IP Library Granted Patent US 8,672,107
Granted Patent B2
US 8,672,107 · App. 13/042,655 · Granted Mar 18, 2014

Compact vibration damper

Inventor: Thomas G. Ivanco (Newport News, VA)
Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
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Quick Facts
Patent No.
US 8,672,107
App. No.
13/042,655
Granted
Mar 18, 2014
Kind
B2
Abstract

A vibration damper includes a rigid base with a mass coupled thereto for linear movement thereon. Springs coupled to the mass compress in response to the linear movement along either of two opposing directions. A converter coupled to the mass converts the linear movement to a corresponding rotational movement. A rotary damper coupled to the converter damps the rotational movement.

Claims (28)

1. A vibration damper, comprising:

a rigid base;

a mass coupled to said base for linear movement thereon; a first spring coupled to said mass, said first spring compressing in response to said linear movement along a first direction;

a second spring coupled to said mass, said second spring compressing in response to said linear movement along a second direction that is opposite to said first direction;

a rotary damper; and

a converter coupled between said mass and said rotary damper, for converting said linear movement to a corresponding rotational movement, wherein said rotational movement is damped by said rotary damper.

2. A vibration damper as in claim 1 , further comprising at least one ballast weight rigidly coupled to said base.

3. A vibration damper as in claim 1 , wherein said mass is adjustable in amount.

4. A vibration damper as in claim 1 , wherein said first spring and said second spring have spring rates that are equal.

5. A vibration damper as in claim 1 , wherein said damping provided by said rotary damper comprises viscous damping.

6. A vibration damper, comprising: a rigid base; a slider assembly including a linear rail rigidly coupled to said base and a block slidingly coupled to said linear rail wherein said block is capable of and constrained to linear movement along said linear rail; a mass coupled to said block; a first spring coupled to said base and said block, said first spring compressing in response to said linear movement along a first direction; a second spring coupled to said base and said block, said second spring compressing in response to said linear movement along a second direction that is opposite to said first direction; a converter coupled to said block for converting said linear movement to a corresponding rotational movement; and a rotary damper coupled to said converter for viscously damping said rotational movement.

7. A vibration damper as in claim 6 , further comprising at least one ballast weight rigidly coupled to said base.

8. A vibration damper as in claim 6 , wherein said mass is adjustable in amount.

9. A vibration damper as in claim 6 , wherein said first spring and said second spring have spring rates that are equal.

10. A vibration damper, comprising:

a rigid U-shaped bracket having opposing legs extending from a flat base;

a slider assembly including a linear rail rigidly coupled to said flat base and a block slidingly coupled to said linear rail wherein said block is capable of and constrained to linear movement along said linear rail;

a support housing coupled to said block wherein said linear movement of said block is imparted to said support housing;

a mass coupled to said support housing;

a first spring coupled between a first of said opposing legs and said one side of said support housing, said first spring compressing in response to said linear movement along a first direction; a second spring coupled between a second of said opposing legs and another side of said support housing, said second spring compressing in response to said linear movement along a second direction that is opposite to said first direction;

a converter coupled to said flat base and said support housing for converting said linear movement to a corresponding rotational movement; and

a rotary damper coupled to said converter for viscously damping said rotational movement.

11. A vibration damper as in claim 10 , further comprising at least one ballast weight rigidly coupled to said flat base.

12. A vibration damper as in claim 10 , wherein said mass is adjustable in amount.

13. A vibration damper as in claim 10 , wherein said first spring and said second spring have spring rates that are equal.

14. A vibration damper as in claim 10 , further comprising a support rod fixed to each of said opposing legs and extending through said support housing wherein said support housing moves relative to said support rod during said linear movement.

15. A vibration damper as in claim 14 , wherein said first spring and said second spring are disposed about said support rod.

16. A vibration damper as in claim 15 , wherein said first spring and said second spring have spring rates that are equal.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 8, 2011
From: IVANCO, THOMAS G.
To: UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION
Reel/Frame 025917/0410 →
Continuity (2)
Provisional Application 61312757 · Mar 11, 2010
Related Publication 20110220443A1 · Sep 15, 2011