Device for damping the vibrations of a structure subjected to dynamic stresses

• US 5,814,963 A
• Filed: 10/09/1996
• Issued: 09/29/1998
• Est. Priority Date: 10/09/1995
• Status: Expired due to Term

• Current Assignee: Airbus Helicopters
• Original Assignee: Eurocopter France
• Inventors: Girard, Laurent Jean Daniel, Manfredotti, Thomas Pierre Louis
• Primary Examiner(s): Shoop, Jr., William M.
• Assistant Examiner(s): LOCKETT, KIMBERLY R
• Application Number:
  US08/728,036
• Time in Patent Office: 720 Days
• Field of Search: 318/460, 318/611, 52/167.1, 52/167.2, 52/167.3, 310/15, 310/16, 310/17
• US Class Current: 318/611
• CPC Class Codes: F16F 2230/0052 Physically guiding or influencing
• CPC Class Codes: F16F 2230/0082 Dimensional tolerances, e.g. play between mechanical elements
• CPC Class Codes: F16F 7/1005 characterised by active control of the mass

Abstract

The present invention relates to a device (1) for damping the vibrations of a structure (2) subjected to dynamic stresses, of the type including a main mass (3) mounted on an elastic plate (4) which is itself fitted into the structure (2) whose vibrations are to be damped.

According to the invention, the damping device (1) additionally comprises at least one auxiliary mass (5) connected to said main mass (3) and capable of being moved at least substantially parallel to said elastic plate (4) as a function of the control pulses which are received from a computer (9) and are computed from signals output by a first (10) and/or a second accelerometer (11) respectively measuring the vibrations of said structure (2) and those of said main mass (3).

Claims

1. A device (1) for damping the vibrations of a structure (2) subjected to dynamic stresses, of the type including a main mass (3) mounted on an elastic plate (4) which is itself fitted into the structure (2) whose vibrations are to be damped, the position of said main mass (3) along said plate (4) being initially adjusted in such a way that the natural frequency (F) of the damping device (1) is equal to the frequency (Fe) of the vibrations of the structure (2) which are to be damped, wherein, in order to match the natural frequency (F) of the damping device (1) continuously to the frequency (Fe) of the vibrations of the structure (2) which are to be damped, the damping device (1) additionally comprises at least one auxiliary mass (5) guided axially without any radial play in a sleeve (13) connected to said main mass (3) by means of a support (6) and capable of being moved at least substantially parallel to said elastic plate (4) by a motor (7) mounted on said support (6) and receiving control pulses from a computer (9), said control pulses being computed from signals output by at least one of two accelerometers (10, 11) respectively measuring the vibrations of said structure (2) and those of said main mass (3).

2. The device as claimed in claim 1, wherein said auxiliary mass (5) consists of two masses (5A, 5B) which are guided axially in said sleeve (13) and are capable of executing a translational movement on shaft (8) of said motor (7), a prestressed spring (14) being provided between the two said masses (5A, 5B) in order to eliminate the axial plays.

3. The device as claimed in claim 1, wherein, in order to eliminate the radial plays, said auxiliary mass (5), guided in said sleeve (13), has a set of contact pads (17) pressed by a spring (18) against the internal face of said sleeve (13).

4. The device as claimed in claim 2, wherein said shaft (8) is produced in the form of an endless screw rotated by said motor (7) fixed to one end of said sleeve (13).

5. The device as claimed in claim 1, wherein said motor (7) is an electric stepper motor.

6. The device as claimed in claim 2, wherein the two said masses (5A, 5B) are prevented from rotating by means of a longitudinal groove (15) made in said sleeve (13), and two threaded rods (16), each fixed in one of said masses (5A, 5B).

7. The device as claimed in claim 2, wherein the auxiliary mass or masses (5) is or are prevented from rotating by shifting the axis of said screw (8) relative to the longitudinal axis of said sleeve (13).

8. The device as claimed in claim 1, wherein said support (6) is fixed, on the one hand, to said main mass (3) and to said elastic plate (4) and, on the other hand, to the assembly consisting of said auxiliary mass (5) and said motor (7).

9. The device as claimed in claim 1, which comprises two end-of-travel contacts (20) for the auxiliary mass (5).

10. The device as claimed in claim 1, wherein the servo control of said device (1) is an analog-type servo control.

11. The device as claimed in claim 10, wherein, in the case of analog servo control:

the signals of the two accelerometers (10,

     11) are filtered by a band-pass filter (100);

the filtered signals are then multiplied in an analog multiplier (101);

a voltage proportional to the cosine of the phase shift between the two signals is then obtained using a low-pass filter (102) and a dynamic detector (103) of the signal produced; and

the motor (7) is controlled using this voltage, the sign of which characterizes the position of the natural frequency (F) of the device (1) relative to the frequency (Fe) of the vibrations of the structure (2) which are to be damped.

12. The device as claimed in claim 1, wherein the servo control of said device (1) is digital-type servo control.

13. The device as claimed in claim 12, wherein, in the case of digital servo control:

after having measured the frequency of the vibrations to be damped, the component at this frequency in the signals of the two accelerometers (10,

     11) is extracted digitally (110); and

the displacement of the auxiliary mass (5) is controlled by calculating the phase shift between the harmonics of the signals of the accelerometers (10,

     11), the value of this shift relative to 90°

characterizing the position of the natural frequency (F) of the device (1) relative to the frequency (Fe) of the vibrations of the structure (2) which are to be damped.