# Patent

## Title
Wide dynamic range interferometric transducer with divergent beam

## Abstract

An apparatus and method for estimating a parameter of interest using values of a beam property from two or more electromagnetic beams that both pass through at least part of an optical displacement device. The apparatus may include a Fabry-Perot interferometer, a collimated light source, and a detection array. At least one mirror of the interferometer may be operably coupled to an element receiving an external stimulus, such as pressure, force, and/or acceleration. The method includes using the apparatus.

## Background
CROSS-REFERENCE TO RELATED APPLICATION
This application claims priority from U.S. Provisional Patent Application Ser. No. 61/444,419, filed on 18 Feb. 2011, the disclosure of which is incorporated herein by reference in its entirety.
BACKGROUND OF THE DISCLOSURE
1. Field of the Disclosure
In one aspect, this disclosure generally relates methods and apparatuses for sensing displacement optically.
2. Background of the Art
Displacement sensors, such as microphones and pressure sensors, are well-known. Many displacement sensors may be based on one or more of electrical capacitance, electrical impedance, or magnetic fields. These electrical and magnetic based displacement sensors may be limited due to one or more of: low sensitivity, the need for high-voltage biasing, poor electrical isolation, environmental factors, and response nonlinearities. These limitations may require a close coupling between transducer design and the sensor mechanical design, which may limit performance and the operational size of the displacement sensor. Optical displacement sensors may be electrically and magnetically insensitive, which may mitigate limitations found in electrical and magnetic based displacement sensors. The present disclosure uses optical displacement to address the need to minimize the impact of these limitations on the performance or structure of devices.
SUMMARY OF THE DISCLOSURE
In aspects, the present disclosure is related to an apparatus and method for estimating a parameter of interest using values of a beam property from two or more electromagnetic beams that both pass through at least part of an optical displacement device.
One embodiment according to the present disclosure includes an apparatus for estimating a parameter of interest, comprising: an optical displacement device configured to receive a first electromagnetic beam with a first value of a beam property and a second electromagnetic beam with a second value of the beam property; and a detector array configured to receive a part of the first electromagnetic beam and a part of the second electromagnetic beam that both pass through at least part of the optical displacement device.
Another embodiment according to the present disclosure includes a method for estimating a parameter of interest, comprising: estimating the parameter of interest using a detector array configured to receive a part of the first electromagnetic beam with a first value of a beam property and a part of the second electromagnetic beam with a second value of the beam property that both pass through at least part of an optical displacement device.
Examples of the more important features of the disclosure have been summarized rather broadly in order that the detailed description thereof that follows may be better understood and in order that the contributions they represent to the art may be appreciated. There are, of course, additional features of the disclosure that will be described hereinafter and which will form the subject of the claims appended hereto.



BRIEF DESCRIPTION OF THE DRAWINGS
For a detailed understanding of the present disclosure, reference should be made to the following detailed description of the embodiments, taken in conjunction with the accompanying drawings, in which like elements have been given like numerals, wherein:
FIG. 1 shows an optical displacement device deployed along a wireline according to one embodiment of the present disclosure;
FIG. 2 shows a graph of reflected and transmitted light in a Fabry-Perot interferometer according to the present disclosure;
FIG. 3 shows a graph of optical responses to a range of incident angles of light in the Fabry-Perot interferometer according to the present disclosure;
FIG. 4 shows a schematic of an optical displacement apparatus according to one embodiment of the present disclosure;
FIG. 5 shows a schematic of the divergent light beams produced in another optical displacement apparatus according to one embodiment of the present disclosure;
FIG. 6 shows a schematic of the interferometer and detection array of an optical displacement apparatus according to one embodiment of the present disclosure;
FIG. 7 shows a schematic of another optical displacement apparatus according to one embodiment of the present disclosure;
FIG. 8 shows a schematic of another optical displacement apparatus according to one embodiment of the present disclosure; and
FIG. 9 shows a flow chart of a method of using an optical displacement apparatus according to one embodiment of the present disclosure.



DETAILED DESCRIPTION OF THE DISCLOSURE
The present disclosure relates to devices and methods for estimating a parameter of interest using values of a beam property from two or more electromagnetic beams that both pass through at least part of an optical displacement device. The present disclosure is susceptible to embodiments of different forms. There are shown in the drawings, and herein will be described in detail, specific embodiments of the present disclosure with the understanding that the present disclosure is to be considered an exemplification of the principles of the present disclosure and is not intended to limit the present disclosure to that illustrated and described herein.
FIG. 1 shows one embodiment according to the present disclosure wherein a cross-section of a subterranean formation 10 in which is drilled a borehole 12 is schematically represented. Suspended within the borehole 12 at the bottom end of a carrier such as a wireline 14 is a device or tool 100. The term “carrier” as used herein means any device, device component, combination of devices, media and/or member that may be used to convey, house, support, or otherwise facilitate the use of another device, device component, combination of devices, media and/or member. Exemplary non-limiting carriers include drill strings of the coiled tube type, of the jointed pipe type, and any combination or portion thereof. Other carrier examples include casing pipes, wirelines, wireline sondes, slickline sondes, drop shots, downhole subs, bottom hole assemblies, drill string inserts, modules, internal housings, and substrate portions thereof. The tool 100 may include an information processing device. Information processing device as used herein means any device that transmits, receives, manipulates, converts, calculates, modulates, transposes, carries, stores, or otherwise utilizes information. In several non-limiting aspects of the disclosure, an information processing device includes a computer that executes programmed instructions for performing various methods. Herein, the term “information” may include one or more of: raw data, processed data, and signals. The wireline 14 may be carried over a pulley 18 supported by a derrick 20. Wireline deployment and retrieval is performed by a powered winch carried by a service truck 22, for example. A control panel 24 interconnected to the tool 100 through the wireline 14 by conventional means controls transmission of electrical power, data/command signals, and also provides control over operation of the components in the device 100. Use of a non-rigid carrier to convey tool 100 is exemplary only. Tool 100 may also be conveyed by a rigid carrier. In some embodiments, the borehole 12 may be utilized to recover hydrocarbons. In other embodiments, the borehole 12 may be used for geothermal applications, water production, mining, tunnel construction, or other uses.
In embodiments, the device 100 may be configured to collect information regarding force or acceleration. The device may also be configured to: (i) actively or passively collect information about the various characteristics of the formation, (ii) provide information about tool orientation and direction of movement, (iii) provide information about the characteristics of the reservoir fluid and/or (iv) evaluate reservoir conditions (e.g., formation pressure, wellbore pressure, temperature, etc.). Exemplary devices may include resistivity sensors (for determining the formation resistivity, dielectric constant and the presence or absence of hydrocarbons), acoustic sensors (for determining the acoustic porosity of the formation and the bed boundary in the formation), nuclear sensors (for determining the formation density, nuclear porosity and certain rock characteristics), nuclear magnetic resonance sensors (for determining the porosity and other petrophysical characteristics of the formation), and gravimeters/gravity gradiometers (for estimating formation density). Other exemplary devices may include gyroscopes, magnetometers, accelerometers, and sensors that collect formation fluid samples and determine the properties of the formation fluid, which include physical properties and chemical properties.
Device 100 may be conveyed to a position in operable communication or proximity with a parameter of interest. In some embodiments, device 100 maybe conveyed into a borehole 12. The parameter of interest may include, but is not limited to, one of: (i) pressure, (ii) force, and (iii) acceleration. Depending on the operating principle of the device 100, the device 100 may be configured to operate under surface and borehole conditions. The ambient temperature in the borehole may exceed 120 degrees Celsius (248 degrees Fahrenheit). In other embodiments, a device 100 may be used at the surface 160.
Device 100 may include an optical displacement sensor. Optical-displacement sensors operate by detecting light reflected by an optical element that changes its reflectivity in response to an environmental stimulus, such as pressure differential, sound, vibration, etc. The detected light may be converted into an electrical signal. This signal may be a function of the reflectivity of the optical element, and, therefore, a function of the stimulus as well. Optical displacement sensor may include an optical interferometer.
Optical interferometers have been proven to have outstanding resolution when used as displacement detectors in physical sensing components, such as microphones, pressure sensors, and accelerometers. One exemplary optical interferometer is the Fabry-Perot interferometer, which is also known as an etalon. An etalon may include an optically resonant cavity that distributes optical energy of an input light signal into a reflected signal and a transmitted signal. The ratio of optical energy in the reflected and transmitted signals may depend on the cavity length of the optically resonant cavity, which is the spacing between its two, substantially-parallel, partially reflective surfaces and its operating wavelength, x, (i.e., the wavelength, x, of the light on which the interferometer operates).
In an etalon, light can be strongly modulated by very small changes in the cavity length, and these changes can be detected using standard optical detection approaches that result in a wide dynamic range. The use of light beam for the readout is very different from the more standard approaches that use charged particles, including electrostatic, capacitive, piezoelectric, or piezoresistive techniques. All of these technologies require a close coupling between the transducer design and the sensor mechanical design. This results in constraints on the sensor that affect the performance adversely, especially as the size is reduced. An etalon-based displacement sensor having high dynamic range and high sensitivity may have many advantages in the field of physical sensing including reduction in size of the optical interferometer transducer and not adversely interacting with the optical interference transducer. This independence between the etalon and the optical interference transducer may result in the benefit of a decoupling of the transducer and the sensor design.
An etalon may be configured to be sensitive to a force or acceleration stimulus by having one surface of the etalon operably connected to a surface of, or disposed on, a movable element. When the element moves in response to the stimulus, the cavity length changes and, therefore, so does the ratio of optical energy in the reflected and transmitted signals. As a result, an electrical output signal based on one of the reflected and transmitted signals may be a function of the stimulus incident on the etalon.
The basic operating principal involves the creation of an optical path whose length is varied when subjected to an external stimulus, such as pressure or acceleration. An etalon may be used for consideration of the design issues in these types of transducers in general. This type of interferometer may have two parallel dielectric mirrors that bound an empty cavity. Light that is incident upon the cavity will be partially transmitted according to the formula:




  
    
      
        
          T
          =
          
            1
            
              
                (
                
                  1
                  +
                  
                    F
                    ⁢
                    
                      
                    
                    ⁢
                    
                      sin
                      2
                    
                    ⁢
                    
                      φ
                      /
                      2
                    
                  
                
                )
              
              2
            
          
        
        ,
      
    
    
      
        (
        1
        )
      
    
  




wherein F (finesse) is determined by the reflectance of the two mirrors,





  
    
      
        
          F
          =
          
            
              4
              ⁢
              
                R
                0
              
            
            
              
                (
                
                  1
                  -
                  
                    R
                    0
                  
                
                )
              
              2
            
          
        
        ,
      
    
    
      
        (
        2
        )
      
    
  




wherein R0 is the reflectance of the mirrors. Herein, it is assumed that the reflectance values of the two minors are equal. φ=4πnd cos θ/λ is the phase that is picked up in a wave with wavelength λ as it makes a roundtrip within the cavity of length d and index of refraction n with angle of incidence θ.

A typical response is shown in FIG. 2, where a transmitted wave 210 is reflected as reflected wave 220. The rate of change of the optical signal may be on the order of several percent per nanometer of motion. The optical signal can be resolved at a level below 100 parts per billion (ppb), which translates to the ability of the transducer to detect femtometer-scale changes in the displacement of one mirror relative to the other mirror. However, the sensitivity of the transducer may be very low throughout most of the typical operating points as can be seen in curves 210 and 220. Sensitivity of the transducer may be proportional to the absolute value of the slope of curves 210 and 220. So it may be observed that the slope, and sensitivity, may be very low when the gap d is between about 60.2 micrometers and 60.4 micrometers, and the slope may observed to be higher between about 60.4 micrometers and 60.6 micrometers.
A high resolution sensor, may require that the optical cavity length be allowed to vary over many wavelengths. One way to maintain sensitivity over a wide range of cavity lengths is to use multiple beams of light where each beam has a different response to changes in cavity length. The multiple beams of light may exhibit different responses by having different wavelengths, different angles of incidence, or a combination thereof.
FIG. 3 shows a chart of curves representing multiple beams on light using an exemplary set of different angles of incidence. The angles of incidence in this example range from 1.00 degrees in curve 310 to 7.00 degrees in curve 320. This range of angles is exemplary and illustrative only, and other ranges of angles may be used as would be understood by one of skill in the art with the benefit of the present disclosure. It may be seen from these curves that more than one beam may be sensitive to a particular cavity length. These beams may be produced using techniques known to those of skill in the art, including, but not limited to, one or more of: (i) directing multiple light beams toward a single lens configured to operate in a pupil division mode and (ii) directing multiple light beams toward an individual lenslets corresponding to each of the multiple light beams.
FIG. 4 shows a schematic of one embodiment according to the present disclosure. The coherent light beam 410, which may be collimated and/or polarized, may be split by a beam splitter 415 to generate a reference signal 420. A cylindrical condenser lens 430 spreads the beam 410 into divergent beams 480 in the far field. The input tilt mirror 440 sets the mean angle of incidence through the etalon 445. In some embodiments, the mean angle may range from about 0 degrees to about θmax degrees, where:




  
    
      
        
          
            
              θ
              max
            
            <
            
              w
              
                2
                ⁢
                
                  d
                  max
                
                ⁢
                
                  k
                  0
                
              
            
          
          ;
        
        ⁢
        
          

        
        ⁢
        
          
            w
            =
            
              width
              ⁢
              
                
              
              ⁢
              of
              ⁢
              
                
              
              ⁢
              beam
            
          
          ;
        
        ⁢
        
          

        
        ⁢
        
          
            
              k
              0
            
            =
            
              100
              ⁢
              
                R
                ⁡
                
                  (
                  
                    2
                    +
                    R
                  
                  )
                
              
              ⁢
              
                
                  (
                  
                    1
                    -
                    
                      R
                      2
                    
                  
                  )
                
                
                  -
                  1
                
              
            
          
          ;
          and
        
        ⁢
        
          

        
        ⁢
        
          R
          =
          
            Reflectivity
            ⁢
            
              
            
            ⁢
            of
            ⁢
            
              
            
            ⁢
            etalon
            ⁢
            
              
            
            ⁢
            surfaces
          
        
      
    
    
      
        (
        3
        )
      
    
  




It may be understood by one of skill in the art with the benefit of the present disclosure that the mean angle may range from about 0 degrees to an angle of such magnitude as causes the light beam to degrade such that the light beam may no longer interfere with itself. The light beams 480, each with its own angle of incidence, may be partially transmitted through the etalon 445 and may be collimated before reaching a detector array 460 by a collimator lens 450. The number of angles of the light beams may vary with the finesse of the etalon 445. Finesse is a parameter characterizing an optical cavity and may be a function of the reflectivity of the mirrored surfaces of the etalon 445, herein defined by eqn. (2). Generally, a higher reflectivity may result in a higher degree of finesse and the higher the number of angles of the light beams that may be required in the etalon 445. The detector array 460 may include two or more light sensitive detectors, such as photodiodes. In this exemplary embodiment, the detector array 460 includes nine (9) detectors with a spot size of each detector at about 10 micrometers and an array spacing of about 575 micrometers. Detector array 460 may distribute the detectors linearly. Detector array 460 may include at least one detector for each of the light beams 480. The detector array 460 may be configured to generate electrical signals in response to receiving energy from the light beams 480. The collimator lens 450 may include a lens array with a plurality of lenses. Condenser lens 470 may focus light beam 410 on a reference detector 490. The light beam 410 may be of any wavelength (infra-red, visible, ultraviolet, etc.) as long as the corresponding lenses, detectors, and etalon are configured and/or selected to properly respond to the wavelength used. In some embodiments, a second light beam (not shown) at a different wavelength from light beam 410 may be used along with light beam 410.
FIGS. 5 & 6 show a schematic of another embodiment according to the present disclosure. Here, coherent light beam 410 passes though a collimator lens 505 and polarizer 508 to a lens 530 that may change the incoming beam 410 into beams 580. Lens 530 may be configured to cause incoming beam 410 to diverge or converge. The beams 580 enter an etalon 445, where part of each of the beams 547 is transmitted to a lens array 450. Lens 530 is shown as a pair of concave cylindrical lenses, however, this is exemplary and illustrative only, as lens 530 may also be a single concave lens, a single convex lens, or a pair of convex lenses. Beams 580 may be divergent or convergent. The lens array 450 focuses the beams on a detector array 460. In some embodiments, a single lens (not shown) may be used in addition to or instead of the lens array 450. In some embodiments, an optical grating (not shown) may be used in addition to or instead of lens 530. The detector array 460 may be configured to generate electrical signals in response to receiving energy from the light beams 580. While there is no reference beam shown, a reference beam may be added to increase sensitivity for some applications. The reference beam may be used to cancel noise caused by intensity variations of the incoming light beam 410. The use of an optional reference beam may be determined by expertise of those of skill in the art.
FIG. 7 shows a schematic of another embodiment according to the present disclosure. Here, coherent light beam 710 from a fiber optic source 720 naturally spreads to form divergent beams 780 that may pass through an etalon 445 to a custom lens 750. The custom lens 750 may include off-axis Fresnel zones 755 that may transfer the incident energy of the light beam from each ring-shaped zone 755 and direct it to an individual detector 765 in a detector array 760. The detector array 760 may include at least two detectors responsive to electromagnetic energy. The detector array 760 may be configured to generate electrical signals in response to receiving energy from the light beams 780. The detector array 760 may include a plurality of detectors forming a linear array. An optional cylindrical lens (not shown) may be added between the fiber optic source 720 and the etalon 345 to collimate the divergent beams 780 along one axis.
FIG. 8 shows a schematic of another embodiment according to the present disclosure. In this design, the natural diffraction from an exemplary fiber-optic source 820 may cause coherent light beam 810 to form divergent beams 880 at a range of angles of approximately +/−6 degrees. This range of angles is exemplary and illustrative only, as other ranges of angles may be formed by a fiber-optic source as would be employed by one of skill in the art with the benefit of the present disclosure. After the divergent beams 880 pass through the etalon 445, the divergent beams 880 may be detected on a two-dimensional detector array 860. The detector array 860 may be configured to generate electrical signals in response to receiving energy from the light beams 880. The two-dimensional detector array 860 may include a charge coupled device (CCD) such as the type used in digital cameras. In some embodiments, an optional collimating lens (not shown) may be positioned between etalon 445 and detector array 860 to collimate the divergent light beams 880.
FIG. 9 shows of flow chart of a method 900 according to one embodiment of the present disclosure. The method 900 may include using device 100. In step 910, a plurality of divergent light beams 880 may be transmitted into an etalon 445 and partially transmitted from the etalon 445 to a detector array 860. Each of the plurality of divergent light beams 880 may enter the etalon 445 with different angles of incidence. The light beams 880 may have the same wavelength, different wavelengths, or a combination thereof. In step 920, an external stimulus (such as force or acceleration) causes a displacement in one of the mirrored surfaces of the etalon 445, which changes the cavity length of the etalon 445. In step 930, electrical signals generated by the detector array 860 due to the partially transmitted light beams may be altered as a result of change in cavity length of the etalon 445. In step 940, an external stimulus may be estimated based on the change in the electrical signals generated by the detector array 860. In some embodiments, the external stimulus estimation may also use a reference signal generated by a reference detector. In some embodiments, step 910 may be performed with a single light beam that is moved through a range of angles of incidence over a period of time, such that the electrical signals generated in step 930 may be produced sequentially. In some embodiments, the device 100 may be located at the surface 160. In some embodiments, device 100 may be conveyed in borehole 12 prior to step 910.
While the disclosure has been described with reference to exemplary embodiments, it will be understood that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the disclosure. In addition, many modifications will be appreciated to adapt a particular instrument, situation or material to the teachings of the disclosure without departing from the essential scope thereof. Therefore, it is intended that the disclosure not be limited to the particular embodiment disclosed as the best mode contemplated for carrying out this disclosure, but that the disclosure will include all embodiments falling within the scope of the appended claims.
While the foregoing disclosure is directed to the one mode embodiments of the disclosure, various modifications will be apparent to those skilled in the art. It is intended that all variations within the scope of the appended claims be embraced by the foregoing disclosure.

## Claims

1. An apparatus for estimating a parameter of interest, comprising:
an optical displacement device configured to receive a first electromagnetic beam with a first angle of incidence value and a second electromagnetic beam with a second angle of incidence value; and
a detector array configured to receive a part of the first electromagnetic beam and a part of the second electromagnetic beam that both pass through at least part of the optical displacement device.

2. The apparatus of claim 1, wherein the detector array comprises at least one of: (i) at least two detectors, (ii) a linear detector array, (iii) a detector and a Fresnel lens, and (iv) a detector and a collimating lens.

3. The apparatus of claim 1, wherein the detector array comprises at least one of: (i) a charge coupled device and (ii) a two-dimensional detector array.

4. The apparatus of claim 1, wherein an absolute value of the first angle of incidence value is not equal to an absolute value of the second angle of incidence value.

5. The apparatus of claim 1, wherein the detector array is configured to receive the electromagnetic beams at least one of: (i) simultaneously and (ii) sequentially.

6. The apparatus of claim 1, further comprising:
a carrier configured to be conveyed in a borehole penetrating an earth formation, wherein the optical displacement device and the detector array are disposed on the carrier.

7. The apparatus of claim 1, wherein the optical displacement device comprises:
a first reflective surface; and
a second reflective surface, wherein a relative motion between the first reflective surface and the second reflective surface is indicative of the parameter of interest.

8. The apparatus of claim 1, wherein the first and second electromagnetic beams are coherent and collimated.

9. The apparatus of claim 1, wherein the parameter of interest comprises at least one of: (i) a force and (ii) an acceleration.

10. The apparatus of claim 1, wherein the first electromagnetic beam and the second electromagnetic beam are divergent beams of a coherent light beam from a single source.

11. A method for estimating a parameter of interest, comprising:
estimating the parameter of interest using a detector array configured to receive a part of a first electromagnetic beam with a first angle of incidence value and a part of a second electromagnetic beam with a second angle of incidence value that both pass through at least part of an optical displacement device.

12. The method of claim 11, wherein the detector array comprises at least one of: (i) at least two detectors, (ii) a linear detector array, (iii) a detector and a Fresnel lens, and (iv) a detector and a collimating lens.

13. The method of claim 11, wherein the detector array comprises at least one of: (i) a charge coupled device and (ii) a two-dimensional detector array.

14. The method of claim 11, wherein an absolute value of the first angle of incidence value is not equal to an absolute value of the second angle of incidence value.

15. The method of claim 11, wherein the detector array is configured to receive the electromagnetic beams at least one of: (i) simultaneously and (ii) sequentially.

16. The method of claim 11, further comprising:
conveying the optical displacement device and the detector array in a borehole penetrating an earth formation.

17. The method of claim 11, wherein the optical displacement device comprises:
a first reflective surface; and
a second reflective surface, wherein a relative motion between the first reflective surface and the second reflective surface is indicative of the parameter of interest.

18. The method of claim 11, wherein the first and second electromagnetic beams are coherent and collimated.