<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">IIM</journal-id><journal-title-group><journal-title>Intelligent Information Management</journal-title></journal-title-group><issn pub-type="epub">2160-5912</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/iim.2016.84007</article-id><article-id pub-id-type="publisher-id">IIM-68236</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Computer Science&amp;Communications</subject></subj-group></article-categories><title-group><article-title>
 
 
  Statistical Fault Diagnosis Methods by Using Higher-Order Correlation Information between Sound and Vibration
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Hisako</surname><given-names>Orimoto</given-names></name><xref ref-type="aff" rid="aff1"><sub>1</sub></xref></contrib></contrib-group><aff id="aff1"><label>1</label><addr-line>Department of Management Information Systems, Prefectural University of Hiroshima, Hiroshima, Japan</addr-line></aff><author-notes><corresp id="cor1">* E-mail:</corresp></author-notes><pub-date pub-type="epub"><day>12</day><month>07</month><year>2016</year></pub-date><volume>08</volume><issue>04</issue><fpage>87</fpage><lpage>97</lpage><history><date date-type="received"><day>6</day>	<month>April</month>	<year>2016</year></date><date date-type="rev-recd"><day>accepted</day>	<month>9</month>	<year>July</year>	</date><date date-type="accepted"><day>12</day>	<month>July</month>	<year>2016</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
  It is important to specify the occurrence and cause of failure of machines without stopping the machines because of increased use of various complex industrial systems. In this study, two new diagnosis methods based on the correlation information between sound and vibration emitted from the machine are derived. First, a diagnostic method which can detect the part of machine with fault among the assumed several faults is proposed by measuring simultaneously the time series data on sound and vibration. Next, a diagnosis method based on the estimation of the changing information of correlation between sound and vibration is considered by using prior information in only normal situation. The effectiveness of the proposed theory is experimentally confirmed by applying it to the observed data emitted from a rotational machine driven by an electric motor.
 
</p></abstract><kwd-group><kwd>Statistical Faults Diagnosis</kwd><kwd> Correlation Information</kwd><kwd> Sound and Vibration</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Recently, various industrial systems have increased and become complicated. The estimation and prediction of damage part in rotational machines without stopping these are required for cost reduction and improvement of safety. Most of studies proposed up to now for the diagnosis have analyzed by use of either of sound or vibration emitted from the machine in frequency domain [<xref ref-type="bibr" rid="scirp.68236-ref1">1</xref>] - [<xref ref-type="bibr" rid="scirp.68236-ref9">9</xref>] . These standard methods in frequency domain are useful for analyzing each mechanical failure based on the internal mechanism. However, these methods require a lot of procedures on signal processing for measured sound and vibration data.</p><p>In the previous study, a faults diagnosis method was proposed by using correlation information between sound and vibration emitted from a machine in time domain [<xref ref-type="bibr" rid="scirp.68236-ref10">10</xref>] . However, this method required correlation information of sound and vibration in both normal and failure situations in advance.</p><p>In this study, by utilizing correlation information between sound and vibration emitted from the machine more effectively, a new faults diagnosis method is derived from two points of view. More specifically, a faults diagnosis method based on the conditional probability distribution reflected liner and non-liner correlation information of lower or higher order between sound and vibration is proposed. When a specific failure occurs among multiple faults established in advance, a diagnosis method able to detect the machine part with the failure is proposed. By adopting expansion expression of conditional probability distribution based on the multinomial distribution to evaluate several failure situations, a new faults diagnosis method of machine is first proposed. Next, a faults diagnosis method to find change of correlation information between sound and vibration is considered by measuring simultaneously the sound and vibration only in normal situation as prior information. Finally, the effectiveness of proposed theoretical method is experimentally confirmed by applying it to measurement data of sound and vibration emitted from a rotational machine.</p></sec><sec id="s2"><title>2. Theory</title><sec id="s2_1"><title>2.1. Estimation of Probability for Fault Occurrence (Summary [<xref ref-type="bibr" rid="scirp.68236-ref10">10</xref>] )</title><p>First, let us introduce a random variable y with two exclusive values of 0 and 1 corresponding to normal situation without fault of machines and a failure situation with the fault. Furthermore, two kinds of variables on sound and vibration are expressed as <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x6.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x7.png" xlink:type="simple"/></inline-formula>. In the case of paying attention to the variables<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x8.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x9.png" xlink:type="simple"/></inline-formula>, and y, all the information on mutual correlations among<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x10.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x11.png" xlink:type="simple"/></inline-formula>, and y is included in the conditional probability distribution<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x12.png" xlink:type="simple"/></inline-formula>. By using the well-known Bayes’ theorem:</p><disp-formula id="scirp.68236-formula121"><label>(1)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x13.png"  xlink:type="simple"/></disp-formula><p>the probability of fault occurrence can be predicted in an expansion expression, as follows:</p><disp-formula id="scirp.68236-formula122"><label>(2)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x14.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula123"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x15.png"  xlink:type="simple"/></disp-formula><p>where, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x16.png" xlink:type="simple"/></inline-formula>denotes the averaging operation with respect to the random variables. As the fundamental probability density function<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x17.png" xlink:type="simple"/></inline-formula>, the generalized binomial distribution is adopted, and the orthonormal functions can be determined as</p><disp-formula id="scirp.68236-formula124"><label>(3)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x18.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula125"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x19.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula126"><label>(4)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x20.png"  xlink:type="simple"/></disp-formula><p>with</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x21.png" xlink:type="simple"/></inline-formula>; the maximum value of y,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x21.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x22.png" xlink:type="simple"/></inline-formula>; the minimum value of y,</p><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x23.png" xlink:type="simple"/></inline-formula>; the level difference interval of y.</p><p>By use of a computer for the observed time series data on sound and vibration, on-line signal processing can easily be carried out.</p></sec><sec id="s2_2"><title>2.2. Expression of Probability Distribution for Diagnosis Method of a Specific Failure among Multiple Faults</title><p>Since the specific correlation relationship between sound and vibration emitted from an identical machine exists, it is possible to diagnose faults of the machine by detecting the change of correlation characteristic between sound and vibration. As examples of multiple faults of machine, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x24.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x24.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x25.png" xlink:type="simple"/></inline-formula> express the state variables corresponding to fault 1 and fault 2. In this section, when a specific failure occurs among multiple faults established in advance, a diagnosis method able to detect the machine part with the failure is proposed.</p><p>First, the joint probability distributions <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x26.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x26.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x27.png" xlink:type="simple"/></inline-formula> are expanded into an orthonormal polynomial series.</p><disp-formula id="scirp.68236-formula127"><label>(5)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x28.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula128"><label>(6)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x29.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula129"><label>(7)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x30.png"  xlink:type="simple"/></disp-formula><p>where, correlation information among variables with lower and higher orders is reflected in the expansion coefficient<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula>. Here, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x32.png" xlink:type="simple"/></inline-formula>and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x33.png" xlink:type="simple"/></inline-formula> are orthonormal polynomials with two weighing functions<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x34.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x35.png" xlink:type="simple"/></inline-formula>, respectively. As the fundamental probability density functions<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x36.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x31.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x32.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x33.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x34.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x35.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x36.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x37.png" xlink:type="simple"/></inline-formula>, Gaussian distribution is adopted.</p><disp-formula id="scirp.68236-formula130"><label>(8)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x38.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula131"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x39.png"  xlink:type="simple"/></disp-formula><p>Thus, from Equation (8), the orthonormal functions can be determined as the Hermite polynomial [<xref ref-type="bibr" rid="scirp.68236-ref11">11</xref>] .</p><disp-formula id="scirp.68236-formula132"><label>(9)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x40.png"  xlink:type="simple"/></disp-formula><p>Furthermore, a trinomial distribution is adopted as the standard distribution <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x41.png" xlink:type="simple"/></inline-formula> expressing two kinds faults states.</p><disp-formula id="scirp.68236-formula133"><label>(10)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x42.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula134"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x43.png"  xlink:type="simple"/></disp-formula><p>Two variables <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x44.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x44.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x45.png" xlink:type="simple"/></inline-formula> correspond to the following states.</p><p>Normal:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x46.png" xlink:type="simple"/></inline-formula>, Fault 1:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x46.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x47.png" xlink:type="simple"/></inline-formula>, Fault 2:<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x46.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x47.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x48.png" xlink:type="simple"/></inline-formula>,</p><p>where<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x49.png" xlink:type="simple"/></inline-formula>, p is probability of fault 1 and q is probability of fault 2. Thus, from Equation (10), the orthonormal function [<xref ref-type="bibr" rid="scirp.68236-ref11">11</xref>] can be determined as</p><disp-formula id="scirp.68236-formula135"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x50.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula136"><label>(11)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x51.png"  xlink:type="simple"/></disp-formula><p>Therefore, the arbitrary constants are determined as<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x52.png" xlink:type="simple"/></inline-formula>, and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x52.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x53.png" xlink:type="simple"/></inline-formula> is a factorial function [<xref ref-type="bibr" rid="scirp.68236-ref11">11</xref>] of th order defined as</p><disp-formula id="scirp.68236-formula137"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x54.png"  xlink:type="simple"/></disp-formula><p><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x55.png" xlink:type="simple"/></inline-formula>,<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x55.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x56.png" xlink:type="simple"/></inline-formula>; discrete level interval of y.</p><p>The coefficients <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x57.png" xlink:type="simple"/></inline-formula> are decided by the normalized condition for the probability.</p><disp-formula id="scirp.68236-formula138"><label>(12)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x58.png"  xlink:type="simple"/></disp-formula><p>Furthermore, in the case of considering more than three kinds of failures, a multinomial distribution can be adopted as the standard distribution of Equation (10). It is possible to derive the fault diagnosis in the same manners as the present study by calculating orthogonal polynomial based on the preciously published method [<xref ref-type="bibr" rid="scirp.68236-ref11">11</xref>] .</p><p>The following expression can be obtained from Equations ((5), (6)), using Bayes’ theorem on conditional probability distribution.</p><disp-formula id="scirp.68236-formula139"><label>(13)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x59.png"  xlink:type="simple"/></disp-formula><p>Therefore, fault occurrence probability <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x60.png" xlink:type="simple"/></inline-formula> is predicted from observation data of sound and vibration by considering the conditional expectation of Equation (13).</p><disp-formula id="scirp.68236-formula140"><label>(14)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x61.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula141"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x62.png"  xlink:type="simple"/></disp-formula></sec><sec id="s2_3"><title>2.3. Expression of Probability Distribution for Fault Diagnosis Based on Only Prior Information</title><p>Since the specific correlation relationship between sound and vibration emitted from an identical machine exists, it is possible to diagnose faults of the machine by detecting the change of correlation characteristic between sound and vibration.</p><p>The fault diagnosis methods proposed in 2.1 and 2.2 require prior information in both situations before and after a failure occurs. However, only the prior information before the failure occurs can be really obtained. In this section, a faults diagnosis method is proposed based on only prior information in normal situation. The variables<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x63.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x63.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x64.png" xlink:type="simple"/></inline-formula>are sound and vibration emitted from rotational machine, respectively. The faults occurrence can be diagnosed from changing information of the correlation of between sound and vibration.</p><p>First, the joint probability distribution <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x65.png" xlink:type="simple"/></inline-formula> is obtained in an orthonormal polynomial series.</p><disp-formula id="scirp.68236-formula142"><label>(15)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x66.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula143"><label>(16)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x67.png"  xlink:type="simple"/></disp-formula><p>Gaussian distribution is used as the standard distributions<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x68.png" xlink:type="simple"/></inline-formula>, and the Hermite polynomial is determined as the orthonormal polynomials. Then, the probability distribution <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x68.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x69.png" xlink:type="simple"/></inline-formula> for sound can be predicted from the vibration data, as follows:</p><disp-formula id="scirp.68236-formula144"><label>(17)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x70.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula145"><label>(18)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x71.png"  xlink:type="simple"/></disp-formula><p>Since the correlation information between <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x72.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x72.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x73.png" xlink:type="simple"/></inline-formula> change when a fault occurs, the prediction of <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x72.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x73.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x74.png" xlink:type="simple"/></inline-formula> becomes difficult from Equation (18). Therefore, it is possible to diagnose the faults occurrence by evaluating the prediction error.</p><p>In general, cumulative distribution is more suitable than probability distribution for evaluating the prediction error.</p><p>There, by using Equation (18) cumulative distribution <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x75.png" xlink:type="simple"/></inline-formula> is given by the following equation.</p><disp-formula id="scirp.68236-formula146"><label>(19)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x76.png"  xlink:type="simple"/></disp-formula><p>with</p><disp-formula id="scirp.68236-formula147"><label>(20)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x77.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula148"><label>(21)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x78.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula149"><label>(22)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x79.png"  xlink:type="simple"/></disp-formula><p>Furthermore, the faults diagnosis based on the prediction error when evaluating the probability distribution of vibration from sound data is also possible by exchanging the variable <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x80.png" xlink:type="simple"/></inline-formula> for <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x80.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x81.png" xlink:type="simple"/></inline-formula> in Equations ((18)-(22)).</p></sec></sec><sec id="s3"><title>3. Experiment</title><p>The proposed method was used to detect faults of a rotational machine by simultaneously observing the sound and vibration emitted from the machine. The correlation relationship between the sound and vibration in the case of failure situations changes from the correlation characteristic in the absence of a fault. Therefore, by detecting information on the change of the correlation characteristic between sound and vibration, it is possible in principle to predict machine faults. The RMS values of the sound pressure level (dB) and the acceleration amplitude (m/s<sup>2</sup>) emitted from a rotational machine driven by an electric motor were simultaneously measured, as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>.</p><p>As an example of fault, three weights were put on the lower part of the bearing and the distortion was made. As the other example of fault, a cogwheel with a small scratch was adopted. The distortion of bearing and the existence of a scratch on a cogwheel were considered for fault 1 and fault 2 as a trial. The 5000 data points were measured for normal, fault 1 and fault 2. The observation data were transformed to the sound pressure level and the acceleration amplitude by use of the following relation.</p><disp-formula id="scirp.68236-formula150"><label>(23)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x82.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula151"><label>(24)</label><graphic position="anchor" xlink:href="http://html.scirp.org/file/1-8701396x83.png"  xlink:type="simple"/></disp-formula><p>P: sound pressure [Pa],<inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x84.png" xlink:type="simple"/></inline-formula>: acceleration amplitude in each axis [m/s<sup>2</sup>].</p><fig id="fig1"  position="float"><label><xref ref-type="fig" rid="fig1">Figure 1</xref></label><caption><title> Experimental equipment</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x85.png"/></fig><p>The scatter diagram between the sound and vibration in three cases before and after occurrence of the fault in the machine is shown in <xref ref-type="fig" rid="fig2">Figure 2</xref>. <xref ref-type="fig" rid="fig2">Figure 2</xref>(a) shows the scatter diagram in normal situation without the fault.</p><fig-group id="fig2"><label><xref ref-type="fig" rid="fig2">Figure 2</xref></label><caption><title> Scatter diagram between sound and vibration for the observed data in three situations. (a) Normal situation without the fault; (b) Failure situation with the fault for a bearing; (c) Failure situation with the fault for a cogwheel.</title></caption><fig id ="fig2_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x86.png"/></fig><fig id ="fig2_2"><label>(c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x87.png"/></fig><fig id ="fig2_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x88.png"/></fig></fig-group><p>Furthermore, <xref ref-type="fig" rid="fig2">Figure 2</xref>(b) and <xref ref-type="fig" rid="fig2">Figure 2</xref>(c) show the scatter diagrams in failure situations with the fault on the bearing and the cogwheel. It is obvious that the correlation relationship between the sound and vibration in the cases of failure situations occurring of the fault changes from the correlation characteristic before the occurrence of the fault. Therefore, by detecting the changing information of the correlation characteristic between the sound and vibration, it is possible to predict the fault of the machine in principle.</p><sec id="s3_1"><title>3.1. Experimental Consideration for Diagnosis Method with Multiple Faults</title><p>First, two different time series data sets (Data Set 1 and Data Set 2) for sound and vibration in three different time intervals were successively measured, in cases with and without fault occurrence. Using the 1500 data points of Data Set 1, which contained both cases of faults occurrence (500 data points for each fault) and fault-free cases (500 data points) as the learning data, the expansion coefficients of Equation (7) were first evaluated. Next, after dividing each data set into 30 sub-data sets consisting of 500 data points with 450 overlapping points, the probability of fault occurrence <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x89.png" xlink:type="simple"/></inline-formula> was predicted by use of Equation (14) based on the 500 sampled data in each sub-data set. The relationship between each Data Set and the sub-data sets is illustrated in <xref ref-type="fig" rid="fig3">Figure 3</xref>.</p><p>The results of prediction of the probability for normal situation, failure situations with the fault 1 and 2 are shown in <xref ref-type="fig" rid="fig4">Figure 4</xref> for Data Set 1 and in <xref ref-type="fig" rid="fig5">Figure 5</xref> for Data Set 2. From these results, we can find that the fault probability clearly exhibits large values in the sub-data sets corresponding to the failure situation. More precise prediction of the fault probability is possible by considering correlation information of lower and higher orders, because the correlation characteristics (of lower and higher orders) between sound and vibration change after failure. Thus, the proposed method to detect precisely the change of correlation information is useful in the detection of machine failures.</p></sec><sec id="s3_2"><title>3.2. Experimental Consideration for Fault Diagnosis Method with Less Prior Information</title><p>The fault diagnosis method with less prior information proposed in 2.3 was applied to real observation data. First, the expansion coefficients in Equation (15) were calculated by using 1000 data points in normal situation. Next, sub-data sets with 1000 data points were made from total 15,000 data points consisting of each 5000 data points in normal, fault 1 and fault 2 situations. Furthermore, probability distribution of vibration (or sound) was predicted by observing the data of sound (or vibration) by using sub-data sets. One of the prediction results is shown in <xref ref-type="fig" rid="fig5">Figure 5</xref> in a form of cumulative distribution. The differences between experimental values and predicted values are shown in <xref ref-type="table" rid="table1">Table 1</xref>. Prediction errors at the 50% level and average of the prediction errors evaluated at every 10% level from the 10% level value to the 90% level value are shown in <xref ref-type="table" rid="table1">Table 1</xref>. The prediction errors were calculated from experimental values <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x90.png" xlink:type="simple"/></inline-formula> and predicted values <inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x90.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="http://html.scirp.org/file/1-8701396x91.png" xlink:type="simple"/></inline-formula> at 9 points, from the 10% level to the 90% level by using the following relationships.</p><fig id="fig3"  position="float"><label><xref ref-type="fig" rid="fig3">Figure 3</xref></label><caption><title> Relationship between data sets and sub-data sets</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x92.png"/></fig><fig id="fig4"  position="float"><label><xref ref-type="fig" rid="fig4">Figure 4</xref></label><caption><title> Prediction by use of the learning data</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x93.png"/></fig><fig id="fig5"  position="float"><label><xref ref-type="fig" rid="fig5">Figure 5</xref></label><caption><title> Prediction by use of the different data from the learning data</title></caption><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x94.png"/></fig><disp-formula id="scirp.68236-formula152"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x95.png"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.68236-formula153"><graphic  xlink:href="http://html.scirp.org/file/1-8701396x96.png"  xlink:type="simple"/></disp-formula><p>When fault 1 and fault 2 occur, large prediction errors are obtained for the probability distribution of vibration based on the observation of sound. As shown in <xref ref-type="fig" rid="fig6">Figure 6</xref>, the experimental values could not be predicted and there are great discrepancy between the experimental values and the theoretical values. <xref ref-type="table" rid="table1">Table 1</xref>, a prediction error is small for normal situation of data point from 1 to 5000. On the other hand, a prediction error becomes big for abnormality situation including a fault of data point from 5001 to 15,000. The validity of the fault diagnosis method based on the prediction error of the cumulative distribution has been confirmed numerically from the experimental result.</p><fig-group id="fig6"><label><xref ref-type="fig" rid="fig6">Figure 6</xref></label><caption><title> Prediction of the probability distribution for vibration based on the measurement data of sound. (a) Normal situation without the fault; (b) Failure situation with the fault for a bearing; (c) Failure situation with the fault for a cogwheel.</title></caption><fig id ="fig6_1"><label>(b)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x97.png"/></fig><fig id ="fig6_2"><label>(c)</label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x98.png"/></fig><fig id ="fig6_3"><label></label><graphic mimetype="image"   position="float"  xlink:type="simple"  xlink:href="http://html.scirp.org/file/1-8701396x99.png"/></fig></fig-group><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Prediction errors for the probability distribution of vibration based on the measurement data of sound</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  colspan="4"   rowspan="2"  >Data point/order</th><th align="center" valign="middle"  colspan="6"  >Averaged prediction errors for several percentile levels</th><th align="center" valign="middle"  colspan="6"  >Prediction errors for 50 percentile levels</th><th align="center" valign="middle" ></th></tr></thead><tr><td align="center" valign="middle"  colspan="2"  >1<sup>st</sup></td><td align="center" valign="middle"  colspan="2"  >2<sup>nd</sup></td><td align="center" valign="middle"  colspan="2"  >3<sup>rd</sup></td><td align="center" valign="middle"  colspan="2"  >1<sup>st</sup></td><td align="center" valign="middle"  colspan="2"  >2<sup>nd</sup></td><td align="center" valign="middle"  colspan="2"  >3<sup>rd</sup></td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle"  colspan="2"   rowspan="5"  >Normal situation</td><td align="center" valign="middle"  colspan="2"  >1-1000</td><td align="center" valign="middle"  colspan="2"  >0.17078</td><td align="center" valign="middle"  colspan="2"  >0.17078</td><td align="center" valign="middle"  colspan="2"  >0.17078</td><td align="center" valign="middle"  colspan="2"  >0.28333</td><td align="center" valign="middle"  colspan="2"  >0.05000</td><td align="center" valign="middle"  colspan="2"  >0.05000</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle"  colspan="2"  >1001-2000</td><td align="center" valign="middle"  colspan="2"  >0.27538</td><td align="center" valign="middle"  colspan="2"  >0.28333</td><td align="center" valign="middle"  colspan="2"  >0.27538</td><td align="center" valign="middle"  colspan="2"  >0.36248</td><td align="center" valign="middle"  colspan="2"  >0.05000</td><td align="center" valign="middle"  colspan="2"  >0.05000</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle"  colspan="2"  >2001-3000</td><td align="center" valign="middle"  colspan="2"  >0.21148</td><td align="center" valign="middle"  colspan="2"  >0.21148</td><td align="center" valign="middle"  colspan="2"  >0.21148</td><td align="center" valign="middle"  colspan="2"  >0.32702</td><td align="center" valign="middle"  colspan="2"  >0.15000</td><td align="center" valign="middle"  colspan="2"  >0.15000</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle"  colspan="2"  >3001-4000</td><td align="center" valign="middle"  colspan="2"  >0.39476</td><td align="center" valign="middle"  colspan="2"  >0.40311</td><td align="center" valign="middle"  colspan="2"  >0.39476</td><td align="center" valign="middle"  colspan="2"  >0.49917</td><td align="center" valign="middle"  colspan="2"  >0.25000</td><td align="center" valign="middle"  colspan="2"  >0.25000</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle"  colspan="2"  >4001-5000</td><td align="center" valign="middle"  colspan="2"  >0.15000</td><td align="center" valign="middle"  colspan="2"  >0.15723</td><td align="center" valign="middle"  colspan="2"  >0.15723</td><td align="center" valign="middle"  colspan="2"  >0.25000</td><td align="center" valign="middle"  colspan="2"  >0.05000</td><td align="center" valign="middle"  colspan="2"  >0.05000</td><td align="center" valign="middle" ></td></tr><tr><td align="center" valign="middle"  rowspan="10"  >Failure situation</td><td align="center" valign="middle"  colspan="2"   rowspan="5"  >for a bearing</td><td align="center" valign="middle"  colspan="2"  >5001 - 6000</td><td align="center" valign="middle"  colspan="2"  >0.84080</td><td align="center" valign="middle"  colspan="2"  >0.84869</td><td align="center" valign="middle"  colspan="2"  >0.84080</td><td align="center" valign="middle"  colspan="2"  >0.92391</td><td align="center" valign="middle"  colspan="2"  >0.65000</td><td align="center" valign="middle"  colspan="2"  >0.65000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >6001 - 7000</td><td align="center" valign="middle"  colspan="2"  >1.12854</td><td align="center" valign="middle"  colspan="2"  >1.13541</td><td align="center" valign="middle"  colspan="2"  >1.14903</td><td align="center" valign="middle"  colspan="2"  >1.22395</td><td align="center" valign="middle"  colspan="2"  >0.95000</td><td align="center" valign="middle"  colspan="2"  >0.95000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >7001 - 8000</td><td align="center" valign="middle"  colspan="2"  >0.73352</td><td align="center" valign="middle"  colspan="2"  >0.74106</td><td align="center" valign="middle"  colspan="2"  >0.73352</td><td align="center" valign="middle"  colspan="2"  >0.81257</td><td align="center" valign="middle"  colspan="2"  >0.55000</td><td align="center" valign="middle"  colspan="2"  >0.55000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >8001 - 9000</td><td align="center" valign="middle"  colspan="2"  >0.80156</td><td align="center" valign="middle"  colspan="2"  >0.80709</td><td align="center" valign="middle"  colspan="2"  >0.80156</td><td align="center" valign="middle"  colspan="2"  >0.88459</td><td align="center" valign="middle"  colspan="2"  >0.55000</td><td align="center" valign="middle"  colspan="2"  >0.55000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >9001 - 10,000</td><td align="center" valign="middle"  colspan="2"  >0.85781</td><td align="center" valign="middle"  colspan="2"  >0.86426</td><td align="center" valign="middle"  colspan="2"  >0.85781</td><td align="center" valign="middle"  colspan="2"  >0.93705</td><td align="center" valign="middle"  colspan="2"  >0.65000</td><td align="center" valign="middle"  colspan="2"  >0.65000</td></tr><tr><td align="center" valign="middle"  colspan="2"   rowspan="5"  >for a cogwheel</td><td align="center" valign="middle"  colspan="2"  >10,001 - 11,000</td><td align="center" valign="middle"  colspan="2"  >1.52179</td><td align="center" valign="middle"  colspan="2"  >1.54209</td><td align="center" valign="middle"  colspan="2"  >1.53632</td><td align="center" valign="middle"  colspan="2"  >1.60078</td><td align="center" valign="middle"  colspan="2"  >1.25000</td><td align="center" valign="middle"  colspan="2"  >1.25000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >11,001 - 12,000</td><td align="center" valign="middle"  colspan="2"  >2.28236</td><td align="center" valign="middle"  colspan="2"  >2.30272</td><td align="center" valign="middle"  colspan="2"  >2.29740</td><td align="center" valign="middle"  colspan="2"  >2.35189</td><td align="center" valign="middle"  colspan="2"  >1.55000</td><td align="center" valign="middle"  colspan="2"  >1.55000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >12,001 - 13,000</td><td align="center" valign="middle"  colspan="2"  >1.52834</td><td align="center" valign="middle"  colspan="2"  >1.53342</td><td align="center" valign="middle"  colspan="2"  >1.54353</td><td align="center" valign="middle"  colspan="2"  >1.60009</td><td align="center" valign="middle"  colspan="2"  >1.05000</td><td align="center" valign="middle"  colspan="2"  >1.05000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >13,001 - 14,000</td><td align="center" valign="middle"  colspan="2"  >2.24456</td><td align="center" valign="middle"  colspan="2"  >2.26526</td><td align="center" valign="middle"  colspan="2"  >2.25985</td><td align="center" valign="middle"  colspan="2"  >2.30513</td><td align="center" valign="middle"  colspan="2"  >1.75000</td><td align="center" valign="middle"  colspan="2"  >1.75000</td></tr><tr><td align="center" valign="middle"  colspan="2"  >14,001 - 15,000</td><td align="center" valign="middle"  colspan="2"  >1.54281</td><td align="center" valign="middle"  colspan="2"  >1.54928</td><td align="center" valign="middle"  colspan="2"  >1.56356</td><td align="center" valign="middle"  colspan="2"  >1.63240</td><td align="center" valign="middle"  colspan="2"  >1.25000</td><td align="center" valign="middle"  colspan="2"  >1.25000</td></tr><tr><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td><td align="center" valign="middle" ></td></tr></tbody></table></table-wrap></sec></sec><sec id="s4"><title>4. Conclusion</title><p>This paper has paid attention to the correlation information between sound and vibration emitted from rotational machine, and a method based on the conditional probability distribution with linear or non-linear correlation information of lower order or higher order has been proposed for the diagnosis of multiple faults and fault diagnosis with less prior information. Furthermore, the proposed method has been applied experimentally to observe data emitted from a rotating equipment. The proposed method focuses on the observational data in time domain, and the complicated preprocessing such as frequency analysis is unnecessary. Therefore, the proposed method is suitable for on-line signal processing. More specifically, the proposed fault diagnosis method can specify the fault part of machine by using fault probability. Furthermore, based on the information in only normal situation, it is possible to diagnose the fault in a form of the estimated error of cumulative distribution. Both methods have advantages to diagnose faults numerically. However, the proposed method is still at the early stage of study. Thus, there are a great number of problems in the future. For example, 1) The practical method should be developed at the actual environment existing background noise, 2) The determination method for the most suitable learning period to grasp correlation characteristic has to be proposed, and 3) It is necessary to extend the theory to simultaneous generation of multiple faults.</p></sec><sec id="s5"><title>Acknowledgements</title><p>This work was supported by JSPS KAKENHI Grant Number 24760322.</p></sec><sec id="s6"><title>Cite this paper</title><p>Hisako Orimoto, (2016) Statistical Fault Diagnosis Methods by Using Higher-Order Correlation Information between Sound and Vibration. 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