Methods and apparatus to monitor a condition of a structure

Patent metadata

Field	Value
Publication number	US-10436759-B2
Application number	US-201715404839-A
Country	US
Kind code	B2
Filing date	Jan 12, 2017
Priority date	Jan 12, 2017
Publication date	Oct 8, 2019
Grant date	Oct 8, 2019

Abstract

Methods, apparatus, and articles of manufacture to monitor a condition of a structure are disclosed. An example apparatus includes an operational collection engine to measure first operational acceleration information from a first sensor installed at a first location and second operational acceleration information from a second sensor installed at a second location on a structure, a first vibration model response calculator to calculate a first vibration model response by entering the measured first and second operational acceleration information into a first vibration model, a second vibration model response calculator to calculate a second vibration model response by entering a calculated number of operational cycles into a second vibration model, a deviation threshold analyzer to determine a difference between the first vibration model response and the second vibration model response and an alert generator to generate an alert to identify a condition of the structure based on the difference between the first vibration model response and the second vibration model response.

First claim

What is claimed is:

1. An apparatus comprising:
an operational collection engine to measure first operational acceleration information from a first sensor installed at a first location and second operational acceleration information from a second sensor installed at a second location on a structure;
a first vibration model response calculator to calculate a first vibration model response by entering the measured first and second operational acceleration information into a first vibration model, the first vibration model response including a first natural frequency, the first natural frequency to be calculated by determining a transmissibility based on a ratio of the first operational acceleration information and the second operational acceleration information;
a second vibration model response calculator to calculate a second vibration model response by entering a calculated number of operating cycles into a second vibration model, the second vibration model response including a second natural frequency, the second vibration model to be generated by:
determining an average natural frequency based on natural frequencies associated with acceleration responses measured by the first sensor and the second sensor; and
determining an average natural frequency difference based on an average of differences between the average natural frequency and the natural frequencies associated with the acceleration responses; and

an alert generator to generate an alert to identify a condition of the structure based on a difference between the first vibration model response and the second vibration model response.

2. The apparatus of claim 1 , further including:
a baseline collection engine to measure first baseline acceleration information from the first sensor and second baseline acceleration information from the second sensor;
a transmissibility model generator to generate the first vibration model for the structure; and
a natural frequency model generator to generate the second vibration model for the structure.

3. The apparatus of claim 2 , wherein the transmissibility model generator is configured to generate the first vibration model for the structure by performing a curve fit for calculated transmissibility information, the calculated transmissibility information based on the first baseline acceleration information and the second baseline acceleration information.

4. The apparatus of claim 2 , wherein the natural frequency model generator is configured to generate the second vibration model for the structure by:
determining calculated natural frequency information based on the first baseline acceleration information and the second baseline acceleration information, the calculated natural frequency information including the average natural frequency and the average natural frequency difference;
determining a slope based on a ratio of the average natural frequency difference and a first quantity of the acceleration responses; and
performing a linear curve fit for the calculated natural frequency information, the linear curve fit based on a sum of (1) the average natural frequency and (2) a multiplication of a second quantity of operating cycles and the slope.

5. The apparatus of claim 1 , wherein the alert generator is configured to identify the condition of the structure when a difference between the first natural frequency and the second natural frequency satisfies a threshold.

6. The apparatus of claim 1 , wherein the condition of the structure is a degradation of the structure.

7. A method comprising:
measuring first operational acceleration information from a first sensor installed at a first location and second operational acceleration information from a second sensor installed at a second location on a structure;
calculating a first vibration model response by entering the measured first and second operational acceleration information into a first vibration model, the first vibration model response including a first natural frequency, the first natural frequency to be calculated by determining a transmissibility based on a ratio of the first operational acceleration information and the second operational acceleration information;
calculating a second vibration model response by entering a calculated number of operating cycles into a second vibration model, the second vibration model response including a second natural frequency, the second vibration model to be generated by:
determining an average natural frequency based on natural frequencies associated with acceleration responses measured by the first sensor and the second sensor; and
determining an average natural frequency difference based on an average of differences between the average natural frequency and the natural frequencies associated with the acceleration responses; and

identifying a condition of the structure based on a difference between the first vibration model response and the second vibration model response.

8. The method of claim 7 , further including:
measuring first baseline acceleration information from the first sensor and second baseline acceleration information from the second sensor; and
generating the first vibration model and the second vibration model for the structure based on the baseline acceleration information measured by the sensors.

9. The method of claim 8 , wherein generating the first vibration model includes performing a curve fit for calculated transmissibility information, the calculated transmissibility information based on the first baseline acceleration information and the second baseline acceleration information.

10. The method of claim 8 , wherein generating the second vibration model includes:
determining calculated natural frequency information based on the first baseline acceleration information and the second baseline acceleration information, the calculated natural frequency information including the average natural frequency and the average natural frequency difference;
determining a slope based on a ratio of the average natural frequency difference and a first quantity of the acceleration responses; and
performing a linear curve fit for the calculated natural frequency information, the linear curve fit based on a sum of (1) the average natural frequency and (2) a multiplication of a second quantity of operating cycles and the slope.

11. The method of claim 8 , wherein the determining of the difference between the first vibration model response and the second vibration model response includes determining a difference between the first natural frequency and the second natural frequency.

12. The method of claim 11 , wherein the identifying the condition of the structure based on the difference between the first vibration model response and the second vibration model response includes determining when the difference between the first and second natural frequencies satisfies a threshold.

13. A tangible computer-readable storage medium comprising instructions which, when executed, cause a machine to at least:
measure first operational acceleration information from a first sensor installed at a first location and second operational acceleration information from a second sensor installed at a second location on a structure;
calculate a first vibration model response by entering the measured first and second operational acceleration information into a first vibration model, the first vibration model response including a first natural frequency, the first natural frequency to be calculated by determining a transmissibility based on a ratio of the first operational acceleration information and the second operational acceleration information;
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Assignees

• Fisher Controls Int Llc

Inventors

• Mann Iii Julian Adin
• Myers Jessica Dawn

Classifications

• G01N29/4418 Primary

  with a model, e.g. best-fit, regression analysis · CPC title

• G01N29/46

  by spectral analysis, e.g. Fourier analysis {or wavelet analysis (spectral signal processing per se G06F17/14)} · CPC title

• G05B23/024 Primary

  Quantitative history assessment, e.g. mathematical relationships between available data; Functions therefor; Principal component analysis [PCA]; Partial least square [PLS]; Statistical classifiers, e.g. Bayesian networks, linear regression or correlation analysis; Neural networks · CPC title

• G01N29/12

  by measuring frequency or resonance of acoustic waves {(measuring frequency or resonant frequency of mechanical vibrations or acoustic waves in general G01H1/06, G01H3/04, G01H13/00; acoustic resonators G10K11/04; vibration or shock testing of structures G01M7/00)} · CPC title

• G05B19/4183 Primary

  characterised by data acquisition, e.g. workpiece identification · CPC title