The aspects of the disclosed embodiments relate to controlling shot peening.
Shot peening may be used for processing the surfaces of critical metallic components, e.g. gas turbine blades, toothed gears, or axles. A shot peening process may be verified by using so called Almen strips. The use of Almen strips may involve considerable amount of manual work.
Some versions may relate to verification of a shot peening apparatus. Some versions may relate to a device for verifying a shot peening process. Some versions may relate to monitoring operation of a shot peening apparatus. Some versions may relate to a device for monitoring a shot peening process. Some versions may relate to controlling operation of a shot peening apparatus. Some versions may relate to a device for controlling a shot peening process. Some versions may relate to a shot peening apparatus, which comprises an optical device for verifying operation of the shot peening apparatus.
According to an aspect, there is provided a method, comprising:
According to an aspect, there is provided a method, comprising:
According to an aspect, there is provided a method, comprising:
According to an aspect, there is provided an apparatus, comprising:
The method may comprise:
The shot peening unit may be arranged to provide a particle jet, which comprises particles moving at a high velocity. The particle jet may be directed to an object so as to process the surface of said object by shot peening.
The monitoring device may comprise an illuminating unit and an imaging unit. The illuminating unit may illuminate a predetermined region of the particle jet. The imaging unit may capture digital images of particles located within the illuminated region. The method may comprise estimating an arc height value (hAS) and/or a time equivalent value (TINT) by analyzing the captured digital images. The device may comprise a data processing unit, which may be configured to analyze the captured images.
The capability of the particle jet to cause irreversible plastic deformation of a surface may be quantitatively measured by using the test strip AS1, which may also be called e.g. as the Almen strip. Arc height values and/or time equivalent values may be measured by exposing the test strip to the particle jet such that the particle jet causes bending of the test strip. The shape of the test strip AS1 after a shot peening test may be defined e.g. by an arc height value hAS.
The method may comprise measuring at least one velocity value by analyzing the captured images. The method may comprise determining a model, which describes a relationship between measured velocity values and the corresponding arc height values. The model may be determined based on measured arc height values and based on measured velocity values.
The method may comprise measuring at least one velocity value by analyzing the captured images. A corresponding deformation of an Almen strip may be subsequently estimated from the measured velocity value by using the model, without deforming the Almen strip.
The monitoring device may provide one or more measured velocity values based on a high number of detected particles. The measurement result may be based on a statistically meaningful portion of all particles which impinge on a target during a shot peening process. Analysis of the captured images may provide a statistically meaningful result within a reasonable time.
The present method may allow substantially continuous monitoring during a shot peening process. The present method may allow detecting transient disturbances of the jet. The present method may allow reducing the amount of manual work needed for handling the Almen strips. The present method may also allow determining the coverage of the particle jet.
Thanks to using the present imaging method, the use of the test strips may be reduced or avoided. Estimating the arc height values hAS by using the measurement device and by using the model may reduce the number of test strips AS1 needed for verifying a shot peening process. The operation of the shot peening unit may be monitored and/or verified before as shot peening process, during the shot peening process and/or after the shot peening process. The operation of the shot peening unit may be monitored and/or verified in real time. The need for manual work may be reduced or avoided. The operation of the shot peening unit may be monitored several times during a shot peening process or even continuously without increasing the amount of manual work needed for the monitoring. The verification may be performed more often and/or with a higher accuracy. Consequently, the quality of a shot peened product may be improved.
Estimating the arc height values hAS by using the measurement device and by using the model may allow on-line control of a shot peening process.
In the following examples, several variations will be described in more detail with reference to the appended drawings, in which
Referring to
Shot peening may be used. e.g. for increasing the operating life of a component OBJ1, which is intended for use in demanding conditions. Shot peening may produce compressive residual stress in the surface layer SRF2 of the component OBJ1. The compressive stress may reduce the risk of propagation of microscopic cracks in the surface layer SRF2. Shot peening may increase operating life of the parts, e.g. by reducing the risk of fatigue failure.
Shot peening may be performed by accelerating macroscopic particles P0 to a high velocity, and directing the moving particles P0 to the surface SRF2 of an object OBJ1. The particles P0 may hit the surface SRF2 and may cause plastic deformation of the surface layer of the object. The moving particles P0 may be called e.g. as the “shots”. The particles may be e.g. steel balls or ceramic balls. Shot peening may comprise providing a particle jet JET0, which comprises a plurality of particles P0k, P0k+1, P0k+2, . . . moving at high velocities vk, vk+1, vk+2, . . . . A shot peening unit 700 may be arranged to provide the particle jet JET0. The particle jet JET0 may be provided e.g. by accelerating the particles with a high velocity gas stream. The particle jet JET0 may also be provided e.g. by accelerating the particles with a rotating mechanical element.
The object OBJ1 may also be called e.g. as a target. The surface SRF2 may be exposed to particles of a particle jet JET0. A shot peening unit 700 may be arranged to provide the particle jet JET0. The jet JET0 may comprise a plurality of particles P0k, P0k+1, P0k+2, . . . . The particles may be e.g. metal balls, pieces of metal wire, or ceramic beads. In particular, the particles may be steel balls.
The jet may be directed to the surface SRF2 of the target. The target OBJ1 may be e.g. a part of a machine, engine and/or a vehicle. The target OBJ1 may be e.g. a mechanical component of a device.
The particle jet JET0 may have central axis AX0. The particles of the jet may propagate substantially in the direction of the axis AX0. The jet may also be slightly diverging such that the particles have a significant velocity component in the direction of the axis AX0.
SX, SY, and SZ denote orthogonal directions. The axis AX0 of the jet may be parallel e.g. with the direction SZ. The reference position POS0 denotes a point where the axis AX0 intersects the surface of the object. POS(x,y,z) may denote an arbitrary position. The position POS(x,y,z) may be specified e.g. by coordinates x,y,z with respect to the reference position POS0.
L2 denotes a distance between the shot peening unit 700 and the surface SRF2. In particular, L0 may denote a distance between the accelerating nozzle of the shot peening unit 700 and the surface SRF2. The position of the shot peening unit 700 and/or the orientation of the target OBJ1 may be selected such that the surface SRF2 is substantially perpendicular to the axis AX0.
Referring to
The dimensions of the test strips AS1 and/or the details of the experimental set-up may be defined e.g. in a standard SAE J442, J443, J2277, J2597, AMS2430, and/or AMS2432. SAE means Society of Automotive Engineers, an organization based in the United States of America.
The particles may hit an exposed area AREA1 of the surface SRF1 of the test strip AS1. L1 may denote the distance between the shot peening unit 700 and the test strip AS1. In particular, L0 may denote the distance between the particle accelerating nozzle of the shot peening unit 700 and the reference area AREA0. The axis of the particle jet JET0 may coincide with the center of the area AREA1.
Referring to
The reference area AREA0 may be positioned e.g. such that the distance L0 is substantially equal to the distance L1. The size of the reference area AREA0 may be equal to the exposed area AREA1 of the test strip AS1. The width Δx of the reference area AREA0 may be equal to the width of the exposed area AREA1 of the test strip AS1, and the height Δy of the reference area AREA0 may be equal to the height of the exposed area AREA1 of the test strip AS1. The jet may have a diameter (wJET0) at the position of the reference area AREA0.
Referring to
The measuring device 500 may be arranged to measure one or more spatial distributions by analyzing the captured images (
The measuring device 500 may be arranged to measure a spatial velocity distribution by analyzing the captured images. A particle P0 may have a velocity component vz in the axial direction SZ. The particle P0 may also have a transverse velocity component vx in the direction SX and/or a velocity component vy in the direction SY. The measuring device 500 may be arranged to measure e.g. the velocity components vz and vy for each particle appearing in a captured image. The measuring device 500 may be arranged to measure a spatial velocity distribution for the axial velocity components vz as a function of the vertical position y. The measuring device 500 may be arranged to measure a spatial velocity distribution for the transverse velocity components vy as a function of the vertical position y.
The measuring device 500 may be arranged to measure a spatial velocity probability distribution by analyzing the captured images.
The measuring device 500 may be arranged to measure a spatial distribution of mass flow by analyzing the captured images.
The measuring device 500 may be arranged to measure a spatial distribution of flux of kinetic energy by analyzing the captured images. The spatial distribution may provide information e.g. about an effective width of the particle jet.
The illuminating unit 100 may provide an illuminating light beam LB0. The particles P0 may reflect, refract and/or scatter light LB1 towards the illuminating unit 100. The particles P0 may provide reflected light LB1 by reflecting, refracting and/or scattering the illuminating light LB0.
The imaging unit 200 may comprise focusing optics 210 and an image sensor SEN1. The focusing optics 210 may be arranged to form an optical image IMG1 on an image sensor SEN1, by focusing the light LB1 received from the particles. The image sensor SEN1 may convert one or more optical images IMG1 into a digital image IMG2. The data processing unit 400 may be configured to analyze one or more digital images IMG2 obtained from the image sensor SEN1. The data processing unit 400 may be configured to perform one or more data processing operations e.g. for determining a model, for verifying a shot peening operation, for controlling operation of the shot peening unit, and/or for providing an indication if one or more measured velocity values are outside a specified range. The image sensor SEN1 may be e.g. a CMOS sensor or a CCD sensor. CMOS means Complementary Metal Oxide Semiconductor. CCD means Charge Coupled Device. The image sensor SEN1 may comprise a plurality of light detector pixels arranged in a two-dimensional array. The digital image IMG2 may have a width ξIMG and a height υIMG in the image space defined by directions Sξ and Sυ. The image of the axis AX0 may be e.g. substantially parallel with the direction Sξ. The direction Sυ may be perpendicular to the direction Sξ.
The field of view of the imaging unit may allow a considerable variation of the position of the particle jet. Thus, the position of the monitoring device of the does not need to be set with a high accuracy with respect to the axis of the particle jet.
The imaging unit 200 may have an optical axis AX2. The measurement region RG0 may have a thickness d0 in the direction of the optical axis AX0. The direction of the illuminating beam LB0 may be specified e.g. by an axis AX1.
The axis AX2 may be e.g. substantially perpendicular to the axis AX0 and substantially perpendicular to the axis AX1. The illuminating light beam LB0 may have e.g. a thickness d0 in the direction of the optical axis AX2. The illuminating unit 100 may be arranged to provide e.g. a substantially planar light beam. The illuminating light beam LB0 may be a light sheet. The illuminating unit 100 may comprise e.g. one or more lasers and/or light emitting diodes to provide the illuminating light beam LB0. Illuminating the jet by the light sheet may allow defining the thickness d0 and/or position of the measurement region RG0 accurately.
The method may comprise illuminating the particle jet JET0 with the illuminating light LB0 such that the thickness d0 of the measurement region RG0 is smaller than the diameter (wJET0) of the particle jet JET0. Thus, each captured image may represent a single slice (RG0) of the particle jet. The method may comprise determining a two-dimensional and/or a three dimensional spatial velocity distribution of the particle jet by analyzing the captured images. The method may comprise determining a two-dimensional and/or a three dimensional spatial particle density distribution of the particle jet by analyzing the captured images. Using the thin (d0<wJET0) measurement region (RG0) may facilitate determining the spatial distributions.
The illuminating unit 100 may be arranged to modulate the illuminating light beam LB0. The illuminating unit 100 may be arranged to modulate the optical intensity of the illuminating light beam LB0 according to control signal S100. The measuring device 500 may be arranged to provide a control signal S100 for modulating the illuminating light beam LB0. The control signal S100 may comprise e.g. timing pulses for controlling timing of operation of the illuminating unit 100. The illuminating unit 100 may be arranged to provide one or more illuminating light pulses LB0.
The position of the illuminating unit 100 may be defined e.g. by a mechanical frame with respect to the imaging unit 200. The units 100, 200 may be attached to a common frame. The device 500 may optionally comprise a robot for setting the position of the illuminating unit 100 and/or for the position of the imaging unit 200. The device 500 may optionally comprise a robot for setting the position of the measurement region RG0 with respect to the shot peening unit 700.
The device 500 may comprise a memory MEM1 for storing computer program code PROG1. For example, the code PROG1 may, when executed by one or more data processors, cause a system or the device 500 to determine a total energy value by analyzing the images IMG2 captured by the imaging device 200. For example, the code PROG1 may, when executed by one or more data processors, cause a system or the device 500 to estimate an arc height value hAS by analyzing the images IMG2.
The device 500 may comprise a memory MEM2 for storing one or more parameters of a model MODEL1.
The device 500 may optionally comprise a memory MEM3 for storing one or more output values OUT1 determined by using the model MODEL1. The output values OUT1 may comprise e.g. one or more arc height values hAS,1, hAS,2, hAS,3 and/or peening intensity rating values TINT.
The device 500 may comprise a user interface UIF1 for receiving user input from a user and/or for providing information to a user. The user interface UIF1 may comprise e.g. a keypad or a touch screen for receiving user input. The user interface UIF1 may comprise e.g. a display for displaying visual information. The user interface UIF1 may comprise e.g. a display for displaying one or more parameter values determined by analyzing the images. The user interface UIF1 may comprise e.g. a display for displaying an indication when one or more parameters measured by the device are outside an acceptable range. The user interface UIF1 may comprise e.g. an audio output device for providing an indication if one or more velocity values measured by the device are outside an acceptable range. The user interface UIF1 may be configured to provide a visual alarm and/or an alarm sound if one or more velocity values measured by the device are outside an acceptable range.
The device 500 may comprise a communication unit RXTX1 for receiving and/or transmitting data. COM1 denotes a communication signal. The device 500 may be arranged to communicate e.g. with the shot peening unit 700 via the communication unit RXTX1. The device 500 may be arranged to communicate e.g. with a control unit of the shot peening unit 700 via the communication unit RXTX1. The device 500 may receive process data via the communication unit RXTX1. The process data may indicate e.g. when the shot peening unit is operating. The process data may indicate e.g. one or more process parameter values of the shot peening unit 700. The device 500 may send process control data via the communication unit RXTX1. The process control data may comprise e.g. data for adjusting one or more process parameters of the shot peening unit 700.
The device 500 may be arranged to receive measured data from a second measuring instrument via the communication unit RXTX1. The second measuring instrument may be e.g. an Almen gage.
The imaging unit 200 may form an image P1 of each particle P0, which is located in the measurement region RG0 during an exposure time Tex of the image sensor SEN1. The optical image IMG1 formed on the active area of the image sensor SEN1 may comprise a plurality of sub-images P1. Each sub-image P1 may be an image of a particle P0. The image sensor SEN1 may convert an optical image IMG1 into a digital (captured) image IMG2.
The image IMG2 captured by the imaging unit 200 may represent a region RG0 of the particle jet JET0. An average number of particles appearing in a single captured image may be e.g. in the range of 2 to 1000. An average number of particles appearing in a single captured image may be e.g. in the range of 10 to 100. The sub-images P1 of the particles P0 may be detected by an image analysis algorithm. The particles P0 may be moving at a high velocity during capturing of an image IMG2. The velocity of each particle appearing in a captured image may be determined from the displacement value Δu and from the timing of the exposure and/or illumination. The optical image P1 of each particle P0 may move during capturing of the image IMG2. The movement of the optical image may define a displacement value Δu, which may be determined from the captured image IMG2 by image analysis. Each substantially sharp image P1 of a particle P0 may be associated with a displacement value Δu. The velocity vk of a particle P0k may be determined from the displacement value Δuk and from the duration (TF) of illumination and/or from the exposure time period Tex.
When using illuminating pulse sequences, the velocity vk of a particle P0k may be determined from the displacement value Δuk and from the timing (e.g. t5−t1) of illuminating light pulses LB0. In particular, the axial velocity of a particle may be substantially proportional to Δuk/TF.
Referring to
Referring to
The sub-images P1k, P1k+1, P1k+2 may be detected e.g. by an image analysis algorithm. The device 500 may be configured to detect the sub-images P1k, P1k+1, P1k+2 by using an image analysis algorithm. The device 500 may be configured to determine the dimensions Δuk, Δuk+1, Δuk+2 from one or more captured images IMG2 by using an image analysis algorithm.
The digital image IMG2 may have a width ξIMG and a height υIMG in the image space defined by directions Sξ and Sυ. The image of the axis AX0 may be parallel with the direction Sξ. The direction Sυ may be perpendicular to the direction Sξ.
The width ξIMG may be e.g. equal to 1024 pixels, and the height υIMG may be e.g. equal to 512 pixels.
The velocity of the particles may also be measured by using continuous illuminating light, i.e. light, which is not pulsed. In that case the velocity vk of the particle P0k may be substantially proportional to the value Δuk/Tex.
The use of pulsed illumination may allow high instantaneous intensity and/or may allow precise timing for forming the sub-images.
Referring to
The exposure time Tex may temporally overlap several light pulses so that each particle P0 may be represented by a group GRP, which is formed of two or more sub-images P1 appearing in the digital image IMG2. For example, the particle P0k may be represented by a first group GRPk formed of sub-images P1k,t1, P1k,t2, P1k,t3, P1k,t4, P1k,t5. The distance between adjacent sub-images P1k,t1, P1k,t2 may depend on the velocity vk of the particle P0k and on the timing of the light pulses. Consequently, the velocity of each particle appearing in the image IMG2 may be determined by analyzing the image IMG2. The sub-images P1k,t1, P1k,t2, P1k,t3, P1k,t4, P1k,t5 may together form a combined shape, which may facilitate reliable detection of the sub-images P1k,t1, P1k,t2, P1k,t3, P1k,t4, P1k,t5, when analyzing the captured image IMG2. A second particle P0k+1 may be represented by a second group GRPk+1 formed of sub-images P1k+1,t1, P1k+1,t2, P1k+1,t3, P1k+1,t4, P1k+1,t5.
Referring to
The velocity of the particles may be determined by analyzing the captured images. For example, the velocity of a first particle P0k may be determined from the dimension Δuk of a first group GRPk formed of the sub-images P1k,t1, P1k,t2, P1k,t3. For example, the velocity of a second particle P0k+1 may be determined from the dimension Δuk+1 of a second group GRPk+1 formed of the sub-images P1k+1,t1, P1k+1,t2, P1k+1,t3.
The method may comprise counting the number of particles appearing in a single captured image. The method may comprise counting the number of particles appearing in the captured images. The particle density may be determined from the counted number of particles. Thus, the particle density may be determined by analyzing the captured images.
The imaging unit 200 may have a certain depth of field (DoF) such that particles which are within the depth of field may have sharp sub-images on the image sensor SEN1, and particles which are outside the depth of field may have blurred sub-images on the image sensor SEN1. The captured image may comprise blurred sub-images e.g. if the thickness of the illuminating light beam LB0 is greater than the depth of field (DoF). On the other hand, sharper images may be provided when the thickness of the illuminating light beam LB0 is smaller than or equal to the depth of field (DoF).
The groups (e.g. GRPk) formed of the sub-images (e.g. P1k,t1, P1k,t2, P1k,t3) may be detected by using a pattern recognition algorithm. Each particle P0 may be assumed to have a substantially constant velocity during the exposure time Tex.
A candidate group representing a particle may be accepted if the sub-images of said group are aligned in a substantially linear manner and if the distance between adjacent sub-images of said candidate group match with the timing (t1,t2,t3) of the illuminating light pulses LB0.
A candidate group may be e.g. discarded if the sub-images of said group are not aligned in a linear manner and/or if the distance between adjacent sub-images of said candidate group do not match with the timing (t1,t2,t3) of the illuminating light pulses LB0.
AX0′ may indicate the position of the axis AX0 of the jet JET0. AREA0′ may indicate the position of the reference area AREA0. The position of the projection of the reference area AREA0 may be indicated by a line AREA0′, which may be superposed on the captured image IMG2. The position of the projection of the axis AX0 may be indicated by a line AX0′, which may be superposed on the captured image IMG2.
Np/bin may indicate the number Np of particles whose velocity is within a velocity range associated with a bin BIN1, BIN2, BIN3, . . . . For example the height of the vertical bar marked with the symbol BIN2 may represent the number Np of particles P0 whose velocity was within the range defined by the velocities vBIN1 and vBIN2 during a measurement time period TMEAS. For example the height of the vertical bar marked with the symbol BIN3 may represent the number Np of particles P0 whose velocity was within the range defined by the velocities vBIN2 and vBIN3 during a measurement time period TMEAS. The predetermined velocity ranges (e.g. from vBIN2 to vBIN3) may be called e.g. as the velocity bins.
The number Np associated with a bin may be indicative of a probability that a (randomly selected) particle of the jet has a velocity, which is within said bin. The velocity distributions of
Referring to
The method may comprise:
Np/bin may indicate the number Np of particles whose kinetic energy is within an energy range associated with a bin BIN21, BIN22, BIN23, . . . . For example the height of the vertical bar marked with the symbol BIN22 may represent the number Np of particles P0 whose kinetic energy was within the range defined by the energy values EBIN21 and EBIN22 during the measurement time period TMEAS. The height of the vertical bar marked with the symbol BIN23 may represent the number Np of particles P0 whose kinetic energy was within the range defined by the values EBIN22 and EBIN23 during said measurement time period TMEAS. For example, the energy bin BIN23 may represent energy values, which are within the range from 24 mJ to 35 mJ, and the number Np of particles having the kinetic energy within said range may be approximately equal to 490 during the measurement time period TMEAS.
The method may comprise fitting a regression function to the measured data.
The velocity distribution pv(v) may also sometimes have two or more peaks.
Referring to
The spatial distributions of
The particles P0 hitting the surface SRF1 may slightly deform the surface SRF1. The particles P0 may irreversibly deform the surface SRF1. For example, a particle P0k may cause a first microscopic dent D0k in the surface SRF1 of the test strip AS1. For example, a particle P0k+1 may cause a second microscopic dent D0k+1 in the surface SRF1 of the test strip AS1. The particles may cause residual compressive stress in the surface layer of the test strip AS1 such that the test strip is bent. The surface of the strip may have a plurality of dents after it has been exposed to the particle jet. The strip may be curved after it has been exposed to the particle jet. The shape of the test strip AS1 may be defined e.g. by an arc height value hAS and/or by a radius of curvature R1. The arc height value hAS may be measured according to a standardized method e.g. by using a measuring instrument called as the Almen gage.
The operating parameters of a (first) shot peening unit 700 may comprise e.g.:
A set of operating parameters of the shot peening unit 700 may refer e.g. to the following group of parameters:
A relationship between operating parameter values and corresponding arc height values hAS may be described by a model MODEL1. The method may comprise determining one or more parameter values of the model MODEL1.
A change of a parameter value may have an effect on the total kinetic energy of particles passing through the reference area per unit time. Thus, said change of a parameter value may have an effect on the capability of the particle jet to cause deformation of a surface. The model MODEL1 may be determined experimentally. The effect of an operating parameter on the total energy may be determined experimentally by varying the operating parameter and by using the measuring instrument 500 for measuring corresponding total energy values EMEAS. The effect of said operating parameter on the arc height value may be determined experimentally by varying the operating parameter and by exposing a test strip AS1 to the particle jet. A data point (e.g. D1 in
The device 500 may be configured to receive one or more measured arc height values hAS e.g. via the user interface UIF1 and/or via the communication unit RXTX1. For example, a user may input one or more measured arc height values hAS via the user interface UIF1. For example, the communication unit RXTX1 may receive one or more measured arc height values hAS from an Almen gage and/or from another measuring instrument. The communication unit RXTX1 may also be called as a communication interface.
The apparatus 500 may comprise:
The method may comprise obtaining one or more data points D1, D2 such that a first data point D1 is obtained by using a first set of operating parameters. The model MODEL1 may be determined by e.g. fitting a function based on the data point D1.
The method may comprise obtaining two or more data points D1, D2 such that a first data point D1 is obtained by using a first set of operating parameters, and a second data point D2 is obtained by using a second different set of operating parameters. The model MODEL1 may be determined by e.g. fitting a function to the obtained data points D1, D2.
A change of an operating parameter of the shot peening unit 700 may have an effect on the total energy value EMEAS, which in turn may have an effect on the corresponding arc height value hAS. Thus, the model MODEL1 may also describe the relationship between total energy values EMEAS and the corresponding arc height values hAS. The model MODEL1 may be used for estimating an arc height value hAS=hAS(EMEAS), which is likely to correspond to a measured energy value EMEAS.
Determining the model MODEL1 may comprise determining a first data point (D1), which comprises a first measured total energy value EMEAS,1, and a first measured arc height value hAS,1. The first height value hAS,1 may be measured by exposing a test strip AS1 to the particle jet during a first measurement time period TMEAS,1A. The first measured total energy value EMEAS,1 may be determined from one or more velocity values obtained by analyzing images IMG2 captured during a second measurement time period TMEAS,1B. The second measurement time period TMEAS,1B may also be called e.g. as a first auxiliary time period. The particle jet may be provided by a first shot peening unit 700 during the measurement time periods TMEAS,1A, TMEAS,1B by using a first set of operating parameters. The distance L1 between the first shot peening unit 700 and the test strip AS1 may be substantially equal to the distance L0 between the first shot peening unit 700 and the reference area AREA0 during the measurement time periods TMEAS,1A, TMEAS,1B. In other words, the measuring device 500 may be arranged to operate such that the measured energy value EMEAS,1 substantially corresponds to the integrated energy of the particle flux passing through a reference area AREA0, wherein the distance between the first shot peening unit 700 and the reference area AREA0 is substantially equal to the distance L1.
A second data point D2 may comprise a second measured total energy value EMEAS,2, and a second measured arc height value hAS,2. The second height value hAS,2 may be measured by exposing a second test strip AS1 to the particle jet during a second measurement time period TMEAS,2A. The second measured total energy value EMEAS,2 may be determined by analyzing images IMG2 captured during a second auxiliary time period TMEAS,2B. The particle jet may be provided by the first shot peening unit 700 during the measurement time periods TMEAS,2A, TMEAS,2B by using a second set of operating parameters. The distance L1 between the first shot peening unit 700 and the test strip AS1 may be substantially equal to the distance L0 between the first shot peening unit 700 and the reference area AREA0 during the measurement time periods TMEAS,1A, TMEAS,1B, TMEAS,2A, TMEAS,2B.
A third data point D3 may comprise a third measured total energy value EMEAS,3, and a third measured arc height value hAS,3. The third height value hAS,3 may be measured by exposing a third test strip AS1 to the particle jet during a third measurement time period TMEAS,3A. The third measured total energy value EMEAS,3 may be determined by analyzing images IMG2 captured during a third auxiliary time period TMEAS,3B. The particle jet may be provided by the first shot peening unit 700 during the measurement time periods TMEAS,3A, TMEAS,3B by using a third set of operating parameters. The distance L1 between the first shot peening unit 700 and the test strip AS1 may be substantially equal to the distance L0 between the first shot peening unit 700 and the reference area AREA0 during the measurement time periods TMEAS,1A, TMEAS,1B, TMEAS,2A, TMEAS,2B, TMEAS,3A, TMEAS,3B.
An estimate (e.g. hE) for an arc height value may be subsequently determined from a measured energy value EMEAS by using the model hAS(EMEAS). The measured energy value EMEAS may correspond e.g. to a point F1 of the regression curve CRV1.
Table 1 shows, by way of example, measured values associated with the measurement time periods TMEAS,1A, TMEAS,1B, TMEAS,2A, TMEAS,2B, TMEAS,3A, TMEAS,3B. The measurement time periods listed in Table 1 have the same length.
pacc denotes a pressure of accelerating gas of the shot peening unit 700. kPa means kiloPascal. The pressure pacc may have an effect of the initial velocity of the particles. The velocity of the accelerating gas may depend on the pressure pacc. The mass flow rate of the accelerating gas may depend on the pressure pacc.
hAS denotes the arc height value of the Almen strip AS1 after the strip AS1 has been exposed to the particle jet during the measurement time period TMEAS,1A, TMEAS,2A, or TMEAS,3A.
NMEAS denotes the number of particles which pass through the reference area AREA0 during the measurement time period TMEAS,1B, TMEAS,2B, or TMEAS,3B. The number NMEAS may be determined by analyzing the images captured by the measuring device 500 during the measurement time period TMEAS,1B, TMEAS,2B, or TMEAS,3B.
vAVE denotes the average velocity of particles which pass through the reference area AREA0 during the measurement time period TMEAS,1B, TMEAS,2B, or TMEAS,3B. The average velocity vAVE may be determined by analyzing the images captured by the measuring device 500 during the measurement time period TMEAS,1B, TMEAS,2B, or TMEAS,3B.
EMEAS denotes the total kinetic energy of particles which pass through the reference area AREA0 during the measurement time period TMEAS,1B, TMEAS,2B, or TMEAS,3B. The energy values EMEAS may be determined by analyzing the images captured by the measuring device 500 during the measurement time period TMEAS,1B, TMEAS,2B, or TMEAS,3B.
The model MODEL1 may be determined from the one or more experimentally measured data points D1, D2, D3. The model MODEL1 may be determined by fitting a function to the one or more determined data points D1, D2, D3. The model MODEL1 may be a regression function hAS(EMEAS), which may be fitted to the data points D1, D2, D3. The model MODEL1 may be e.g. a polynomial function, which is fitted to the data points D1, D2, D3. The function hAS(EMEAS) may be represented e.g. by a curve CRV1 shown in
The model MODEL1 may be used for estimating an arc height value hAS,E from a measured energy value EMEAS. The method may comprise:
NMEAS may denote the number of particles hitting the test strip AS1 during a measurement time period TMEAS. NMEAS may also denote the number of particles passing through the reference area AREA0 during a measurement time period TMEAS. The length of the measurement time period TMEAS may be e.g. in the range of 1 s to 1000 s. Ek may denote the kinetic energy of an individual particle P0k. mk may denote the mass of the individual particle P0k. The kinetic energy Ek of an individual particle P0k may be calculated from the velocity vk of said particle P0k by using the equation:
The total kinetic energy EMEAS of particles P0k, P0k+1, P0k+2, . . . passing through the reference area AREA0 during the measurement time period TMEAS may be calculated by using the following equation:
The particles P0k, P0k+1, P0k+2, . . . may have a narrow size distribution. For example, more than 90% of the total mass of the particles may be represented by particles, whose mass is in the range of 70% to 150% of the average mass of the particles. For example, more than 90% of the total mass of the particles may be represented by particles, whose diameter is in the range of 70% to 150% of the mass median diameter of the particles.
Consequently, the mass mk, mk+1, mk+2, . . . of each individual particle P0k, P0k+1, P0k+2, . . . may be approximated by the average mass mAVG:
mk≈mAVG (3)
The square (vRMS)2 of the RMS velocity vRMS may be defined and calculated by using the following equation:
RMS means root mean square. The RMS velocity vRMS may be determined by analyzing images IMG2 captured during the measurement time period TMEAS.
Combining the equations (2), (3), (4) may provide:
The number of particles appearing in each captured image may be proportional to the instantaneous number density of particles of the jet. The number of sub-images P1k, P1k+2, Pk+2, . . . may be proportional to the instantaneous number density of particles of the jet. The number NMEAS may be determined by analyzing images IMG2 captured during the measurement time period TMEAS.
The total number NMEAS may be estimated e.g. according to the following equation:
NIMG,AVE may denote an average number of particles appearing in a single captured image. Cg may denote a proportionality constant, i.e. a coefficient. The coefficient Cg may depend e.g. on dimensions of the measuring region RG0 in the directions SX and SZ. The size of the measuring region RG0 may depend on the field of view of the imaging unit 200 and on the optical magnification of the imaging unit 200.
vAVE may denote the average velocity of the particles. To the first approximation, the number density of particles in the jet may be inversely proportional to the average velocity vAVE of the particles, in a situation where the mass flow rate of the particles is substantially constant.
d0 may denote the thickness of the measurement region RG0 in a direction, which is parallel to the optical axis AX2 of the imaging unit 200. To the first approximation, the relative fraction of particles passing through the reference area AREA0 without passing through the measurement region RG0 may be inversely proportional to the thickness d0 of the measurement region RG0.
The coefficient Cg may also be determined experimentally e.g. by positioning an aperture to the jet, collecting all particles which pass through the aperture during a test period, determining the total mass of the collected particles by weighing, and by dividing the total mass by the average mass of single particles. The coefficient Cg may be determined experimentally and/or theoretically for each measurement set-up.
Combining (5) with (6) gives:
Equation (7) may be re-arranged e.g. into the following form:
The values NIMG,AVE, vRMS, and vAVE associated with the measurement time period TMEAS may be determined by analyzing the images captured by the measuring device 500. The total energy EMEAS may be calculated from the values NIMG,AVE, vRMS, and vAVE e.g. by using the equation (8). A corresponding arc height value hAS may be subsequently estimated from the total energy EMEAS by using the model MODEL1.
The velocity value vRMS and the velocity value vAVE may be determined separately e.g. in order to improve the accuracy of the estimated energy value.
However, the velocity value vRMS may also be calculated from the velocity value vAVE by using information about the velocity probability distribution function. The velocity value vAVG may be calculated from the velocity value vRMS by using information about the velocity probability distribution function. The velocity probability distribution function may be measured e.g. by analyzing the captured images. The velocity probability distribution may also be assumed to match with a predetermined function. The velocity probability distribution may be assumed to match e.g. with a Gaussian function.
The model MODEL1 may also be determined based on the measured values vRMS, vAVE and NIMG,AVE and based on one or more measured arc height values hAS such that it is not necessary to separately determine the value of the coefficient Cg. The contribution of the coefficient Cg may be incorporated in the model by fitting the regression function to the experimentally measured data vRMS, vAVE, NIMG,AVE, hAS. The method may comprise determining a model hAS(NIMG,AVE,vAVE,vRMS) which may provide the arc height values as the function of the measured values NIMG,AVE,vAVE,vRMS. The arc height value hAS may be subsequently estimated from the measured values vRMS, vAVE and NIMG,AVE, by using the model MODEL1.
Some particles of the jet JET0 may travel though the measurement region RG0 such that they are not directly detected by the measuring device 500. Some particles of the jet JET0 may travel though the measurement region RG0 such that the sub-images of those particles do not appear in any digital image captured by the imaging unit 200. Some particles may travel outside the depth of field (DoF) of the imaging unit 200. Some particles may travel through the measurement region RG0 when the jet is not illuminated by the illuminating unit. Some particles may travel through the measurement region REG0 when the image sensor SEN1 is not in the active light-detecting state, i.e. between two consecutive exposure time periods. The un-detected particles may be taken into consideration by using the coefficient Cg.
The number NMEAS may also be determined e.g. by measuring the mass flow and/or volumetric flow of the particles supplied to the shot peening unit 700. The number NMEAS may also be determined e.g. by collecting and weighing the particles after they have been accelerated by the shot peening unit 700. However, even in that case determining the particle density from the captured images may improve the reliability of the method.
A shot peening process may need to be verified when producing critical parts. A shot peening process may need to be verified e.g. when producing critical parts of an airplane. Shot peening may e.g. relieve tensile stresses built up in a grinding or welding process and replace them with beneficial compressive stresses. Depending on the part geometry, part material, shot material, shot quality, shot intensity, and shot coverage, shot peening may increase fatigue life e.g. more than 100%, or even more than 1000%.
The curve CRV2 has a first point C1 and a second point C2. The points C1 and C2 may be determined by using the model MODEL1. The first point C1 has an arc height value hC1, and the second point C2 has an arc height value hC2. The first point C1 is attained at the processing time TC1, and the second point C2 is attained at the processing time TC2.
The points C1 and C2 may be selected such that the following two conditions are simultaneously fulfilled:
T
C2
−T
C1
=T
C1 (9b)
When the points have been selected such that the equations (9a) and (9b) are fulfilled, then the value TC1 is equal to a time equivalent value TINT of the shot peening process, when using said first set of operating parameters. The time equivalent value TINT may also be called e.g. as the “intensity” of the particle jet JET0. The time equivalent value TINT may also be called e.g. as the “peening intensity rating”. The peening intensity rating TINT may be valid for said first set of operating parameters, at the position of the reference area AREA0. Each peening intensity rating TINT may be associated with a specified position and with a specified set of operating parameters.
The particle jet JET0 may be provided according to a first set of operating parameters (step 1010). For example, the pressure pACC of accelerating gas may be set to a first value.
A plurality of images of the particle jet may be captured (step 1015) when the particle jet JET0 is provided according to the first set of operating parameters.
One or more velocity values (e.g. vRMS, vAVG) may be determined by analyzing the captured images (step 1020). The velocity distribution and the particle density may be determined by analyzing the captured images. The energy flux and/or total energy may be determined from the one or more measured velocity values (step 1030).
One or more test strips AS1 may be exposed to the particle jet JET0 when the particle jet JET0 is provided according to said first set of operating parameters (step 1040).
A deformation value may be obtained by measuring the deformation of a test strip AS1 after it has been exposed to the particle jet JET0. The deformation value may be e.g. an arc height value (hAS).
One or more deformation values may be obtained by measuring the deformation of one or more test strips AS1. For example, a first test strip may be exposed to the particle jet during a first time period, and a second test strip may be exposed to the particle jet during a second time period.
The model MODEL1 may be determined by fitting one or more parameters of a regression function to the measured deformation value and to the one or more measured velocity values (step 1060). An energy value may be determined from the one or more measured velocity values. The model MODEL1 may be determined by fitting one or more parameters of a regression function to the measured deformation value and to the energy value.
The step 1040 may be performed after performing the step 1015 or before performing the step 1015. The steps 1015 and 1040 may also be performed simultaneously. Performing the step 1015 may temporally overlap performing the step 1040.
The particle jet JET0 may be provided in step 1110.
A plurality of images of the particle jet may be captured in step 1120.
One or more velocity values (e.g. vRMS, vAVG) may be determined by analyzing the captured images (step 1130). The energy flux and/or total energy may be determined from the one or more velocity values (e.g. vRMS, vAVG), in step 1140. The velocity distribution and/or the particle density may be determined by analyzing the captured images.
A deformation value may be estimated from the measured velocity distribution and from the measured particle density by using the model MODEL1 (step 1150). The deformation value may be e.g. an arc height value (hAS).
The length of a processing time period may be selected according to the estimated deformation value (step 1160).
A value of an operating parameter may also be selected based on the estimated deformation value in step 1160. For example the pressure of accelerating gas may be selected and/or adjusted based on the estimated deformation value.
The surface SRF2 of an object OBJ1 may subsequently be processed according to the selected length of a processing time period (step 1170).
The particle jet may be provided according to selected operating parameters (step 1210).
A plurality of images IMG2 may be captured by the imaging device 500 (step 1220). The particle jet JET0 may be illuminated with a sequence SEQ1 of illuminating light pulses such that a captured image IMG2 comprises two or more adjacent sub-images of the same particle. In particular, the particle jet JET0 may be illuminated with a sequence SEQ1 of illuminating light pulses such that a captured image IMG2 comprises three or more adjacent sub-images of the same particle.
One or more velocity values (e.g. vRMS, vAVG) may be determined by analyzing the captured images (step 1230).
The velocity distribution and the particle density may be determined by analyzing the captured images. The energy flux and/or total energy may be determined from the one or more measured velocity values. The images may be captured when the shot peening unit 700 is operated according to said selected operating parameters.
The measured values obtained by analyzing the images may be compared with one or more reference values in order to check whether the shot peening capability of the jet is in a predetermined range (step 1240).
An energy value may be determined by analyzing the captured images, and a deformation value may be determined from the energy value by using the model MODEL1. The deformation value may be compared with a reference value in order to check whether the shot peening capability of the jet is in a predetermined range. The deformation value may be e.g. arc height value hAS or a time equivalent value TINT. The energy value may represent e.g. the flux of kinetic energy of particles passing through the reference area AREA0 or the total kinetic energy of particles passing through the reference area AREA0 during a predetermined time period. The method may comprise determining the energy value from the measured velocity distribution and from the measured particle distribution.
A deformation value may be determined from the measured velocity distribution and the particle distribution by using the model MODEL1, and the deformation value may be compared with a reference value in order to check whether the shot peening capability of the jet is in a predetermined range. The deformation value may be e.g. arc height value hAS or a time equivalent value TINT.
The method may comprise:
The method may comprise:
The estimate may be compared with one or more reference values in order to determine whether the estimate is in the predetermined range. The shot peening operation may refer to a method which comprises operating the first shot peening unit (700) according to a specified set of operating parameters during a specified time period.
An energy value may be determined by analyzing the captured images, and the energy value may be compared with a reference value in order to check whether the shot peening capability of the jet is in a predetermined range. The deformation value may be e.g. arc height value hAS or a time equivalent value TINT.
The measured velocity distribution may be compared with one or more first reference values, and/or the measured particle distribution may be compared with one or more second reference values in order to check whether the shot peening capability of the jet is in a predetermined range.
The steps 1210, 1220, 1230 and 1240 may be performed as discussed above with reference to
The adjustable and/or selectable parameters of the shot peening process may comprise e.g. one or more of the following:
The velocity of a particle may have significant transverse component, i.e. the velocity is not always parallel with the axis AX0 of the jet. The velocity vk of a particle may have an axial component vk,z and a transverse component vk,y. The axial component vk,z is parallel with the axis AX0, and the transverse component vk,y is perpendicular to the axis AX0. When evaluating the shot peening capability, the kinetic energy of each particle may be calculated from the axial component vk,z, by omitting the transverse component vk,y. The capability of a particle P0k to deform a surface SRF1 may mainly depend on the axial velocity component vk,z of said particle. The velocity values (vRMS, vAVE) used e.g. in equations (1) to (8) may be determined from the axial velocity values vz of the individual particles P0. The axial velocity values vz of the individual particles P0 may be determined from the captured images.
The velocity of an individual particle P0k may also be determined by capturing a first image by using first single illumination pulse at a time t1, and capturing a second image by using a second single illumination pulse at a time t2. The first image may comprise a first sub-image P1k,t1 of the particle P0k. The second image may comprise a second sub-image P1k,t2 of the particle P0k. The spatial displacement Δuk associated with the particle P0k may be determined by comparing the first image with the second image. The velocity of the particle P0k may be determined from the displacement Δuk and from the time difference t2−t1.
The method may comprise determining an angular divergence of the particle jet JET0 by analyzing the captured images IMG1.
The method may comprise determining a width and/or a radial dimension of the particle jet JET0 by analyzing the captured images IMG1.
Shot peening may be used e.g. for processing a gear part, camshaft, clutch spring, coil spring, leaf spring, suspension spring, connecting rod, crankshaft, gearwheel, part of an aircraft, part of a landing gear, components of an engine of an aircraft, engine housing, rock drill and/or turbine blade.
For the person skilled in the art, it will be clear that modifications and variations of the devices and the methods according to the present invention are perceivable. The figures are schematic. The particular embodiments described above with reference to the accompanying drawings are illustrative only and not meant to limit the scope of the invention, which is defined by the appended claims.
Number | Date | Country | Kind |
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20165678 | Sep 2016 | FI | national |
Filing Document | Filing Date | Country | Kind |
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PCT/FI2017/050623 | 9/5/2017 | WO | 00 |
Publishing Document | Publishing Date | Country | Kind |
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WO2018/046795 | 3/15/2018 | WO | A |
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Number | Date | Country |
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2016-049571 | Apr 2016 | JP |
2017-226024 | Dec 2017 | JP |
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Number | Date | Country | |
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20190299361 A1 | Oct 2019 | US |