Vibration control apparatus

• US 6,501,203 B2
• Filed: 06/01/2001
• Issued: 12/31/2002
• Est. Priority Date: 06/01/2001
• Status: Expired due to Fees

• Current Assignee: Canadian Space Agency (Government of Canada)
• Original Assignee: Canadian Space Agency (Government of Canada)
• Inventors: Tryggvason, Bjarni V.
• Primary Examiner(s): Lavinder, Jack
• Assistant Examiner(s): Pezzlo, Benjamin A
• Application Number:
  US09/870,635
• Publication Number:
  US 20020179385A1
• Time in Patent Office: 578 Days
• Field of Search: 267/140.15, 267/150, 267/140.5, 267/136, 244/158.R, 244/166, 248/550, 248/638, 310/90.5, 335/285, 335/306, 335/286, 335/287, 361/144, 361/142, 361/146, 188/266.1
• US Class Current: 310/90.5
• 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 15/03 using magnetic or electromagnetic means F16F9/53, F16F15/005 take precedence

Abstract

A vibration control apparatus designed specifically for use on space vehicles includes a stator for mounting in the vehicle, a lower flotor, magnetically levitated on the stator, an upper flotor nested in and magnetically levitated on the lower flotor, and position, orientation and motion sensors carried by the stator and flotors. When any changes in position, orientation or movement, i.e. vibration of apparatus is detected, magnetic force actuators are energized to compensate for such changes to keep a work platform on the upper flotor virtually vibration-free. Moreover, controlled and induced vibration of the work platform and an experiment carried thereby can be effected using the lower flotor as a reaction mass, i.e. without feedback to the vehicle.

Claims

1. A vibration control apparatus comprising:

(a) stator means for mounting on a fixed surface;

(b) lower flotor means normally spaced apart from said stator means in nesting relationship thereto;

(c) an upper flotor means normally spaced apart from said lower flotor means in nesting relationship thereto;

(d) overlapping fence means on said stator means and on said lower and upper flotor means;

(e) work platform means on said upper flotor means;

(f) position sensing means associated with said stator means, lower flotor means and upper flotor means for determining the position and orientation of said lower flotor means and said upper flotor means relative to said stator means;

(g) accelerometer means associated with said stator means, lower flotor means and upper flotor means for determining acceleration of said lower flotor means and upper flotor means with respect to inertial space; and

(h) vertical and horizontal magnetic force actuator means associated with said stator means, lower flotor means and upper flotor means for imparting motion to said lower flotor means and to said upper flotor means to compensate for vibration of said stator means, whereby vibration of said work platform is minimized, said force actuator means including;

(i) coil means on said stator means and on said upper flotor means; and

(ii) magnet means on said lower flotor means aligned with said coil means for interacting with said coil means to magnetically levitate the lower and upper flotors with respect to said stator means.

2. The vibration control apparatus of claim 1, wherein said position sensing means includes light emitting diodes on said lower and upper stator means for emitting collimated horizontal beams of light longitudinally and transversely of the apparatus;

and position sensing detectors on said stator means for receiving light from said light emitting diodes to provide an indication of the position and orientation of the lower and upper flotor means relative to said stator means.

3. The vibration control apparatus of claim 2, wherein said accelerometer means includes:

(i) first accelerometers on said lower flotor means for detecting vertical and horizontal movement and rotational acceleration of said lower flotor means relative to inertial space; and

(ii) second accelerometer means on said upper flotor means for detecting vertical and horizontal movement of said upper flotor means relative to inertial space.

4. The vibration control apparatus of claim 1, wherein said fence means includes:

(i) a first square fence extending upwardly from said stator means;

(ii) a second square fence on said lower flotor means overlapping said first fence; and

(iii) a third square fence nested in said second fence on said lower flotor means.

5. The vibration control apparatus of claim 4, wherein said second fence defines a hollow square, the sides of the square having a crenellated cross section defining pockets for receiving said first and third square fences.