Method for vibration analysis

• US 6,779,404 B1
• Filed: 05/03/2002
• Issued: 08/24/2004
• Est. Priority Date: 11/03/1999
• Status: Expired due to Term

• Current Assignee: Structural Vibrations Solutions A/S
• Original Assignee: Palle Andersen, Rune Brincker
• Inventors: Andersen, Palle, Brincker, Rune
• Primary Examiner(s): Williams, Hezron
• Assistant Examiner(s): SAINT SURIN, JACQUES M
• Application Number:
  US10/129,302
• Time in Patent Office: 844 Days
• Field of Search: 736/59, 736/60, 736/62, 735/83, 735/86, 735/79, 735/97, 735/98, 736/00, 736/02, 702/182, 702/189, 702/56, 381/71
• US Class Current: 73/659
• CPC Class Codes: G01M 5/0066 by exciting or detecting vibration or acceleration vibration testing of structures G01M7/00
• CPC Class Codes: G01M 7/00 Vibration-testing of structures; Shock-testing of structures G01M9/00 takes precedence
• CPC Class Codes: G01M 7/025 Measuring arrangements

Abstract

Output-only modal testing of an object. Vibrations are excited in said object and measured by a number of vibration sensitive detectors. From the data of the measurements, a spectral density matrix function is determined. From this density matrix, auto spectral densities for the individual modes are identified performing a decomposition based on the Singular Value Decomposition technique. From the auto spectral densities of the individual modes, natural frequencies and damping ratios for the modes can be estimated, and from the singular vectors of the Singular Value Decomposition, the modes shapes can be estimated.

Claims

1. Method for testing an object with respect to its vibration modes, comprising exciting vibrations in said object, measuring said excited vibrations by at least one vibration sensitive detector, and obtaining data quantitative of said excited vibrations of said object, wherein the method further comprises;

determining a spectral density function

identifying in said spectral density function at least one auto spectral density function corresponding to a single degree of freedom system and obtaining a decomposition of said excited vibrations into mutually independent vibration modes.

2. Method according to claim 1, wherein the decomposition comprises the Singular Value Decomposition of the spectral density matrix at individual frequency lines.

3. Method according to claim 1, wherein said auto spectral densities are identified using the known modal assurance criterion (MAC).

4. Method according to claim 1, wherein said auto spectral function is transformed by Inverse Fourier Transform for determination of the vibration damping characteristics of said object and/or the natural frequency of the vibration mode.

5. Method according to claim 1, wherein the determination of said spectral density function comprises Fast Fourier Transform.

6. Computer program using a method according to claim 1.

7. A method according to claim 1, wherein said object is

biomechanical systems as the human body, animal body, plants, or parts thereof,

civil engineering structures such as buildings, bridges or dams,

structural parts such as wood members, concrete members, or metal members, or

members in mechanical structures like heavy machinery, rotating machinery, brake disks, engine blocks, turbines, aeroplanes, rockets, or satellites.

8. Method for testing an object with respect to its vibration modes, comprising exciting vibrations in said object, measuring said excited vibrations by at least one vibration sensitive detector, and obtaining data quantitative of said excited vibrations of said object, wherein the method further comprises

determining a spectral density function

identifying in said spectral density function at least one auto spectral density function corresponding to a single degree of freedom system and obtaining a decomposition of said excited vibrations into mutually independent vibration modes,

wherein the determination of said spectral density function comprises Fast Fourier Transform, and wherein the determination of said spectral density function further comprises Random Decrement Transform of said data preceded by the Fast Fourier Transform.

9. Method according to the claim 8, wherein said the determination of said spectral density function comprises Random Decrement Transform at different trigger levels as a control for non-linearities of the system response.

10. Method for testing an object with respect to its vibration modes, comprising exciting vibrations in said object, measuring said excited vibrations by at least one vibration sensitive detector, and obtaining data quantitative of said excited vibrations of said object, wherein the method further comprises

determining a spectral density function

identifying in said spectral density function at least one auto spectral density function corresponding to a single degree of freedom system and obtaining a decomposition of said excited vibrations into mutually independent vibration modes,

wherein said determination of said spectral density function comprises the derivative of the covariance function obtained by the Random Decrement Transform of the time data.