EP2359122A2 - An inspection system and method - Google Patents

Abstract

A system and method for measuring the physical characteristics of a component where the system includes a light source, a sensing device, a reflecting device, and a retention mount. The method includes associating a component with the system such that the component is positioned within the retention mount and operating the system to cause the light source to emit a collimated light beam along a source optical path, where the collimated light beam is reflected to cause a reflected collimated light beam to propagate along a sensor optical path to be incident upon the component to produce a component silhouette where the sensing device generates data responsive to the silhouette. The image data is processed to generate resultant data responsive to the component, wherein the resultant data is further responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm.

Description

AN INSPECTION SYSTEM AND METHOD

RELATED APPLICATIONS

[0001] This application claims priority to U.S. Provisional Patent Application Serial No. 61/134,497 filed July 10, 2008 and U.S. Utility Patent Application Serial No. 12/383,141 filed March 20, 2009 the contents and disclosure of which are incorporated herein by reference in their entirety.

FIELD OF THE INVENTION

[0002] This disclosure relates generally to a method and system for inspecting components and more particularly to a method and system for optically inspecting the physical characteristics of externally threaded components, such as thread gages, screws, bolts and other externally threaded components having varied configurations.

BACKGROUND OF THE INVENTION

[0003] As society becomes increasingly reliant upon technology, mechanical and electromechanical systems, such as aircraft, automobiles, weapons systems and power systems, are called upon to perform an ever increasing number of functions. One downside to this is that, in some situations, a failure of a single threaded component in the system may cause a catastrophic failure of the entire system possibly resulting in the loss of millions of dollars and hundreds of lives. In an attempt to reduce the probability of a catastrophic systems failure, critical and some non-critical systems are required to satisfy predetermine operating tolerances before they may be used. As such, key threaded components within these systems, i.e. threaded components whose failure may cause a catastrophic system failure such as screws and/or gages, must also satisfy operating tolerances. If a threaded component fails to satisfy these required design tolerances and/or performance specifications, a degradation of system performance and/or a total system failure may occur resulting in damage to the system and/or injury/loss of life to an operator.

[0004] One of the current systems used for inspecting the physical characteristics of a threaded component employ an attribute inspection approach that measures the characteristics of the threaded component via a contact measurement technique which does not protect product design limits. This technique uses GO and/or No Go ring gages that are adjusted, or calibrated, to a desired thread measurement via Go and/or No Go setting plugs. Unfortunately, this technique does not ensure the integrity of design limits and because this approach is dependent upon human interaction, this technique has the disadvantage of being time consuming, subjectively inaccurate and unreliably repeatable for tight operating tolerances, thus permitting threaded components having dimensionally non-conforming characteristics to pass inspections. Moreover, there is a considerable wear factor on the measuring instruments, requiring the Go, No Go setting plugs to be inspected and replaced often.

[0005] Another approach used for measuring external thread gages utilizes three wires communicated to the gage being measured. The three wires are of a known diameter and are typically disposed between the threads of a component such that the wires protrude from the threads, wherein two wires are disposed on one side of the threaded component and one wire is disposed on the opposing side of the threaded component. The diameter over the wires is then measured via a human inspector. Because the wires are of a known diameter, this allows certain characteristics of the threads to be determined by measuring the width of the wires disposed between the threads. Unfortunately, this approach is also dependent upon human interaction. If the inspector measuring the distance over the wires compresses the wires too much, the wires may become deformed resulting in an inaccurate measurement. Additionally, the surface finish of a threaded component may adversely affect the accuracies of these measurements. Moreover, because the wires are loose and are not held between the threads, the wires may be dropped which may result in the wires becoming contaminated with dirt, the wires being lost or, if someone steps on them, the wires being deformed.

[0006] Furthermore, different operators will generate different gage pressures on the wires which may cause erroneous readings. Thus, this approach has the similar disadvantage of being time consuming, subjectively inaccurate and unreliably repeatable for tight operating tolerances, thus also permitting threaded components having dimensionally non-conforming characteristics to pass inspections. Additionally, the reliability and repeatability of this measurement is very poor because an operator must measure angles using an optical projection which is also time consuming, inaccurate and often fails to satisfy current product and gage calibration specifications. As such, the Measurement Uncertainty Factor (MUF) in many situations exceeds the required tolerances and as a result, the required accuracies for complete certification of these methods have thus far been unobtainable.

[0007] Another disadvantage to current measuring systems involves the human element required to obtain the actual physical measurement of the component and the data obtained from that measurement. As such, the accuracy of the equipment used to obtain the measurements is very questionable. For example, using current technology and methods, if two different people measure the same characteristics of a single component, it is highly probable that they will obtain different results. Another example involves when the component being measured is not be correctly aligned within the inspection system. This is undesirable because data obtained from the measurement of an incorrectly aligned component will most likely contain errors related to the misaligned component and thus the resultant measurement will be incorrect. Still yet another example involves errors in the functional size of the component due to deviations or waviness in the helical path of the thread. This creates an assembly problem in that parts may not assemble correctly. This is undesirable because data obtained responsive to an incorrect function size is unreliable and may result in a failure of the component or assembly. Another example involves deviations (in lead, flank angle error, pd error, major & minor diameter error, root radius roundness, etc..) from the true line measurements of the component.

SUMMARY OF THE INVENTION

[0008] An inspection system is provided and includes a collimated light source defining a source optical path, wherein the collimated light source is operable to cause a collimated light beam to propagate along the source optical path. The inspection also includes a sensing device defining a sensor optical path, wherein the sensor optical path is substantially perpendicular to the source optical path. Furthermore, the inspection system includes a positioning device having a positioning device stage, a reflecting device, wherein the reflecting device is disposed on the positioning device to be within the source optical path to receive the collimated light beam. The reflecting device causes a reflected collimated light beam to propagate along the sensor optical path to the sensing device. The inspection system also includes a retention mount, where a portion of the retention mount is disposed within the sensor optical path such that when a component is retained within the retention mount, the component blocks at least a portion of the reflected collimated light beam such that a silhouette is generated and incident upon the sensing device, where the sensing device generates data responsive to the silhouette. Moreover, the inspection system includes at least one processing device, wherein the at least one processing device is communicated with the sensing device to receive at least a portion of the data, wherein the processing device is configured to process the data responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm.

[0009] A method for measuring physical characteristics of a component using an inspection system is provided wherein the inspection system includes a light source, a sensing device, a reflecting device, and a retention mount, at least one of which is movably associated with the inspection system. The method includes associating a component with the inspection system such that the component is disposed within the retention mount, operating the inspection system to cause the light source to emit a collimated light beam propagating along a source optical path, reflecting the collimated light beam via the reflecting device to cause a reflected collimated light beam to propagate along a sensor optical path such that the reflected collimated light beam is incident upon the component to produce a component silhouette which is incident upon the sensing device, generating image data responsive to the component silhouette and processing the image data to generate resultant data responsive to at least one of a plurality of physical characteristics of the component, wherein the resultant data is responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm.

[0010] A machine-readable computer program code is provided, where the program code including instructions for causing a controller to implement a method for measuring physical characteristics of a component using an inspection system, wherein the inspection system includes a light source, a sensing device, a reflecting device, and a retention mount, at least one of which is movably associated with the inspection system. The method includes associating a component with the inspection system such that the component is disposed within the retention mount, operating the inspection system to cause the light source to emit a collimated light beam propagating along a source optical path, reflecting the collimated light beam via the reflecting device to cause a reflected collimated light beam to propagate along a sensor optical path such that the reflected collimated light beam is incident upon the component to produce a component silhouette which is incident upon the sensing device, generating image data responsive to the component silhouette and processing the image data to generate resultant data responsive to at least one of a plurality of physical characteristics of the component, wherein the resultant data is responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm. [0011] Asdf [0012] An inspection system for measuring the threaded surface of an internally threaded component is provided and includes at least one measuring probe, wherein the at least one measuring probe includes an emitter and a receiver and is sized and shaped to be positionable adjacent at least a portion of the threaded surface at an offset distance, wherein the emitter is configured to emit electromagnetic energy that is incident upon the threaded surface to generate reflected electromagnetic energy responsive to the threaded surface and wherein the receiver is configured to receive at least a portion of the reflected electromagnetic energy and generate threaded surface data. A processing device is also provided and is in signal communication with the measuring probe to receive the threaded surface data and process the threaded surface data to determine physical characteristics of the threaded surface.

[0013] A method for measuring the threaded surface of an internally threaded component using an inspection system is provided, wherein the inspection system includes a measuring probe having an emitter and a receiver and is sized and shaped to be positionably adjacent at least a portion of the threaded surface at an offset distance. The emitter is configured to emit electromagnetic energy incident upon the threaded surface to generate reflected electromagnetic energy responsive to the threaded surface and wherein the receiver is configured to receive at least a portion of the reflected electromagnetic energy and generate threaded surface data. The method includes associating the internally threaded component with the inspection system via an electromagnetic and positioning the measuring probe inside a cavity of the internally threaded component. The method further includes deactivating the electromagnet to cause the internally threaded component to be positioned relative to measuring probe such that an offset distance exists between the measuring probe and the threaded surface. The method also includes activating the electromagnet to securely re-associate the internally threaded component with the inspection system and operating the inspection system to cause the measuring probe to measure at least a portion of the threaded surface and to generate initial threaded surface data. Furthermore, the method includes processing the threaded surface data to generate physical characteristics of the at least a portion of the threaded surface.

[0014] A computer-readable storage medium encoded with machine-readable computer program code is provided, where the program code includes instructions for causing a controller to implement a method for measuring the threaded surface of an internally threaded component using an inspection system, wherein the inspection system includes a measuring probe having an emitter and a receiver and is sized and shaped to be positionably adjacent at least a portion of the threaded surface at an offset distance, wherein the emitter is configured to emit electromagnetic energy incident upon the threaded surface to generate reflected electromagnetic energy responsive to the threaded surface and wherein the receiver is configured to receive at least a portion of the reflected electromagnetic energy and generate threaded surface data. The method includes associating the internally threaded component with the inspection system via an electromagnetic and positioning the measuring probe inside a cavity of the internally threaded component. Furthermore, the method includes deactivating the electromagnet to cause the internally threaded component to be positioned relative to measuring probe such that an offset distance exists between the measuring probe and the threaded surface. The method further includes activating the electromagnet to securely re-associate the internally threaded component with the inspection system and operating the inspection system to cause the measuring probe to measure at least a portion of the threaded surface and to generate initial threaded surface data. Moreover, the method includes processing the threaded surface data to generate physical characteristics of the at least a portion of the threaded surface.

BRIEF DESCRIPTION OF THE DRAWINGS

[0015] The foregoing and other features and advantages of the present invention will be more fully understood from the following detailed description of illustrative embodiments, taken in conjunction with the accompanying drawings in which like elements are numbered alike in the several Figures:

[0016] Figure 1 shows a perspective side view of a component inspection system;

[0017] Figure 2 shows a side view of a component inspection system;

[0018] Figure 3 shows a close up side view of a component inspection system;

[0019] Figure 4 shows a front view of a component inspection system;

[0020] Figure 5 shows a close up perspective front view of a component inspection system; [0021] Figure 6 shows a close up front offset view of a component inspection system having a component disposed between arbors;

[0022] Figure 7 shows a schematic block diagram of a collimated light source;

[0023] Figure 8 shows a front view of a component disposed between arbors of a component inspection system;

[0024] Figure 9 shows a schematic block diagram of a component inspection system;

[0025] Figure 10 shows a side view of a threaded component;

[0026] Figure 1 1 show a side view of a threaded component;

[0027] Figure 12 shows a block diagram illustrating an overall method for measuring the characteristics of a component using a component inspection system;

[0028] Figure 13 shows a block diagram illustrating a component/gage selection algorithm;

[0029] Figure 14 shows a GUI screen capture of a component/gage selection screen;

[0030] Figure 15 shows a GUI screen capture of a component/gage selection screen;

[0031] Figure 16 shows a GUI screen capture of a component/gage selection screen;

[0032] Figure 17 shows a GUI screen capture of a component/gage selection screen;

[0033] Figure 18 shows a GUI screen capture of a component/gage selection screen;

[0034] Figure 19 shows a block diagram illustrating a calibration algorithm;

[0035] Figure 20 shows a reference arbor knee and a search box; [0036] Figure 21 shows a display device illustrating lens distortion measurements;

[0037] Figure 22 shows a block diagram illustrating a component measurement algorithm;

[0038] Figure 23 shows a block diagram illustrating an R&R algorithm;

[0039] Figure 24 shows a side view of a symmetrically threaded component;

[0040] Figure 25 shows a side view of a silhouette being projected onto a sensing device of the component inspection system of Figure 1 generated by a collimated light beam incident upon the symmetrically threaded component of Figure 24;

[0041] Figure 26 shows a front view of a sensing device of the component inspection system of Figure 1 with a silhouette of the symmetrically threaded component of Figure 24;

[0042] Figure 27 is a graph of the x-z plane showing a parametric representation of the embedding of the flank of a symmetrically threaded component onto the x-z plane;

[0043] Figure 28 is a graph of the x-z plane showing a parametric representation of the embedding of the flank of a symmetrically threaded component onto the x-z plane, including an aberration;

[0044] Figure 29 is a block diagram illustrating a method for measuring the physical characteristics of a component using the component inspection system of Figure 1; and

[0045] Figure 30 is a block diagram illustrating a method for correcting aberrations in a component silhouette generated by the component inspection system of Figure 1;

[0046] Figure 31 is a block diagram illustrating a method for accounting for deviations from true line measurements of a threaded component in a component silhouette generated by the component inspection system of Figure 1 ; [0047] Figure 32 is a block diagram illustrating a method for determining the functional size of a product or gage in a component silhouette generated by the component inspection system of Figure 1 ;

[0048] Figure 33 is a block diagram illustrating a method for accounting for misalignment of a component in the component inspection system of Figure 1 ;

[0049] Figure 34 shows a side view of an internal inspection system in accordance with one embodiment of the invention;

[0050] Figure 35 shows a side view of an internal inspection system of Figure 34;

[0051] Figure 36 shows a side view of an internal inspection system of Figure 34;

[0052] Figure 37 shows a side view of an internal inspection system of Figure 34;

[0053] Figure 38a shows a side view of an internal inspection system of Figure 34;

[0054] Figure 38b shows a side view of an alternative embodiment of an internal inspection system having multiple measuring probes;

[0055] Figure 39 shows a side view of an internal inspection system of Figure 34;

[0056] Figure 40a shows a side view of an internal inspection system of Figure 34;

[0057] Figure 40b shows a front view of a component associated with the internal inspection system of Figure 34;

[0058] Figure 41 shows a block diagram of a method for implementing the internal inspection system of Figure 34.

[0059] Figure 42 shows a side sectional view of an internally threaded component; [0060] Figure 43 shows a side sectional view of an internally threaded component;

[0061] Figure 44 illustrates a representation of the thread image of an internally threaded component showing data aberration (shadow image);

[0062] Figure 45 is a graph of the x-z plane showing a parametric representation of the embedding of the flank of a internally symmetrically threaded component onto the x- z plane;

[0063] Figure 46 is a graph of the x-z plane showing a parametric representation of the embedding of the flank of a symmetrically threaded component onto the x-z plane, including an aberration;

[0064] Figure 47 is a block diagram illustrating a method for measuring the physical characteristics of an internally threaded component using the component inspection system of Figure 34; and

[0065] Figure 48 is a block diagram illustrating a method for correcting aberrations in the data generated using the component inspection system of Figure 34.

DETAILED DESCRIPTION OF THE INVENTION

[0066] An exemplary embodiment is described herein by way of illustration as may be applied to the measurement and inspection of threaded gages and product, such as screws, bolts and other externally threaded components. However, while an exemplary embodiment is shown and described hereinbelow, it should be appreciated by those skilled in the art that the invention is not limited to the embodiment(s) and application(s) as described herein, but also to any component and/or measurement where accuracy in tolerance measurement is critical, such as taps, splines, gears, internal bores, integral plane cylindrical bores, internal threads, internal/external diameters and/or material composition and/or strength. Moreover, those skilled in the art will appreciate that a variety of potential implementations and configurations are possible within the scope of the disclosed embodiments.

[0067] Referring to Figures 1-8, an inspection system 100 is shown and described. In accordance with an exemplary embodiment, inspection system 100 includes a collimated light source 102, a sensing device 104, a reflecting device 106, a component support device 108 and a system support structure 1 10. System support structure 1 10 includes a base support structure 1 12, a base structure 1 14, a bridge structure 1 16 defining a bridge cavity 1 18, a light source mounting device 120 and a sensor mounting device 122. Base support structure 1 12 is disposed to be supportingly associated with base structure 1 14 and base structure 1 14 is disposed to be supportingly associated with bridge structure 116, wherein bridge cavity 1 18 is disposed between bridge structure 116 and base structure 1 14. It should be appreciated that as is well known in physics, the term light refers to and includes electromagnetic radiation of any wavelength (i.e. any wavelength along the electromagnetic spectrum). Accordingly, the collimated light source 102 may be any type of source that emits electromagnetic radiation suitable to the desired end purpose and the sensing device 104 is any type of sensing device that senses the emitted electromagnetic radiation suitable to the desired end purpose.

[0068] Collimated light source 102 may be associated with base structure 1 14 via light source mounting device 120 such that light emitted from collimated light source 102 propagates along a source optical path which is defined by collimated light source 102 and which is parallel to base structure 1 14. Sensing device 104 may be associated with bridge structure 1 16 via sensor mounting device 122, wherein sensing device 104 defines a sensor optical path which perpendicularly intersects the source optical path. Although, base structure 1 14 and bridge structure 1 16 may be constructed from a non-metallic polymer casting, it is contemplated that base structure 1 14 and bridge structure 1 16 may be constructed from any shock, vibration and/or movement attenuating material(s) and/or composite(s) suitable to the desired end purpose.

[0069] Component support device 108 includes a positioning device 124 and a mounting base 126, wherein mounting base 126 is associated with base structure 1 14. Positioning device 124 includes a positioning stage 128 and a component retainer 130, wherein component retainer 130 is associated with positioning stage 128 and includes a first arbor 132 separated from a second arbor 134 via an arbor cavity 136 and wherein at least one of first arbor 132 and/or second arbor 134 includes a notched potion, or arbor reference "knee" position 220. Positioning stage 128 may be positionally and controllably configurable in all planes (such as x-plane, y-plane, z- plane) relative to mounting base 126 via a motor operated by a motor controller. At least one of first arbor 132 and second arbor 134 are configurable for retaining a component within component retainer 130. Reflecting device 106 may be associated with positioning stage 128 such that reflecting device 106 is disposed at an angle of 45° relative to the surface of positioning stage 128 and such that reflecting device 106 is disposed in the same plane as first arbor 132, second arbor 134 and arbor cavity 136 (i.e. sensor optical path). Additionally, component support device 108 may be disposed within bridge cavity 118 such that reflecting device 106 is disposed at the intersection of the source optical path and the sensor optical path. Although reflecting device 106 is shown as a high quality 0.25 wave length first surface style mirror, reflecting device 106 may be any high quality reflective surface device suitable to the desired end purpose.

[0070] Sensing device 104 includes a high resolution camera 137 having a microscope-type telecentric optical lens 138 and although sensing device 104 is shown as being powered via an external power source, sensing device 104 may be powered using any power source suitable to the desired end purpose, such as a battery. Moreover, although microscope type tele-centric optical lens 138 is shown as having a magnification factor of 2.6X, microscope type tele-centric optical lens 138 may have any magnification factor suitable to the desired end purpose. Furthermore, although sensing device 104 is a VISICS CCD camera having a microscope type telecentric optical lens system with 2.6X magnification, it is contemplated that sensing device 104 may be any sensing device suitable to the desired end purpose.

[0071] Referring to Figure 7, collimated light source 102 includes a Light Emitting Diode (LED) 140, a collimating lens 142 and a lens cap 144 having a lens slot 146 disposed to minimize the stray emission of light emitted from collimating lens 142. In addition, collimated light source 102 may be associated with base structure 114 such that collimating lens 142 is in optical line of sight with reflecting device 106. Moreover, although collimated light source 102 is shown as being powered via an external power source, collimated light source 102 may be powered using any power source suitable to the desired end purpose, such as a battery.

[0072] Inspection system 100 is constructed such that when LED 140 is energized a beam of light is emitted from LED 140 and is projected such that the beam of light becomes incident upon collimating lens 142. Collimating lens 142 collimates the beam of light to create a collimated light beam 148, which is then emitted from collimating lens 142. Upon exiting collimating lens 142, collimated light beam 148 propagates along the source optical path and becomes incident upon reflecting device 106, which is disposed at an angle of 45° relative to the surface of positioning stage 128. Reflecting device 106 then reflects incident collimated light beam 148 and the reflected collimated light beam 150 propagates along the sensor optical path to become incident upon sensing device 104. However, because reflecting device 106 is disposed in the same plane as first arbor 132, second arbor 134 and arbor cavity 136 (i.e. sensor optical path), before reflected collimated light beam 150 becomes incident upon sensing device 104, reflected collimated light beam 150 becomes incident upon first arbor 132, second arbor 134 and arbor cavity 136. As such, when a component is disposed within component retainer 130 to be between first arbor 132 and second arbor 134, reflected collimated light beam 150 becomes partially blocked by the component, first arbor 132 and/or second arbor 134 and as a result, a shadow or silhouette of the component, first arbor 132 and/or second arbor 134 is created and communicated to sensing device 104.

[0073] Referring to Figure 9, an overall block diagram of inspection system 100 is shown and described. Inspection system 100 is shown as including a processing device 152 having a display device 154, camera controller circuitry 156 and a communications port 158, wherein processing device 152 is disposed to be in communication with collimated light source 102, sensing device 104 and positioning device 124. In accordance with an exemplary embodiment, collimated light source 102 is shown in optical communication with reflecting device 106 such that collimated light beam 148 emitted from collimated light source 102 is incident upon reflecting device 106. Reflecting device 106 reflects collimated light beam 148 to produce reflected collimated light beam 150. Sensing device 104 is shown in optical communication with reflecting device 106 such that reflected collimated light beam 150 is incident upon sensing device 104 to be received by high resolution camera 137 via microscope type tele-centric optical lens 138. Thus, when a component is disposed between first arbor 132 and second arbor 134, the silhouette of the component, first arbor 132 and/or second arbor 134 is also received by high resolution camera 137.

[0074] High resolution camera 137 converts the silhouette image into image data and communicates this image data to processing device 152, wherein the image data is responsive to the interaction between the component and reflected collimated light beam 148 received by telecentric optical lens 138. Processing device 152 then examines this image data to determine if more image data is required. If more image data is required, processing device 152 instructs sensing device 104 to obtain more image data. If necessary, processing device 152 may control the position of positioning device 126 via communications port 158 to dispose positioning device 126 as necessary in a manner responsive to the desired image data. Although processing device 152 is shown as being communicated with positioning device 126 via an RS-232 or RS-422 communications port, processing device 152 may be communicated with positioning device 126 via any device and/or method suitable to the desired end purpose, such as via wireless communications. Moreover, camera controller circuitry 156 may be communicated with processing device 152 via any method and/or device suitable to the desired end purpose. Furthermore, although high resolution camera 137 is shown as an electronic camera being able to support an image size of up to at least 1296x1016 pixels, high resolution camera 137 may be any high resolution camera 137 suitable to the desired end purpose.

[0075] It is further contemplated that, although display device 150 is shown as a flat panel display device having a 1280x1024 display capability, display device 150 may be any display device and/or method suitable to the desired end purpose. Additionally, although processing device 152 is shown as a computer system operating an MS Windows 2000 operating system (or higher version) and having a Pentium processor with at least 128 Mb RAM, Ethernet network capability and a wireless communications device, such as a modem, DSL or Tl line, processing device 148 may be any processing device suitable to the desired end purpose. Positioning device 126 may also include a cast iron stage with a glass slide and a linear motor having crossed rollers with patented anti-creep technology. The linear motor allows for at least plus and minus three (3) inches of travel in both X and Y axes and allows for a maximum load of at least 635 Kg. Positioning device 126 may also include a digital motor (servo) controller having an integral drive with a digital current loop and is communicated with processing device 152 via an RS- 232/RS-422 communications port. Additionally, the digital motor (servo) controller may be capable of supporting a 10-30 amp peak, 6-15 amps continuous and a 170-300 VDC bus and although the digital motor (servo) controller shown as being capable of supporting movement in the X and Y axis, it should be appreciated that digital motor (servo) controller may also be capable of supporting movement in the Z axis, as well.

[0076] Referring to Figure 10 and Figure 1 1, a side view of an externally threaded component, such as a threaded product is shown and discussed. A component thread is a combination of a thread ridge and groove, typically of uniform section, that is produced by forming a groove with a helix on an external or internal surface of a cylinder or cone. Because the component thread is designed to operate in association with an opposing component thread, it is essential that certain key physical characteristics relating to thread size and thread form be tightly controlled. As such, it is desirable to measure these thread size characteristics and thread form characteristics as accurately as possible. The thread size characteristics include the major diameter, the minor diameter, the functional diameter and the pitch diameter and the thread form characteristics include the pitch, the lead, the uniformity of helix angle, the flank angle and the included angle, each one of which is discussed in more detail hereinbelow.

[0077] The major diameter of the component is the diameter or width of an imaginary cylinder, called the major cylinder, whose surface would be parallel to the straight axis of the component and whose surface would bound the crests of an external thread or the roots of an internal thread. However, although both threaded gages and threaded products typically have a full form major diameter, threaded gages also typically have a truncated major diameter. As such, a threaded gage includes a full form major diameter and a truncated major diameter and a threaded product only includes a full form major diameter. The full form major diameter, for both a threaded gage and a threaded product, may be defined as a composite measurement responsive to the major radius (which may be defined as the distance between the component axis and one surface of the major cylinder or one half of the major diameter) measured on the 0° side of the full form threads and the major radius measured on the 180° side of the full form threads. However, for a threaded gage, the truncated major diameter may be defined as a composite measurement responsive to the major radius measured on the 0° side of the truncated threads and the major radius measured on the 180° side of the truncated threads.

[0078] The minor diameter of the component is the diameter of an imaginary cylinder, or minor cylinder, whose surface would be parallel to the straight axis of the component and whose surface would bound the roots of an external thread or the crests of an internal thread. Thus, the minor radius, which may be defined as the distance between the component axis and one surface of the minor cylinder or one half of the minor diameter, and which is typically measured using the first thread on the 0° side, is typically determined using a best fit radius that is tangential to the flanks and that has no reversals.

[0079] The pitch of a thread having uniform spacing may be defined as the distance, measured parallel to the axis, between corresponding points on adjacent thread forms in the same axial plane and on the side of the axis. Thus, the pitch may be defined as the number of threads per inch (TPI) and the pitch distance may be defined as 1/TPI, wherein TPI is measured parallel to the thread axis, from a point on one flank to the corresponding point on the next available flank. The pitch diameter of the component is the diameter or width of an imaginary cylinder, called the pitch cylinder, whose surface would be parallel to the axis of the thread or component and whose surface would intersect the profile of a straight thread such that the width of the thread ridge and the thread groove are equal.

[0080] Thus, the pitch diameter of a threaded gage, which typically includes full form threads and truncated threads, includes a pitch diameter front and a pitch diameter back, wherein the pitch diameter front is responsive to the leading and trailing angles of the thread, the lead and the crest width of the threads at the truncated location and wherein the pitch diameter back is responsive to the leading and trailing angles of the thread, the lead and the crest width of the threads at the full form location. Whereas the pitch diameter of a threaded component, which typically includes only full form threads, includes only a pitch diameter front, wherein the pitch diameter front is responsive to the leading and trailing angles of the thread, the lead and the crest width of the threads.

[0081] The lead may be defined as the axial distance moved by the component in relation to the amount of angular rotation, when a threaded component is rotated about its axis with respect to a fixed mating thread. Thus, the lead is the amount of axial travel when the threaded component is turned one full turn or 360° and pitch is the distance measured parallel to the axis from a point on one flank to the corresponding point on the adjacent flank. Any deviation in lead tends to increase the functional diameter of the external thread (or decrease the functional diameter of the internal thread) and rapidly consumes the allowed operating pitch diameter tolerance of a threaded component. A deviation in lead may result in non-engagement of a screw thread with its mating part at all but a few points. Thus, when the threaded parts are assembled, and torque is applied, the result is pressure being applied to only a few, and possibly only one pressure flank. As such, any deviation in lead may produce a non-engagement condition for some threads and cause a failure in engaging threads at the point of pressure flank engagement due to non-engagement.

[0082] The helical path deviation of a thread is a wavy deviation from a true helical advancement or a non-uniformity of helix angle. In a similar manner as the lead, a deviation in the helical path causes an increase in the functional size of the component in proportion to the amount of waviness. Thus, all of the statements that were made concerning a deviation in lead also apply to a deviation in helical path and similarly, a deviation of helical path may result in partial engagement of the thread flanks with the result that torque pressures may not be evenly distributed and may result in pre-load relaxation.

[0083] The included angle of a thread is the angle between the flanks of the thread measured in an axial plane. The flank angles are the angles between the individual flanks and the perpendicular to the axis of the thread measured in an axial plane. A flank angle of a symmetrical thread is commonly referred to as the half included angle or the half angle of a thread. A deviation in the flank angle may result in a failure of the thread when the product is exposed to line loads or when torque is applied. This is because an improper flank engagement may create an unevenly distributed pressure load along the flank rather than the pressure load being distributed evenly along the flank.

[0084] Other important physical characteristics of the component include the functional size diameter, the taper characteristic of the pitch cylinder and the out-of-roundness, all of which can generate a non-engagement condition. In fact, distortion or deviation from specifications of any of the physical characteristics discussed herein may cause varying degrees of non-engagement.

[0085] The functional, or virtual, diameter of a thread (external or internal) may be defined as the resultant size of the product thread taking into account the effect of lead, helical path deviation, flank angle deviation, taper and out-of-roundness. As such, it may be seen that the functional diameter is the pitch diameter of the enveloping thread of perfect pitch, lead and flank angles, having full depth of engagement, but that are clear at crests and roots, of specified lengths of engagement. For an external thread, the functional diameter may be derived by adding the cumulative effects of deviations to the pitch diameter (for internal threads subtracting the cumulative effects of deviations), including variations in lead and flank angles over a specified length of engagement. Thus, it should be clear that the effects of taper, out-of-roundness and surface defects may be positive or negative on either external or internal threads, respectively.

[0086] The taper characteristic of the pitch cylinder is simply a tapering of the pitch cylinder of the thread. As can be seen, a tapered thread fails to give a complete thread engagement, which may lead to a product failure caused by uneven torque pressure conditions on pressure flanks and pre-load relaxation. [0087] The out-of-roundness of the pitch cylinder, which is any deviation of the pitch cylinder from round, limits the thread engagement and allows for only line contact with the mating thread and typically includes two types of out-of-roundness: Multi-lobe or Oval.

[0088] With the desired physical characteristics of a threaded component to be measured explained hereinabove, an overall method for measuring these characteristics is provided and described hereinbelow. Furthermore, it is contemplated that each of the methods, calculations and algorithms described herein, may be performed via a system operator and/or via an automated system.

[0089] Referring to Figure 12, an overall method 300 for measuring the characteristics of a component using inspection system 100 is shown and discussed. In accordance with an exemplary embodiment, inspection system 100 and component 162 may be obtained, as shown in block 302, wherein inspection system 100 includes a light source 102, a sensing device 104, a reflecting device 106, and a component support device 108. Information regarding the type of threaded component 162 such as a screw, gage, bolt and/or other component, to be measured is determined and communicated to inspection system 100 via system software, as shown in block 304. Although, this may be accomplished via a system operator who enters information regarding threaded component 162 into processing device 152 via a mouse or keyboard in a manner responsive to a component/gage selection algorithm 400, it should be appreciated that component information may be stored in a database and retrieved via sensors, such as bar code readers.

[0090] Once component 162 has been selected and component information communicated to processing device 152 has been completed, component 162 is associated with inspection system 100 to be disposed within component support device 108, as shown in block 306. This may be accomplished by a system operator disposing component 162 within component retainer 130 such that component 162 is retained within arbor cavity 136 via first arbor 132 and second arbor 134. Inspection system 100 is then operated to perform a pre-calibration lens distortion analysis to determine any parabolic lens distortion factors, as shown in block 308. This pre-calibration lens distortion analysis is a curve fitting routine that is performed prior to the calibration procedure and that is separate from the system lens distortion measurement and correction that is part of the calibration procedure and that is used to compensate for any parabolic distortion that is inherent in optical lens 138. Moreover, although the lens distortion analysis is provided by the lens manufacturer, it should be appreciated that any suitable lens distortion analysis method may be independently developed and/or used.

[0091] In order to perform this analysis, collimated light source 102 emits a collimated light beam that becomes incident upon reflecting device 106, thus causing a reflected collimated light beam to become incident upon sensing device 104. Sensing device 104 receives this reflected collimated light beam and generates image data responsive to this reflected collimated light beam. Because the reflected collimated light beam is unimpeded, the image data generated by sensing device 104 is only responsive to the characteristics of collimated light source 102, reflecting device 106 and sensing device 104. Thus, the image data may be examined to determine if lens 138 of sensing device 104 contains any imperfections or distortions. As such, processing device 152 examines the image data to determine whether any variations of image intensity exist within a predefined field of view of lens 138. This may be accomplished by examining portions of the generated image data responsive to a number of various image locations within the field of view of lens 138, wherein the examined portions are responsive to locations within the vertical and horizontal span of the field of view, ranging from the bottom to the top and from the left hand side to the right hand side of the field of view.

[0092] For example, the image data to be examined may include data points responsive to a plurality of locations on lens 138 that represent the vertical span of lens 138 (or of the field of view of lens 138) for both the 0° and 180° side of at least one arbor. The results for each of these data points, which represent the actual vertical distortion characteristics of lens 138, may then be plotted on an actual vertical gradient chart (and compared with an ideal vertical gradient chart provided by the manufacturer of lens 138, wherein the ideal vertical gradient chart represents the ideal lens characteristics. In a similar fashion, the image data to be examined may also include data points responsive to a plurality of locations on lens 138 that represent the horizontal span of lens 138 (or of the field of view of lens 138). As above, the results for each of these data points, which represent the actual horizontal distortion characteristics of lens 138, are then plotted on an actual horizontal gradient chart and compared with an ideal horizontal gradient chart provided by the manufacturer of lens 138, wherein the ideal horizontal gradient chart represents ideal lens characteristics. Any deviations between the actual vertical/horizontal gradient charts and the ideal vertical/horizontal gradient charts are recorded and stored for later application in subsequent calculations and/or measurements. It should be noted that, in order to minimize any effect of lens distortion on the measurements, the areas of interest, i.e. areas of component 162 to be measured, are almost always disposed in the center of the field of view for lens 138.

[0093] Once this has been completed, inspection system 100 is operated to cause positioning stage 128 to be disposed such that the reflected collimated light beam is incident upon component 162, as shown in block 310. The reflected collimated light beam incident upon component 162 produces a silhouette of component 162 and/or first arbor 132 which is projected to be incident upon sensing device 104. Sensing device 104 generates image data responsive to silhouette of component 162 and first arbor 132 and communicates this image data to processing device 152 which processes the image data to generate resultant data, as shown in block 312. Processing device 152 then instructs inspection system 100 to perform a system calibration in a manner responsive to a predetermined calibration algorithm 500, as shown in block 314. Upon completion of predetermined calibration algorithm 500, inspection system 100 performs a component measurement in a manner responsive to a predetermined component measurement algorithm 600, predetermined calibration algorithm 500 and/or the results of lens distortion analysis, as shown in block 316. Once the component measurement has been completed, component information is then displayed to the system operator via display device 154 and/or via a printed certificate or report. In accordance with an exemplary embodiment, component/gage selection algorithm 400, predetermined calibration algorithm 500 and predetermined component measurement algorithm 600 are discussed in more detail below.

[0094] Referring to Figure 13, a block diagram of a component/gage selection algorithm 400 is shown and described. It should be noted that although component/gage selection algorithm 400 is described for component/gage selection screen 214 herein, as configured for a threaded product, component/gage selection algorithm 400 may be modified as required for various component selections.

[0095] Referring to Figure 14, upon starting inspection system 100, a component/gage selection screen 200 is displayed to a system operator via display device 154. Component/gage selection screen 200 may be created in a Graphical User Interface (GUI) format having a plurality of pull-down menus 202 and software buttons 204 that allow known physical characteristics of a component to be measured to be communicated to inspection system 100 via a mouse and/or keyboard. Pull-down menus 202 may include at least one of a component size selection pull down menu 206, a TPI pull down menu 208, a Class selection pull down menu 210 and a thread length pull down menu 21 1 and software buttons 204 may include at least one of a unit selection button 212, a component selection button 214, a set plug/work plug selection button 216 and a go/not go selection button 218. It should be appreciated that component selection button 214 allows for the selection of a plurality of types of components to be inspected, including a plain diameter gage, a threaded gage, a product, an X-calibration block, a Y-calibration block and a Roll. It should also be appreciated that pull-down menus 202 and software buttons 204 may be displayed to a system operator in a manner responsive to component selection button 214.

[0096] For example, referring to Figure 15, if component selection button 214 is configured for a plain diameter gage, plurality of pull-down menus 202 and plurality of selection buttons 204 displayed to a system operator include at least one of a unit selection button 212 and a plain diameter gage size pull down-menu 213. Referring to Figure 16, if component selection button 214 is configured for a threaded gage, plurality of pull-down menus 202 and plurality of selection buttons 204 displayed to a system operator include at least one of unit selection button 212, set plug/work plug selection button 216, go/not go selection button 218, component size selection pull down menu 206, TPI pull down menu 208 and Class selection pull down menu 210. Referring to Figure 17, if component selection button 214 is configured for a threaded product, plurality of pull-down menus 202 and plurality of selection buttons 204 displayed to a system operator include at least one of a unit selection button 212, set plug/work plug selection button 216, go/not go selection button 218, component size selection pull down menu 206, TPI pull down menu 208, Class selection pull down menu 210 and a thread length menu 21 1. Additionally, when component selection button 214 is configured for a threaded product, a pitch diameter measurement menu 217 may be displayed. Referring to Figure 18, a component/gage selection screen 202 is shown for component selection button 214 configured for a calibration block.

[0097] In the case of a threaded component 162, once component/gage selection screen 200 is displayed, the system operator selects the system of units inspection system 100 is to use when measuring threaded component 162, such as English or Metric units, via unit selection button 212, as shown in block 402. The system operator then selects the type of component that inspection system 100 will be measuring (i.e. a threaded component), via gage/product selection button 214, as shown in block 404, and (in the case of a gage) whether it is a set plug or a work plug, via set plug/work plug selection button 216, as shown in block 406. Also in the case of a gage, once this has been accomplished, the system operator selects whether this is a go or not/go, via go/not go selection button 218, and the gage size of the component is selected, via gage size selection pull-down menu 206, as shown in block 408. In the case of a component, the Threads Per Inch (TPI) and the Class of the component are then selected, via TPI pull down menu 208, as shown in block 410 and Class selection pull down menu 210, respectively, as shown in block 412.

[0098] Upon completion of the system startup procedure, inspection system 100 begins performing a system calibration procedure responsive to predetermined calibration algorithm 500. Referring to Figure 19 and Figure 20, once the system calibration procedure has been initiated, positioning stage 128 is moved to a predetermined starting position, or HOME position, as shown in block 502. It is contemplated that any location of positioning stage 128 may be selected as the HOME position. At this point, all encoders are zeroed and all positional measurements are determined with reference to this HOME position. An Arbor reference adjustment is then performed to properly locate the arbor reference "knee" position 220, as shown in block 404, wherein arbor reference "knee" position 220 is a notch disposed on at least one of first arbor 132 and/or second arbor 134. A software "constraint window" or search box is created within the field of view of lens 138 and image data representing the image contained within this search box is then examined to locate arbor reference "knee" position 220. Arbor reference "knee" position 220 may be located by analyzing this image data for differences in pixel intensities to identify where the horizontal arbor surface ends and the vertical arbor surface begins. This vertical arbor surface is arbor reference "knee" position 220. Once arbor reference "knee" position 220 is located, blue crosshairs 222 are disposed at arbor reference "knee" position 220 and displayed to the system operator via display device 154 to allow the system operator to visually confirm arbor reference "knee" position 220. It should be stated that arbor reference "knee" position 220 must be contained with this search box for predetermined calibration algorithm to continue. If arbor reference "knee" position 220 is not disposed within the search box, predetermined calibration algorithm terminates.

[0099] In accordance with an exemplary embodiment, the lens system distortion measurements are then conducted, as shown in block 506. Referring to Figure 21 , this may be accomplished by operating inspection system 100 such that positioning stage 128 relocates arbor reference "knee" position 220 to four distinct position/locations within the field of view of lens 138 on the 0° side of at least one of first arbor 132 and/or second arbor 134. These four distinct position/locations are located at a lower vertical field of view position 135, a lower middle vertical field of view position 137, a upper middle vertical field of view position 139 and an upper vertical field of view position 141. At each of these four vertical locations, three horizontal measurements are made and include a left measurement 143, a center measurement 145 and a right measurement 147. This measurement data may be obtained by observing and/or analyzing the image data corresponding to the particular points of measurement. The results of this observation/analysis may then be recorded for use in subsequent calculation. This sequence is then repeated on the 180° side of at least one of first arbor 132 and/or second arbor 134. It should be appreciated that a total of 24 measurements (i.e. 12 on the 0° side and 12 on the 180° side) are stored and thus, become part of the calculated lens distortion measurement performed near the end of the calibration cycle. As discussed above, the lens system distortion routine, and thus the distortion equations, may be provided by the manufacturer of lens system 138 or may be generated responsive to the component to be inspected.

[00100] Once the lens system distortion measurements have been conducted, the X-Axis calibration is performed, as shown in block 508. The X-Axis calibration may be accomplished by locating the center position, the left extreme and the right extreme of field of view 230 of lens 138 and using these data points to calculate the inches per step, inches per pixel and/or the steps per inch calibration factors for the X-Axis. One way to determine center position, left extreme and right extreme of field of view 230 is to move arbor reference knee position 220 to the extreme left hand side of field of view 230 and register this location as the left extreme. Arbor reference knee position 220 is then moved to the extreme right hand side of field of view 230 and this location is registered as the right extreme. Arbor reference knee position 220 should then be moved to a point midway between the left extreme and the right extreme of field of view 230. This point will be the center of field of view 230 and should be registered as the center position. This ensures minimal distortion from lens 138.

[00101] Upon completion of the X-Axis calibration, a Y-Axis calibration at the 1^st 0° diameter is performed, as shown in block 510. The Y-Axis calibration at the 1^st 0° diameter may be accomplished by using the lower middle center location and upper middle center location obtained during the lens system distortion measurement to calculate the inches per step, inches per pixel and/or the steps per inch calibration factors for the Y-Axis. The lower middle vertical location is then determined and is used to measure the radius for the 0° side (which may later be added to the radius for the 180° side to determined the diameter of the arbor). [00102] Upon completion of the Y- Axis calibration at the 1^st 0° diameter, a Y-Axis 2^nd 0° diameter determination is performed, as shown in block 512. The determination of the Y-Axis 2^nd 0° diameter may be accomplished by moving positioning stage 128 such that arbor reference knee position 220 on the 0° side of the arbor is disposed at a lower vertical location, a lower middle vertical location, an upper middle vertical location and an upper vertical location of field of view 230. At each of these locations, inspection system 100 performs three horizontal measurements, a left horizontal measurement, a center horizontal measurement and a right horizontal measurement. This data may be stored and may become part of the calculated lens distortion factors determined toward the end of the calibration cycle. It should be appreciated that the lower middle vertical location may be the final position to be measured and may be used to measure the radius for the 180° side, which may later be added to the radius of the 0° side to determine the arbor diameter.

[00103] Upon completion of the Y-Axis 2^nd 0° diameter determination, a Y-Axis 2^nd diameter determination is performed, as shown in block 514. The determination of the Y-Axis 2^nd diameter may be accomplished by moving the left arbor reference location to determine the location of the arbor relative to the right arbor reference and lens 138. A single measurement is taken in the center of field of view 230 to minimize distortion and is used to determine the radius and to compute the tangent correction factor that is used to compensate for any misalignment of the Y-Axis of positioning stage 128 with the Y-Axis of lens 138.

[00104] Once this has been completed, a Y-Axis 2^nd 180° diameter determination is performed, as shown in block 516, by moving positioning stage 128 to the 180° side (same X- Axis position) to measure the radius. The Y-Axis tangent correction factor is then determined, as shown in block 518. This compensates for a component that may be disposed between first arbor 132 and second arbor 134 in a non-level (i.e. horizontal) manner. Moreover, this may be accomplished by using the measurements taken at the right and left sides of the arbor and both the X and Y measurement information from the encoders and the image measurement tools are used to compute the tangent correction factor. It should be noted that all subsequent Y-Axis measurements include this compensation factor. All of the information obtained above are then used to determine the lens distortion factor, as shown in block 520, which is then used for all subsequent X and Y measurements, including any light source and/or system stage positional distortions/errors (i.e. Abbe* stage errors). [00105] It is contemplated that predetermined component measurement algorithm 600 is responsive to the component being measured. As such, predetermined component measurement algorithm 600 is explained for various types of components to be measured and includes a threaded product and a threaded gage. It should be appreciated that all measurements may be conducted by observing and/or analyzing image data to determine desired points of interest on threaded component 162, such as the thread ridges and grooves. These points of interest may be located by examining the image data and identifying variations in pixel intensities to establish silhouette edge points of threaded component 162. Once these points of interest have been identified, desired physical characteristics of threaded component 162 may be determined using known mathematical, geometric and/or trigonometric relationships.

[00106] Upon completion of predetermined calibration algorithm 500, positioning stage 128 is positioned back to arbor reference knee position 220 and component measurement algorithm 600 is initiated, as shown Figure 22. At this point, the Flank registration is performed, as shown in block 602. This may be accomplished by disposing positioning stage 128 such that component 162 is positioned to an initial X and Y location by moving positioning stage 128 one half inch away from arbor reference knee position 220 in the X direction and toward component 162. Positioning stage 128 is then moved in the Y direction such that the lower limit of the pitch diameter at the centerline of field of view 230 is approximated. A software measurement tool is then placed at the centerline to find the flank angel crossings at the centerline. The stage is then moved again away from arbor reference knee position 220 in the X-axis direction to align the minor diameter with the left edge of field of view 230. All subsequent measurements rely on moving in pitch lead increments in the X-axis direction. It should be noted that the pitch lead increments are determined by the component selection and are published at the top of the Lead Standards readouts. It should be appreciated that, for threaded gages, the truncated measurements will be conducted at thread #2 and the full form measurements will be conducted at thread #6. The term 4X refers to the number of threads for the third lead measurement and indicates that it is being made over a span of four threads and the term /10 indicates that there are ten threads available on this component.

[00107] Once the flank registration has been performed, the 1^st full thread 0° side truncated measurements are conducted, as shown in block 604. This may be accomplished by repositioning positioning stage 128 on the first thread on the 0° side designated as the truncated thread location. This designation is dependent upon the thread numbers and thus upon the selection of component 162. Using the silhouette image data, processing device 152 then determines the minor radius, the major radius (for set plug only), the pitch radius, the lead pitch, the lead/trail flank angles and the included angles. The major radius is determined via the major diameter, which is a composite measurement based on the major radius of the 0° and corresponding 180° side of the threads. Thus, the major radius is determined by summing the individual measurements along the thread flat and dividing by the number of measurements collected. The number of measurement locations may be determined by taking 70% of the thread width, as determined by predetermined thread tables, and centering them on the center of the thread. This major radius average is then combined from both the 0° and the 180° sides to get the major diameter. For a gage, this process is performed for both truncated and full form locations and for a product, this process is performed only for the full form location.

[00108] The pitch diameter calculation (for both truncated and full form location), which is based on the leading and trailing angles, major diameter, pitch lead and crest width at the location in question (i.e. truncated or full form), may be determined by the equation:

PD=MD-(Cot(PL/2)-CW),

[00109] Where, PD is pitch diameter, MD is major diameter, PL is pitch lead and CW is crest width. The lead front measurement, which is responsive to the difference between the groove distance and the ridge distance along the leading/trailing/leading flanks may be determined by positioning a software measurement tool along the X-axis and moving the tool vertically around the pitch diameter until the groove distance minus the ridge distance is minimized. The tool is then repositioned at the minimized location and the groove distance and the ridge distance are added to determine the lead front. The lead back measurement, which is responsive to the difference between the groove distance and the ridge distance along the trailing/leading/trailing flanks may similarly be determined by positioning a software measurement tool along the X-axis and moving the tool vertically around the pitch diameter until the groove distance minus the ridge distance is minimized. The tool is then repositioned at the minimized location and the groove distance and the ridge distance are added to determine the lead back.

[00110] In an additional embodiment, the determination of the Pitch Diameter (PD) may include a Correction Factor (CF) to adjust for any aberrations that may be present in the silhouette image data. Referring to Figure 24, a symmetrically threaded object 800 is shown having a plurality of threads 802. The Pitch Diameter (PD) for the threaded object 800 having thread grooves 804 and thread ridges 806 may be described simply as the distance between a point on the 0° side of the object and the 180° of the object where the width of the thread ridge, gi, and the thread groove, g₂, are equal. However referring to Figure 25 and Figure 26, as the collimated light beam 808 falls incident upon the object 800, a shadow image 810 may be created and may fall incident upon the sensing device 812 along with the silhouette image 814. As such, the silhouette image data generated by the sensing device 812 may include data responsive to the shadow image 810 and as such, the physical characteristics of the object 800, such as the Pitch Diameter (PD) may be skewed and inaccurate.

[00111] To compensate for any aberrations of the shadow image 810 within the silhouette image data, a Correction Factor (CF) may be generated and applied to the process for determining the Pitch Diameter (PD). As such, the Pitch Diameter (PD) may be represented by the equation:

PD Final ⁼ PD observed ~ CF,

wherein PD_Fi_nai is the Pitch Diameter (PD) adjusted for any aberrations, PD_Obse_rved >s the Pitch Diameter (PD) as measured and containing any aberrations and CF is the Correction Factor (CF) representing any aberrations.

[00112] For example, one embodiment for compensating for any aberrations includes generating a Correction Factor (CF) responsive to the shadow image and subtracting the Correction Factor (CF) from the silhouette image data generated by the sensing device, wherein the Correction Factor (CF) may be determined by parametrically representing one flank of a thread (i.e. the rear side of a thread ridge) in 3-D space having an x-axis, a y-axis and a z-axis as an embedding of a strip into a 2-D space having only the x-axis and the z-axis. Referring to Figure 27, for objects or components having symmetrical threads, using only two variables (r, t), a first point, ri, representing the minor diameter of the thread on the x-z axis, and a second point, r₂, representing the major diameter of the thread on the x-z axis, is shown in the x-z plane connected via a straight line, K_x-Z, which is drawn between the two points r* and r₂. The variable R is the 2-D representation of the Pitch Diameter (PD) in the x-z plane and t is the flank angle which may be represented as the angle between the line K_x-1 drawn between the two points, ri and r₂, in the x-z plane and the projection K_x._y of the line K_x-1 onto the x-y plane. Additionally, the variable L_x-Z is the lead angle of the thread and the variable m is the tangent of the flank angle, t. The variable r is a point on the x-z plane which represents the distance between the z-axis and a point on the line K_x._z and thus may range from half of the minor diameter to half of the major diameter. As such, we can parameterize the above relationships using the following equations:

x = r cos (t), y = r sin (t), and z = mr + Lt/2n.

[00113] This embedding can then be projected onto the x-z plane by using the equations:

x = r cos (t), and Z — mr + Lt/2n,

to obtain the determinant of the Jacobian matrix, wherein the Jacobian matrix is defined by:

&1 dz\ dx\ dxn

J(x\ ....xn) = dzn dzn δxl dxn

As is well known, the Jacobian matrix is the matrix of all first-order partial derivatives of a vector-valued function and may be representative of the 'best' linear approximation to a differential function near a given point.

Thus, using the equations as derived hereinabove,

x = r cos (t), and z = mr + Lt/2n,

the Jacobian matrix J(xi...X_n) may be represented as:

Solving the Jacobian matrix J(X₁...X_n) to find the set of points of the shadow image (i.e. ribbon) on the x-z plane gives the following:

J = {{L I 2π) cos(0 + mr sin(0) = 0 ,

where,

r = -(I /(2Λ?w tan(0)) .

[00114] Referring to Figure 28, if the value of R is set to half of the Pitch Diameter (PD) of the thread, the point on the projection of the ribbon that is directly to the "right" of the point where r=R and t=0 may be determined. This is a point on the ribbon that has the same z- coordinate as the Pitch Diameter (PD) point (x,y,z) = (R,0,mR) and thus, it can be seen that at the Pitch Diameter (PD) point (x,y,z), z = mR. Plugging z=mR into the equation for z gives the following:

Lt z = mR = mr + ^■

{2πm)

Lt r = R -

{2πm) and combining equation (1) with equation (2) gives the following:

- L Lt

= R -

2πm tan(t) 2πm and

L + {2πmR - Lt) tan(t) = 0 ,

which must be solved for each given value of L, m and R. Having the flank angle, t, these equations may be solved to obtain r, wherein half of the displacement of the Pitch Diameter (PD) is the x-coordinate of the point on the ribbon minus the x-coordinate of the Pitch Diameter (PD) point (x,y,z) = (R,0,mR) or simply, r cos (t) - R. Thus, it should be appreciated that the Correction Factor (CF) may be assumed to be twice this amount and may be given by the equation:

CF = 2(r cos(0 ~ R) .

Thus, the Pitch Diameter for a symmetrically threaded object adjusted for any aberrations, PD_Fma|, may be determined by applying the Correction Factor (CF) above into equation (1 ) to give the following equation:

PD_Fma, = PDotserved - 2(rcos(t) - R),

In a similar fashion, for objects or components having asymmetrical threads, such as buttresses, the methodology applied hereinabove may be used for both flanks (due to the asymmetry the calculations should be conducted for each flank). As such, a simple geometric argument using the above approach for both flanks may combine the two results in a kind of weighted average to give:

„ „ (dl tan(αl) + dl tan(α2))

Cr =

(tan(αl) + tan(α2))

wherein dl and d2 are the shadow corrections for the two flank angles treated separately as symmetrical threads and al and a2 are the respective flank angles. Given the above, the Pitch Diameter for an asymmetrically threaded object adjusted for any aberrations, PD_Fιna|, may be determined by applying the Correction Factor (CF) above into equation (1) to give the following equation:

(rfl tan(al) + </2tan(a2)) r L>Final ~ r observed ; ~~ T~ZT_^ •

(tan(αl) + tan(α2))

[00115] Referring to figure 29, a block diagram illustrating a method 900 for measuring the physical characteristics of a component using an inspection system is shown and includes associating an object with the inspection system 100 such that the object is disposed within the retention mount, as shown in operational block 902. The inspection system is operated to cause the light source to emit a source collimated light beam which propagates along the source optical path, as shown in operational block 904. As the source collimated light beam propagates along the source optical path the source collimated light beam is at least partially incident upon the reflecting device to generate a reflected collimated light beam that propagates along the sensor optical path to be at least partially incident upon the object, as shown in operational block 906. This creates a silhouette of the object, wherein at least a portion of the silhouette is incident upon the sensing device which in response generates initial image data. This initial image data is processed to generate resultant image data responsive to at least one of a plurality of physical characteristics of the object, as shown in operational block 908, wherein the initial image data is processed responsive to at least one predetermined algorithm to correct for any aberrations in the initial image data. As discussed hereinabove, the predetermined algorithm may be responsive to the type of object being inspected. For example, if the object is a threaded object having symmetrical threads, then the predetermined algorithm may be at least partially responsive to the equation:

CF = 2{r cos(t) - R) ,

However, if the object is a threaded object having asymmetrical threads, then the predetermined algorithm may be at least partially responsive to the equation:

„„ (d\ tan(αl) + di tan(α2))

Cr =

(tan(αl) + tan(α2))

[00116] Referring to Figure 30, a block diagram illustrating a method 1000 for correcting aberrations in a component silhouette generated by inspection system 100 is shown and includes associating the object 800 with the inspection system 100, as shown in operational block 1002, and operating the inspection system 100 to cause the light source to emit a source light beam that propagates along the source optical path to at least partially incident upon the object 800, as shown in operational block 1004. The source light beam is reflected to create a reflected light beam that propagates alone a sensor optical path to be at least partially incident upon the object 800 to produce a silhouette 814 of the object 800 that is at least partially incident upon the sensing device 812, as shown in operational block 1006, wherein the sensing device 812 generates initial image data responsive to the silhouette and any aberrations in the silhouette. The initial image data is then processed to generate resultant image data, as shown in operational block 1008. This may be accomplished by generating initial Pitch Diameter (PD) data from the initial image data, as shown in operational block 1010. This initial Pitch Diameter (PD) data is then parameterized and expressed in a Jacobian Matrix, J(X₁....x_n), as shown in operational block 1012, and the Jacobian Matrix, J(xi....x_n), is solved responsive to a plurality of physical characteristics of the object to generate Correction Factor (CF) data, as shown in operational block 1014, wherein the plurality of physical characteristics may include at least one of the lead angle, the flank angle, the major diameter and the minor diameter. Once the Correction Factor (CF) data is determined, the initial Pitch Diameter (PD) data is processed responsive to the Correction Factor (CF) data to obtain the resultant Pitch Diameter (PD) data, as shown in operational block 1016.

[00117] The multi thread lead, which is responsive to the distance between the lead front and the lead back measurements, may now be determined. Additionally, the lead angle may be determined by an optimistic theoretical line of best fit along the leading flanks of the thread on the 0° side at the truncated location. The trailing angle may be determined by an optimistic theoretical line of best fit along the trailing flanks of the thread on the 0° side at the truncated location. The included angle may then be determined by adding the leading angle and trailing angle.

[00118] At this point, the 2^nd thread 0° side full form measurements are then made, as shown in block 606. This may be accomplished by repositioning positioning stage 128 on the second thread on the 0° side designated as the full form thread location. As discussed above, this designation is dependent upon the thread numbers and thus upon the selection of component 162. Using the silhouette image data, processing device 152 then determines the minor radius, the major radius, the pitch radius and the lead pitch.

[00119] The 1^st full thread 180° side truncated measurements are then conducted, as shown in block 608, and may be accomplished by repositioning positioning stage 128 on the first thread on the 180° side designated as the truncated thread location. Using the silhouette image data, processing device 152 then determines the minor radius, the major radius (for set plug only), the pitch radius and the lead pitch.

[00120] The 2^nd thread 180° side full form measurements are then made, as shown in block 610. This may be accomplished by repositioning positioning stage 128 on the second thread on the 180° side designated as the full form thread location. Using the silhouette image data, processing device 152 then determines the major radius, the pitch radius and the lead pitch. [00121] The component values and limits are then updated and the results are displayed to a system operator and/or printed out in certificate form and positioning stage 128 is repositioned to arbor reference knee position 220, as shown in block 612.

[00122] It is further contemplated that inspection system 100 may perform an R&R (reliability & repeatability) measurement procedure in a manner responsive to a predetermined R&R algorithm 700. Referring to Figure 23, a block diagram illustrating predetermined R&R algorithm 700 is shown and discussed. Upon initiation of predetermined R&R algorithm 700, positioning stage 128 is positioned into the load position and component 162 is disposed to be retained between first arbor 132 and second arbor 134, as shown in block 702. R&R algorithm 700 is then activated, as shown in block 704. As discussed hereinabove, inspection system 100 then performs predetermined calibration algorithm 500 and predetermined component measurement algorithm 600, as shown in block 706. At this point, once predetermined component measurement algorithm 600 has been completed, the system operator may elect to have inspection system 100 pause every seven cycles for rotation of component 162, as shown in block 708. The measurement cycle may then repeated as many times as desired and the results may then be displayed to the system operator via display device 154 or via a printed certificate or report, as shown in block 710.

[00123] In accordance with an additional embodiment, it should be appreciated that the inspection system 100 may also operate by configuring other elements of the inspection system 100 other than the positioning stage 128, such as by moving at least one of the collimated light source 102, the sensing device 104 and/or the reflecting device 106. For example, instead of the positioning stage 128 being positionally and controllably configurable in all planes (such as x- plane, y-plane, z-plane) relative to the mounting base 126 via a motor operated by a motor controller, at least one of the collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be positionally and controllably configurable in all planes (such as x- plane, y-plane, z-plane) relative to the mounting base 126 via at least one motor operated by at least one motor controller such that the component being measured is kept stationary.

[00124] In this embodiment, the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be positionally and controllably configurable in all planes (such as x-plane, y-plane, z-plane) relative to the mounting base 126 via communications port 158 as necessary in a manner responsive to the desired image data. The at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be positionally and controllably configurable in all planes (such as x-plane, y-plane, z-plane) relative to the mounting base 126 using the processing device 152 which may be communicated with the at least one motor controller via an RS-232 and/or an RS-422 communications port and/or any device and/or method suitable to the desired end purpose, such as via wireless communications.

[00125] In this embodiment the inspection system 100 may be operated as discussed hereinbefore. For example, consider the overall method 300 for measuring the characteristics of the component 162. Once the pre-calibration lens distortion analysis has been conducted, the inspection system 100 may be operated to cause the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 to be disposed such that the reflected collimated light beam is incident upon component 162, as shown in operational block 310. The reflected collimated light beam incident upon component 162 produces a silhouette of component 162 and/or first arbor 132 which is projected to be incident upon the sensing device 104. As discussed hereinbefore, the sensing device 104 generates image data responsive to the silhouette of the component 162 and the first arbor 132 and communicates this image data to processing device 152 which processes the image data to generate resultant data, as shown in operational block 312. The processing device 152 then instructs the inspection system 100 to perform a system calibration in a manner responsive to the predetermined calibration algorithm 500, as discussed in further detail herein and as shown in operational block 314. Upon completion of the predetermined calibration algorithm 500, the inspection system 100 performs a measurement of the component 162 in a manner responsive to the predetermined component measurement algorithm 600 as discussed in further detail herein, the predetermined calibration algorithm 500 and/or the results of lens distortion analysis, as shown in operational block 316. Once the component measurement has been completed, component information may then be displayed to the system operator via the display device 154 and/or via the printed certificate or report.

[00126] As above, upon completion of the system startup procedure, the inspection system 100 may begin by performing a system calibration procedure responsive to the predetermined calibration algorithm 500. Referring again to Figure 19 and Figure 20, once the system calibration procedure has been initiated, the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be configured to be disposed in a HOME position, as shown in operational block 502., wherein it is contemplated that any location of at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be selected as the HOME position. At this point, all encoders are zeroed and all positional measurements are determined with reference to this HOME position. An Arbor reference adjustment is then performed to properly locate the arbor reference "knee" position 220, as shown in operational block 504, wherein the arbor reference "knee" position 220 is a notch disposed on at least one of first arbor 132 and/or second arbor 134. A software "constraint window" or search box is created within the field of view of lens 138 and image data representing the image contained within this search box is then examined to locate arbor reference "knee" position 220. Arbor reference "knee" position 220 may be located by analyzing this image data for differences in pixel intensities to identify where the horizontal arbor surface ends and the vertical arbor surface begins. This vertical arbor surface is arbor reference "knee" position 220. Once arbor reference "knee" position 220 is located, blue crosshairs 222 are disposed at arbor reference "knee" position 220 and displayed to the system operator via display device 154 to allow the system operator to visually confirm arbor reference "knee" position 220. It should be stated that arbor reference "knee" position 220 must be contained with this search box for predetermined calibration algorithm to continue. If arbor reference "knee" position 220 is not disposed within the search box, predetermined calibration algorithm terminates.

[00127] As discussed in more detail hereinbefore, the lens system distortion measurements may then be conducted, as shown in operational block 506. Referring again to Figure 21, this may be accomplished by operating inspection system 100 such that the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 is configured to locate the arbor reference "knee" position 220 to four distinct position/locations within the field of view of lens 138 on the 0° side of at least one of first arbor 132 and/or second arbor 134. These four distinct position/locations are located at a lower vertical field of view position 135, a lower middle vertical field of view position 137, a upper middle vertical field of view position 139 and an upper vertical field of view position 141. At each of these four vertical locations, three horizontal measurements are made and include a left measurement 143, a center measurement 145 and a right measurement 147. This measurement data may be obtained by observing and/or analyzing the image data corresponding to the particular points of measurement. The results of this observation/analysis may then be recorded for use in subsequent calculation. This sequence is then repeated on the 180° side of at least one of first arbor 132 and/or second arbor 134. It should be appreciated that a total of 24 measurements (i.e. 12 on the 0° side and 12 on the 180° side) are stored and thus, become part of the calculated lens distortion measurement performed near the end of the calibration cycle. As discussed above, the lens system distortion routine, and thus the distortion equations, may be provided by the manufacturer of lens system 138 or may be generated responsive to the component to be inspected.

[00128] Once the lens system distortion measurements have been conducted, the X-Axis calibration is performed, as shown in operational block 508. The X-Axis calibration may be accomplished by locating the center position, the left extreme and the right extreme of field of view 230 of lens 138 and using these data points to calculate the inches per step, inches per pixel and/or the steps per inch calibration factors for the X-Axis. One way to determine center position, left extreme and right extreme of field of view 230 is to move arbor reference knee position 220 to the extreme left hand side of field of view 230 and register this location as the left extreme. Arbor reference knee position 220 is then moved to the extreme right hand side of field of view 230 and this location is registered as the right extreme. Arbor reference knee position 220 should then be moved to a point midway between the left extreme and the right extreme of field of view 230. This point will be the center of field of view 230 and should be registered as the center position. This ensures minimal distortion from lens 138.

[00129] Upon completion of the X-Axis calibration, a Y-Axis calibration at the 1^st 0° diameter is performed, as shown in operational block 510. The Y- Axis calibration at the 1^st 0° diameter may be accomplished by using the lower middle center location and upper middle center location obtained during the lens system distortion measurement to calculate the inches per step, inches per pixel and/or the steps per inch calibration factors for the Y-Axis. The lower middle vertical location is then determined and is used to measure the radius for the 0° side (which may later be added to the radius for the 180° side to determined the diameter of the arbor).

[00130] Upon completion of the Y-Axis calibration at the 1^st 0° diameter, a Y-Axis 2^nd 0° diameter determination is performed, as shown in operational block 512. The determination of the Y-Axis 2^nd 0° diameter may be accomplished by configuring the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 such that arbor reference knee position 220 on the 0° side of the arbor is disposed at a lower vertical location, a lower middle vertical location, an upper middle vertical location and an upper vertical location of field of view 230. At each of these locations, inspection system 100 performs three horizontal measurements, a left horizontal measurement, a center horizontal measurement and a right horizontal measurement. This data may be stored and may become part of the calculated lens distortion factors determined toward the end of the calibration cycle. It should be appreciated that the lower middle vertical location may be the final position to be measured and may be used to measure the radius for the 180° side, which may later be added to the radius of the 0° side to determine the arbor diameter.

[00131] Upon completion of the Y-Axis 2^nd 0° diameter determination, a Y-Axis 2^nd diameter determination is performed, as shown in operation block 514. The determination of the Y-Axis 2^nd diameter may be accomplished by moving the left arbor reference location to determine the location of the arbor relative to the right arbor reference and lens 138. A single measurement is taken in the center of field of view 230 to minimize distortion and is used to determine the radius and to compute the tangent correction factor that is used to compensate for any misalignment of the Y-Axis of positioning stage 128 with the Y-Axis of lens 138.

[00132] Once this has been completed, a Y-Axis 2^nd 180° diameter determination is performed, as shown in operational block 516, by configuring the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 to the 180° side (same X-Axis position) to measure the radius. The Y-Axis tangent correction factor is then determined, as shown in operation block 518. This compensates for a component that may be disposed between first arbor 132 and second arbor 134 in a non-level (i.e. horizontal) manner. Moreover, this may be accomplished by using the measurements taken at the right and left sides of the arbor and both the X and Y measurement information from the encoders and the image measurement tools are used to compute the tangent correction factor. It should be noted that all subsequent Y-Axis measurements include this compensation factor. All of the information obtained above may then be used to determine the lens distortion factor, as shown in operational block 520, which is then used for all subsequent X and Y measurements, including any light source and/or system stage positional distortions/errors (i.e. Abbe* stage errors).

[00133] Referring again to the predetermined component measurement algorithm 600 and upon completion of the predetermined calibration algorithm 500, the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be positioned back to arbor reference knee position 220 and component measurement algorithm 600 is initiated, as shown Figure 22. At this point, the Flank registration is performed, as shown in operational block 602. This may be accomplished by disposing the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 such that component 162 is positioned to an initial X and Y location approximately one half inch away from the arbor reference knee position 220 in the X direction and toward the component 162. The at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may then be configured such that the lower limit of the pitch diameter at the centerline of field of view 230 is approximated. A software measurement tool is then placed at the centerline to find the flank angel crossings at the centerline. The at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may then be configured to align the minor diameter with the left edge of field of view 230. All subsequent measurements rely on moving in pitch lead increments in the X-axis direction. It should be noted that the pitch lead increments are determined by the component selection and are published at the top of the Lead Standards readouts. It should be appreciated that, for threaded gages, the truncated measurements will be conducted at thread #2 and the full form measurements will be conducted at thread #6. The term 4X refers to the number of threads for the third lead measurement and indicates that it is being made over a span of four threads and the term /10 indicates that there are ten threads available on this component.

[00134] As above, once the flank registration has been performed, the 1^st full thread 0° side truncated measurements are conducted, as shown in operational block 604. This may be accomplished by configuring the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 to the first thread on the 0° side designated as the truncated thread location. This designation is dependent upon the thread numbers and thus upon the selection of component 162. Using the silhouette image data, processing device 152 then determines the minor radius, the major radius (for set plug only), the pitch radius, the lead pitch, the lead/trail flank angles and the included angles. The major radius is determined via the major diameter, which is a composite measurement based on the major radius of the 0° and corresponding 180° side of the threads. Thus, the major radius is determined by summing the individual measurements along the thread flat and dividing by the number of measurements collected. The number of measurement locations may be determined by taking 70% of the thread width, as determined by predetermined thread tables, and centering them on the center of the thread. This major radius average is then combined from both the 0° and the 180° sides to get the major diameter. For a gage, this process is performed for both truncated and full form locations and for a product, this process is performed only for the full form location.

[00135] It should be appreciated that all of the measurments taken by configuring the postioning stage 128 relative the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 may be conducted by configuring the at least one collimated light source 102, the sensing device 104 and/or the reflecting device 106 relative to the component, either individually or as a group. As such, the present invention contemplates that any element of the inspection system 100 may be configured to provide the proper perspective to conduct the any of the measurements disclosed and/or contemplated herein. It should also be appreciated that the inspection system 100 may be configured with digital recognition capability to automatically determine the component and/or component charateristic to be measured. For example, the component 162 may include a bar code (either printed and/or etched) that describes the type of component and/or the component characteristic to be measured.

[00136] It is contemplated that certain anomalies related to the centering of the component, the functional size of the component and excessive deviations from the true line may be present in the component measurements. To account for these anomalies, the following novel and unique algorithms can be applied to the inspection system (as disclosed herein and in U.S. Application Serial Nos. 1 1/391,521 and 1 1/502,678 and U.S. Patent Serial No: 7,227,163, the contents and disclosures of which are incorporated herein by reference in their entireties). It is contemplated that these algorithms can be applied to an inspection system where the component to be measured is moved into place for measurements or to an inspection system where the components of the inspection system (i.e. mirrors, camera, light source, etc) are moved into place for measurements relative to the component.

[00137] To address and account for excessive deviations from true line measurements of the threaded component, various parameters of the threaded component measurements (as desired) may be 'smoothed', where outlier measurement values are removed & the remaining measurement values are averaged (single or multiple averages may be obtained as desired). This operation may be repeated as desired. To accomplish this task, regression analysis may be used to obtain final smoothing data which accounts for these deviations and may include one or more of:

1) Conducting a standard least square linear regression analysis;

2) Conducting a q-trimmed linear regression analysis; and

3) Conducting a resistant regression procedure; where, the terminal residuals (outliers) outside of about ± 2 sigma standard deviation may be generated and the refits may be generated or measured. It is contemplated that continuous and/or repeated measurements may be made as desired. Also, other sigma standard deviation values may be used responsive to a desired accuracy. For example, a ± 10 sigma standard deviation or a ± 0.2 sigma Standard deviation may be used.

[00138] Accordingly, one embodiment of a method for removing excessive deviations from the "true line" may include generating and fitting a least squares line by minimizing

∑ ^®*(Λ - (« + K))² .

Where, a is the intercept of b, b is the determined/theoretical slope (can be estimated, calculated or measured), k is the number of values generated, X_{k and}y_k are the residuals (outliers) for each coordinate pair, and w_k is the included/excluded least square lines fit, where the values of w_k will be either zero (excluded) or one (included). The theoretical estimates for the slope b and the intercept a are then determined as follows,

where, x and y are the means of the x and y coordinates of where the measurements were taken and a and b are the estimates of a and b. From this estimate, the residuals for each of the coordinate pairs (x_k, y_k) may be calculated using,

h = y« - (^a-+ ^{b χ}k ) -

This is the amount by which the data points differ from the corresponding points predicted to lie on the line and r(k) is the residual for each of the coordinate pairs x_k, y_k. The residuals may be sorted from lowest to highest (or highest to lowest if desired) as given by, r, < r₂ < .... < /^•„ .

These values may be trimmed by identifying those points whose residuals have the highest absolute values and either remove them or weight them using a weighting variable w, where w may be responsive to the measurements taken and acceptable repeatability and accuracy tolerances. For example, if the weighting variable w is set to w_k=0 for the points to be trimmed this would effectively make the acceptable repeatability and accuracy tolerances equal to 0. Once this is done, refit the least squares line and use that refit line to determine the required parameters for the product or gage. Although as many as approximately 30% of the points may be trimmed, typically only about 5% - 10% of the points may be trimmed (depending on the surface finish of the component) prior to the refit of the least squares line. [00139] An alternative approach also involves fitting the least squares line and calculating the residuals. However, this approach involves trimming the residuals outside of about 2 or 2.5 standard deviations as given by, where n is the number of residuals. By using a two (2) standard deviation criterion, approximately about 5% of the data may be trimmed and the line can be refit by using the least squares estimates on the reduced (trimmed) data set.

[00140] Accordingly, in both of the above approaches, the algorithm can be simply stated as,

1) Fit the line to original data generated in accordance with the thread profile; a. Calculate residuals; b. Sort residuals; c. Trim data set; i. Fit line to trimmed data; ii. Calculate new residuals; iii. Sort new residuals; iv. Trim new data set; v. Repeat as desired or necessary; and

2) Compute screw thread geometric parameters using the re-trimmed data set (e.g. flank angles (leading, trailing & included), leads, major diameter, minor diameter & pitch diameter).

[00141] Referring to Figure 31, a block diagram illustrating a method 1100 for accounting for excessive deviations from the true line measurements of a threaded component by smoothing at least one parameter (individually or together) of the threaded component measurement(s) (as desired) is shown and includes fitting a least squares line to original data generated responsive to the thread profile of the threaded component, as shown in operational block 1102. The residuals are then determined as discussed herein and sorted into a new data set, as shown in operational block 1104. The new data set is then trimmed by fitting a second least squares line to the new data set, as shown in operational block 1106 and determining and sorting new residuals, as shown in operational block 1108. It is contemplated that one or more of the operational blocks 1 102-1 108 may be repeated as many times as desired. The 'adjusted' (new) screw thread geometric parameters are then determined using the re-trimmed data set, as shown in operational block 1110.

[00142] It should be appreciated that the above approaches can be applied to all measurements of the component including the major diameter, the pitch diameter, lead, angles, minor diameter, and helix variation. It is contemplated that, rather than using a least squares fit approach, another approach may use a minimum absolute deviation fit, where it is minimized by, n Jt=I

Additionally, it is also contemplated that an orthogonal least squares approach could also be used, i.e. measure the deviations perpendicular to the screw thread flank. However, the calculations for this approach are more complex. It should be appreciated that the full data set should be retained and each point referenced by whether it is retained or trimmed. In general, the higher the standard deviation of the residuals, the lower the quality of the screw thread.

[00143] In accordance with the invention, the functional size (f_s) of a component is the measurement of the pitch diameter plus the cumulative effect of the profile variations (lead, angle, helical path deviation). One method for accounting for deviations in the functional size of the threaded product or gage or portions of measurements of the threaded product or gage is described hereinafter and includes determining the functional size f_s of the product or gage responsive to, f_s = pd + L(HP) + A,

where, pd = actual measured pitch diameter; avg = (leading flank angle + trailing flank angle)/2; std = 30 degrees standard flank angle (which may be given in deg or rad);

HP = Helical Path; p = specified pitch distance = IfTPl (Threads per Inch); dp = error in pitch distance = error in lead assuming 1 start thread (may be neg or pos);

L = axial travel advance per unit rotation; and

A = I 1.5 * p * tan(avg - std) |, (where 1 1 means absolute value); Accordingly, pd is the diameter of the cylinder that passes through the thread profile where the thread groove and the thread ridge are equal on the 0° side and the 180 ° side of the component parallel to the axis of the thread. Essentially, the functional size (f_s) may be represented by the value of the pitch diameter plus the cumulative effect of all of the thread profile variations. Accordingly, it should be appreciated that if there is no error (i.e. dp=0), then the f_s=pd. However, if an error is present (i.e. dp=±) then the f_s=pd+L+A, where pd = pitch diameter of the thread profile, L= lead error of the thread profile and A=angle error of the thread profile.

[00144] Referring to Figure 32, a block diagram illustrating a method 1200 for determining the functional size f_s of a product or gage in accordance with one embodiment of the invention is shown and includes determining the actual pitch diameter pd, as shown in operational block 1202. The average flank avg is determined, as shown in operational block 1204, where avg is the sum of the leading flank and the trailing flank divided by 2. The standard flank angle std, the specified pitch distance p and the error in pitch distance dp is determined, as shown in operational block 1206, where the standard flank angle is 30 degrees (may be given in rads or degs), the specified pitch distance is the threads per inch and the error in pitch distance is the error in lead assuming a 1 start thread (may be neg or pos). The lead error of the thread profile L is determined, as shown in operational block 1208, and is given axial travel advance per unit rotation. The angle error A (deviation from 30°) of the thread profile is determined, as shown in operational block 1210, and is given by | 1.5 * p * tan(avg - std) |, (where | | means absolute value). The functional size f_s is then determined, as shown in operational block 1212, and is given as the sum of the pitch diameter pd of the thread profile, the lead error L of the thread profile and the angle error A of the thread profile.

[00145] In accordance with the invention, in making measurements of a product (or gage), it is important to make sure that the product or gage is as straight as possible relative to the lens system of the inspection system. Any deviation from a straightly aligned product or gage may have an adverse affect on the measure of the component. Accordingly, one embodiment of a method for centering a product or gage in an inspection system is described herein. It is contemplated that the centering algorithm can be applied to an inspection system where the component to be measured is moved into place for measurements or to an inspection system where the component of the inspection system (i.e. mirrors, camera, light source, etc) are moved into place for measurements relative to the component. [00146] Referring to Figure 33, a block diagram 1300 illustrating one embodiment of a method for accounting for misalignment of a component using a centering algorithm is shown. Once the product or gage is staged or disposed in the measuring device, a centerline value is determined, as shown in operational block 1302. This may be accomplished by taking a measurement of the product or gage at a first point on the 0° side of the product or gage (preferably on the longest threaded side first, but other locations are also contemplated). A measurement is also taken at the first point on the 180° side of the product or gage (again, preferably on the longest threaded side, but other locations are also contemplated). The center point at the first point is then determined, as shown in operational block 1304, by subtracting these measurement values and dividing by two (2). This step is repeated for at least one other point (for both 0° side and 180° side) along the product or gage, as shown in operational block 1306 and operational block 1308, preferably at the other end of the product or gage. A centerline of the product or gage is then established by projecting a line between the center point of the first measured center position and the center point of the second measured center position, as shown in operational block 1310. It should be appreciated that if more than two center points along the product or gage are used, then a centerline of the product or gage may be determined by using a line of best fit between the center points of the first point, the second point, the third point, etc.

[00147] It should be appreciated that the measurements described hereinabove for lens distortion analysis, predetermined calibration algorithm 500, predetermined component measurement algorithm 600 and/or R&R algorithm 700 may be accomplished by examining the image data for pixel intensity. This allows inspection system 100 to locate and record known positions on lens 138, first arbor 132, second arbor 134 and/or component 162 as data points. Using these data points, the physical characteristics of lens 138, first arbor 132, second arbor 134 and/or component 162 may be calculated via any method suitable to the desired end purpose, such as geometric/trigonometric relations, estimations and/or predictions.

[00148] In accordance with an exemplary embodiment, it is contemplated that multiple measurements may be made at each of the measurement locations in a manner responsive to predetermined component thread specifications. Moreover, the image data may be processed to include a plurality of discrete pixel elements. Processing device 142 then conducts each of the measurements by examining each pixel of the plurality of discrete pixel elements to determine the physical characteristics of component 154 as discussed hereinabove. It is further contemplated that image data may be displayed via any display device suitable to the desired end purpose, such as a paper printout, a computer screen, a television, a plasma display and/or a Liquid Crystal Display (LCD). Although the component physical characteristics are determined by processing the image data as discussed hereinabove, the component physical characteristics may be determined by processing the image data using any device and/or method suitable to the desired end purpose. Inspection system 100 may also be operated and/or monitored via a network connection, such as a wireless network (cellular, pager, RP), Local Area Network, Wide Area Network, Ethernet and/or Modem.

[00149] It is contemplated that processing device 152 may store image data and measurement results in a data storage device and/or a volatile memory of processing device 152 (e.g. RAM). It should also be noted that image data may be stored in a volatile and/or a non-volatile memory location which may be disposed in any location suitable to the desired end purpose, such as a remote server. In addition, the data storage device may be used to store individual component data and/or group component data which may be specific to a desired purpose, such as data for a specific user, component part and/or a specific end user device, wherein the component data may include a large range of information, such as user specific data and/or component part history data.

[00150] In accordance with an exemplary embodiment, inspection system 100 may be a self- calibrating and automated for inspection of multiple components. Moreover, inspection system 100 allows for non-contact measurements which reduce and/or eliminate high inspection costs, operator feel, fatigue, uncertainties and/or error. Inspection system 100 allows for the generation of automatic certificates and information output files. Moreover, inspection system 100 includes built-in repeatability and reliability (R&R) qualification and testing programs and allows for an extremely fast measurement cycle. The measurement and reporting cycles are typically performed in less than two minutes duration. Furthermore, inspection system 100 has an accuracy of about 0.000020 or less. This could never be realized using the current "Attributes" or variables measuring system. Also, inspection system 100 is about 25 times faster than using an "Attributes" or variables measuring system, which will only measure one of the multiple component characteristics required for inspection to satisfy current specifications.

[00151] A machine-readable computer program code and/or a medium encoded with a machine-readable computer program code for measuring the characteristics of component 162 using inspection system 100, the code and/or medium including instructions for causing a controller to implement a method including operating inspection system 100, wherein inspection system 100 includes collimated light source 102, a sensing device 104 optically communicated with collimated light source 102 and processing device 152, wherein processing device 152 is communicated with the sensing device 104, disposing component 162 such that component 162 is associated with inspection system 100, positioning component 162 such that component 162 is disposed to partially impede the optical communication between the sensing device 104 and the collimated light source 102, operating the collimated light source 102 such that a collimated light beam is incident upon component 162 to cause a silhouette of component 162 to be received by the sensing device 104, wherein the sensing device 104 generates image data responsive to the silhouette, communicating the image data to processing device 152, processing the image data to determine desired characteristics of component 162 and displaying the characteristics to a user.

[00152] In accordance with an exemplary embodiment, the processing of Figures 12-13, Figure 19, Figures 22-23 and Figures 29-30 may be implemented by a controller disposed internal, external or internally and externally to inspection system 100. In addition, processing of Figures 12-13, Figure 19, Figures 22-23 and Figures 29-30 may be implemented through a controller operating in response to a computer program. In order to perform the prescribed functions and desired processing, as well as the computations therefore (e.g. execution control algorithm(s), the control processes prescribed herein, and the like), the controller may includes, but not be limited to, a processor(s), computer(s), memory, storage, register(s), timing, interrupt s), communication interface(s), and input/output signal interface(s), as well as combination including at least one of the foregoing.

[00153] The invention may be embodied in the form of a computer or controller implemented processes. The invention may also be embodied in the form of computer program code containing instructions embodied in tangible media, such as floppy diskettes, CD-ROMs, hard drives, and/or any other computer-readable medium, wherein when the computer program code is loaded into and executed by a computer or controller, the computer or controller becomes an apparatus for practicing the invention. The invention can also be embodied in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed by a computer or controller, or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein when the computer program code is loaded into and executed by a computer or a controller, the computer or controller becomes an apparatus for practicing the invention. When implemented on a general-purpose microprocessor the computer program code segments may configure the microprocessor to create specific logic circuits.

[00154] The discussion hereinafter applies to an inspection system 2000 for measuring the internal characteristics of an internally threaded article. An exemplary embodiment is described herein by way of illustration as may be applied to the measurement and inspection of internally threaded gages, products and components, such as nuts and other internally threaded components. However, while an exemplary embodiment is shown and described hereinbelow, it should be appreciated by those skilled in the art that the invention is not limited to the embodiment(s) and application(s) as described herein, but also to any component and/or measurement where accuracy in tolerance measurement is critical, such as gears, internal bores, integral plain cylindrical bores, internal threads, internal diameters and/or material composition and/or strength. Moreover, those skilled in the art will appreciate that a variety of potential implementations and configurations are possible within the scope of the disclosed embodiments.

[00155] In accordance with the invention, an inspection system is provided and may be used to inspect and measure internal characteristics of an internally threaded product (and/or gage, plain and/or threaded ring gage) using a measuring device, such as an optical triangulation probe which uses a Laser to map the surface being measured. In fact, the internal inspection may be used to inspect and measure the physical characteristics of most apparatus or structures having an internal surface and/or enclosure and is not limited to threaded/non-threaded products, working GO & NO GO ring gages and/or master threaded rings. In accordance with the present invention, the desired internal characteristics may include, but are not limited to, the Lead, Flank Angle (Included), Flank Angle (Leading), Flank Angle (Trailing), Pitch Diameter, Taper, Minor Diameter, Major Diameter, Major Diameter Clearance, Out-of-Round and/or Functional Size.

[00156] Referring to Figure 34, one embodiment of an internal inspection system 2000 is shown and includes a measuring probe 2002, a measuring probe collar 2004, a measuring probe locating device 2006, a measuring probe support device 2008, a processing device 2010 and a product retention device 2012. Although, the product retention device 2012 is illustrated and referred to herein as an electromagnetic device which is easily switched on and off to hold and release a product being inspected, the product retention device 2012 may be any type of product retention device 2012 suitable to the desired end purpose. For example, the product retention device 2012 may retain the product via friction, suction, clamps, clips, etc. This alternative type of product retention device would be useful in securely holding a non-metallic (plastic, ceramic, etc.) product. It is also contemplated that the product may simply rest on a surface without the aid of a retention device while being inspected.

[00157] In accordance with the invention, the measuring probe 2002 is shown as being an optical triangulation type probe having a Laser emitter/receiver portion 2014 that is capable of emitting and receiving a Laser beam with a measurement resolution of about 20 millionths of an inch and which is configured to emit a Laser beam having a spot size ranging from about one ten thousandths of an inch to about five ten thousandths of an inch. It should be appreciated that the resolution may be based, at least in part, upon the mirror configuration within the optical triangulation probe. The measuring probe 2002 may be communicated with the processing device 2010 via a fiber optic cable 2016 to communicate data (such as a surface map data and/or image data (shadow or picture)) between the measuring probe 2002 and the processing device 2010. It is contemplated that a signal (data) conditioning circuit may be associated (internally or externally) with the processing device 2010 to condition the signal before and/or after receipt of the data by the processing device 2010. Additionally, it is contemplated that the data may be transmitted to the processing device 2010 via a wireless method/device or via a hard-wired connection where the data is converted into electrical signals prior to being transmitted to the processing device 2010. Furthermore, the measuring probe collar 2004 may be provided to cover the measuring probe 2002 to ensure that there is a sufficient standoff distance between the measuring probe 2002 and the surface of the product being measured. It should be appreciated that although the measuring probe 2002 is shown and described herein as being an optical triangulation type probe that uses a Laser source, any type of measuring device which emits electromagnetic energy (all along the electromagnetic spectrum) and which is suitable to the desired end purpose may be used, such as non-Laser collimated light, optical, borescope, MASER, electron beam, etc.

[00158] The measuring probe locating device 2006 is supported by the measuring probe support device 2008 such that the measuring probe locating device 2006 can move the measuring probe 2002 into and out of the internal space of the product being measured. This measuring probe locating device 2006, which is disclosed herein as a ball slide unit, but which may be any locating device suitable to the desired end purpose (such as, for example, an electric or pneumatic positionable device), allows the measuring probe 2002 to be precisely located within the product and adjacent the surface being measured where the measuring probe locating device 2006 may be precisely controlled via the processing device 2010 or some other (external or internal) device. The product retention device 2012 is provided to securely hold and position the product being measured.

[00159] In accordance with one embodiment of the present invention, the internal inspection system 2000 operates as follows. Referring again to Figure 34, a threaded product/component 2018 (such as an internally threaded product or threaded ring) is positioned adjacent the product retention device 2012, where the component 2018 may be positioned via hand or via an automated device. The product retention device 2012 is operated to activate an electromagnet to magnetically hold the component 2018 stationary and securely against the surface of the electromagnet of the product retention device 2012. The measuring probe 2002 with the measuring probe collar 2004 positioned to cover the Laser emitter/receiver portion 2014 of the measuring probe 2002, is positioned within the cavity of the component 2018 (or area of the product/component to be measured) to be adjacent the product surface to be measured. This initial component orientation is referred to as the 0° position. Referring to Figure 35, once the measuring probe 2002 is positioned within the cavity of the product 2018, the product retention device 2012 is operated to cause the electromagnet to be deactivated (i.e. de-magnetized). This allows the product 2018 to be positioned onto the measuring probe collar 2004 of the measuring probe 2002. Accordingly, the product becomes 'centered' onto the measuring probe collar 2004 to be adjacent the product retention device 2012 (electromagnet).

[00160] The product retention device 2012 is then reactivated to cause the electromagnet to magnetize causing the product 2018 to be securely held in place against the electromagnet of the product retention device 2012 as shown in Figure 36. At this point the measuring probe 2002 may be withdrawn from the cavity of the product 2018, as shown in Figure 37 and the measuring probe collar 2004 may be positioned (at least in part) away from the Laser emitter/receiver portion 2014 to allow the Laser emitter/receiver portion 2014 to emit/receive Laser light, as shown in Figure 38a. It should be appreciated that the width of the collar 2004 may be sized to provide a standoff distance between the product surface to be measured and the measuring probe 2002 that is sufficient enough to allow the measuring probe 2002 to emit Laser light and receive the reflected (and/or refracted) Laser light from the surface of the component 2018 being sensed. This standoff distance may be dependent (at least in part) on the mirrors in the optical triangulation probe and/or the product itself. For example, in one embodiment the standoff distance may be equal to the distance between the minor diameter of the product and the measuring probe 2002.

[00161] It is contemplated that (as described above) the measuring probe 2002 may be removed from the cavity (at least in part) prior to removing the measuring probe collar 2004. Or the measuring probe collar 2004 may be removed (at least in part) while the measuring probe 2002 is still positioned within the cavity. Or the measuring probe 2002 may not include a measuring probe collar 2004, but rather that the standoff distance be determined and implemented by determining the location of the probe relative to the surface being measured and adjusting the standoff distance by moving either the probe 2002, the component 2018 or both of the probe 2002 and the component 2018. In accordance with one embodiment of the invention, this allows the proper positioning of the product 2018 relative to the measuring probe 2002. It is contemplated that the positioning of the measuring probe 2002 and/or measuring probe collar 2004 may be accomplished (at least in part) using the measuring probe locating device 2006 or a separate positioning device controlled in whole or in part via the processing device 2010 or via any other device/method suitable to the desired end purpose. It is also contemplated that multiple measuring probes 2002 (or one measuring probe 2002 having multiple emitter/receiver portions 2014) may be implemented and may be used to measure both the 0° position and the 180° position, as shown in Figure 38b. It is further contemplated that one or more probes (by rotating the probes in an annular fashion or by arranging the probes as a annular ring) may be used to simultaneously measure 360° (i.e. 0° to 360°) of the surface to generate a complete (or partial) surface map of the internal surface. In this case, the standoff distance may be determined and implemented as above or the probes 2002 may be positioned relative to each other for the proper standoff distance for a particular product 2018.

[00162] Referring to Figure 39, the measuring probe 2002 is positioned within the cavity of the product 2018 to be adjacent the surface to be measured and the measuring probe 2002 is operated such that the Laser light illuminates the surface of the product 2018 being measured. Typically, the measuring probe 2002 is initially positioned adjacent to the face of the product retention device 2012 so that the entire internal product surface can be measured as the measuring probe 2002 is being withdrawn from the cavity. However, it is contemplated that the measuring probe 2002 may be positioned partially within the cavity so that only a desired portion of the surface is measured. The measuring probe 2002 may then be withdrawn from the cavity (i.e. through the cavity toward the measuring probe locating device 2006) while the measuring probe 2002 is illuminating the surface being measured with Laser light, as shown in Figure 40a. The Laser light that is incident on the surface being measured 'bounces' off of the surface and is directed toward the measuring probe 2002 where at least a portion of the reflected Laser light is received by the probe 2002 as the measuring probe 2002 traverses the cavity. It should be appreciated that this measurement may also be accomplished by starting at the outer most point of the cavity and illuminating the surface as the measuring probe 2002 traverses the cavity toward the product retention device 2012. This Laser light received by the measuring probe 2002 allows a profile of the surface being measured (such as an internal threaded surface) to be generated as the measuring probe 2002 is pulled through the cavity of the product 2018 at a constant and/or variable speed which rate may be dependent and responsive to the desired data, such as a desired image quality/resolution. This process may then be repeated for other orientations of the product 2018 as desired, for example the 90°, 180° and/or 270° positions, as shown in Figure 40b.

[00163] It should be appreciated that in one embodiment, the optical triangulation probe that is being used as the measuring probe 2002 may operate by emitting a Laser beam which is incident upon the surface being measured. The reflection (or a portion of the reflection) of the Laser beam from the surface is received by the measuring probe 2002 thus allowing for the generation of a surface profile image (such as a shadow image). It is also contemplated that other frequencies of the electromagnetic spectrum (such as Radar, Masers, etc) may be used and/or that other measuring devices may be used, such as a camera which may be used in place of an optical triangulation probe to generate an image of the surface. It should be appreciated that all measurements and characteristics may then be generated using the same (or similar) methods and/or algorithms as discussed herein. For the internal measurements, the major diameter may be measured to assure clearance of maximum material conditions of the major diameter of external threads. It is further contemplated that the product may be associated with the product retention device 2012 using any method/device suitable to the desired end purpose, such as by hand or by a device configured to perform such a task. It is also contemplated that the components herein may be configured differently to obtain the desired end result. For example, although the measuring probe 2002 is illustrated as being movable and the product 2018 is illustrated as being stationary, it is contemplated that the measuring probe may 2002 be stationary and the product 2018 (or product retention device 2012) may be movable.

[00164] Referring to Figure 41, a block diagram illustrating one embodiment of a method 3000 for implementing the internal inspection system 2000 is shown and includes associating the product 2018 with the product retention device 2012 (via the electromagnet) and the measuring probe collar 2004 with the measuring probe 2002 to cover the emitter/receiver portion 2014, as shown in operational block 3002. The measuring probe 2002 is then positioned inside the cavity of the product 2018 to be measured to be adjacent with and/or against the face of the product retention device 2012, as shown in operational block 3004. The electromagnet of the product retention device 2012 is deactivated to let the 0° side of the product 2018 be located onto the measuring probe collar 2004 of the measuring probe 2002, as shown in operational block 3006. This aligns and centers the product and assures the proper standoff distance (which in this embodiment is the width of the measuring probe collar 2004). The electromagnet of the product retention device 2012 is reactivated to re-secure the product 2018 and to ensure that the proper standoff distance between the measuring probe 2002 and the product 2018 is achieved and maintained, as shown in operational block 3008, and the measuring probe collar 2004 is positioned away from (at least partially) the emitter/receiver portion 2014 of the measuring probe 2002, as shown in operational block 3010. The measuring probe 2002 is then moved within the cavity to traverse at least a portion of the cavity to measure the physical characteristics of the surface (such as threads) of the product 2018 for the 0° side (or both the 0° side and 180° side for a system with a double measuring probe 2002), as shown in operational block 3012. It is contemplated that the probe 2002 may be moved into and/or out of the cavity of the product 2018 (once or multiple times as desired) during surface measurement. Any or all of the above operations may be repeated as desired for the same or for other orientations of the product 2018 (180° side), as shown in operational block 3014.

[00165] In accordance with an exemplary embodiment, it is contemplated that multiple measurements may be made at each of the measurement locations in a manner responsive to component thread specifications or other factors. Moreover, the data may be processed to comprise a plurality of discrete pixel elements. The processing device 2010 may examine each pixel (or selected pixels) of the plurality of discrete pixel elements to determine the physical characteristics of the surface as discussed hereinabove. It is further contemplated that the data may be displayed (as an image or other output) via any display device suitable to the desired end purpose, such as a paper printout, a computer screen, a television, a plasma display and/or a Liquid Crystal Display (LCD). Although the component physical characteristics are determined by processing the data as discussed hereinabove, the component physical characteristics may be determined by processing the data using any device and/or method suitable to the desired end purpose. Inspection system 2000 may also be operated and/or monitored via a network connection, such as a wireless network (cellular, pager, RP), Local Area Network, Wide Area Network, Ethernet and/or Modem.

[00166] It is further contemplated that processing device 2010 may cause the data and/or measurement results to be stored in a data storage device and/or a volatile memory of the processing device 2010 (e.g. RAM). It should also be noted that the data may be stored in a volatile and/or a non-volatile memory location which may be disposed in any location suitable to the desired end purpose, such as a remote server. In addition, the data storage device may be used to store individual component data and/or group component data which may be specific to a desired purpose, such as data for a specific user, component part and/or a specific end user device, wherein the component data may include a large range of information, such as user specific data and/or component part history data.

[00167] It is further contemplated that the system 2000 may include a display device, such as a flat panel display device, for displaying obtained or resultant data (such as an image). Although the display device is described herein above as being a flat panel display, the display device may be any display device suitable to the desired end purpose. Additionally, although the processing device 2010 may be a computer system operating an MS Windows operating system (or higher version), the processing device 2010 may be any processing device suitable to the desired end puφose. Although measuring probe locating device 2006 may include a stage with a glass slide and a linear motor having crossed rollers with anti-creep technology, any measuring probe locating device 2006 suitable to the desired end purpose may be used. The linear motor may allow for sufficient travel in any direction to accomplish the desired measurement (for example, plus and minus five (5) inches of travel in any desired direction). Measuring probe locating device 2006 may also be configured to operate via a hardwired and/or a wireless controller and may be capable of supporting movement in the X, Y and/or Z axis, as shown in Figure 40b.

[00168] As is known, a component thread is a combination of a thread ridge and thread groove, typically of uniform section, that is produced by forming a groove with a helix on an external or internal surface of a cylinder or cone. Because the component thread is designed to operate in association with an opposing component thread, it is essential that certain key physical characteristics relating to thread size and thread form be tightly controlled. Deviation from acceptable tolerances of these key characteristics can result in catastrophic failure of the system and/or loss of life. As such, it is desirable to measure these thread size characteristics and thread form characteristics as accurately as possible. The thread size characteristics include the major diameter, the minor diameter, the functional diameter and the pitch diameter and the thread form characteristics include the pitch, the lead, the uniformity of helix angle, the flank angle and the included angle, each one of which is discussed in more detail herein.

[00169] Referring to Figure 42 and Figure 43, side sectional views of an internally threaded component 2018 is shown and discussed. The major diameter of the component is the diameter or width of an imaginary cylinder, called the major cylinder, whose surface would be parallel to the straight axis of the component and whose surface would bound the roots of an internal thread. As such, a threaded ring gage includes a clearance diameter and a threaded product includes a full form major diameter. The full form major diameter, for both an internally threaded gage and an internally threaded product, may be defined as a composite measurement responsive to the major radius (which may be defined as the distance between the component axis and one surface of the major cylinder or one half of the major diameter) measured on the 0° side of the full form threads and the major radius measured on the 180° side of the full form threads. The minor diameter of the component is the diameter of an imaginary cylinder, or minor cylinder, whose surface would be parallel to the straight axis of the component and whose surface would bound the crests of an internal thread.

[00170] The pitch of an internal thread having uniform spacing may be defined as the distance, measured parallel to the axis, between corresponding points on adjacent thread forms in the same axial plane and on the side of the axis. Thus, the pitch may be defined as the number of threads per inch (TPI) and the pitch distance may be defined as 1/TPI, wherein TPI is measured parallel to the thread axis, from a point on one flank to the corresponding point on the next available flank. The pitch diameter of the component is the diameter or width of an imaginary cylinder, called the pitch cylinder, whose surface would be parallel to the axis of the thread or component and whose surface would intersect the profile of a straight thread such that the width of the thread ridge and the thread groove are equal.

[00171] The lead may be defined as the axial distance moved by the component in relation to the amount of angular rotation, when a threaded component is rotated about its axis with respect to a fixed mating thread. Thus, the lead is the amount of axial travel when the threaded component is turned one full turn or 360° and pitch is the distance measured parallel to the axis from a point on one flank to the corresponding point on the adjacent flank. Any deviation in lead tends to decrease the functional diameter of the internal thread and rapidly consumes the allowed operating pitch diameter tolerance of a threaded component. A deviation in lead may result in non-engagement of a thread with its mating part at all but a few points. Thus, when the threaded parts are assembled, and torque is applied, the result is pressure being applied to only a few, and possibly only one pressure flank. As such, any deviation in lead may produce a non-engagement condition for some threads and cause a failure in engaging threads at the point of pressure flank engagement due to non-engagement.

[00172] The helical path deviation of a thread is a wavy deviation from a true helical advancement or a non-uniformity of helix angle. In a similar manner as the lead, a deviation in the helical path causes a decrease in the functional size of the internally threaded component in proportion to the amount of waviness. Thus, all of the statements that were made concerning a deviation in lead also apply to a deviation in helical path and similarly, a deviation of helical path may result in partial engagement of the thread flanks with the result that torque pressures may not be evenly distributed and may result in pre-load relaxation.

[00173] The included angle of a thread is the angle between the flanks of the thread measured in an axial plane. The flank angles are the angles between the individual flanks and the perpendicular to the axis of the thread measured in an axial plane. A flank angle of a symmetrical thread is commonly referred to as the half included angle or the half angle of a thread. A deviation in the flank angle may result in a failure of the thread when the product is exposed to line loads, when torque is applied or when vibration occurs. This is because an improper flank engagement may create an unevenly distributed pressure load along the flank rather than the pressure load being distributed evenly along the flank.

[00174] Other important physical characteristics of the component include the functional size diameter, the taper characteristic of the pitch cylinder and the out-of-roundness, all of which can generate a non-engagement condition. In fact, distortion or deviation from specifications of any of the physical characteristics discussed herein may cause varying degrees of non-engagement.

[00175] The functional, or virtual, diameter of an internal thread may be defined as the resultant size of the product thread taking into account the effect of lead, helical path deviation, flank angle deviation, taper and out-of-roundness. As such, it may be seen that the functional diameter is the pitch diameter of the enveloping thread of perfect pitch, lead and flank angles, having full depth of engagement, but that are clear at crests and roots, of specified lengths of engagement. For an internal thread, the functional diameter may be derived by subtracting the cumulative effects of deviations to the pitch diameter, including variations in lead and flank angles over a specified length of engagement. Thus, it should be clear that the effects of taper, out-of-roundness and surface defects may be positive or negative on the functional size of the internal threads.

[00176] The taper characteristic of the pitch cylinder is simply a tapering of the pitch cylinder of the thread. Thus, a tapered thread fails to give a complete thread engagement, which may lead to a product failure caused by uneven torque pressure conditions on pressure flanks and pre-load relaxation.

[00177] The out-of-roundness of the pitch cylinder, which is any deviation of the pitch cylinder from round, limits the thread engagement and allows for only line contact with the mating thread and typically includes two types of out-of-roundness: Multi-lobe or Oval.

[00178] With the desired physical characteristics of a threaded component to be measured explained hereinabove, an overall method for measuring these characteristics is provided and described hereinbelow. Furthermore, it is contemplated that each of the methods, calculations and algorithms described herein, may be performed via a system operator and/or via an automated system.

[00179] Once data for the surfaces being measured (i.e. the 0° and 180° sides of the threads) is obtained, the Flank angle may be determined. Using the data, the minor radius, the major radius, the pitch radius, the lead pitch, the leading/trailing flank angles and/or the included angles can be determined. The major radius may be determined via the major diameter, which is a composite measurement based on the major radius of the 0° and corresponding 180° side of the threads. Thus, the major radius can be determined by summing the individual measurements and dividing by the number of measurements collected. The number of measurement locations may be determined by taking 70% of the thread width, as given by thread tables, and centering them on the center of the thread. This major radius average may then be combined from both the 0° and the 180° sides to get the major diameter. The pitch diameter calculation, which is based on the leading and trailing angles, major diameter, pitch lead and crest width at the location in question, may be determined by the equation: PD=MD-(Cot(PL/2)-CW), where, PD is pitch diameter, MD is major diameter, PL is pitch lead and CW is crest width. The lead front measurement, which is responsive to the difference between the groove distance and the ridge distance along the leading/trailing/leading flanks may be determined by various known methods.

[00180] In an additional embodiment, the determination of the Pitch Diameter (PD) may include a Correction Factor (CF) to adjust for any aberrations that may be present in the data. Referring to Figure 44, for illustration purposes a symmetrically internally threaded object 4000 is shown having a plurality of threads 4002. The Pitch Diameter (PD) for the threaded object 4000 having thread grooves 4004 and thread ridges 4006 may be described simply as the distance between a point on the 0° side of the object and the 180° of the object where the width of the thread ridge, gi, and the thread groove, gι, are equal (See Figure 43). However, in some cases, as the Laser beam is reflected from the surface being measured, unwanted reflections may fall incident upon the sensing device of the measuring probe 2002 causing aberrations in the data. As such, the data generated may include data responsive to unwanted higher and/or lower order reflections and thus the physical characteristics of the object 4000, such as the Pitch Diameter (PD) may be skewed and inaccurate, as represented by the shadow image 4008.

[00181] To compensate for any aberrations of the shadow image 4008 within the image data, a Correction Factor (CF) may be generated and applied to the process for determining the Pitch Diameter (PD). As such, the Pitch Diameter (PD) may be represented by the equation:

PD Final ⁼ PD Observed ~ CF,

wherein PD_Finaι is the Pitch Diameter (PD) adjusted for any aberrations, PD_Observed is the Pitch Diameter (PD) as measured and containing any aberrations and CF is the Correction Factor (CF) representing any aberrations.

[00182] For example, as illustrated for internal threads, one embodiment for compensating for any aberrations includes generating a Correction Factor (CF) responsive to unwanted reflections or 'splash' and 'subtracting' the Correction Factor (CF) from the data generated by the sensing device, wherein the Correction Factor (CF) may be determined by parametrically representing one flank of a thread (i.e. the rear side of a thread ridge) in 3-D space having an x-axis, a y-axis and a z-axis as an embedding of a strip into a 2-D space having only the x-axis and the z-axis. Referring to Figure 45, for objects or components having symmetrical threads, using only two variables (r, t), a first point, r_1} representing the minor diameter of the thread on the x-z axis, and a second point, r₂, representing the major diameter of the thread on the x-z axis, is shown in the x-z plane connected via a straight line, K_x-1, which is drawn between the two points π and r₂. The variable R is the 2-D representation of the Pitch Diameter (PD) in the x-z plane and t is the flank angle which may be represented as the angle between the line K_x-Z drawn between the two points, ri and r₂, in the x-z plane and the projection K_x._y of the line K_x._z onto the x-y plane. Additionally, the variable L_x-Z is the lead angle of the thread and the variable m is the tangent of the flank angle, t. The variable r is a point on the x-z plane which represents the distance between the z-axis and a point on the line K_x-Z and thus may range from half of the minor diameter to half of the major diameter. As such, we can parameterize the above relationships using the following equations:

x = r cos (t), y = r sin (t), and

Z = mr +Lt/2n.

[00183] This embedding can then be projected onto the x-z plane by using the equations:

x = r cos (t), and Z = mr + Lt/2n,

to obtain the determinant of the Jacobian matrix, wherein the Jacobian matrix is defined by:

&1 dz\ dx\ dxn

J(x\....xn) = dzn dzn dx\ dxn

As is well known, the Jacobian matrix is the matrix of all first-order partial derivatives of a vector-valued function and may be representative of the 'best' linear approximation to a differential function near a given point. Thus, using the equations as derived hereinabove,

x = r cos (t), and z = ntr + Lt/2n,

the Jacobian matrix J(x_t...X_n) may be represented as:

Solving the Jacobian matrix J(X₁...X_n) to find the set of points of the shadow image (i.e. ribbon) on the x-z plane gives the following:

J = ((L 12π) cos(0 + ™r sin(t)) = 0 ,

where, r = -(L I(2πm \an(t))) .

[00184] Referring to Figure 46, if the value of R is set to half of the Pitch Diameter (PD) of the thread, the point on the projection of the ribbon (i.e. shadow image) that is directly to the "right" of the point where r=R and t=0 may be determined. This is a point on the ribbon that has the same z-coordinate as the Pitch Diameter (PD) point (x,y,z) = (R,0,mR) and thus, it can be seen that at the Pitch Diameter (PD) point (x,y,z), z = mR. Plugging z=mR into the equation for z gives the following:

Lt z = mR = mr +

(2πm)

Lt r = R -

(2πm)

and combining equation (1) with equation (2) gives the following: - L Lt

= R -

Inm tan(t) 2πm and

L + (2πmR - Lt) tan(/) = 0 ,

which must be solved for each given value of L, m and R. Having the flank angle, t, these equations may be solved to obtain r, wherein half of the displacement of the Pitch Diameter (PD) is the x-coordinate of the point on the ribbon minus the x-coordinate of the Pitch Diameter (PD) point (x,y,z) = (R,0,mR) or simply, r cos (t) - R. Thus, it should be appreciated that the Correction Factor (CF) may be assumed to be twice this amount and may be given by the equation:

CF = 2(r cos(0 - Λ) .

Thus, the Pitch Diameter for a symmetrically internally threaded object adjusted for any aberrations, PDpi_nai, may be determined by applying the Correction Factor (CF) above into equation (1) to give the following equation:

PD_Fim, = PD observed ~ 2(rCOs(t) - R),

In a similar fashion, for objects or components having asymmetrical threads, such as buttress threads, the methodology applied hereinabove may be used for both flanks (due to the asymmetry the calculations should be conducted for each flank). As such, a simple geometric argument using the above approach for both flanks may combine the two results in a kind of weighted average to give:

__„ (</l tan(al) + </2tan(α2))

Cr =

(tan(αl) + tan(α2))

wherein dl and d2 are the shadow corrections for the two flank angles treated separately as symmetrical internal threads and al and a2 are the respective flank angles. Given the above, the Pitch Diameter for an asymmetrically internally threaded object adjusted for any aberrations, PD_Finai, may be determined by applying the Correction Factor (CF) above into equation (1) to give the following equation:

(</l tan(αl) + </2 tan(a2)) r Upjnai - rU_Observed ; 7—

(tan(αl) + tan(α2))

[00185] Referring to Figure 47, a block diagram illustrating a high level method 5000 for measuring the physical characteristics of an internally threaded component using an inspection system 2000 is shown and includes associating an object with the inspection system 2000, as shown in operational block 5002. The inspection system 2000 is operated to cause the measuring probe 2002 to emit a Laser light beam which is incident upon a surface to be measured, as shown in operational block 5004, causing a reflected Laser beam to be at least partially incident upon the sensing device of the measuring probe 2002. In response initial data is generated/obtained. This initial data is processed to generate resultant data responsive to at least one of a plurality of physical characteristics of the component 2018, as shown in operational block 5006, wherein the initial data may be processed responsive to at least in part to the algorithm above to correct for any aberrations in the initial data. As discussed herein, the algorithm may be at least partially responsive to the type of component being measured. For example, if the object is an internally threaded object having symmetrical threads, then the predetermined algorithm may be at least partially responsive to the equation:

CF = 2(r COS(I) - R) ,

However, if the object is an internally threaded object having asymmetrical threads, then the predetermined algorithm may be at least partially responsive to the equation:

„ __, (d\ tan(βl) + dl tan(α2))

Cr =

(tan(αl) + tan(α2))

[00186] Referring to Figure 48, a block diagram illustrating a method 6000 for correcting aberrations in data generated by inspection system 2000 is shown and includes generating initial data via the inspection system 2000, as shown in operational block 6002, wherein the sensing device of the measuring probe 2002 generates initial image data responsive to the surface being measured and any aberrations included with the reflected Laser beam. The initial image data may then be processed to generate resultant data, as shown in operational block 6004. This may be accomplished by generating initial Pitch Diameter (PD) data from the initial data, as shown in operational block 6006. This initial Pitch Diameter (PD) data is then parameterized, as shown in operational block 6008, and solved via a Jacobian Matrix, J(xi....x_n), where the Jacobian Matrix, J(X₁....x_n), is solved responsive to a plurality of physical characteristics of the component to generate Correction Factor (CF) data, as shown in operational block 6010, wherein the plurality of physical characteristics may include at least one of the lead angle, the flank angle, the major diameter and the minor diameter. Once the Correction Factor (CF) data is determined, the initial Pitch Diameter (PD) data is processed responsive to the Correction Factor (CF) data to obtain the resultant Pitch Diameter (PD) data, as shown in operational block 6012. The multi thread lead, which is responsive to the distance between the lead front and the lead back measurements, the trailing angle and the included angle may be determined as known.

[00187] At this point, the 2^nd thread 0° side measurements, the 1^st full thread 180° side measurements may be conducted on the first full thread on the 180° side and the minor radius, the major radius, the pitch ra_dius and the lead pitch may be determined. The 2^nd thread 180° side measurements may be made on the second full thread on the 180° side and the major radius, pitch radius and lead pitch may be determined. The component values and limits may be updated and the results may be stored, displayed to a system operator and/or printed out.

[00188] To account for anomalies in the measurements as described herein, the following novel and unique algorithms can be applied to the invention as disclosed herein and in U.S. Application Serial Nos. 1 1/391,521 and 1 1/502,678 and U.S. Patent Serial No: 7,227,163, the contents and disclosures of which are incorporated herein by reference in their entireties.

[00189] For 'smoothing' various parameters of the internally threaded component measurements (as desired), the following regression analysis approach may be used to obtain final smoothing data and includes:

4) Conduct a standard least square linear regression analysis;

5) Conduct a q-trimmed linear regression analysis; and

6) Conduct a resistant regression procedure.

This approach may be conducted in whole or in part and in any order desired and suitable to the desired end result. The terminal residuals outside of ± 2 sigma standards may be generated and the refits may be generated. Accordingly, excessive deviations from the "true line" can be removed using at least one of two approaches as follows:

1) The first approach includes fitting a least squares line, which consists of minimizing,

It where, a is the intercept of b, b is the determined/theoretical slope (can be estimated), k is the number of values generated, X_{k and}y_k are the residuals for each coordinate pair, w_k is included/excluded least square lines fit, where the values of w_k will be either zero (excluded) or one (included). Then determine the theoretical estimates for the slope b and the intercept a as follows,

ύ = ~^ = _n ^■ — , a = y -~ bx,

2__^ w_k {x_k - x) Jt=I where x~and y"are the means of the x and y coordinates and a and b are tne estimates of a and b. From this estimate, the residuals may be calculated for each coordinate pair (x_k, y_k) using,

This is the amount by which the data points differ from the corresponding points predicted to lie on the line and r(k) is the residual for each coordinate pair x_k, y_k. Sort the residuals from lowest to highest (or highest to lowest if desired) as given by,

These values may be trimmed by identifying those points whose residuals have the highest absolute values and either remove them or weight them using a weight variable w. One way to generate the weight variable w is by setting w_k=0 for the points to be trimmed. Once this is done, the least squares line may be refit and used to determine the required parameters for the internally threaded component. Although as many as about 30% of the points may be trimmed, typically only about 5% - 10% of the points are trimmed prior to the refit of the least squares line.

[00190] The second approach may include:

2) fitting the least squares line and calculating the residuals. However, this approach involves trimming those residuals outside of about 2 or 2.5 standard deviations given by, where n is the number of residuals,

By using a two (2) standard deviation criterion, approximately about 5% of the data will be trimmed and the line can be refit by using the least squares estimates on the reduced data set. In both of the above approaches, the algorithm can be simply stated as,

3) Fit line to original data generated in accordance with the thread profile; a. Calculate residuals; b. Sort residuals; c. Trim data set; i. Fit line to trimmed data; ii. Calculate new residuals; iii. Sort new residuals; iv. Trim new data set;

4) Compute screw thread geometric parameters using re-trimmed data set.

[00191] To account for anomalies in the measurements as described herein, the following novel and unique algorithms can be applied to the invention as disclosed herein and in U.S. Application Serial Nos. 1 1/391,521 and 1 1/502,678 and U.S. Patent Serial No: 7,227, 163, the contents and disclosures of which are incorporated herein by reference in their entireties. It should be appreciated that the above approaches can be applied to all measurements including the major diameter, the pitch diameter, lead, angles, minor diameter, and helix variation. It is contemplated that, rather than using a least squares fit, another approach may use a minimum absolute deviation fit, where it is minimized by, 2Z^Wk ^^{k ~} tø + ^k**⁾! ^•

It is also contemplated that an orthogonal least squares approach could also be used, i.e. measure the deviations perpendicular to the screw thread flank. However, the calculations for this approach are more complex. It should be further appreciated that the full data set should be retained and each point referenced by whether it is retained or trimmed. In particular, the higher the standard deviation of the residuals, the lower quality the screw thread.

[00192] To account for deviations in the functional size of the internally threaded component 2018, the following algorithm may be used:

- Let avg = (leading flank + trailing flank)/2;

- Let std = 30 degrees standard flank angle (which may be represented in degrees or radians);

- Let p = specified pitch = 1/TPI (Threads per Inch);

- Let dp = error in pitch = error in lead assuming 1 start thread (this can be positive or negative);

- Let pd = actual measured pitch diameter;

- Let L = I dp/tan(avg) | (absolute value may or may not be used as desired);

- Let A = I 1.5 * p * tan( avg - std) |, where 1 1 means absolute value;

- Let fs = functional size.

Thus, the functional size (fs) is represented by the value of pitch diameter plus the cumulative effect of all thread profile variations and is given by, fs = pd + L + A.

Accordingly, it should be appreciated that if there is no error (i.e. dp=0), then fs=pd. However, if error is present (i.e. dp=±) then fs=pd+L+A, where pd = pitch diameter of the thread profile, L= lead error of the thread profile and A=angle error of the thread profile.

[00193] In accordance with an exemplary embodiment, inspection system 2000 may be a self- calibrating and automated system for inspection of multiple components in a single fashion or an assembly line fashion. Moreover, inspection system 2000 allows for non-contact measurements which reduce and/or eliminate high inspection costs, operator feel, fatigue, uncertainties and/or error. Inspection system 2000 allows for the generation of automatic certificates and information output files. Moreover, inspection system 2000 may include built-in repeatability and reliability (R&R) qualification and testing programs and allow for an extremely fast measurement cycle.

[00194] A machine-readable computer program code and/or a medium encoded with a machine-readable computer program code for causing a controller to implement the methods disclosed herein (in whole or in part) via the inspection system 2000 is also provided, where the processing of the methods may be implemented via a controller that is disposed internal to, external to or internally and externally to the inspection system 2000. Thus, the controller may operate in response to a computer program where in order to perform the prescribed functions and desired processing, as well as the computations therefore (e.g. execution control algorithm(s), the control processes prescribed herein, and the like), the controller may includes, but not be limited to, a processor(s), computers), memory, storage, register(s), timing, interrupt(s), communication interface(s), and input/output signal interface(s), as well as combination comprising at least one of the foregoing.

[00195] The invention may be embodied in the form of a computer or controller implemented processes. The invention may also be embodied in the form of computer program code containing instructions embodied in tangible media, such as floppy diskettes, CD-ROMs, hard drives, and/or any other computer-readable medium, wherein when the computer program code is loaded into and executed by a computer or controller, the computer or controller becomes an apparatus for practicing the invention. The invention can also be embodied in the form of computer program code, for example, whether stored in a storage medium, loaded into and/or executed by a computer or controller, or transmitted over some transmission medium, such as over electrical wiring or cabling, through fiber optics, or via electromagnetic radiation, wherein when the computer program code is loaded into and executed by a computer or a controller, the computer or controller becomes an apparatus for practicing the invention. When implemented on a general-purpose microprocessor the computer program code segments may configure the microprocessor to create specific logic circuits.

[00196] While the invention has been described with reference to an exemplary embodiment, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. For example, although the internal inspection system is discussed herein in reference to a Laser frequency source, other measuring sources/devices (optical or non-optical) or combination of sources/devices suitable to the desired end purpose may be used, such as but not limited to collimated light, x-rays, cameras, borescope, MASER, electron-microscopes, etc... In addition, modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiments) disclosed herein as the best mode contemplated for carrying out this invention.

Claims

What is claimed is:

1. An inspection system, comprising: a collimated light source defining a source optical path, said collimated light source being operable to cause a collimated light beam to propagate along said source optical path; a sensing device defining a sensor optical path, said sensor optical path being substantially perpendicular to said source optical path; a positioning device including a positioning device stage; a reflecting device, wherein said reflecting device is disposed on said positioning device to be within said source optical path to receive said collimated light beam, said reflecting device causing a reflected collimated light beam to propagate along said sensor optical path to said sensing device; a retention mount, where a portion of said retention mount is disposed within said sensor optical path such that when a component is retained within said retention mount, said component blocks at least a portion of said reflected collimated light beam such a silhouette is generated and incident upon said sensing device, wherein said sensing device generates data responsive to said silhouette; and at least one processing device, wherein said at least one processing device is communicated with said sensing device to receive at least a portion of said data, wherein said processing device is configured to process said data responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm.

2. The inspection system of claim 1, wherein said smoothing algorithm includes fitting a least squares line responsive to n

∑ ^β>*(Λ - (a + δ**))² . k=\ where a is an intercept of b, b is a slope, k is a number of values generated, X_k a_ndy_k are residuals for each coordinate pair, and w_k is a least square lines fit.

3. The inspection system of claim 2, wherein said intercept a and slope b are responsive to,

where , x and y are the means of x and y coordinates and a and b are estimates of a and b.

4. The inspection system of claim 2, wherein said residuals for each coordinate pair (X_{k and} yi_t) are responsive to,

Λ Λ rk = y_k - (^a-^{+ b χ}k ) where r(k) is the residual for each of the coordinate pairs X_k, y_k-

5. The inspection system of claim 1, wherein said functional size algorithm is responsive to, f, = pd + L + A, where f_s is functional size of said component, pd is pitch diameter of thread profile of said component, L is lead error of a thread profile of said component and A is angle error of said thread profile of said component.

6. The inspection system of claim 5, wherein said lead error of a thread profile L is responsive to,

L = axial travel advance per unit rotation, and avg = (leading flank + trailing flank)/2, where dp is error in pitch distance.

7. The inspection system of claim 5, wherein said lead error of a thread profile L is responsive to,

L = I axial travel advance per unit rotation |, and avg = (leading flank + trailing flank)/2, where dp is error in pitch distance.

8. The inspection system of claim 5, wherein said angle error of a thread profile A is responsive to,

A = | 1.5 * p * tan(avg - std) I, where p is a specified pitch distance and std is standard flank angle.

9. A method for measuring physical characteristics of a component using an inspection system including a light source, a sensing device, a reflecting device, and a retention mount, at least one of which is movably associated with the inspection system, the method comprising: associating a component with the inspection system such that said component is disposed within the retention mount; operating the inspection system to cause the light source to emit a collimated light beam propagating along a source optical path; reflecting said collimated light beam via the reflecting device to cause a reflected collimated light beam to propagate along a sensor optical path such that the reflected collimated light beam is incident upon the component to produce a component silhouette which is incident upon the sensing device; generating image data responsive to said component silhouette; and processing said image data to generate resultant data responsive to at least one of a plurality of physical characteristics of the component, wherein said resultant data is responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm.

10. The method of claim 9, wherein said smoothing algorithm includes, fitting a least squares line of said component to at least a portion of said image data generated responsive to said component; determining a plurality of residual data points responsive to said least squares line; and sorting said plurality of residual data points.

1 1. The method of claim 10, wherein said smoothing algorithm further includes, trimming said plurality of residual data points by fitting a residual least squares line to said plurality of residual data points; determining a second plurality of residual data points responsive to said residual least squares line; sorting said second plurality of residual data points; and determining screw thread geometric parameters responsive to said second plurality of residual data points.

12. The method of claim 9, wherein said functional size algorithm includes, determining a pitch diameter of said component, an average flank angle (avg) of said component, a specified pitch (p) of said component, and an error in pitch distance (dp) of said component; and determining a lead error (L) of a thread profile of said component, wherein said lead error (L) is responsive to said error in pitch distance (dp) of said component and said average flank angle (avg) of said component and is given by at least one of,

L = I axial travel advance per unit rotation |, and .

L = axial travel advance per unit rotation.

13. The method of claim 12, wherein said functional size algorithm further includes, determining an angle error (A) of a thread profile of said component, wherein said angle error (A) is responsive to said specified pitch distance (p) of said component and said average flank angle (avg) of said component and is given by

A = | 1.5 * p * tan(avg - std) |.

14. The method of claim 9, wherein said centering algorithm includes, determining a centerline value for each of a plurality of locations along said component retained within said retention mount; and identifying a centerline by projecting a line connecting said centerline value for each of said plurality of locations.

15. The method of claim 14, wherein if said plurality of locations is greater than two, then said centerline may be established by identifying a line of best fit between said centerline value for each of said plurality of locations.

16. A machine-readable computer program code, the program code including instructions for causing a controller to implement a method for measuring physical characteristics of a component using an inspection system including a light source, a sensing device, a reflecting device, and a retention mount, at least one of which is movably associated with the inspection system, the method comprising: associating a component with the inspection system such that said component is disposed within the retention mount; operating the inspection system to cause the light source to emit a collimated light beam propagating along a source optical path; reflecting said collimated light beam via the reflecting device to cause a reflected collimated light beam to propagate along a sensor optical path such that the reflected collimated light beam is incident upon the component to produce a component silhouette which is incident upon the sensing device; generating image data responsive to said component silhouette; and processing said image data to generate resultant data responsive to at least one of a plurality of physical characteristics of the component, wherein said resultant data is responsive to at least one of a smoothing algorithm, a functional size algorithm and a centering algorithm.

17. The method of claim 16, wherein said smoothing algorithm includes, fitting a least squares line of said component to at least a portion of said image data generated responsive to said component; determining a plurality of residual data points responsive to said least squares line; sorting said plurality of residual data points; trimming said plurality of residual data points by fitting a residual least squares line to said plurality of residual data points; determining a second plurality of residual data points responsive to said residual least squares line; sorting said second plurality of residual data points; and determining screw thread geometric parameters responsive to said second plurality of residual data points.

18. The method of claim 16, wherein said functional size algorithm includes, determining a pitch diameter of said component, an average flank angle (avg) of said component, a specified pitch (p) of said component, and an error in pitch distance (dp) of said component; and at least one of, determining an angle error (A) of a thread profile of said component, wherein said angle error (A) is responsive to said specified pitch distance (p) of said component and said average flank angle (avg) of said component and is given by

A = I 1.5 * p * tan(avg - std) |, and determining a lead error (L) of a thread profile of said component, wherein said lead error (L) is responsive to said error in pitch distance (dp) of said component and said average flank angle (avg) of said component and is given by at least one of,

L = axial travel advance per unit rotation, and avg = (leading flank + trailing flank)/2.

19. The method of claim 16, wherein said centering algorithm includes, determining a centerline value for each of a plurality of locations along said component retained within said retention mount; and identifying a centerline by projecting a line connecting said centerline value for each of said plurality of locations, wherein if said plurality of locations is greater than two, then said centerline may be established by identifying a line of best fit between said centerline value for each of said plurality of locations.

20. The machine-readable computer program code of Claim 16, wherein said machine- readable computer program code is encoded onto a computer-readable storage medium.

21. An inspection system for measuring the threaded surface of an internally threaded component, the inspection system comprising: at least one measuring probe, wherein said at least one measuring probe includes an emitter and a receiver and is sized and shaped to be positionable adjacent at least a portion of the threaded surface at an offset distance, wherein said emitter is configured to emit electromagnetic energy that is incident upon the threaded surface to generate reflected electromagnetic energy responsive to the threaded surface and wherein said receiver is configured to receive at least a portion of said reflected electromagnetic energy and generate threaded surface data; and a processing device, wherein said processing device is in signal communication with said measuring probe to receive said threaded surface data and process said threaded surface data to determine physical characteristics of the threaded surface.

22. The inspection system of claim 21, wherein said at least one measuring probe includes two or more measuring probes.

23. The inspection system of claim 21, further comprising a measuring probe locating device associated with said measuring probe, wherein said measuring probe locating device is controllably configurable to allow said measuring probe traverse along at least a portion of the threaded surface at said offset distance.

24. The inspection system of claim 21 , further comprising a measuring probe collar, wherein said measuring probe collar is configurable between a first configuration and a second configuration and wherein at least a portion of said measuring probe collar includes a collar width, said collar width being substantially equal to said offset distance.

25. The inspection system of claim 24, wherein when said measuring probe collar is in said first configuration, said measuring probe collar is positioned to cover said emitter and said receiver and when said measuring probe collar is in said second configuration, said measuring probe collar is positioned away from said emitter and said receiver.

26. The inspection system of claim 21, further comprising a component retention device, said component retention device being configurable to securely position the internally threaded component.

27. The inspection system of claim 26, wherein the component retention device includes an electromagnetic device, wherein when said electromagnetic device is activated the internally threaded component is securely retained against a component retention device surface.

28. The inspection system of claim 21, wherein said processing device is in signal communication with said measuring probe via at least one of a hardwire connection, a fiber optical connection or a wireless connection.

29. The inspection system of claim 21, wherein said threaded surface data is processed responsive to at least one of a smoothing algorithm and a correction factor.

30. The inspection system of claim 29, wherein said smoothing algorithm includes fitting a least squares line responsive to n k=\ where a is an intercept of b, b is a slope, k is a number of values generated, X_k a_ndy_k are residuals for each coordinate pair, and w_k is a least square lines fit.

31. The inspection system of claim 30, wherein said intercept a and slope b are responsive to, where , x and y"are the means of x and y coordinates and a and b are estimates of a and b.

32. The inspection system of claim 30, wherein said residuals for each coordinate pair (x_{k aπd} Y_k) are responsive to,

Λ Λ rk = y_k - (^a-+ b^χ _k) where r(k) is the residual for each of the coordinate pairs x_k, y_k.

33. The inspection system of claim 29, wherein said correction factor is responsive to, f_s = pd + L + A, where f_s is functional size of the internally threaded component, pd is pitch diameter of the thread profile of the internally threaded component, L is lead error of a thread profile of the internally threaded component and A is angle error of said thread profile of the internally threaded component.

34. The inspection system of claim 33, wherein said lead error of a thread profile L is responsive to,

L = axial travel advance per unit rotation, and avg = (leading flank + trailing flank)/2, where dp is error in pitch distance.

35. The inspection system of claim 29, wherein said angle error of a thread profile A is responsive to,

A = | 1.5 * p * tan(avg - std) I, where p is a specified pitch distance and std is standard flank angle.

36. A method for measuring the threaded surface of an internally threaded component using an inspection system, wherein the inspection system includes a measuring probe having an emitter and a receiver and is sized and shaped to be positionably adjacent at least a portion of the threaded surface at an offset distance, wherein the emitter is configured to emit electromagnetic energy incident upon the threaded surface to generate reflected electromagnetic energy responsive to the threaded surface and wherein the receiver is configured to receive at least a portion of the reflected electromagnetic energy and generate threaded surface data, the method comprising: associating the internally threaded component with the inspection system via an electromagnetic; positioning the measuring probe inside a cavity of the internally threaded component; deactivating said electromagnet to cause the internally threaded component to be positioned relative to measuring probe such that an offset distance exists between the measuring probe and the threaded surface; activating said electromagnet to securely re-associate the internally threaded component with the inspection system; operating the inspection system to cause the measuring probe to measure at least a portion of the threaded surface and to generate initial threaded surface data; and processing said threaded surface data to generate physical characteristics of said at least a portion of the threaded surface.

37. The method of claim 36, wherein said processing includes processing said initial threaded surface data to responsive to at least one of a smoothing algorithm and a correction factor.

38. The method of claim 37, wherein said smoothing algorithm includes at least one of, fitting a least squares line of said component to at least a portion of said image data generated responsive to said internally threaded component; determining a plurality of residual data points responsive to said least squares line; sorting said plurality of residual data points; trimming said plurality of residual data points by fitting a residual least squares line to said plurality of residual data points; determining a second plurality of residual data points responsive to said residual least squares line; sorting said second plurality of residual data points; and determining screw thread geometric parameters responsive to said second plurality of residual data points.

39. The method of claim 37, wherein said correction factor is responsive to, f_s = pd + L + A, where f_s is functional size of the internally threaded component, pd is pitch diameter of the thread profile of the internally threaded component, L is lead error of a thread profile of the internally threaded component and A is angle error of said thread profile of the internally threaded component.

40. A computer-readable storage medium encoded with machine-readable computer program code, the program code including instructions for causing a controller to implement a method for measuring the threaded surface of an internally threaded component using an inspection system, wherein the inspection system includes a measuring probe having an emitter and a receiver and is sized and shaped to be positionably adjacent at least a portion of the threaded surface at an offset distance, wherein the emitter is configured to emit electromagnetic energy incident upon the threaded surface to generate reflected electromagnetic energy responsive to the threaded surface and wherein the receiver is configured to receive at least a portion of the reflected electromagnetic energy and generate threaded surface data, the method comprising: associating the internally threaded component with the inspection system via an electromagnetic; positioning the measuring probe inside a cavity of the internally threaded component; deactivating said electromagnet to cause the internally threaded component to be positioned relative to measuring probe such that an offset distance exists between the measuring probe and the threaded surface; activating said electromagnet to securely re-associate the internally threaded component with the inspection system; operating the inspection system to cause the measuring probe to measure at least a portion of the threaded surface and to generate initial threaded surface data; and processing said threaded surface data to generate physical characteristics of said at least a portion of the threaded surface.