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CA2348320A1 - Modal analysis method and apparatus therefor - Google Patents

Modal analysis method and apparatus therefor Download PDF

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Publication number
CA2348320A1
CA2348320A1 CA 2348320 CA2348320A CA2348320A1 CA 2348320 A1 CA2348320 A1 CA 2348320A1 CA 2348320 CA2348320 CA 2348320 CA 2348320 A CA2348320 A CA 2348320A CA 2348320 A1 CA2348320 A1 CA 2348320A1
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CA
Canada
Prior art keywords
sets
acoustic pressure
input
data
vibration
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
CA 2348320
Other languages
French (fr)
Other versions
CA2348320C (en
Inventor
Marc Thomas
Frederic Laville
Francois Lafleur
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Centre de Recherche Industrielle du Quebec CRIQ
Original Assignee
Centre de Recherche Industrielle du Quebec CRIQ
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Centre de Recherche Industrielle du Quebec CRIQ filed Critical Centre de Recherche Industrielle du Quebec CRIQ
Priority to CA 2348320 priority Critical patent/CA2348320C/en
Publication of CA2348320A1 publication Critical patent/CA2348320A1/en
Application granted granted Critical
Publication of CA2348320C publication Critical patent/CA2348320C/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00Vibration-testing of structures; Shock-testing of structures

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)

Abstract

A modal analysis method and apparatus for acoustically determining dynamic vibration characteristics of a structure, including natural frequencies, mode shapes and damping factors, is based on a Multiple-Input-Single-Output (MISO) model. The method and apparatus involve generation of an acoustic excitation signal toward n spatially distributed locations associated with the structure while the latter is held to allow vibration thereof, one of the locations being chosen as a reference location. A series of microphones are disposed at the locations to produce m complementary sets of n input acoustic pressure-related electrical signals, one of these being chosen as a reference signal associated with the reference location. A Fourier analysis is performed on the sets of input acoustic pressure-related electrical signals to provide corresponding sets of correlated input acoustic pressure-related data in the frequency domain including reference data associated with the reference signal. A vibration transducer such as an accelerometer is used to sense induced output vibration in response to the acoustic excitation at a reference point on the excited structure corresponding to the reference location to produce m complementary sets of output vibration response electrical signals, which are then converted through Fourier analysis into corresponding sets of output vibration response data in the frequency domain. Then, from relations between m corresponding complementary sets of n input transfer functions characterizing the correlation between each set of input acoustic pressure-related data and the reference data from one hand, and m sets of output vibration response data on the other hand, the structural transfer functions characterizing each said set of input acoustic pressure- related data are obtained. Finally, the dynamic vibratory characteristics of the acoustically excited structure are derived from the resulting structural transfer functions through usual calculation techniques.
CA 2348320 2001-05-18 2001-05-18 Modal analysis method and apparatus therefor Expired - Lifetime CA2348320C (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CA 2348320 CA2348320C (en) 2001-05-18 2001-05-18 Modal analysis method and apparatus therefor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA 2348320 CA2348320C (en) 2001-05-18 2001-05-18 Modal analysis method and apparatus therefor

Publications (2)

Publication Number Publication Date
CA2348320A1 true CA2348320A1 (en) 2002-11-18
CA2348320C CA2348320C (en) 2006-01-17

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CA 2348320 Expired - Lifetime CA2348320C (en) 2001-05-18 2001-05-18 Modal analysis method and apparatus therefor

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114659765A (en) * 2022-02-28 2022-06-24 东风柳州汽车有限公司 Method, equipment, storage medium and device for testing constrained mode of gearbox shell
CN116299147A (en) * 2023-03-13 2023-06-23 中国科学院声学研究所 A sound source localization method in one-dimensional structure based on acoustic coherence technology

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114659765A (en) * 2022-02-28 2022-06-24 东风柳州汽车有限公司 Method, equipment, storage medium and device for testing constrained mode of gearbox shell
CN114659765B (en) * 2022-02-28 2024-07-16 东风柳州汽车有限公司 Method, equipment, storage medium and device for testing constraint mode of gearbox shell
CN116299147A (en) * 2023-03-13 2023-06-23 中国科学院声学研究所 A sound source localization method in one-dimensional structure based on acoustic coherence technology
CN116299147B (en) * 2023-03-13 2023-11-28 中国科学院声学研究所 One-dimensional structure internal sound source positioning method based on acoustic coherence technology

Also Published As

Publication number Publication date
CA2348320C (en) 2006-01-17

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Effective date: 20210518