CN106949959B - A kind of method of impulse response signal sound intersity measurement - Google Patents

A kind of method of impulse response signal sound intersity measurement Download PDF

Info

Publication number
CN106949959B
CN106949959B CN201710160108.0A CN201710160108A CN106949959B CN 106949959 B CN106949959 B CN 106949959B CN 201710160108 A CN201710160108 A CN 201710160108A CN 106949959 B CN106949959 B CN 106949959B
Authority
CN
China
Prior art keywords
response signal
impulse response
signal
inner product
value
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.)
Active
Application number
CN201710160108.0A
Other languages
Chinese (zh)
Other versions
CN106949959A (en
Inventor
赵晓丹
韩俊阳
王�琦
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.)
Dongtai Chengdong science and Technology Pioneer Park Management Co.,Ltd.
Original Assignee
Jiangsu University
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 Jiangsu University filed Critical Jiangsu University
Priority to CN201710160108.0A priority Critical patent/CN106949959B/en
Publication of CN106949959A publication Critical patent/CN106949959A/en
Application granted granted Critical
Publication of CN106949959B publication Critical patent/CN106949959B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01HMEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H17/00Measuring mechanical vibrations or ultrasonic, sonic or infrasonic waves, not provided for in the preceding groups

Abstract

The present invention provides a kind of method of impulse response signal sound intersity measurement, include the following steps: that, with two microphones probe A, B acquisition pulse response signal acoustic pressure data, the acoustic pressure data importing computer that two probes are measured is denoted as P' respectivelyA(t)、P'B(t);Determine impulse response signal pAi(t) natural frequency valueWith impulse response signal pBi(t) natural frequency valueAccording to impulse response signal pAi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseImpulse response signal pBi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseParameter Reconstruction Impulse response signal, is denoted as respectivelyBy Reconstruction Impulse response signalSubstitute into instantaneous METHOD FOR SOUND POWER CALCULATION formula.The present invention can decompose impulse response signal without using Fourier transformation, but each impulse response signal is extracted from original signal, directly calculate its sound intensity;The sound intensity value for identifying impulse response signal can be clearly measured, the characteristic for accurately judging impulse response sound wave is facilitated.

Description

A kind of method of impulse response signal sound intersity measurement
Technical field
The present invention relates in particular to a kind of methods of impulse response signal sound intersity measurement.
Background technique
The intensity of sound intensity characterization acoustic wave energy.Sound intersity measurement method is widely used in acoustic power level and calculates, vibrates identifing source Equal fields.Engineer judges each vibration component actual contribution by the corresponding sound intensity value of Frequency point each on observation sound intensity frequency spectrum Acoustic energy, and then take targetedly noise reduction measure.Noise Intensity Testing Technique is always problem concerned by people.
Currently, most common sound intersity measurement method is two microphones Mutual spectrum, Fourier transformation is that Mutual spectrum surveys the sound intensity Core procedure, the time-domain sound pressure signal p that Fourier transformation measures two microphones A, channel BA(t)、pB(t) it is transformed into frequency domain Sound pressure signal PA(ω)、PB(ω), substitution frequency domain METHOD FOR SOUND POWER CALCULATION formula finds out the sound intensity after calculating its cross-spectrum.For stable state just, cosine Noise waves, using its sound intensity of Mutual spectrum survey calculation, the frequency spectrum of acquisition can effectively and reasonably reflect the feature of sound wave.
But in practical projects, sound wave existence form is numerous, and pulse shock is a kind of common exiting form, and impact produces Raw impulse response.When calculating the sound intensity of impulse response wave using Mutual spectrum, impulse response signal is decomposed into more by Fourier transformation A different frequency just, cosine signal, cause the sound intensity value on frequency spectrum to be dispersed on multiple and different Frequency points, in some instances it may even be possible to Occurs the negative sound intensity on component frequency point, survey calculation result reflects that the impulse response noise sound intensity is not easy enough, and physical features are unknown It is aobvious.
The present invention proposes that a kind of new sound intersity measurement calculates method.This method is pressed not using Fourier transformation as core According to impulse response signal, itself inherent feature carrys out constructed fuction, and the items for calculating impulse response signal using inner product approach are special Parameter is levied, according to the characteristic parameter Reconstruction Impulse response signal of acquisition, reconstruction signal is finally directly substituted into time domain sound intensity integral Formula calculates, and solves the sound intensity value of impulse response sound wave.The method of the present invention effectively measuring can identify impulse response sound The feature of wave, explicit physical meaning.
Summary of the invention
It in response to the deficiencies in the existing technology, can the present invention provides a kind of method of impulse response signal sound intersity measurement To extract each impulse response signal from original signal, its sound intensity is directly calculated, clearly measurement identifies in this way The sound intensity value of impulse response signal facilitates the characteristic for accurately judging impulse response sound wave.
The present invention achieves the above technical objects by the following technical means.
A kind of method of impulse response signal sound intersity measurement, includes the following steps:
S01: using two microphones probe A, B acquisition pulse response signal acoustic pressure data, and the acoustic pressure data measured is imported and is counted Calculation machine, is denoted as P' respectivelyA(t)、PB'(t);
S02: tracer signal P'A(t) and P'B(t) time span is T, to signal P'A(t) and P'B(t) direct computation of DFT is done Leaf transformation determines that the impulse response signal quantity for including in channel is m by the peak value number of frequency spectrum, wherein i-th of arteries and veins of probe A It rushes response signal and is set as pAi(t), i-th of impulse response signal of probe B is set as pBi(t), pA(t) and pB(t) it is denoted as respectively:
Wherein 0 < t < T;
S03: impulse response signal p is determinedAi(t) natural frequency valueWith impulse response signal pBi(t) intrinsic frequency Value
Construct signal:
As initial value i=1, LA0(t)=pA(t)、LB0(t)=pB(t);
Construct signal LAi-1(t) Fourier transformation is done, determines maximum amplitude and respective frequencies point, determines building signal LAi-1 (t) frequency estimationDetermine frequency search sectionIn frequency search sectionIt is interior to obtain the H subdivision thereof points divided equallyWherein, w=0, 1,…,H;Constructed fuctionBy constructed fuctionWith building signal LAi-1(t) inner product operation is done, inner product module is found Extreme point obtains response signal p according to the frequency at extreme pointAi(t) natural frequency value
Construct signal LBi-1(t) Fourier transformation is done, maximum amplitude and respective frequencies point is determined, determines constructor LBi-1 (t) frequency estimationDetermine frequency search sectionIn frequency search sectionIt is interior to obtain the H subdivision thereof points divided equallyWherein, w=0, 1,…,H;Constructed fuctionBy constructed fuctionWith building signal LBi-1(t) inner product operation is done, inner product module is found Extreme point obtains response signal p according to the frequency at extreme pointBi(t) natural frequency value
S04: according to impulse response signal pAi(t) natural frequency valueConstruct the function moved on a timeline:
According to impulse response signal pBi(t) natural frequency valueConstruct the function moved on a timeline:
Wherein: Δ T is the time span of function, and τ is variable and τ ∈ (0, T- Δ T);
Construct signal LAi-1(t) with constructed fuction cAi(t) inner product operation, constructor LB arei-1(t) with constructed fuction cBi (t) inner product operation is done, determines inner product modulus maximum, according to determining inner product modulus maximum, so that it is determined that impulse response signal pAi (t) initial timeSignal pBi(t) initial time
S05: interception building signal LAi-1(t) in the periodOn sound pressure signal, be denoted asInterception building Signal LBi-1(t) in the periodOn sound pressure signal, be denoted as
Constructed fuction:
Wherein, nAiAnd nBiFor variable;
Constructed fuction normalized is obtained:
yAi(t)=uAi(t)/||uAi(t)||
yBi(t)=uBi(t)/||uBi(t)||
By function yAi(t) and intercept signalInner product operation is carried out, by function yBi(t) and intercept signalInto Row inner product operation, obtains XAi、XBiExpression formula:
Inner product module is found using thinning method step by step | | XAi| | and | | XBi| | maximum value, according to XAi、XBiExpression formula meter Calculate attenuation coefficientWith
S06: according to inner product value Xmax Ai、Xmax BiWith constructed fuction uAi(t)、uBi(t) numerical value is calculated:
Wherein:
Xmax Ai、Xmax BiRespectively | | XAi||、||XBi| | obtain corresponding numerical value when maximum value;
According to C is calculatedAiAnd CBiPhase and amplitude:
Wherein:
Arg(CAi) indicate to seek CAiArgument, Arg (CBi) indicate to seek CBiArgument;
|CAi| plural C is sought in expressionAiAbsolute value, | CBi| plural C is sought in expressionBiAbsolute value;
S07: according to impulse response signal pAi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseImpulse response signal pBi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseParameter Reconstruction Impulse response signal, is denoted as respectivelyWherein:
S08: by Reconstruction Impulse response signalSubstitute into instantaneous METHOD FOR SOUND POWER CALCULATION formula:
Wherein, ρ: atmospheric density;
D: the spacing of probe A and B;
The time average for taking the signal transient sound intensity obtains the sound intensity of this impulse response signal:
S09: if when i < m, i=i+1, to LAi-1(t) and LBi-1(t) S03-S08 is executed, calculates remaining m-1 The sound intensity of impulse response signal;
As i=m, circulation terminates.
Further, in the S03 step
Beneficial effects of the present invention:
1. the method for impulse response signal sound intersity measurement of the present invention can decompose pulse without using Fourier transformation Response signal, but each impulse response signal is extracted from original signal, directly calculate its sound intensity.
2. the method for impulse response signal sound intersity measurement of the present invention, can clearly measure and identify impulse response The sound intensity value of signal facilitates the characteristic for accurately judging impulse response sound wave.
3. the method for impulse response signal sound intersity measurement of the present invention, can avoid the occurrence of the negative sound intensity.
Detailed description of the invention
Fig. 1 is the flow chart of the method for impulse response signal sound intersity measurement of the present invention.
Fig. 2 is the impulse response signal of embodiment of the present invention.
Fig. 3 is the sound intensity level spectrogram of the present invention obtained using Mutual spectrum measurement embodiment.
Specific embodiment
Present invention will be further explained with reference to the attached drawings and specific examples, but protection scope of the present invention is simultaneously It is without being limited thereto.
As shown in Figure 1, a kind of method of impulse response signal sound intersity measurement, includes the following steps:
S01: using two microphones probe A, B acquisition pulse response signal acoustic pressure data, and the acoustic pressure data measured is imported and is counted Calculation machine, is denoted as P' respectivelyA(t)、PB'(t);
S02: tracer signal pA(t) and pB(t) time span is T, to signal pA(t) and pB(t) discrete fourier change is done It changes, determines that the impulse response signal quantity for including in channel is m by the peak value number of frequency spectrum, wherein i-th of pulse of probe A is rung Induction signal is set as pAi(t), i-th of impulse response signal of probe B is set as pBi(t), pA(t) and pB(t) it is denoted as respectively:
Wherein 0 < t < T;
S03: impulse response signal p is determinedAi(t) natural frequency valueWith impulse response signal pBi(t) intrinsic frequency Value
Construct signal:
As initial value i=1, LA0(t)=pA(t)、LB0(t)=pB(t);
Construct signal LAi-1(t) Fourier transformation is done, determines maximum amplitude and respective frequencies point, determines building signal LAi-1 (t) frequency estimationDetermine frequency search sectionIn frequency search sectionIt is interior to obtain the H subdivision thereof points divided equallyWherein, w=0, 1,…,H;Constructed fuctionBy constructed fuctionWith building signal LAi-1(t) inner product operation is done, inner product module is found Extreme point obtains response signal p according to the frequency at extreme pointAi(t) natural frequency value
Construct signal LBi-1(t) Fourier transformation is done, maximum amplitude and respective frequencies point is determined, determines constructor LBi-1 (t) frequency estimationDetermine frequency search sectionIn frequency search sectionIt is interior to obtain the H subdivision thereof points divided equallyWherein, w=0, 1,…,H;Constructed fuctionBy constructed fuctionWith building signal LBi-1(t) inner product operation is done, inner product module is found Extreme point obtains response signal p according to the frequency at extreme pointBi(t) natural frequency value
S04: according to impulse response signal pAi(t) natural frequency valueConstruct the function moved on a timeline:
According to impulse response signal pBi(t) natural frequency valueConstruct the function moved on a timeline:
Wherein: Δ T is the time span of function, and τ is variable and τ ∈ (0, T- Δ T);
Construct signal LAi-1(t) with constructed fuction cAi(t) inner product operation, constructor LB arei-1(t) with constructed fuction cBi (t) inner product operation is done, determines inner product modulus maximum, according to determining inner product modulus maximum, so that it is determined that impulse response signal pAi (t) initial timeSignal pBi(t) initial time
S05: interception building signal LAi-1(t) in the periodOn sound pressure signal, be denoted asInterception building Signal LBi-1(t) in the periodOn sound pressure signal, be denoted as
Constructed fuction:
Wherein, nAiAnd nBiFor variable;
Constructed fuction normalized is obtained:
yAi(t)=uAi(t)/||uAi(t)||
yBi(t)=uBi(t)/||uBi(t)||
By function yAi(t) and intercept signalInner product operation is carried out, by function yBi(t) and intercept signalInto Row inner product operation, obtains XAi、XBiExpression formula:
Inner product module is found using thinning method step by step | | XAi| | and | | XBi| | maximum value, according to XAi、XBiExpression formula meter Calculate attenuation coefficientWith
S06: according to inner product value Xmax Ai、Xmax BiWith constructed fuction uAi(t)、uBi(t) numerical value is calculated:
Wherein:
Xmax Ai、Xmax BiRespectively | | XAi||、||XBi| | obtain corresponding numerical value when maximum value;
According to C is calculatedAiAnd CBiPhase and amplitude:
Wherein:
Arg(CAi) indicate to seek CAiArgument, Arg (CBi) indicate to seek CBiArgument;
|CAi| plural C is sought in expressionAiAbsolute value, | CBi| plural C is sought in expressionBiAbsolute value;
S07: according to impulse response signal pAi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseImpulse response signal pBi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseParameter Reconstruction Impulse response signal, is denoted as respectivelyWherein:
S08: by Reconstruction Impulse response signalSubstitute into instantaneous METHOD FOR SOUND POWER CALCULATION formula:
Wherein, ρ: atmospheric density;
D: the spacing of probe A and B;
The time average for taking the signal transient sound intensity obtains the sound intensity of this impulse response signal:
S09: if when i < m, i=i+1;To LAi-1(t) and LBi-1(t) S03-S08 is executed, calculates remaining m-1 The sound intensity of impulse response signal;
As i=m, circulation terminates.
In the S03 stepWhen, calculated natural frequency value is more accurate.
Embodiment: as shown in Fig. 2,
Assuming that there are one by 3 impulse responses into the plane sound wave being grouped as:
Wherein, Ai、ni、τi、fiThe amplitude of respectively i-th (i=1,2,3) a impulse response signal, rises attenuation coefficient Begin time, intrinsic frequency, initial phase.Design parameter value is shown in Table 1.Response signal 2,3 occurs simultaneously, and response signal 1 is below Occur on time.
Response signal Intrinsic frequency (Hz) Initial time (s) Amplitude (pa) Attenuation coefficient Phase
Signal 1 450.21 1.3 20 4.2 0.2
Signal 2 250.82 0.3 20 4.6 0.2
Signal 3 100.15 0.3 20 5.3 0.5
Table 1: the characteristic parameter of each impulse response acoustic signals
S01: using two microphones probe A, B acquisition pulse response signal acoustic pressure data, and the acoustic pressure data measured is imported and is counted Calculation machine, probe A are denoted as P' in rear end in front end, probe B respectivelyA(t)、P'B(t);
Signal pB(t) than signal pA(t) a tiny time section is laggedWherein d is A, B The spacing (unit: m) of probe, c are sound propagation velocity (unit: m/s) in air.
S02: tracer signal P'A(t) and P'B(t) time span is that T is 3s, does discrete Fourier transform to signal, is led to The peak value number for crossing frequency spectrum determines that wherein i-th of impulse response signal of probe A is set as comprising 3 impulse response signals in channel pAi(t), i-th of impulse response signal of probe B is set as pBi(t), pA(t) and pB(t) it is denoted as respectively:
Wherein 0 < t < 3;
S03: impulse response signal p is determinedAi(t) natural frequency valueWith impulse response signal pBi(t) intrinsic frequency Value
Construct signal:
As initial value i=1, LA0(t)=pA(t)、LB0(t)=pB(t);
Construct signal LAi-1(t) Fourier transformation is done, determines maximum amplitude and respective frequencies point, determines building signal LAi-1 (t) frequency estimationDetermine frequency search sectionWherein,It is searched in frequency Rope sectionIt is interior to obtain the H subdivision thereof points divided equally, as H=100,ThenWherein, w=0,1 ..., 100;Constructed fuctionBy constructed fuctionWith building Signal LAi-1(t) inner product operation is done, inner product module extreme point is found, according to the frequency at extreme point, obtains response signal pAi(t) Natural frequency value
Construct signal LBi-1(t) Fourier transformation is done, maximum amplitude and respective frequencies point is determined, determines constructor LBi-1 (t) frequency estimationDetermine frequency search sectionWherein,It is searched in frequency Rope sectionIt is interior to obtain 100 subdivision thereof points divided equallyIts In, w=0,1 ..., 100;Constructed fuctionBy constructed fuctionWith building signal LBi-1(t) inner product operation is done, Inner product module extreme point is found, according to the frequency at extreme point, obtains response signal pBi(t) natural frequency value
S04: according to impulse response signal pAi(t) natural frequency valueConstruct the function moved on a timeline:
According to impulse response signal pBi(t) natural frequency valueConstruct the function moved on a timeline:
Wherein: Δ T is the time span of function, value 0.02s.τ is variable and τ ∈ (0, T- Δ T);
Construct signal LAi-1(t) with constructed fuction cAi(t) inner product operation, constructor LB arei-1(t) with constructed fuction cBi (t) inner product operation is done, determines inner product modulus maximum, according to determining inner product modulus maximum, so that it is determined that impulse response signal pAi (t) initial timeSignal pBi(t) initial time
S05: interception building signal LAi-1(t) in the periodOn sound pressure signal, be denoted asInterception building Signal LBi-1(t) in the periodOn sound pressure signal, be denoted as
Constructed fuction:
Wherein, nAiAnd nBiFor variable;
Constructed fuction normalized is obtained:
yAi(t)=uAi(t)/||uAi(t)||
yBi(t)=uBi(t)/||uBi(t)||
By function yAi(t) and intercept signalInner product operation is carried out, by function yBi(t) and intercept signalInto Row inner product operation, obtains XAi、XBiExpression formula:
Inner product module is found using thinning method step by step | | XAi| | and | | XBi| | maximum value, according to XAi、XBiExpression formula meter Calculate attenuation coefficientWith
S06: according to inner product value Xmax Ai、Xmax BiWith constructed fuction uAi(t)、uBi(t) numerical value is calculated:
Wherein:
Xmax Ai、Xmax BiRespectively | | XAi||、||XBi| | obtain corresponding numerical value when maximum value;
According to C is calculatedAiAnd CBiPhase and amplitude:
Wherein:
Arg(CAi) indicate to seek CAiArgument, Arg (CBi) indicate to seek CBiArgument;
|CAi| plural C is sought in expressionAiAbsolute value, | CBi| plural C is sought in expressionBiAbsolute value;
S07: according to impulse response signal pAi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseImpulse response signal pBi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitial phaseParameter Reconstruction Impulse response signal, recognition result are shown in Table 2, are denoted as respectivelyWherein:
Reconstruction signal is as shown in Figure 2;
Table 2: each impulse response signal characteristic parameter that the method for the present invention is extracted
S08: by Reconstruction Impulse response signalSubstitute into instantaneous METHOD FOR SOUND POWER CALCULATION formula:
Wherein, ρ=1.293: atmospheric density (unit: Kg/m3);D=0.01: the spacing (unit: m) of probe A and B;
The time average for taking the signal transient sound intensity obtains the sound intensity of this impulse response signal:
S09: if when i < m, i=i+1, to LAi-1(t) and LBi-1(t) step 3- step 8 is executed, remaining m-1 is calculated The sound intensity of a impulse response signal, calculated result are shown in Table 3;
Response signal The theoretical sound intensity (W/m2) Calculated result (W/m of the present invention2) Relative error
Signal 1 0.01813109 0.01806788 0.3486%
Signal 2 0.01655058 0.01663622 0.5174%
Signal 3 0.01427526 0.01433991 0.4528%
Table 3: the method for the present invention METHOD FOR SOUND POWER CALCULATION result
As i=m, circulation terminates.
Comparison calculates the sound intensity of impulse response signal using two microphones Mutual spectrum, and Mutual spectrum has used many description arteries and veins The sound intensity of response signal is rushed, can not be indicated in the table.It is indicated using third-octave method.As shown in Figure 3, it can be seen that sound It is dispersed in by force on different Frequency points, or even the negative sound intensity occurs.And the calculated sound intensity value result of this method is accurate, and it is each Impulse response signal corresponds to each other, explicit physical meaning.
The embodiment is a preferred embodiment of the present invention, but present invention is not limited to the embodiments described above, not In the case where substantive content of the invention, any conspicuous improvement that those skilled in the art can make, replacement Or modification all belongs to the scope of protection of the present invention.

Claims (2)

1. a kind of method of impulse response signal sound intersity measurement, which comprises the steps of:
S01: using two microphones probe A, B acquisition pulse response signal acoustic pressure data, and the acoustic pressure data measured is imported computer, It is denoted as P' respectivelyA(t)、P'B(t);
S02: tracer signal P'A(t) and P'B(t) time span is T, to signal P'A(t) and P'B(t) discrete fourier change is done It changes, determines that the impulse response signal quantity for including in channel is m by the peak value number of frequency spectrum, wherein i-th of pulse of probe A is rung Induction signal is set as pAi(t), i-th of impulse response signal of probe B is set as pBi(t), pA(t) and pB(t) it is denoted as respectively:
Wherein 0 < t < T;
S03: impulse response signal p is determinedAi(t) natural frequency valueWith impulse response signal pBi(t) natural frequency valueConstruct signal:
As initial value i=1, LA0(t)=pA(t)、LB0(t)=pB(t);
Construct signal LAi-1(t) Fourier transformation is done, determines maximum amplitude and respective frequencies point, determines building signal LAi-1(t) Frequency estimationDetermine frequency search sectionIn frequency search sectionIt is interior to obtain the H subdivision thereof points divided equallyWherein, w=0, 1,…,H;Constructed fuctionBy constructed fuctionWith building signal LAi-1(t) inner product operation is done, inner product module is found Extreme point obtains response signal p according to the frequency at extreme pointAi(t) natural frequency value
Construct signal LBi-1(t) Fourier transformation is done, maximum amplitude and respective frequencies point is determined, determines constructor LBi-1(t) Frequency estimationDetermine frequency search sectionIn frequency search sectionIt is interior to obtain the H subdivision thereof points divided equallyWherein, w=0, 1,…,H;Constructed fuctionBy constructed fuctionWith building signal LBi-1(t) inner product operation is done, inner product module is found Extreme point obtains response signal p according to the frequency at extreme pointBi(t) natural frequency value
S04: according to impulse response signal pAi(t) natural frequency valueConstruct the function moved on a timeline:
According to impulse response signal pBi(t) natural frequency valueConstruct the function moved on a timeline:
Wherein: Δ T is the time span of function, and τ is variable and τ ∈ (0, T- Δ T);
Construct signal LAi-1(t) with constructed fuction cAi(t) inner product operation, constructor LB arei-1(t) with constructed fuction cBi(t) Inner product operation is done, determines inner product modulus maximum, according to determining inner product modulus maximum, so that it is determined that impulse response signal pAi(t) Initial timeSignal pBi(t) initial time
S05: interception building signal LAi-1(t) in the periodOn sound pressure signal, be denoted asInterception building signal LBi-1(t) in the periodOn sound pressure signal, be denoted as
Constructed fuction:
Wherein, nAiAnd nBiFor variable;
Constructed fuction normalized is obtained:
yAi(t)=uAi(t)/||uAi(t)||
yBi(t)=uBi(t)/||uBi(t)||
By function yAi(t) and intercept signalInner product operation is carried out, by function yBi(t) and intercept signalCarry out inner product Operation obtains XAi、XBiExpression formula:
Inner product module is found using thinning method step by step | | XAi| | and | | XBi| | maximum value, according to XAi、XBiExpression formula calculate Attenuation coefficientWith
S06: according to inner product value XmaxAi、XmaxBiWith constructed fuction uAi(t)、uBi(t) numerical value is calculated:
Wherein:
XmaxAi、XmaxBiRespectively | | XAi||、||XBi| | obtain corresponding numerical value when maximum value;
According to C is calculatedAiAnd CBiPhase and amplitude:
Wherein:
Arg(CAi) indicate to seek CAiArgument, Arg (CBi) indicate to seek CBiArgument;
|CAi| plural C is sought in expressionAiAbsolute value, | CBi| plural C is sought in expressionBiAbsolute value;
S07: according to impulse response signal pAi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeJust Beginning phaseImpulse response signal pBi(t) initial timeIntrinsic frequencyAttenuation coefficientAmplitudeInitially PhaseParameter Reconstruction Impulse response signal, is denoted as respectivelyWherein:
S08: by Reconstruction Impulse response signalSubstitute into instantaneous METHOD FOR SOUND POWER CALCULATION formula:
Wherein, ρ: atmospheric density;
D: the spacing of probe A and B;
The time average for taking the signal transient sound intensity obtains the sound intensity of this impulse response signal:
S09: if when i < m, i=i+1, to LAi-1(t) and LBi-1(t) S03-S08 is executed, remaining m-1 pulse is calculated The sound intensity of response signal;
As i=m, circulation terminates.
2. the method for impulse response signal sound intersity measurement according to claim 1, which is characterized in that in the S03 step
CN201710160108.0A 2017-03-17 2017-03-17 A kind of method of impulse response signal sound intersity measurement Active CN106949959B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710160108.0A CN106949959B (en) 2017-03-17 2017-03-17 A kind of method of impulse response signal sound intersity measurement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710160108.0A CN106949959B (en) 2017-03-17 2017-03-17 A kind of method of impulse response signal sound intersity measurement

Publications (2)

Publication Number Publication Date
CN106949959A CN106949959A (en) 2017-07-14
CN106949959B true CN106949959B (en) 2019-10-01

Family

ID=59472160

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710160108.0A Active CN106949959B (en) 2017-03-17 2017-03-17 A kind of method of impulse response signal sound intersity measurement

Country Status (1)

Country Link
CN (1) CN106949959B (en)

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1250559A (en) * 1997-03-12 2000-04-12 诺基亚电信公司 Estimating CIR using correlation with line removal
CN102854006A (en) * 2011-06-22 2013-01-02 霍尼韦尔国际公司 Severity analysis apparatus and method for shafts of rotating machinery
CN103424183A (en) * 2013-08-06 2013-12-04 常州大学 Method for eliminating abnormal interference on detection for mechanical vibration signals
CN103605880A (en) * 2013-10-25 2014-02-26 江苏大学 Closely spaced mode damping ratio precisely-diagnosing method
CN103778291A (en) * 2014-01-16 2014-05-07 江苏大学 Variable-period integrated signal damping ratio diagnosis method
CN105424167A (en) * 2015-11-09 2016-03-23 哈尔滨工程大学 Underwater self-contained sound intensity instrument and sound intensity measurement method
CN106052852A (en) * 2016-06-01 2016-10-26 中国电子科技集团公司第三研究所 Pulse sound signal detection method and device

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5672317A (en) * 1979-11-16 1981-06-16 Nissan Motor Co Ltd Detector for knocking oscillation
JPH09101199A (en) * 1995-10-06 1997-04-15 Mitsubishi Heavy Ind Ltd Rotary vane vibration measurement device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1250559A (en) * 1997-03-12 2000-04-12 诺基亚电信公司 Estimating CIR using correlation with line removal
CN102854006A (en) * 2011-06-22 2013-01-02 霍尼韦尔国际公司 Severity analysis apparatus and method for shafts of rotating machinery
CN103424183A (en) * 2013-08-06 2013-12-04 常州大学 Method for eliminating abnormal interference on detection for mechanical vibration signals
CN103605880A (en) * 2013-10-25 2014-02-26 江苏大学 Closely spaced mode damping ratio precisely-diagnosing method
CN103778291A (en) * 2014-01-16 2014-05-07 江苏大学 Variable-period integrated signal damping ratio diagnosis method
CN105424167A (en) * 2015-11-09 2016-03-23 哈尔滨工程大学 Underwater self-contained sound intensity instrument and sound intensity measurement method
CN106052852A (en) * 2016-06-01 2016-10-26 中国电子科技集团公司第三研究所 Pulse sound signal detection method and device

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
"汽车振动测试分析系统的研究";陈伟;《中国优秀硕士学位论文全文数据库工程科技Ⅱ辑》;20081130;C035-119 *
"脉冲激振模态分析法在300MW汽轮机松装叶片静频测量中的应用";王柏仁 等;《湖北电力技术》;19940331(第3期);第2-6页 *

Also Published As

Publication number Publication date
CN106949959A (en) 2017-07-14

Similar Documents

Publication Publication Date Title
US9909863B2 (en) Determination of a room dimension estimate
TWI525334B (en) Sonic-assisted localization of wireless devices
CN101600144B (en) Method and system for obtaining a plurality of parameters of electro-acoustic product by adopting continuous logarithmic swept-frequency signal
Sinha et al. The impulse response of a high-speed jet forced with localized arc filament plasma actuators
CN106643982B (en) A kind of level measuring method based on resonance frequency of sound wave
CN106255027B (en) A kind of the sound quality Small Enclosure appraisal procedure and system of non-linear audio system
CN101852638B (en) Liquid level measurement method based on resonance frequency of sound wave on fixed frequency range
CN101674520A (en) Method and device for analyzing and testing parameter of vibration type pickup
CN104270208B (en) Method and device for detecting standing-wave ratio of RRU
CN101426169A (en) Time-domain tracking filter fast detecting acoustic response parameter of sounding body and system
CN107064846A (en) The sensitivity detection method and device of live testing apparatus for local discharge
CN101874744B (en) Ultrasonic guided wave parameter measurement method used for long bone analysis
CN113472390B (en) Frequency hopping signal parameter estimation method based on deep learning
CN111811617A (en) Liquid level prediction method based on short-time Fourier transform and convolutional neural network
CN105675126B (en) A kind of new method for stablizing sound field acoustic pressure for detecting multifrequency multi-source complexity
CN104792450A (en) Method for indirectly measuring exciting force of equipment acting on mounting base
CN203100824U (en) Level measurement device based on standing sound wave method and audio card
CN105674065A (en) Variational mode decomposition-based method for locating leakage point of pipeline by acoustic emission
CN106949959B (en) A kind of method of impulse response signal sound intersity measurement
Willmarth Space-time correlations and spectra of wall pressure in a turbulent boundary layer
JP2004061361A (en) Piping breakage investigating apparatus
CN104568137B (en) The decision method of specific noise source contribution rate in noise testing
CN107741263B (en) Liquid level estimation method based on frequency domain information fusion
CN109696660B (en) Method for accurately measuring amplitude sensitivity and phase of microphone for detecting free sound field
CN201435826Y (en) Vibrating sound pick-up parameter analyzing and testing device

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
TR01 Transfer of patent right

Effective date of registration: 20201230

Address after: No. 101, Nanxu Avenue, Zhenjiang City, Jiangsu Province, 212000

Patentee after: JIANGSU HUIZHI INTELLECTUAL PROPERTY SERVICES Co.,Ltd.

Address before: Zhenjiang City, Jiangsu Province, 212013 Jingkou District Road No. 301

Patentee before: JIANGSU University

Effective date of registration: 20201230

Address after: 224200 No.8 Beihai Road, Dongtai City, Yancheng City, Jiangsu Province

Patentee after: Dongtai science and Technology Service Center

Address before: No. 101, Nanxu Avenue, Zhenjiang City, Jiangsu Province, 212000

Patentee before: JIANGSU HUIZHI INTELLECTUAL PROPERTY SERVICES Co.,Ltd.

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20210517

Address after: 224200 No. 48 Dongjin Avenue, Chengdong New District, Dongtai City, Yancheng City, Jiangsu Province

Patentee after: Dongtai Chengdong science and Technology Pioneer Park Management Co.,Ltd.

Address before: 224200 No.8 Beihai Road, Dongtai City, Yancheng City, Jiangsu Province

Patentee before: Dongtai science and Technology Service Center

TR01 Transfer of patent right
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20170714

Assignee: Dongtai tepusong Machinery Equipment Co.,Ltd.

Assignor: Dongtai Chengdong science and Technology Pioneer Park Management Co.,Ltd.

Contract record no.: X2023980043158

Denomination of invention: A Method for Measuring Sound Intensity of Pulse Response Signals

Granted publication date: 20191001

License type: Common License

Record date: 20231012

EE01 Entry into force of recordation of patent licensing contract
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20170714

Assignee: Dongtai Donggao Electronic Information Technology Co.,Ltd.

Assignor: Dongtai Chengdong science and Technology Pioneer Park Management Co.,Ltd.

Contract record no.: X2023980045160

Denomination of invention: A Method for Measuring Sound Intensity of Pulse Response Signals

Granted publication date: 20191001

License type: Common License

Record date: 20231102

EE01 Entry into force of recordation of patent licensing contract
EE01 Entry into force of recordation of patent licensing contract

Application publication date: 20170714

Assignee: Dongtai Gaoxin Mechanical Equipment Co.,Ltd.

Assignor: Dongtai Chengdong science and Technology Pioneer Park Management Co.,Ltd.

Contract record no.: X2023980046304

Denomination of invention: A Method for Measuring Sound Intensity of Pulse Response Signals

Granted publication date: 20191001

License type: Common License

Record date: 20231110

EE01 Entry into force of recordation of patent licensing contract