass (43) statically stresses a preferably disc-shaped flexible plate (58) thereby changing its stiffness. Preferably, a reducer (78) gears down the speed of the motor (64). In another aspect, a TVA system includes a base sensor (40) providing a base vibration signal, a mass sensor (38) for providing a vibration signal of the tuned mass (43), and an electronic controller (42) for generating a control signal to the TVA (35). The TVA finds application for absorbing vibration in vibrating structures, such as in aircraft.

Claims

1. A tuned vibration absorber (35) adapted for attachment to a vibrating structure (32, 33), said absorber (35) having a stiffness and tuned mass (43) defining a resonant frequency, said absorber (35) comprising:

(a) at least one flexible plate (58) exhibiting said tuned stiffness and having an elastic center (EC),

(b) said tuned mass (43) exhibiting a center of gravity (CG) which is offset from said elastic center (EC), said tuned mass (43) interconnected to, and suspended by, said at least one flexible plate (58),

(c) a base (28) interconnecting said at least one flexible plate (58) to a vibrating structure (32), and

(d) means for adaptively moving a position of said tuned mass (43) relative to said base (28) thereby changing said resonant frequency.

2. An absorber (35) of claim 1 wherein said means for adaptively moving includes a motor (64).

3. An absorber (35) of claim 2 wherein said motor (64) moves said tuned mass (43) along a rigid frame (53) interconnected to said at least one flexible plate (58).

4. An absorber (35) of claim 3 further comprising roller bearings (61) located between said tuned mass (43) and said rigid frame (53).

5. An absorber (35) of claim 4 wherein said roller bearings (61) are hollow.

6. An absorber (35) of claim 2 wherein said motor (64) is interconnected to a threaded rod (68) which threadedly engages with said tuned mass (43) whereby rotating said threaded rod (68) moves said tuned mass (43) axially.

7. An absorber (35) of claim 6 wherein the motor (64) is a stepper motor.

8. An absorber (35) of claim 6 wherein said motor (64) is mounted within a hollow (65) formed in said rigid frame (53).

9. A system (25) including an absorber (35) of claim 2 including:

(a) a mass sensor (38) for generating a first input signal representative of a vibration of said tuned mass (43),

(b) a base sensor (40) for generating an second input signal representative of a vibratory characteristic of said vibrating structure, and

(c) a controller (42) for processing said first and second signals to generate a control signal to adjust said position of said tuned mass (43).

10. An absorber (35) of claim 1 for controlling vibration within a structural component of an aircraft (20), said absorber (35) being oriented such that said vibration is absorbed by a radial and/or tangential vibration of said tuned mass (43).

11. An absorber (35) of claim 1 wherein said means for adaptively moving said position of said tuned mass (43) statically deforms and stresses said at least one flexible plate (58) thereby adaptively changing said stiffness thereby changing said resonant frequency.

12. An absorber (35) of claim 11 wherein said at least one flexible plate (58) includes a first conical disc portion which when flexed changes a pivotal stiffness thereby changing said resonant frequency.

13. An absorber (35) of claim 12 further comprising a second conical disc portion cooperative with said first conical disc portion and forming a conical disc set which when flexed changes a combined pivotal stiffness of said conical disc set thereby changing said resonant frequency.

14. An absorber (35) of claim 12 wherein said means for adaptively moving a position of said tuned mass (43) moves said mass (43) further away from said base (28) and flattens out said first conical disc portion.

15. An absorber (35) of claim 12 wherein said means for statically stressing is a motor (64) interconnected to a reducer (78) which applies static axial loading thereby flexing said at least one flexible plate (58).

16. An absorber (35) of claim 15 further including a reducer (78).

17. An absorber (35) of claim 16 wherein said reducer (78) exhibits a gear reduction ratio of 80:

1 or higher.

18. An absorber (35) of claim 16 wherein said reducer (78) is a harmonic drive.

19. An absorber (35) of claim 11 wherein said means for statically stressing includes a motor (64) and a rod (68) including a power thread interconnected by a reducer (78).

20. An absorber (35) of claim 19 wherein said power thread is threadedly engaged in a like threaded portion (70) in said base (28).

21. An absorber (35) of claim 19 wherein said rod (68) includes a projection (74) which is translationally restrained relative to said tuned mass (43).

22. An absorber (35) of claim 11 wherein said at least one flexible plate (58) is comprised of interconnected first and a second flexible plates (58, 58'"'"').

23. An absorber (35) of claim 11 wherein said means for statically stressing includes hydraulic pressure.

24. An absorber (35) of claim 23 wherein said hydraulic pressure acts against a piston (82) thereby applying a static axial force between said tuned mass (43) and said base (28).

25. An absorber (35) of claim 11 wherein said means for statically stressing includes pneumatic pressure.

26. An absorber (35) of claim 25 wherein said pneumatic pressure is supplied within a chamber (84) which applies a static axial force to separate said tuned mass (43) from said base (28).

27. An absorber (35) of claim 11 wherein said flex plate (58) is circular disc shaped.

28. A tuned vibration absorber (35) including a tuned mass (43), a stiffness, and a resonant frequency, comprising:

(a) a base (28),

(b) a rigid frame (53),

(c) a flexible plate (58) interconnecting between said base (28) and said rigid frame (53), said flexible plate (58) substantially providing said stiffness,

(d) a tuned mass (43) slideable on said rigid frame (53), and

(e) means for moving said tuned mass (43) along said rigid frame (53) to effectuate a change in resonant frequency of said tuned vibration absorber (35).

29. A tuned vibration absorber (35), comprising:

(a) a circular flexible disc (58),

(b) a tuned mass (43) interconnecting and suspended by said flexible disc (58), and

(c) means for statically and elastically deforming said flexible disc (58) to effectuate a change in stiffness thereby adjusting a resonant frequency of said absorber (35).

30. A tuned vibration absorber (35) of claim 29 wherein said means for statically deforming said flexible disc (58) includes a reducer (78).

31. A tuned vibration absorber (35) of claim 29 further including means for coupling to said reducer (78) whereby energizing said motor (64) causes said tuned mass (43) to adaptively move relative to said base (28).

32. A tuned vibration absorber (35) of claim 29 wherein said means for statically deforming said flexible disc (58) includes a motor (64), a reducer (78) interconnected to said motor (64), and a threaded rod (68) interconnected to said reducer (78) which threadedly engages said base (28) whereby energizing said motor (64) rotates said rod (68) thereby moving a position of said tuned mass (43) relative to said base (28).

33. A tuned vibration absorber (35) of claim 29 wherein said tuned mass (43) is generally annular-shaped and secured to said flexible disc (58) at its outermost periphery.

34. A tuned vibration absorber (35) of claim 29 wherein said flexible disc (58) includes a conical disc shaped portion which when deformed changes said stiffness of said a flexible disc (58) thereby changing a natural frequency of said tuned absorber (35).

35. A tuned vibration absorber (35) of claim 29 wherein an Elastic Center (EC) of said circular flexible disc (58) is offset from a Center of Gravity (CG) of said tuned mass (43).

36. A tuned vibration absorber (35), comprising:

(a) a base (28),

(b) a flexible plate (58) extending from said base (28),

(c) a tuned mass (43) suspended by said flexible plate (58),

(d) a motor (64),

(e) a reducer (78) interconnecting to said motor (64), and

(f) means for coupling to said reducer (78) whereby energizing said motor (64) causes said tuned mass (43) to adaptively move relative to said base (28) stressing said flexible plate.

37. A method for controlling vibration of an engine (30) at its operating frequency, said engine (30) having a plurality of spokes (22) providing radial support between a bearing housing (24) and a casing (26) of said engine (30), comprising the steps of:

a) attaching at least one adaptive tuned absorber (35) directly to said engine (30) at a location adjacent to at least one of said spokes (22), said tuned vibration absorber (35) having a base (28), at least one flexible member extending from said base (28), and a tuned mass (43) suspended by said flexible member,

b) moving said tuned mass (43) relative to said base (28) to effectuate a change in a resonant frequency of said at least one tuned absorber (35) which tracks said engine operating frequency.

38. A method for controlling vibration of an engine (30) of claim 37 including the further steps of:

(d) attaching a motor (64) to said at least one tuned absorber (35),

(e) interconnecting a reducer (78) to said motor (64), and

(f) coupling to said reducer (78) to said base (28) whereby energizing said motor (64) causes said tuned mass (43) to adaptively move relative to said base (28) elastically stressing and deforming said flexible plate.

39. A method for controlling vibration of an engine (30) of claim 37 including the further steps of:

(a) providing at least one flexible disc as least one flexible member (58),

(b) interconnecting said tuned mass (43) by said flexible disc, and

(c) statically stressing said flexible disc responsive said adaptively moving said tuned mass (43) to effectuate a change in axial stiffness.

40. A method for controlling vibration of an engine (30) of claim 37 including the further steps of:

a) attaching said flexible member to a rigid frame (53), said flexible member being a flexible plate (58),

b) sliding said tuned mass (43) on said rigid frame (53).