Classifications

• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
  • G01M13/00—Testing of machine parts
  • G01M13/02—Gearings; Transmission mechanisms
  • G01M13/028—Acoustic or vibration analysis
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
  • G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
  • G01H1/003—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
  • G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
  • G01H1/003—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines
  • G01H1/006—Measuring characteristics of vibrations in solids by using direct conduction to the detector of rotating machines of the rotor of turbo machines
• • G—PHYSICS
  • G01—MEASURING; TESTING
  • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
  • G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds

Definitions

• the present invention relates to the field of vibration signal acquisition systems of an engine and more particularly, the acquisition of vibratory signals for an on-board diagnostic of an engine.
• a rotary motor is subjected to mechanical stresses that can cause wear of its rotating elements.
• the latter comprises accelerometer-type vibration sensors for detecting the vibrations emitted by the engine.
• the vibratory signals collected are then analyzed to detect anomalies or defects in one or more rotating components. This analysis includes a frequency analysis of the signals detected by the vibration sensors.
• the vibration analysis requires signal sampling operations at a single very high constant frequency and oversampling operations of the signal at frequencies proportional to the harmonics to be analyzed and their multiple harmonics.
• the interpolated signals are oversampled and involve performing Fourier transforms on a very large number of points.
• the filtering operations impose frequency analyzes over the entire width signal band, which is very expensive in computing time.
• the object of the present invention is therefore to provide a system and a method of real-time acquisition of a vibratory signal without the aforementioned drawbacks and in particular, by implementing simplified calculations requiring reduced electronic means.
• the present invention is defined by a system for acquiring a vibratory signal for a diagnosis of a rotary engine, comprising:
• sampling means for sampling in real time said temporal vibratory signal with at least one sampling signal synchronized with said at least one current rotation speed thus generating a corresponding synchronous vibratory signal.
• this system makes it possible to minimize the calculation time and the data storage volume.
• the acquisition system can thus be advantageously used for an onboard diagnostic of the engine without monopolizing the calculation time or the memory space of an onboard computer.
• said sampling signal is parameterized by a predetermined maximum harmonic ratio and a predetermined sampling ratio.
• the system comprises a buffer for buffering a sample consisting of a predetermined number of periods of said synchronous vibratory signal, the temporal length of said buffer being determined according to a minimal harmonic ratio.
• the system comprises calculation means for extracting, from said buffered sample, frequency signals at multiple harmonics of the minimum harmonic and frequencies proportional to the corresponding current rotation speed.
• the calculation means are configured to extract said frequency signals by multiplying said buffered sample with Fourier coefficients of the only harmonics to be extracted.
• the input means are configured to receive first and second current rotational speeds respectively relative to first and second shafts of said engine, and
• the sampling means are configured to directly generate first and second synchronous vibratory signals by sampling in real time said temporal vibratory signal with respectively a first sampling signal synchronized with said first current rotation speed, and a second signal of synchronized sampling at said second current rotation speed.
• the sampling means are configured to directly generate a third synchronous vibratory signal by sampling in real time said temporal vibratory signal with a third sampling signal synchronized with the sum or the difference of said first and second velocities. rotation, said third sampling signal being reconstructed from a trigonometric combination of said first and second sampling signals.
• the system includes first, second, and third buffers for buffering respectively, a first sample consisting of a predetermined number of periods of said first synchronous vibratory signal, a second sample consisting of a predetermined number of periods of said second synchronous vibrating signal, and a third sample consisting of a predetermined number of periods of said third synchronous vibratory signal, and in that the calculation means are configured to respectively extract from said first, second and third buffered samples, first frequency signals at frequencies proportional to said first current rotation rate, second frequency signals at frequencies proportional to said second current rotation speed, and third frequency signals at frequencies proportional to said sum or difference of said first and second frequency signals at frequencies proportional to said sum or difference of said first and second frequency signals; second rotation speeds.
• the invention also relates to a system for monitoring a rotary engine, comprising the acquisition system according to any one of the above characteristics, and further comprising analysis means for analyzing the signal (s) ) frequency (s) to diagnose the condition of the motor.
• the invention also relates to a method of acquiring a vibratory signal for a diagnosis of a rotary engine, comprising the following steps:
• Fig. 1 schematically illustrates a system for acquiring a vibratory signal of a rotary motor, according to the invention
• Figs. 2A-2B illustrate an example of sampling of a temporal vibratory signal and the extraction of the frequency signals, according to the invention
• Fig. 3 illustrates a monitoring system for an on-board diagnosis of the state of an aircraft engine, according to the invention
• Fig. 4 illustrates an algorithm for acquiring and processing a vibratory signal of an engine, according to the invention.
• Fig. 5 illustrates a logic diagram for acquisition block and processing a vibratory signal of a motor, according to the invention.
• the concept underlying the invention is based on the acquisition of the vibration signals at frequencies directly synchronized by the rotation signals of the motor.
• Fig. 1 schematically illustrates a system for acquiring a vibratory signal from a rotary engine, according to the invention.
• the acquisition system 1 comprises input means 3 and sampling means 5.
• the input means 3 are configured to receive a temporal vibration signal X (t) representative of the operating state of the motor 7.
• the vibratory signal comes from at least one vibration sensor 9 of the accelerometer type installed on the motor 7.
• the input means 3 are configured to receive at least one current rotation speed N (t) of at least one shaft 11 of the motor 7.
• N (t) current rotation speed of at least one shaft 11 of the motor 7.
• the motor 7 may comprise two or more rotors having shafts rotating at different speeds.
• the sampling means 5 are configured to sample in real time the temporal vibratory signal X (t) with a sampling signal synchronized with the current rotation speed N (t) thus generating a synchronous vibratory signal x (n t ) corresponding .
• Fig. 2A illustrates an example of sampling of a temporal vibratory signal according to the invention.
• the temporal vibratory signal X (t) is a continuous signal acquired over time, for example at a frequency of the order of 250 kHz.
• the sampling signal S is a square signal synchronized with the speed of rotation N (t) of the motor 7.
• the sampling signal S is parameterized by a predetermined maximum harmonic ratio kh and a sampling ratio. r predetermined.
• the sampling frequency varies in real time with the speed of rotation of the motor 7 and depends on the maximum order kh of the harmonic to be extracted and the minimum number of dots per desired period (for example, 6 to 8 points).
• the temporal vibratory signal X (t) is sampled to generate the synchronous vibratory signal x (n t ).
• the signal x (n t ) is then a discrete signal subsampled at a frequency synchronous with the speed of rotation N (t) of the motor 7.
• the temporal vibratory signal X (t) is directly transformed into a digital signal x (n t ) synchronized with the speed of rotation N (t) of the motor.
• Processing means 13 are then used to apply a Fourier transform to the synchronous vibratory signal x (n t ) in order to extract frequency signals that are proportional to the speed of rotation N (t) of the motor 7.
• the processing means 13 may be included in the acquisition system 1 as illustrated in FIG. 1. Alternatively, they may be part of another electronic system (not shown) in connection with the acquisition system 1.
• the processing means 13 comprise calculation means 15 and storage means 17 comprising at least one buffer 19.
• the storage means 17 may comprise a code computer program for implementing the acquisition method according to the invention. 'invention.
• the buffer 19 is configured to buffer a sample consisting of a predetermined number of periods of the synchronous vibratory signal x (n t ).
• the temporal length of the buffer 19 is determined according to a minimum harmonic ratio.
• FIG. 2A illustrates a sample consisting of two periods of the synchronous vibratory signal x (n t ) with a minimum harmonic of period equal to 0.1 s. This saves the memory space because we just need to keep in the buffer 19 a very small number of points of the synchronous vibratory signal (for example, 8 points per harmonic).
• the calculation means 15 are configured to extract frequency signals Xi, ... X kh by multiplying the buffered point-to-point sample with Fourier coefficients of the only harmonics to be extracted and not over the entire analysis band.
• These frequency signals Xi, ... X kh have multiple harmonics of the minimum harmonic and frequencies proportional to the corresponding speed of rotation N (t) (see Fig. 2B).
• the imaginary parts (not shown) of the Fourier coefficients are out of phase by n / 2.
• the present invention makes it possible to directly extract the harmonic components at multiple frequencies from the rotation of the motor in a very small number of operations, without interpolations, and keeping in memory only a very small number of points. This saves a lot of computing time and memory space.
• Fig. 3 illustrates a monitoring system for an on-board diagnosis of the state of an aircraft engine, according to the invention.
• the monitoring system 2 comprises an acquisition system 1 and an anomaly detection system 21.
• the aircraft engine 7 comprises a low-pressure compressor 23 upstream of a high-pressure compressor 25 and a high-pressure turbine 27 upstream of a low-pressure turbine 29.
• the compressor 23 and the turbine 29 at low pressures are coupled by a first shaft 11a of rotation speed Ni.
• the compressor 25 and the turbine 27 at high pressures are coupled by a second shaft 11b of rotation speed N 2 .
• the second shaft 11b is a tube coaxial with the first shaft 11a and the two shafts are separated by inter shaft bearing bearings (not shown).
• the two shafts 11a, 11b can be counter-rotating and the bearings then have a rotation speed Ni + N 2 .
• the two shafts can be co-rotating and the inter-shaft bearings then have a rotation speed N1-N2.
• Vibration sensors 9 of the accelerometer type are placed in the motor 7 to detect the vibrations emitted by the latter.
• the motor 7 includes censors 31 for measuring the first and second rotational speeds Ni, N 2 of the first and second trees 11a, 11b respectively.
• the present invention proposes to extract directly and in real time three groups of frequency signals proportional to the rotational speeds Ni, N 2 , and Ni + N 2 respectively. to detect in real time any abnormal operation of one of the components of the engine 7.
• Figs. 4 and 5 respectively illustrate an algorithm and a logic diagram for acquisition and processing block of a vibratory signal of an engine according to FIG. 3.
• the input means 3 receive, during a predefined period of operation of the motor 7, a temporal vibratory signal X (t) representative of the operating state of the motor and first and second speeds current Ni (t) and N 2 (t) relating respectively to the first and second trees 11a, 11b of the motor 7.
• the predefined period during which the temporal vibration signal X (t) and the current speeds Ni (t) and N 2 (t) are obtained can for example correspond to a particular phase of flight or to a complete flight.
• the sampling means 5 are configured to directly generate first and second synchronous vibration signals xi (n) and x 2 ( nt ) by sampling in real time the temporal vibratory signal.
• X (t) with respectively a first sampling signal S1 synchronized with the first current rotation speed N (t), and a second sampling signal S2 synchronized with the second current rotation speed N 2 (t).
• steps E4 and E5 (blocks B4 and B5), the first and second sampling signals are generated.
• the first sampling signal SI has a frequency defined as a function of the first speed Ni, a predetermined maximum harmonic ratio kh and a predetermined sampling ratio r.
• the sampling ratio is here chosen equal to eight to facilitate the Fourier transform calculations.
• the second sampling signal S2 is a signal whose frequency is defined as a function of the second speed N 2 , a predetermined maximum harmonic ratio kh 2 and a predetermined sampling ratio r.
• steps E6 and E7 the rising edges of the first and second sampling signals S1, S2 are detected to form square signals for sampling the temporal vibration signal X (t).
• step E8 the time signal X (t) is first filtered using a first low pass filter B81 whose cutoff frequency is a function of the maximum frequency of the harmonic khi to extract.
• the first low pass filter B81 is driven by the first sampling signal SI whose instantaneous frequency is proportional to the first rotation speed Nl (t). Filtering the vibration signal X (t) upstream of the sampling makes it possible to avoid any risk of spectral aliasing.
• the previously filtered vibratory signal X (t) is then sampled by a first asynchronous DAC analog-to-digital converter B82 according to each rising edge of the first sampling signal to generate a first synchronous vibratory signal Xi (n t ).
• step E9 the temporal signal X (t) is filtered using a second low pass filter B92 whose cutoff frequency is a function of the maximum frequency of the harmonic kh 2 to extract, or is driven by the second sampling signal S2 whose instantaneous frequency is proportional to the second rotation speed N2 (t).
• the filtered vibratory signal X (t) is then sampled by a second asynchronous DAC B92 according to the second sampling signal S2 to generate a second synchronous vibratory signal x 2 (n t ).
• the signals Xi (n t ) x 2 (n t ) are discrete signals synchronized respectively with the speeds of rotation Ni and N 2 .
• step E10 (blocks B10), a first sample consisting of a predetermined number of periods of the first synchronous vibratory signal xi (n t ) is buffered in a first buffer B10 whose temporal length is determined according to the ratio of harmonic minimal ru.
• step Eli (blocks B11) a second sample consisting of a predetermined number of periods of the second synchronous vibratory signal x 2 (n t ) is buffered in a second buffer B11 whose temporal length is determined according to of the minimal harmonic ratio h 2 .
• the first and second buffers B10, B11 are respectively triggered at each turn of rotations NI and N2 (blocks B101, Bill). Indeed, the calculations downstream of the Fourier transforms are done at frequencies in multiples of the refresh rate of the buffers. The execution frequencies of these calculations are synchronized with the rotational speeds of the motor shafts.
• step E12 the calculation means will extract first and second groups of frequency signals Xn, ... Xikhi and X 2 i, ... X 2 kh2- More particularly, in step E12 (block B12) the calculation means 15 generate first Fourier coefficients of the only harmonics to be extracted concerning the first rotational speed i: (sm (2nnk) + j cos 2nnk)) / 8x Nh, the increment of the Fourier analysis nk satisfying 0 ⁇ nk ⁇ kh l x 8-1; Nh is the number of the harmonic computed with Nh-1,2, kh and chi is the maximal order of the harmonic to be analyzed for the speed of rotation Ni.
• step E14 the first Fourier coefficients are multiplied in a matrix manner with the first sample of the first synchronous vibration signal Xi ( nt ) to generate the first group of frequency signals Xn, ... Xi kh i (E16, B16).
• step E15 the second Fourier coefficients are multiplied in a matrix manner with the second sample of the second synchronous vibratory signal x 2 (n t ) to generate the second group of frequency signals X 2 i, ... X 2kh2 (E17, B17).
• the sampling means 5 are further configured to directly generate a third synchronous vibratory signal x 3 (n t ) by sampling in real time the temporal vibratory signal X (t) with a third sampling signal S3 synchronized with the sum Ni + N 2 of the first and second rotational speeds.
• the third sampling signal S3 is reconstructed by the processing means 13 from a trigonometric combination of the first and second sampling signals S1, S2.
• a first synchronization intermediate signal is generated whose frequency is defined as a function of the first speed N 1 and a predetermined maximum harmonic ratio kh 3 .
• first sampling signal step E4, block B4
• a second synchronization intermediate signal is generated whose frequency is defined as a function of the second speed N 2 and a predetermined maximum harmonic ratio kh 3 .
• a sinusoidal sine signal and a sinusoidal cosine signal of frequency N2 * kh 3 * 8: sin (8 x N 2 x kh 3) are generated.
• step E21 the sin (8 ⁇ N ⁇ X kh 3 ) of step E19 is multiplied (B211, B212) by the cos (8 ⁇ N 2 ⁇ kh 3 ) of step E20. and secondly, the cos (8 x N! x kh 3) of step E19 with the sin (8 x 2 x N kh 3) step E20 to form the signals sin respectively (8 x N 1 x kh 3 ) x cos (8 x N 2 x kh 3 ) and cos (8 x N ! x kh 3 ) x sin (8 x N 2 x kh).
• step E22 (block B22) the rising edges of this third sampling signal are extracted to form a square signal for sampling the time signal X (t).
• step E23 the temporal vibratory signal X (t) is first filtered using a third low pass filter B231 whose cutoff frequency is a function of the frequency maximum of the harmonic kh 3 to extract.
• the third low pass filter B231 is driven by the third sampling signal S3.
• the filtered vibratory signal X (t) is then sampled by a third asynchronous DAC B232 according to the third sampling signal S3 to generate a third synchronous vibratory signal x 3 (n t ).
• the signal x 3 (n t ) is a discrete signal synchronized with the rotation speed Ni + N 2 .
• step E24 a third sample consisting of a predetermined number of periods of the third synchronous vibratory signal x 3 (n t ) is buffered in a third buffer B24 whose temporal length is determined according to the ratio of minimal harmonic h 3 .
• the third buffer B24 is triggered at each turn of rotation N1 + N2 (block B241).
• step E25 the calculation means 13 generate third Fourier coefficients of the only harmonics to be extracted concerning the speed of rotation N x + N 2 : (sin (27rn / t) + j cos (2nnk)) / 8 x Nh, the increment of the Fourier analysis nk satisfying 0 ⁇ nk ⁇ kh 3 x 8-1; Nh is the number of the harmonic calculated with Nh-1,2, ..., kh 3 and kh 3 is the maximal order of the harmonic to be analyzed for the rotation speed! + 2 .
• step E26 the third Fourier coefficients are multiplied in a matrix manner with the third sample of the third synchronous vibratory signal x 3 (n t ) to generate a third group of frequency signals X 3 i, ... X 3 i ⁇ h3 (E27, B27).
• the system or method according to the invention does not use sub or sampling operations, and uses simplified FFT Fourier transform calculations. Indeed, only the harmonics signals relevant for the motor diagnosis are retrieved with a minimum of computation and memory. In addition, no tracking filters are used.
• the first, second and third groups of frequency signals make it possible to diagnose, respectively, the first shaft, the second shaft and the inter-shaft bearing bearings of the motor.
• the detection system 21 recovers in real time the first, second and third groups of frequency signals for analysis.
• the detection system 21 comprises analysis means 23 for, for example, correlating the frequency signals with other signals or for comparing them with predefined threshold values in order to monitor the state of the engine in real time. detection can for example follow the amplitude evolution of the different harmonics of the frequency signals with respect to relative relative thresholds. A threshold overrun can thus trigger alarms or alert messages 31.
• the analysis of the frequency signals can be performed offline to further minimize the calculation time during the flight.
• the first, second and third groups of frequency signals can be stored in flight in a database to analyze the evolution over time of the state of the engine 7.
• the monitoring system can be integrated in a specific housing or be part of an existing electronic box.

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• Physics & Mathematics (AREA)
• General Physics & Mathematics (AREA)
• Acoustics & Sound (AREA)
• Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
• Control Of Electric Motors In General (AREA)
• Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
• Combined Controls Of Internal Combustion Engines (AREA)
• Testing Of Engines (AREA)

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• 2012
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• 2013
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  • 2013-01-14 WO PCT/FR2013/050083 patent/WO2013110878A1/fr active Application Filing
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