JP2009186191A - Dimension measuring device and method - Google Patents

Abstract

<P>PROBLEM TO BE SOLVED: To provide a dimension measuring device and a dimension measuring method capable of accurately detecting a peak position of interference fringe and precisely measuring a dimension in dimension measurement using white interference. <P>SOLUTION: The dimension measuring device 1 includes a first interferometer 3 diverging light from a white light source 2 into a first luminous flux and a second luminous flux and causing a first optical path difference corresponding to a measured object dimension of a measured object between the two luminous fluxes; a second interferometer 4 diverging the luminous flux emitted from the first interferometer 3 into a third luminous flux and a fourth luminous flux and causing a second optical path difference between the two luminous fluxes; a detector 5b receiving the third and fourth luminous fluxes and detecting an interference signal; a phase shift signal-generating sections 44, 5a generating an interference signal having a phase different by 90 degrees from that of the interference signal; and a controller 6 calculating a Lissajous waveform based on the two interference signals, obtaining the peak position of interference fringe corresponding to the measured object from the maximum value, and obtaining a measured object dimension from the second optical path difference corresponding to the peak position. <P>COPYRIGHT: (C)2009,JPO&INPIT

Description

  The present invention relates to a dimension measuring apparatus and a dimension measuring method, and more particularly to a dimension measuring apparatus and a dimension measuring method using white interference.

  Conventionally, a method using the principle of white interference has been proposed as a method for accurately measuring the dimension or surface roughness of an object to be measured, such as a machined part, in a non-contact manner. In such a method, the measurement light emitted from the white light source is divided into two light beams, one is reflected by the object to be measured, and the other is reflected by the reference mirror. Give rise to At this time, white interference fringes are observed when the optical path lengths between the two light beams are substantially equal. The white interference fringe has the largest amplitude when the optical path difference between the two light fluxes becomes zero, and the amplitude sharply decreases as the optical path difference increases. Further, the white interference fringe vibrates at a period depending on the center wavelength of the measurement light (for example, a period that is 1/2 times the center wavelength). Therefore, the measurement target dimension of the object to be measured is obtained by measuring the peak position where the amplitude of the white interference fringe is maximum. Therefore, in this measurement method, it is necessary to accurately obtain the peak position of the observed white interference fringes in order to accurately measure the measurement target dimension of the object to be measured. For this purpose, it is known that the envelope of the observed white interference fringes is obtained and the position where the maximum value of the obtained envelope is the peak position of the white interference fringes (see Patent Document 1).

US Pat. No. 6,597,460

  When obtaining the envelope of the white interference fringe, in order to remove the vibration component of the interference fringe depending on the wavelength of the measurement light, the interference signal obtained by converting the interference fringe into an electric signal is passed through a low-pass filter and its high frequency Remove ingredients. However, unless the cut-off frequency of the low-pass filter is appropriately set with respect to the period of interference fringes and the sampling pitch for acquiring the interference fringes, high-frequency components cannot be removed from the interference signals. FIG. 1 shows an interference signal in such a case. In FIG. 1, the horizontal axis represents the optical path difference, and the vertical axis represents the interference fringe intensity. As shown in FIG. 1, the signal value of the ideal envelope 101 varies with respect to the detected white interference signal 100 only depending on the increase or decrease of the amplitude of the white interference fringes. For this reason, the position of the maximum signal value of the envelope 101 coincides with the position where the optical path difference becomes 0 with very high accuracy. However, it has been difficult to appropriately set the cutoff frequency of the low-pass filter. Since the cut-off frequency cannot be set appropriately, the signal value of the envelope 102 when the high-frequency component of the white interference fringes cannot be removed varies depending on the vibration period of the white interference fringes. For this reason, it has been difficult to accurately obtain the position where the optical path difference is 0 from such an envelope 102.

  In view of the above problems, an object of the present invention is to provide a dimension measuring apparatus and a dimension measuring apparatus capable of accurately detecting a peak position of interference fringes and measuring a dimension accurately in dimension measurement using white interference. It is to provide a method.

According to one embodiment of the present invention, a dimension measuring device for measuring a dimension of an object to be measured is provided. Such a dimension measuring apparatus splits a white light source and light emitted from the white light source into a first light beam and a second light beam directed to the object to be measured, and reflects the first light beam on the object to be measured. A first interferometer that generates a first optical path difference corresponding to the measurement target dimension of the object to be measured between the two light beams and emits the first light beam and the second light beam according to one light beam; A reference mirror whose position is fixed, a movable mirror movable along the optical path, and a light beam emitted from the first interferometer, and a third light beam directed to the reference mirror. A second beam interferometer that includes a beam splitting unit that splits the beam into a fourth beam traveling toward the movable mirror, and that generates a second optical path difference between the third beam and the fourth beam, A white interference fringe generated when the first light path difference and the second optical path difference are approximately equal is detected by receiving the light flux and the fourth light flux, A detector that outputs a corresponding first interference signal, a phase shift signal generation unit that generates a second interference signal that is 90 degrees out of phase with the first interference signal, and a controller that determines a measurement target dimension of the object to be measured Have
The controller includes a signal synthesis unit that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal, and the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as a peak position of the white interference fringes. And a dimension determining unit that calculates a measurement target dimension of the object to be measured by calculating a second optical path difference with respect to the peak position.

  In the present invention, the phase shift signal generation unit is disposed between the reference mirror and the light beam splitting unit, transmits a part of the third light beam, and delays the phase of a part of the light beam by 90 degrees. And a second detector for detecting, as a second interference signal, an interference signal corresponding to a white interference fringe generated between a part of the third light beam whose phase is delayed by 90 degrees and the fourth light beam. It is preferable to have.

  Alternatively, in the present invention, the phase shift signal generation unit is disposed between the moving mirror and the light beam splitting unit, transmits a part of the fourth light beam, and delays the phase of a part of the light beam by 90 degrees. And a second detector for detecting, as a second interference signal, an interference signal corresponding to a white interference fringe generated between a part of the fourth light beam whose phase is delayed by 90 degrees and the third light beam. It is preferable to have.

According to another embodiment of the present invention, a dimension measuring device for measuring a dimension of an object to be measured is provided. The dimension measuring apparatus is a white light source, an interferometer, a movable mirror that can move along an optical path, and a light beam emitted from the white light source toward the first light beam and the movable mirror that are directed to the object to be measured. An interferometer that includes a light beam splitting unit that branches into a second light beam, reflects the first light beam by an object to be measured, and generates an optical path difference between the first light beam and the second light beam; The first light flux and the second light flux emitted from the meter are received, and a white interference fringe generated when the optical path length for the first light flux and the optical path length for the second light flux are substantially equal is detected. A detector that outputs a first interference signal corresponding to an interference fringe, a phase shift signal generation unit that generates a second interference signal that is 90 degrees out of phase with the first interference signal, and a measurement target dimension of the object to be measured A controller for determining
The controller includes a signal synthesis unit that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal, and the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as a peak position of the white interference fringes. And a dimension determining unit that calculates a measurement target dimension by calculating a difference between the position of the movable mirror with respect to the peak position and a predetermined reference position of the movable mirror.

  In the present invention, the phase shift signal generation unit is disposed between the DUT and the light beam splitting unit, transmits a part of the first light beam, and changes the phase of a part of the first light beam to 90. And a second wave plate for detecting an interference signal corresponding to a white interference fringe generated between a part of the first light beam whose phase is delayed by 90 degrees and the second light beam, as a second interference signal. It is preferable to have a detector.

  Alternatively, in the present invention, the phase shift signal generation unit is disposed between the movable mirror and the light beam splitting unit, transmits a part of the second light beam, and sets the phase of a part of the second light beam to 90 degrees. Second detection for detecting, as a second interference signal, a wave plate to be delayed and an interference signal corresponding to a white interference fringe generated between a part of the second light beam whose phase is delayed by 90 degrees and the first light beam. It is preferable to have a container.

  According to still another embodiment of the present invention, a dimension measuring device for measuring a dimension of an object to be measured is provided. The dimension measuring apparatus includes a white light source, a first interferometer, a reference mirror having a fixed position, a movable mirror movable along an optical path, and light emitted from the white light source. A first beam that splits into a first beam that travels toward the moving mirror and a second beam that travels toward the moving mirror, and a first optical path difference is generated between the first beam and the second beam. The interferometer, the first light beam and the second light beam emitted from the first interferometer are branched into a third light beam and a fourth light beam directed to the object to be measured, and the third light beam is divided into the object to be measured. The second optical path difference corresponding to the measurement target size of the object to be measured is generated between the first light beam and the fourth light beam, and the third light beam and the fourth light beam are emitted in accordance with one light beam. 2 interferometer, 3rd light beam and 4th light beam are received, and white interference fringes generated when the first optical path difference and the second optical path difference are substantially equal are detected. A detector that outputs a first interference signal corresponding to the white interference fringe, a phase shift signal generation unit that generates a second interference signal that is 90 degrees out of phase with the first interference signal, It has a controller that determines the dimensions to be measured. The controller includes a signal synthesis unit that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal, and the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as a peak position of the white interference fringes. And a dimension determining unit for determining a measurement target dimension by calculating a first optical path difference with respect to the peak position.

  According to still another embodiment of the present invention, a dimension measuring device for measuring a dimension of an object to be measured is provided. Such a dimension measuring apparatus splits a white light source and light emitted from the white light source into a first light beam and a second light beam directed to the object to be measured, and reflects the first light beam by the object to be measured. A first interferometer that causes a first optical path difference corresponding to the measurement target dimension of the object to be measured between the second light flux and emits the first light flux and the second light flux according to one light flux. And a second interferometer, a reference mirror, a movable mirror movable along the optical path, and a light beam emitted from the first interferometer toward a third light beam toward the reference mirror and the movable mirror A second beam interferometer that includes a beam splitting unit that splits the beam into a fourth beam, and that generates a second optical path difference between the third beam and the fourth beam, and is attached to a reference mirror. A modulator that vibrates the mirror back and forth along the third light flux; and an oscillation signal connected to the modulator and having a predetermined oscillation frequency. A high-frequency oscillator that inputs to the tuner and vibrates the modulator at the predetermined oscillation frequency, and receives the third light beam and the fourth light beam, and the first optical path difference and the second optical path difference are substantially equal. The white interference fringes generated in the case are detected, and the white interference fringes are connected to the detector and the high frequency oscillator, which outputs a high frequency modulation interference signal in which the high frequency modulation is performed at a predetermined oscillation frequency. By comparing the phase of the high-frequency modulation interference signal with the phase of the oscillation signal input from the high-frequency oscillator, the first and second interference signals corresponding to the white interference fringe and shifted by 90 degrees from each other are output. And a controller for obtaining a measurement target dimension of the object to be measured based on the first and second interference signals. The controller includes a signal synthesis unit that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal, and the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as a peak position of the white interference fringes. And a dimension determining unit that calculates a second optical path difference with respect to the peak position to obtain a measurement target dimension.

  According to still another embodiment of the present invention, a dimension measuring device for measuring a dimension of an object to be measured is provided. The dimension measuring apparatus is a white light source, a first interferometer, a reference mirror, a movable mirror movable along the optical path, and a light emitted from the white light source toward the reference mirror. A first interferometer that includes a light beam and a light beam splitting part that branches into a second light beam that is directed to the movable mirror, and that generates a first optical path difference between the first light beam and the second light beam; The first light beam and the second light beam emitted from the first interferometer are branched into a third light beam and a fourth light beam directed to the object to be measured, and the third light beam is reflected by the object to be measured. A second interferometer that generates a second optical path difference corresponding to the measurement target dimension of the object to be measured between the fourth light flux and emits the third light flux and the fourth light flux in accordance with one light flux. And a modulator that is attached to the reference mirror and vibrates back and forth along the first light flux, and is connected to the modulator and has a predetermined oscillation frequency A high-frequency oscillator that inputs the oscillation signal to the modulator and vibrates the modulator at the predetermined oscillation frequency, and receives the third and fourth light beams, and the first optical path difference and the second optical path difference. Is connected to a detector that detects a white interference fringe generated when the white interference fringes are substantially equal, and outputs a high-frequency modulation interference signal in which the white interference fringe is high-frequency modulated at a predetermined oscillation frequency. By comparing the phase of the high frequency modulation interference signal input from the high frequency oscillator with the phase of the oscillation signal input from the high frequency oscillator, the first and second phases corresponding to the white interference fringes are shifted by 90 degrees with respect to each other. A phase detector that outputs an interference signal; and a controller that determines a measurement target dimension of the object to be measured based on the first and second interference signals. The controller includes a signal synthesis unit that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal, and the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as a peak position of the white interference fringes. And a dimension determining unit that calculates a second optical path difference with respect to the peak position to obtain a measurement target dimension.

According to still another embodiment of the present invention, the light emitted from the white light source is branched into a first light beam and a second light beam that are directed toward the object to be measured, and the first light beam is divided by the object to be measured. A first optical path difference corresponding to the measurement target dimension of the object to be measured is generated between the reflected light and the second light flux, and the first light flux and the second light flux are emitted in accordance with one light flux. Interferometer, a second interferometer, a reference mirror having a fixed position, a movable mirror movable along the optical path, and a light beam emitted from the first interferometer toward the reference mirror A second interferometer that includes a third light beam and a light beam splitting unit that branches into a fourth light beam that travels toward the movable mirror, and that generates a second optical path difference between the third light beam and the fourth light beam. , Receiving the third light beam and the fourth light beam, and detecting a white interference fringe generated when the first optical path difference and the second optical path difference are substantially equal to each other. Dimension measuring method of the object to be measured is provided in the measurement system having a detector which outputs a first interference signal corresponding to Watarushima.
The dimension measuring method includes a step of generating a second interference signal whose phase is 90 degrees different from that of the first interference signal, and a step of calculating a Lissajous waveform signal based on the first interference signal and the second interference signal. Determining the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringe, and calculating the second optical path difference with respect to the peak position, Have
In each of the above embodiments, the white light source is not limited to a light source that emits light in a broad band in the visible light range, but a light source that emits light in a certain wavelength band with a predetermined wavelength as a center wavelength.

  According to the present invention, it is possible to provide a dimension measuring apparatus and a dimension measuring method capable of accurately detecting a peak position of an interference fringe and measuring a dimension accurately in dimension measurement using white interference. It became.

Hereinafter, a first embodiment in which the present invention is applied to an inner diameter measuring apparatus that measures the inner diameter of a cylindrical object to be measured, such as a ring gauge or a cylinder, will be described with reference to the drawings.
The inner diameter measurement apparatus according to the first embodiment of the present invention causes light from a white light source to enter a first interferometer, and the first interferometer has an optical path difference corresponding to the inner diameter of the object to be measured. Produces two luminous fluxes. The two light beams are incident on the second interferometer, and the light beams are divided and interfered with each other in two optical paths that generate an optical path difference substantially equal to the optical path difference, thereby generating white interference fringes. The detector detects the position where the amplitude of the white interference fringe is maximum, that is, the peak position of the white interference fringe, and measures the optical path difference between the two optical paths of the second interferometer. Find the inner diameter. At that time, the inner diameter measuring device generates two interference fringes whose phases are shifted from each other by 90 degrees in the second interference fringe, and obtains a Lissajous waveform signal from the two interference fringes. Then, the position corresponding to the maximum value of the Lissajous waveform signal is set as the peak position of the white interference fringe, and the inner diameter dimension of the object to be measured is obtained.

  FIG. 2 is a diagram showing a schematic configuration of the inner diameter measuring apparatus 1 according to the first embodiment of the present invention. The inner diameter measuring device 1 includes a white light source 2, a first interferometer 3 that generates an optical path difference corresponding to twice the inner diameter of the object to be measured, and an optical path difference generated by the first interferometer 3. A second interferometer 4 that generates an optical path difference and generates two white interference fringes that are 90 degrees out of phase with each other; detectors 5a and 5b that detect the respective white interference fringes; A controller 6 is provided for determining the inner diameter of the object to be measured from the detected interference fringes. Further, the inner diameter measuring device 1 includes an optical fiber 7 that transmits light from the white light source 2 to the first interferometer 3 and an optical fiber 8 that transmits light emitted from the first interferometer 3 to the second interferometer. Have.

  The white light source 2 is a light source that has a short coherence length and can emit light having a broad wavelength. As the white light source 2, for example, an LED, an SLD (super luminescent diode), an SOA (Semiconductor Optical Amplifier) light source, an ASE (Amplified Spontaneous Emission) light source, or the like can be used. The center wavelength of the light emitted from the white light source 2 can be set to 750 nm, 1300 nm, 1550 nm, and the like, for example. In the present embodiment, an infrared LED having a center wavelength of 1550 nm is used as the white light source 2.

  FIG. 3 shows a schematic configuration diagram of the first interferometer 3. In the first interferometer 3, two light beams B 1 and B 2 having an optical path difference corresponding to twice the inner diameter of the DUT 10 arranged on the XYZ stage 36 are generated. For this purpose, in the first interferometer 3, the light incident from the white light source 2 through the first optical fiber 7 is converted into parallel light by the collimator lens 31, and the first position for adjusting the output position with respect to the incident parallel light is adjusted. To the wedge prism 32. Then, the light emitted from the wedge prism 32 is incident on a beam splitter 33 disposed substantially at the center of the inner diameter of the DUT 10. The incident light is reflected by the beam splitter 33 and branched into a light beam traveling toward the inner surface S1 of the DUT 10 and a light beam B2 that passes through the beam splitter 33 and travels straight. The light beam traveling toward the inner surface S1 of the device under test 10 returns to the beam splitter 33 after being reflected by the inner surface S1 of the device under test 10. A part of the light beam returned to the beam splitter 33 passes through the beam splitter 33 and travels to the inner surface S2 opposite to the inner surface S1 of the DUT 10. Then, the light beam directed toward S2 is reflected by the inner surface S2 and returns to the beam splitter 33 again. A part of the light beam returned to the beam splitter 33 is reflected by the beam splitter 33. This light beam is called B1. The light beam B1 and the light beam B2 are emitted together when emitted from the beam splitter 33. The light beam B1 and the light beam B2 are emitted from the beam splitter 33, then enter the second wedge prism 34 for position adjustment, and the position is adjusted so as to enter the condenser lens 35. Then, the light beam B 1 and the light beam B 2 are collected through the condensing lens 35, exit from the first interferometer 3, and enter the optical fiber 8.

  At this time, since the light beam B1 emitted from the first interferometer 3 reciprocates between the inner surfaces S1 and S2 of the object to be measured 10, if the inner diameter of the object to be measured 10 is D, the light beam B1 and the light beam B2 2D, a 2D optical path difference occurs. A light beam B 1 and a light beam B 2 having a 2D optical path difference are incident on the second interferometer 4 through the optical fiber 8.

  Note that the XYZ stage 36 has an axial direction of the device under test 10 (that is, a direction parallel to the light beam B2), a direction parallel to the light beam B1 and a direction perpendicular to the light beam B1 within a cylindrical cross section orthogonal to the axial direction of the device under test 10. It can be moved in three directions, and is driven by the stage controller 37. The stage controller 37 is electrically connected to the controller 6 and is controlled by the controller 6.

  FIG. 4 shows a schematic configuration diagram of the second interferometer 4. The light beams B1 and B2 emitted from the optical fiber 8 pass through the collimator lens 41 of the second interferometer 4 and become parallel light. Then, the light enters the beam splitter 42. The light beams B1 and B2 are reflected by the beam splitter 42 and branched into light beams B11 and B21 that travel toward the first optical path, and light beams B12 and B22 that pass through the beam splitter 42 and travel toward the second optical path. A light beam B11 represents a light beam that travels to the first optical path of the second interferometer 4 among the light beams B1 emitted from the first interferometer 3, and the light beam B21 emitted from the first interferometer 3. Of the light beam B2, the light beam traveling toward the first optical path of the second interferometer 4 is represented. Similarly, a light beam B12 represents a light beam that travels to the second optical path of the second interferometer 4 among the light beams B1 emitted from the first interferometer 3, and a light beam B22 is emitted from the first interferometer 3. Of the measured light beams B2, the light beams traveling toward the second optical path of the second interferometer 4 are represented.

A reference mirror 43 whose position is fixed is installed in the first optical path. A 1/8 wavelength plate 44 is arranged between the reference mirror 43 and the beam splitter 42 so that only a part of the light beams B11 and B21 are transmitted. The light beams B <b> 11 and B <b> 21 going to the first optical path are reflected by the reference mirror 43 and return to the beam splitter 42, and part of the light passes through the beam splitter 42 and goes to the detector 5. At this time, a part of the light beams B11 and B21 is transmitted through the 1/8 wavelength plate 44 twice, so that the phase of the light beams B11 and B21 is different from that of the other light beams B11 and B21 that do not transmit the 1/8 wavelength plate 44. 90 degrees off. In FIG. 4, for easy understanding, the light beam that passes through the 1/8 wavelength plate 44 and the light beam that does not pass through the 1/8 wavelength plate 44 are shown separately.
On the other hand, a movable mirror 45 that can move along the optical path is provided in the second optical path. The light beams B12 and B22 traveling toward the second optical path are reflected by the moving mirror 45 and returned to the beam splitter 42, and a part of the light beams B12 and B22 are reflected by the beam splitter 42 and travel to the detectors 5a and 5b together with B11 and B21. .

The movable mirror 45 is attached to the support member 46. The movable mirror 45 and the support member 46 are installed on a piezo fine movement stage 47 in which the position of the movable mirror 45 can be finely adjusted although the movement range is narrow. The movable mirror 45 and the support member 46 are installed on a coarse movement stage 48 that, together with the piezo fine movement stage 47, has a relatively large movement range and roughly determines the position of the movement mirror 45. The piezo fine movement stage 47 and the coarse movement stage 48 are electrically connected to the piezo controller 51 and the stage controller 52, respectively. Then, the piezo fine movement stage 47 and the coarse movement stage 48 move the movable mirror 45 along the second optical path based on control signals from the piezo controller 51 and the stage controller 52.
In the case where the interference signal is continuously measured during the movement while moving the movable mirror 45, the piezo fine movement stage 47 and the piezo controller 51 may be omitted.

  A corner cube 49 is attached to the back surface of the support member 46. Further, a position measurement interferometer 50 for the movable mirror 45 is installed behind the support member 46 (that is, on the opposite side of the beam splitter 42 with the support member 46 as the center). The position measurement interferometer 50 is irradiated to the corner cube 49, reflected by the corner cube 49, and returned to the position measurement interferometer 50, and the interference observed between the reference light and the reference light. The amount of movement of the movable mirror 45 can be measured by counting the number of moving stripes.

  The beam splitting mirror 53 has a triangular prism shape whose apex is directed to the beam splitter 42, and is disposed between the beam splitter 42 and the detectors 5a and 5b. The beam splitting mirror 53 has two reflecting surfaces 53a and 53b across the apex. The light splitting mirror 53 detects, on one reflection surface 53a, a part of the light beams B11 and B21 that has passed through the 1/8 wavelength plate 44 and a part of the light beams B12 and B22 as a detector 5a. Reflect towards The beam splitting mirror 53 detects the other part of the light beams B11 and B21 and the other part of the light beams B12 and B22 that did not pass through the ８ wavelength plate 44 on the other reflecting surface 53b. Reflects toward 5b.

The detectors 5a and 5b output the detected light amount as an electrical signal. As the detectors 5a and 5b, for example, a semiconductor detection element such as a photodiode, CCD, or C-MOS can be used. In this embodiment, the detectors 5a and 5b are CCD elements arranged in a two-dimensional array.
The detectors 5 a and 5 b are electrically connected to the controller 6, and transmit an electrical signal corresponding to the detected light amount to the controller 6. Then, the detector 5a detects white interference fringes generated between the light beams transmitted through the 1/8 wavelength plate 44 and the light beams B12 and B22 among the light beams B11 and B21. On the other hand, the detector 5b detects a white interference fringe generated between the light fluxes B11 and B22 and the light flux that has not passed through the 1/8 wavelength plate 44 among the partial light fluxes B11 and B21. Here, as described above, a part of the light beams B11 and B21 transmitted through the ８ wavelength plate 44 has a phase of 90 relative to the other part of the light beams B11 and B21 that do not transmit through the ８ wavelength plate 44. Deviate. Therefore, the white interference fringes detected by the detector 5a and the white interference fringes detected by the detector 5b are out of phase with each other by 90 degrees. Thus, the 1/8 wavelength plate 44 and the detector 5a function as a phase shift signal generation unit.

FIG. 5 shows a functional block diagram of the controller 6.
The controller 6 is configured by a so-called PC, and is in accordance with a storage unit 61 including an electrically rewritable nonvolatile memory, a magnetic disk, an optical disk, and a reading device thereof, and communication standards such as RS232C and Ethernet (registered trademark). The communication unit 62 includes software such as the configured electronic circuit and device driver.
Further, the controller 6 includes a white interference signal acquired by the detector 5a and the detector 5b as functional modules realized by a CPU, ROM, RAM and peripheral circuits (not shown) and a computer program executed on the CPU. , A signal synthesizer 63 for calculating the Lissajous waveform signal, a peak position determining unit 64 for determining the position of the movable mirror 45 corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringes, A dimension determining unit 65 for obtaining the inner diameter D of the object to be measured 10 from the peak position, each part of the controller 6, an interferometer for position measurement 50, a piezo controller 51, a stage controller 52, and detectors 5a and 5b are connected to the controller 6. And a control unit 66 for controlling the devices.

Hereinafter, an operation for measuring the inner diameter of the DUT 10 by the inner diameter measuring apparatus 1 will be described.
Since the light from the white light source 2 has a short coherence length, interference fringes are generated only when the optical path differences are substantially equal. Here, the distance from the beam splitter 42 to the reference mirror 43 in the first optical path of the second interferometer 4 is L1, and the distance from the beam splitter 42 to the movable mirror 45 in the second optical path is L2. If there is, an optical path difference of 2 (L2−L1) is generated between the third light flux and the fourth light flux (where L2> L1). At this time, if (L2−L1) and D are equal, the first interferometer 3 uses the first interferometer 4 out of the light beams B1 reflected by the inner surfaces S1 and S2 of the DUT 10. The optical path difference between the light beam B11 passing through the optical path and the light beam B2 passing through the beam splitter 33 in the first interferometer 3 and the light beam B22 passing through the second optical path in the second interferometer 4 is 0. It becomes. Therefore, the amplitude of the interference fringe is maximized. As the difference between (L2−L1) and D increases, the amplitude of the interference fringes rapidly decreases. Therefore, the inner diameter D of the DUT 10 can be obtained by measuring (L2-L1) when the amplitude of the interference fringes is maximized.

  Further, when the movable mirror 45 is brought closer to the beam splitter 42, the optical path difference 2 (L1-L2) generated between the third light beam and the fourth light beam is twice the inner diameter D of the DUT 10. Interference fringes can be observed even at equal points (however, L1> L2). In this case, among the light beams B1 reflected by the inner surfaces S1 and S2 of the object to be measured 10 in the first interferometer 3, the light beams B12 that have passed through the second optical path in the second interferometer 4 and the first This is because, in the second interferometer 4, the optical path difference between the light beam B 2 that has passed through the beam splitter 33 in the interferometer 3 and the light beam B 21 that has passed through the first optical path becomes zero. Therefore, the position of the movable mirror 45 where the amplitude of the interference fringe generated between the light beams B11 and B22 is maximized, and the position of the movable mirror 45 where the amplitude of the interference fringe generated between the light beams B12 and B21 is maximized. The inner diameter D of the object to be measured 10 can be obtained by dividing the difference by 2 by 2.

移動鏡４５を移動しつつ検出器５ａ、５ｂで干渉信号を検出する際、各検出器の信号取得周期と白色干渉縞の周期または位相のずれにより、白色干渉縞の強度が最大であるときの干渉信号を取得できない場合がある。特に、移動鏡４５を高速に移動させるほど、白色干渉縞に対する各信号取得点間の間隔が大きくなるので、白色干渉縞の強度が最大であるときの干渉信号を取得できない可能性が高くなる。しかし、リサージュ波形信号I_lis(x)は、そのような周期または位相のずれとは無関係に、移動鏡４５の各位置における白色干渉縞の振幅に相当する値をとる。そのため、リサージュ波形信号I_lis(x)の最大値は、正確に白色干渉縞の最大値と一致する。 Hereinafter, the procedure for obtaining the position of the movable mirror 45 when the amplitude of the white interference fringe is maximized will be described with reference to the flowchart shown in FIG.
First, the signal synthesizer 63 of the controller 6 detects the interference signal I obtained from the detector 5a in order to accurately detect the position of the movable mirror 45 where the amplitude of the white interference fringe is maximum, that is, the peak position of the white interference fringe. _A Lissajous waveform signal I _lis (x) is obtained based on _a (x) and the interference signal I _b (x) obtained from the detector 5b (step S101). In each of the signals I _a (x), I _b (x), and I _lis (x), x is a variable that represents the position of the moving mirror 45. The two interference signals I _a (x) and I _b (x) are 90 degrees out of phase with each other, but are the same in terms of period and amplitude. Therefore, the signal synthesis unit 63 can obtain the Lissajous waveform signal I _lis (x) by the following equation.

When the interference signal is detected by the detectors 5a and 5b while moving the movable mirror 45, when the intensity of the white interference fringes is maximum due to a shift in the signal acquisition period of each detector and the period or phase of the white interference fringes. Interference signal may not be acquired. In particular, as the moving mirror 45 is moved at a higher speed, the interval between the signal acquisition points with respect to the white interference fringe becomes larger, so that there is a higher possibility that the interference signal cannot be obtained when the intensity of the white interference fringe is maximum. However, the Lissajous waveform signal I _lis (x) takes a value corresponding to the amplitude of the white interference fringes at each position of the movable mirror 45 regardless of such a period or phase shift. Therefore, the maximum value of the Lissajous waveform signal I _lis (x) exactly matches the maximum value of the white interference fringes.

Next, the peak position determination unit 64 of the controller 6 obtains the maximum value of the Lissajous waveform signal obtained by the signal synthesis unit 63 (step S102). The Lissajous waveform signal I _lis (x) is a discrete signal having the same sampling interval as long as the white interference signal acquired by each detector is discrete. Therefore, the peak position determination unit 64 may perform an interpolation operation such as spline interpolation on the Lissajous waveform signal to obtain a maximum signal value for the interpolated waveform signal. Then, the peak position determination unit 64 acquires the position of the movable mirror 45 when the Lissajous waveform signal reaches the maximum value from the position measurement interferometer 50 (step S103). The peak position determination unit 64 sets the acquired position of the movable mirror 45 as the peak position of the white interference fringes.

In FIG. 7, the operation | movement flowchart of the internal diameter measuring apparatus 1 at the time of measuring the internal diameter D of the to-be-measured object 10 is shown.
When the measurement is started, first, as an initialization procedure, the reference position of the movable mirror 45, that is, the movable mirror 45 in which the optical path difference between the first optical path and the second optical path of the second interferometer 4 becomes zero. Is determined (step S201). Therefore, the position where the object to be measured 10 is not installed in the first interferometer 3 of the inner diameter measuring device 1 and the interference fringe is detected by the second interferometer 4 is obtained. At this time, since there is no light beam reflected by the inner surface of the DUT 10, all the light beams emitted from the first interferometer 3 are B2. Therefore, in the second interferometer 4, the difference between the distance L1 from the beam splitter 42 to the reference mirror 43 in the first optical path and the distance L2 from the beam splitter 42 to the movable mirror 45 in the second optical path is zero. Sometimes the amplitude of the observed interference fringes is maximized. Therefore, the controller 66 of the controller 6 drives the piezo fine movement stage 47 through the piezo controller 51 to move the movable mirror 45. At this time, the controller 6 acquires interference signals corresponding to the white interference fringes from the detectors 5a and 5b. Then, a Lissajous waveform signal is generated according to the above procedure. Controller 6, the position of the moving mirror 45 when the Lissajous waveform signal becomes maximum value, received from the position measurement interferometer 50, as a position X ₀ of the L1 = L2, stored in the storage unit 61 of the controller 6 To do. The reference position may be measured once and the procedure of step S201 may be omitted at the second and subsequent measurements.

  Next, the DUT 10 is installed on the first interferometer 3 of the inner diameter measuring device 1. At this time, as described above, the white interference fringes are observed at a position where the inner diameter D of the DUT 10 and (L2−L1) are substantially equal. Therefore, the control unit 66 of the controller 6 drives the coarse movement stage 48 through the stage controller 52 to retract the moving mirror 45 of the second interferometer 4 by a distance substantially equal to the inner diameter D of the DUT 10. Thereafter, the controller 66 of the controller 6 drives the piezo fine movement stage 47 through the piezo controller 51 to move the movable mirror 45 in the same manner as described above. Further, the controller 6 acquires interference signals corresponding to the white interference fringes from the detectors 5a and 5b (step S202).

When acquiring the respective interference signal values, the controller 6, in accordance with the procedure shown in FIG. 6, determine the position X _p of the moving mirror 45 corresponding to the peak position of the white light interference fringes (step S203).
If the position X _p of the moving mirror 45 that corresponds to a peak position of the white light interference fringe is obtained, the dimension determining unit 65 of the controller 6 reads the position X ₀ of the moving mirror 45 in the case of the storage unit 61 L1 = L2 X The value of _p− X ₀ is calculated, and the measured value of the inner diameter D of the device under test 10 is obtained (step S204).

  Further, in the first interferometer 3, when the position of the beam splitter 33 does not exactly coincide with the center of the inner diameter of the device under test 10, the light beam B 1 is shifted from the diameter of the inner diameter of the device under test 10. The measured value is not accurate. In order to solve the problem, the measurement of the inner diameter is repeated by shifting the positional relationship between the beam splitter 33 and the DUT 10 in the direction perpendicular to the light beam B1 within the cylindrical cross section orthogonal to the axial direction of the DUT 10. Then, the value at which the obtained measurement value is maximum is taken as the inner diameter of the DUT 10.

  Therefore, once the controller 6 obtains the measured value of the inner diameter by the above procedure, it stores it in the storage unit 61. Next, the controller 6 transmits a control signal to the stage controller 37 of the first interferometer 3 to drive the XYZ stage 36, and the measured object 10 is changed to the light beam B1 by a predetermined amount (for example, 0.1 μm). It is moved in a direction perpendicular to the direction. Then, the inner diameter is measured again to obtain a measured value. The obtained measurement value is compared with the measurement value stored in the storage unit 61 of the controller 6. If the newly obtained measurement value is larger than the stored measurement value, the measurement value stored in the storage unit 61 is updated with the newly obtained measurement value. Thereafter, the DUT 10 is moved again in the same direction, and the measurement of the inner diameter is repeated. And when the measured value memorize | stored in the memory | storage part 61 becomes more than the newly measured value, let the measured value memorize | stored in the memory | storage part 61 be the internal diameter D of the to-be-measured object 10. FIG.

On the other hand, when the measured value of the inner diameter measured first is equal to or larger than the measured value measured next, the controller 6 moves the DUT 10 in the direction opposite to the direction in which the measured object 10 is first moved. Then, the measurement is repeated in the same manner as described above, and when the measured value stored in the storage unit 61 becomes equal to or greater than the newly measured value, the measured value stored in the storage unit 61 is used as the measured object 10. The inner diameter D of
In this way, by searching for the maximum measured value of the inner diameter D while changing the positional relationship between the object to be measured 10 and the beam splitter 33, the inner diameter measuring apparatus 1 accurately sets the beam splitter 33 to the center of the object to be measured 10. Since the inner diameter measurement result in the state of being placed in the position can be obtained, the inner diameter of the DUT 10 can be measured with high accuracy.

Instead of measuring the reference position X ₀ of the moving mirror 45 at step S201, as close to the beam splitter 42 than the reference mirror 43 to move mirror 45, the peak of the white light interference fringes generated between the light beam B12 and the light beam B21 The position X _p ′ of the movable mirror 45 serving as the position may be obtained according to the procedure shown in FIG. Then, a value of (X _p −X _p ′) / 2 is calculated, and the value may be used as the inner diameter D of the DUT 10. The intensity of the interference signal observed at the reference position X ₀ and the intensity of the interference signal observed at the position X _p are greatly different due to the difference in the light amount between the light beam B1 and the light beam B2. On the other hand, the interference signal observed at the position X _p and the interference signal observed at the position X _p ′ have substantially the same intensity. Therefore, when the measured value of the inner diameter of the DUT 10 is obtained based on the difference between the position X _p and the position X _p ′, the measured inner diameter value is obtained based on the difference between the reference position X ₀ and the position X _p. Since the change in the output signal with respect to the change in the amount of light received by the detectors 5a and 5b can be increased, the position of the movable mirror 45 where the amplitude of the white interference fringe is maximum can be specified more accurately.

  As described above, the inner diameter measuring apparatus 1 according to the first embodiment of the present invention acquires two interference signals whose phases are shifted by 90 degrees with respect to each other, and obtains a Lissajous waveform signal of the two interference signals. The inner diameter of the DUT 10 is measured based on the position of the movable mirror 45 corresponding to the maximum signal value of the Lissajous waveform signal. Therefore, the position of the movable mirror 45 that is the peak position of the white interference fringes can be accurately obtained regardless of the sampling position of the white interference fringes, so that the inner diameter of the object to be measured can be accurately measured. Further, the inner diameter measuring apparatus 1 can calculate the Lissajous waveform signal without changing the above-described configuration even if the moving speed of the movable mirror 45 at the time of acquiring the interference signal (that is, the interference signal acquisition cycle) is changed. By increasing the moving speed of the movable mirror 45, the time required for measuring the inner diameter of the DUT 10 can be shortened.

Next, an inner diameter measuring device 1 ′ according to the second embodiment of the present invention will be described. In the inner diameter measuring device 1 ′ according to the second embodiment of the present invention, instead of generating two interference signals whose phases are optically shifted by 90 degrees from each other, two such interference signals are electrically generated. Generate. In the following, only differences from the first embodiment will be described.
FIG. 8 shows a schematic configuration diagram of the second interferometer 4 of the inner diameter measuring device 1 ′ according to the second embodiment of the present invention. 8 having the same reference numbers as those shown in FIG. 4 have the same functions as those having the same reference numbers in FIG. Further, other configurations (such as the white light source 2 and the first interferometer 3) of the inner diameter measuring device 1 ′ not shown in FIG. 8 have the same configuration as the inner diameter measuring device 1 according to the first embodiment. Since it has this and performs the same function, description is abbreviate | omitted below.

  As shown in FIG. 8, the inner diameter measuring device 1 ′ uses one detector 5 to detect white interference fringes. The inner diameter measuring device 1 ′ further includes a high frequency oscillator 54, a phase detector 55, and a modulator 56. Further, in the inner diameter measuring device 1 ′, the 1/8 wavelength plate and the beam splitting mirror are omitted.

The high frequency oscillator 54 outputs a high frequency oscillation signal toward the modulator 56 attached to the reference mirror 43 in accordance with a control signal from the controller 6. Then, the modulator 56 moves the reference mirror 43 back and forth at the transmission frequency of the high-frequency oscillation signal during measurement of white interference fringes. At this time, the transmission frequency of the high-frequency oscillation signal is set so that the white interference fringe observed by the detector 5 is high-frequency modulated at a frequency higher than the formation frequency of the interference fringe. For example, the oscillation frequency is set so that the reference mirror 43 reciprocates around several times to several tens of times while the moving mirror 45 moves a distance corresponding to half the center wavelength λ of the white light source 2. The moving range of the reference mirror 43 is set to about λ / 4 to λ / 20. The modulator 56 is composed of, for example, a piezo element.
The phase detector 55 has two input terminals. One input terminal receives an interference signal corresponding to the white interference fringe modulated from the detector 5 and subjected to high frequency modulation. A high frequency oscillation signal output from the high frequency oscillator 54 is input to the other input terminal as a reference signal. At this time, the phase detector 55 extracts only the signal component having the same frequency as the reference signal by comparing the phase of the interference signal and the phase of the reference signal, and outputs the sine wave and the cosine wave. Therefore, the controller 6 receives the two output signals from the phase detector 55 and averages the squares to obtain a Lissajous waveform signal corresponding to the white interference fringes.

  In addition, this invention is not limited to said embodiment. For example, the 1/8 wavelength plate 44 may be disposed between the beam splitter 42 and the movable mirror 45 instead of being disposed between the beam splitter 42 and the reference mirror 43. In addition, when the light emitted from the white light source 2 is linearly polarized light, or before the first light beam and the second light beam are incident on the second interferometer 4, a linear polarizer is disposed, When the first and second light beams incident on the second interferometer 4 are linearly polarized light, a polarization beam splitter can be used instead of the light beam splitting mirror. Furthermore, the device under test is not limited to a cylindrical one. The measuring apparatus of the above embodiment can be applied as it is when measuring the distance between two opposing surfaces of an object to be measured. In the measurement apparatus of the above embodiment, the second interferometer may be a Fizeau interferometer. When using a Fizeau interferometer, place a 1/8 wavelength plate on the optical path through which only one of the light beams split by the second interferometer passes so that only a part of the light beam is transmitted. That's fine.

Furthermore, the present invention can be applied to a configuration in which only one Michelson interferometer is used.
FIG. 9 shows a schematic configuration diagram of a configuration of the dimension measuring apparatus 11 that uses only one Michelson interferometer. In this configuration, the measurement light emitted from the white light source 12 is converted into a first light beam directed to the object to be measured 10 ′ by the beam splitter 13 and a second light beam directed to the movable mirror 15 movable along the optical path. To divide. In addition, a ８ wavelength plate 14 is disposed between the beam splitter 13 and the DUT 10 ′. Then, a part of the first light flux is 1/2 twice when going from the beam splitter 13 to the object to be measured 10 ′ and when reflected from the object to be measured 10 ′ and conversely going to the beam splitter 13. The light passes through the 8-wavelength plate 14. The other part of the first light flux does not pass through the 1/8 wavelength plate 14. As in FIG. 4, FIG. 9 also shows a light beam that passes through the 1/8 wavelength plate 14 and a light beam that does not transmit through the 1/8 wavelength plate 14 for ease of understanding. Therefore, the first light flux includes two light fluxes that are 90 degrees out of phase with each other. This first light beam and the second light beam reflected by the movable mirror 15 are again made into one light beam by the beam splitter 13. Then, the light beam emitted from the beam splitter 13 is transmitted by the beam splitting mirror 16 to a part of the light beam and the second light beam transmitted through the 1/8 wavelength plate 14 out of the first light beam and the first light beam. The light beam that has not passed through the 1/8 wavelength plate 14 and the other part of the second light beam are branched. The respective light beams are detected by the detectors 17a and 17b, and interference signals whose phases are shifted by 90 degrees are detected. Signals output from the detectors 17a and 17b are transmitted to the controller 18, respectively. The controller 18 has the same configuration as the controller 6 in the above embodiment. And controller 18 calculates | requires a Lissajous waveform signal from each interference signal as demonstrated about said 1st Embodiment. The controller 18 estimates at the position X _p of the moving mirror 15 that corresponds to the maximum value of the Lissajous waveform signal, the optical path difference between the first beam and the second light flux is zero. Finally, by calculating the difference between the reference position X ₀ of the movable mirror 15 predetermined in relation to the measured object 10 ′ and the obtained position X _p of the movable mirror 14, the measured object 10 ′ is measured. Determine the dimensions (eg surface height, etc.).

Furthermore, in the embodiment using two interferometers, the white light source arranged on the first interferometer 3 side and the detector arranged on the second interferometer 4 side may be interchanged. . In this case, two light beams having an optical path difference corresponding to the measurement target dimension of the object to be measured are generated in advance on the second interferometer 4 side, and these light beams are sent to the first interferometer 3 side through the optical fiber. In the first interferometer 3, the received two light beams are further divided into a light beam reflected by the inner surfaces S 1 and S 2 of the object to be measured 10 and two light beams traveling straight through the beam splitter 33, and one of them. The white interference fringes are observed by detecting with a detector. Also in this case, the measured value of the inner diameter D of the DUT 10 can be obtained by measuring the optical path difference generated on the second interferometer 4 side. At that time, by connecting a lock-in amplifier to the detector, two interference signals whose phases are shifted from each other by 90 degrees can be acquired. Alternatively, a 1/8 wavelength plate is arranged on the optical path from the beam splitter 33 to the DUT 10 so that only a part of the light beam is transmitted, and the light beam transmitted through the 1/8 wavelength plate and the beam splitter 33 are arranged. The white interference fringes generated between the light beam traveling straight and the white interference fringes generated between the light beam not transmitted through the 1/8 wavelength plate and the light beam traveling straight through the beam splitter 33 are respectively provided by different detectors. It is also possible to acquire two interference signals that are 90 degrees out of phase with respect to each other. And a Lissajous waveform signal can be calculated | required similarly to said embodiment, and the internal diameter D can be measured based on the maximum signal value.
As described above, various modifications can be made within the scope of the present invention according to the embodiment to be implemented.

It is a figure which shows the outline of a white interference fringe and its envelope. It is a schematic block diagram of the internal diameter measuring apparatus which concerns on the 1st Embodiment of this invention. It is a schematic block diagram of the 1st interferometer which comprises an internal diameter measuring apparatus. It is a schematic block diagram of the 2nd interferometer which comprises an internal diameter measuring apparatus. It is a functional block diagram of the controller of an internal diameter measuring device. It is the flowchart which showed the procedure which calculates | requires the position of the movable mirror corresponding to the maximum amplitude of a white interference fringe. It is an operation | movement flowchart of an internal diameter measuring apparatus. It is a schematic block diagram of the dimension measuring apparatus by 2nd Embodiment to which this invention is applied. It is a schematic block diagram of the dimension measuring apparatus by 3rd Embodiment to which this invention is applied.

Explanation of symbols

1, 1 'inner diameter measuring device (dimension measuring device)
DESCRIPTION OF SYMBOLS 11 Dimension measurement apparatus 10, 10 'Measured object 2, 12 White light source 3, 4 Interferometer 5, 5a, 5b, 17a, 17b Detector 6, 18 Controller 31, 41 Collimator lens 32, 34 Wedge prism 33, 42, 13 Beam splitter 35 Condensing lens 36 XYZ stage 37 Stage controller 43 Reference mirror 44, 14 1/8 wavelength plate 45, 15 Moving mirror 46 Support member 47 Piezo fine movement stage 48 Coarse movement stage 49 Corner cube 50 Position measurement interferometer 51 Piezo controller 52 Stage controller 53, 16 Beam splitting mirror 54 High frequency oscillator 55 Phase detector 56 Modulator 61 Storage unit 62 Communication unit 63 Signal synthesis unit 64 Peak position determination unit 65 Size determination unit 66 Control unit 7, 8 Optical fiber

Claims (10)

A dimension measuring device for measuring a dimension of an object to be measured,
A white light source,
The light emitted from the white light source is branched into a first light beam and a second light beam that are directed toward the object to be measured, and the first light beam is reflected by the object to be measured, and the second light beam A first interferometer that causes a first optical path difference corresponding to a measurement target dimension of the object to be measured to emit the first light flux and the second light flux in accordance with one light flux;
A reference mirror having a fixed position, a movable mirror movable along the optical path, a light beam emitted from the first interferometer, a third light beam directed toward the reference mirror, and a fourth beam directed toward the movable mirror A second interferometer that includes a light beam splitting unit that branches the light beam, and that generates a second optical path difference between the third light beam and the fourth light beam;
A white interference fringe generated when the third light flux and the fourth light flux are received and the first optical path difference and the second optical path difference are substantially equal is detected, and a first interference fringe corresponding to the white interference fringe is detected. A detector that outputs one interference signal;
A phase shift signal generating unit that generates a second interference signal that is 90 degrees out of phase with the first interference signal;
A controller for obtaining a measurement target dimension of the object to be measured,
A signal synthesizer that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal;
A peak position determination unit that determines the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringes;
By calculating the second optical path difference with respect to the peak position to obtain the measurement target dimension;
A controller having
A dimension measuring apparatus comprising:   The phase shift signal generation unit is disposed between the reference mirror and the light beam splitting unit, transmits a part of the third light beam, and delays the phase of a part of the light beam by 90 degrees, A second detector for detecting, as the second interference signal, an interference signal corresponding to a white interference fringe generated between a part of the third light beam whose phase is delayed by 90 degrees and the fourth light beam; The dimension measuring device according to claim 1, comprising:   The phase shift signal generation unit is disposed between the movable mirror and the light beam splitting unit, transmits a part of the fourth light beam, and delays the phase of a part of the light beam by 90 degrees, A second detector for detecting, as the second interference signal, an interference signal corresponding to a white interference fringe generated between a part of the fourth light beam whose phase is delayed by 90 degrees and the third light beam; The dimension measuring device according to claim 1, comprising: A dimension measuring device for measuring a dimension of an object to be measured,
A white light source,
A movable mirror movable along the optical path; and a light beam splitting unit that splits the light emitted from the white light source into a first light beam directed to the object to be measured and a second light beam directed to the movable mirror. An interferometer that reflects the first light beam by the object to be measured to generate an optical path difference between the first light beam and the second light beam;
White interference fringes generated when the first light flux and the second light flux emitted from the interferometer are received, and the optical path length for the first light flux and the optical path length for the second light flux are substantially equal. And detecting a first interference signal corresponding to the white interference fringes,
A phase shift signal generating unit that generates a second interference signal that is 90 degrees out of phase with the first interference signal;
A controller for obtaining a measurement target dimension of the object to be measured,
A signal synthesizer that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal;
A peak position determination unit that determines the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringes;
A dimension determining unit for obtaining the measurement target dimension by calculating a difference between the position of the movable mirror with respect to the peak position and a predetermined reference position of the movable mirror;
A controller having
A dimension measuring apparatus comprising:   The phase shift signal generation unit is disposed between the device under test and the light beam splitting unit, transmits a part of the first light beam, and delays the phase of a part of the first light beam by 90 degrees. A second interference signal corresponding to a white interference fringe generated between the wave plate and a part of the first light beam whose phase is delayed by 90 degrees and the second light beam is detected as the second interference signal. The dimension measuring apparatus according to claim 4, further comprising:   The phase shift signal generation unit is disposed between the movable mirror and the light beam splitting unit, transmits a part of the second light beam, and delays the phase of a part of the second light beam by 90 degrees. A second interference signal corresponding to a white interference fringe generated between the plate and a part of the second light beam whose phase is delayed by 90 degrees and the first light beam is detected as the second interference signal. The dimension measuring apparatus according to claim 4, further comprising a detector. A dimension measuring device for measuring a dimension of an object to be measured,
A white light source,
A reference mirror having a fixed position, a movable mirror movable along an optical path, a first light beam directed toward the reference mirror, and a second light beam directed toward the movable mirror. And a first interferometer that generates a first optical path difference between the first light flux and the second light flux;
The first light beam and the second light beam emitted from the first interferometer are branched into a third light beam and a fourth light beam that are directed toward the object to be measured, and the third light beam is divided into the measured light. A second optical path difference corresponding to the measurement object size of the object to be measured is generated between the fourth light flux and the fourth light flux, and the third light flux and the fourth light flux are combined into one light flux. A second interferometer that emits together,
A white interference fringe generated when the third light flux and the fourth light flux are received and the first optical path difference and the second optical path difference are substantially equal is detected, and a first interference fringe corresponding to the white interference fringe is detected. A detector that outputs one interference signal;
A phase shift signal generating unit that generates a second interference signal that is 90 degrees out of phase with the first interference signal;
A controller for obtaining a measurement target dimension of the object to be measured,
A signal synthesizer that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal;
A peak position determination unit that determines the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringes;
By calculating the first optical path difference with respect to the peak position, thereby determining the measurement target dimension; and
A controller having
A dimension measuring apparatus comprising: A dimension measuring device for measuring a dimension of an object to be measured,
A white light source,
The light emitted from the white light source is branched into a first light beam and a second light beam that are directed toward the object to be measured, and the first light beam is reflected by the object to be measured, and the second light beam A first interferometer that causes a first optical path difference corresponding to a measurement target dimension of the object to be measured to emit the first light flux and the second light flux in accordance with one light flux;
A reference mirror, a movable mirror movable along the optical path, and a light beam that splits the light beam emitted from the first interferometer into a third light beam directed toward the reference mirror and a fourth light beam directed toward the movable mirror A second interferometer that includes a splitting unit and that generates a second optical path difference between the third light flux and the fourth light flux;
A modulator attached to the reference mirror for vibrating the reference mirror back and forth along the third light flux;
A high-frequency oscillator that is connected to the modulator, inputs an oscillation signal having a predetermined oscillation frequency to the modulator, and vibrates the modulator at the predetermined oscillation frequency;
The third light flux and the fourth light flux are received, a white interference fringe generated when the first optical path difference and the second optical path difference are substantially equal is detected, and the white interference fringe is A detector that outputs a high-frequency modulated interference signal that is high-frequency modulated at an oscillation frequency;
The white interference fringes are connected to the detector and the high-frequency oscillator by comparing the phase of the high-frequency modulation interference signal input from the detector with the phase of the oscillation signal input from the high-frequency oscillator. Corresponding phase detectors for outputting first and second interference signals that are 90 degrees out of phase with each other;
A controller for obtaining a measurement target dimension of the object to be measured,
A signal synthesizer that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal;
A peak position determination unit that determines the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringes;
By calculating the second optical path difference with respect to the peak position to obtain the measurement target dimension;
A controller having
A dimension measuring apparatus comprising: A dimension measuring device for measuring a dimension of an object to be measured,
A white light source,
A reference mirror, a movable mirror movable along an optical path, and a light beam splitting light emitted from the white light source into a first light beam traveling toward the reference mirror and a second light beam traveling toward the movable mirror A first interferometer that generates a first optical path difference between the first light flux and the second light flux;
The first light beam and the second light beam emitted from the first interferometer are branched into a third light beam and a fourth light beam that are directed toward the object to be measured, and the third light beam is divided into the measured light. A second optical path difference corresponding to the measurement object size of the object to be measured is generated between the fourth light flux and the fourth light flux, and the third light flux and the fourth light flux are combined into one light flux. A second interferometer that emits together,
A modulator attached to the reference mirror for vibrating the reference mirror back and forth along the first light flux;
A high-frequency oscillator that is connected to the modulator, inputs an oscillation signal having a predetermined oscillation frequency to the modulator, and vibrates the modulator at the predetermined oscillation frequency;
The third light flux and the fourth light flux are received, a white interference fringe generated when the first optical path difference and the second optical path difference are substantially equal is detected, and the white interference fringe is A detector that outputs a high-frequency modulated interference signal that is high-frequency modulated at an oscillation frequency;
The white interference fringes are connected to the detector and the high-frequency oscillator by comparing the phase of the high-frequency modulation interference signal input from the detector with the phase of the oscillation signal input from the high-frequency oscillator. Corresponding phase detectors for outputting first and second interference signals that are 90 degrees out of phase with each other;
A controller for obtaining a measurement target dimension of the object to be measured,
A signal synthesizer that calculates a Lissajous waveform signal based on the first interference signal and the second interference signal;
A peak position determination unit that determines the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as the peak position of the white interference fringes;
By calculating the second optical path difference with respect to the peak position to obtain the measurement target dimension;
A controller having
A dimension measuring apparatus comprising: The light emitted from the white light source is branched into a first light beam and a second light beam that are directed to the object to be measured, and the first light beam is reflected by the object to be measured and is between the second light beam and the second light beam. A first interferometer that generates a first optical path difference corresponding to a measurement target dimension of the object to be measured and emits the first light flux and the second light flux according to one light flux; A reference mirror having a fixed position; a movable mirror movable along the optical path; a light beam emitted from the first interferometer; a third light beam directed toward the reference mirror; A second beam interferometer that includes a beam splitting unit that branches into a fourth beam directed to the mirror, and that generates a second optical path difference between the third beam and the fourth beam, 3 and the fourth light beam are detected, white interference fringes generated when the first optical path difference and the second optical path difference are substantially equal are detected, and the white interference is detected. A dimension measuring method of an object to be measured in the measurement system having a detector which outputs a first interference signal which corresponds to,
Generating a second interference signal that is 90 degrees out of phase with the first interference signal;
Calculating a Lissajous waveform signal based on the first interference signal and the second interference signal;
Determining the position of the movable mirror corresponding to the maximum value of the Lissajous waveform signal as a peak position of the white interference fringes;
Calculating the measurement target dimension by calculating the second optical path difference with respect to the peak position;
A dimension measuring method characterized by comprising:

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