Source: http://www.patentgenius.com/patent/8307528.html
Timestamp: 2018-08-21 00:05:28
Document Index: 337726214

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Low clearance machined part mating system - Patent # 8307528 - PatentGenius
8307528 Low clearance machined part mating system
Inventor: DeRoche, et al.
U.S. Class: 29/407.05; 29/407.04; 29/407.09; 29/407.1; 29/445; 700/95
Field Of Search: 29/407.01; 29/407.04; 29/407.05; 29/407.06; 29/407.09; 29/407.1; 29/705; 29/445; 33/813; 33/819; 700/95; 702/84
Foreign Patent Documents: 1736278; 2005059102
Other References: Schnitzler, Gerry, Honing: It's no lapping matter! Manufacturing Engineering; vol. 125 No. 3; pp. 56-64; Sep. 2000. cited by other.
W.Q. Zhao, Z. Xue, J.B. Tan and Z.B. Wang; SSEST: A new approach to higher accuracy cylindricity measuring instrument; ScienceDirect--International Journal of Machine Tools and Manufacturing; http://www.sciencedirect.com; Mar. 13, 2009. cited byother.
Measurement of Out-Of-Roundness; The American Society of Mechanical Engineers; American National Standard; ANSI B89.3.1--1972; reaffirmed 1979; pp. 1-27. cited by other.
1. A method of making parts with a predetermined tolerance relationship to one another, comprising: providing a measurement device; providing a first part; mounting saidfirst part in relation to said measuring device; producing rotational and translational movement as between said measurement device and said first part; generating a first data set with the measuring device representing at least a first parameter ofsaid first part, said first data set having as an input a distance between a reference point and the surface of said first part; generating a second data set with the measuring device representing at least a second parameter of said first part, saidsecond data set having as an input a distance between opposing points on the surface of said first part; determining, based on said second data set, at least a dimension of said first part, and, based on said first data set, at least one geometric errorrepresentative of said first part shape, wherein said determining includes the elimination of at least one of a tilt error and a positional error; and manufacturing a second part based on a combination of said at least one dimension and said at leastone geometric error.
2. The method according to claim 1, wherein said generating steps comprise a single measurement operation that obtains both said first data set and said second data set.
3. The method according to claim 2, wherein said single measurement operation comprises the measurement device indicating opposed plural edge data on said first part, and wherein the diameter is determined as the distance between said pluraledge data, and a radius is determined as a distance between one of said plural edge data and a reference line.
4. The method according to claim 1, wherein said determining step includes eliminating a dust error from at least one of said first data set and said second data set.
5. The method according to claim 1, wherein said positional error is removed by steps comprising: identifying a 1 Hz harmonic having a phase angle, an amplitude, and an offset that corresponds to position error in at least one of said firstdata set and/or said second data set; and subtracting the amplitude value of said 1 Hz harmonic from said at least one of said first data set and/or said second data set at he appropriate phase angles.
6. The method according to claim 1, wherein said tilt error is removed by steps comprising: identifying a 2 Hz harmonic having a phase angle, an amplitude, and an offset that corresponds to said tilt error in at least one of said first data setand/or said second data set; and subtracting said amplitude value of said 2 Hz harmonic from said at least one of said first data set and/or said second data set at appropriate phase angles.
7. The method according to claim 6, wherein said second part, when slidingly engaged with said first part, has a clearance tolerance of less than about 0.00005 inches.
8. The method according to claim 1, wherein the steps of mounting, producing, generating the first data set, generating the second data set, determining, and manufacturing occur in less than about 9 minutes.
9. The method according to claim 1, wherein the steps of mounting, producing, generating the first data set, generating the second data set, determining, and manufacturing occur in less than about 2 minutes.
10. The method according to claim 9, wherein said second part, when slidingly engaged with said first part, has a clearance tolerance of less than about 0.00005 inches.
11. The method according to claim 1, wherein said first part includes an anodized coating.
12. The method according to claim 1, wherein said first data set comprises a maximum of 360 sets of data.
13. The method according to claim 1, wherein said first part has a plurality of lands, said plurality of lands having at least a first diameter and a second diameter, and wherein said first parameter represents a distance between said referencepoint and the surface of said first part at said first diameter and wherein said second parameter represents a distance between opposing points on the surface of said first part at said first diameter, and wherein said method further includes the stepsof: generating a third data set with the measuring device representing at least a third parameter of said first part, said third data set having as an input a distance between a reference point and the surface of said first part at said second diameter; and generating a fourth data set with the measuring device representing at least a fourth parameter of said first part, said fourth data set having as an input a distance between opposing points on the surface of said first part at said second diameter.
14. The method according to claim 13, wherein said determining step includes: determining, based on said second data set, at least a dimension of said first part at at least one of said plurality of lands having a first diameter, and, based onsaid first data set, at least one geometric error representative of said first part shape at at least one of said plurality of lands having a first diameter; and determining, based on said fourth data set, at least a second dimension of said first partat at least one of said plurality of lands having said second diameter, and, based on said third data set, at least one geometric error representative of said first part shape at at least one of said plurality of lands having said second diameter.
Manufacturing a set of mating parts, e.g., a sleeve with a bore and a spool valve that is slidably received in the bore, with very small clearances is challenging, particularly with respect to low-cost parts. Typically, in order to achieve verysmall clearances, a batch of one part, e.g., Part A, having a specified size and certain geometric tolerances, is made and then a batch of its corresponding part, e.g., Part B, having a specified size and certain geometric tolerances, is made. Understatistical theory, both parts A and B, individually, would exhibit a normal distribution around a mean, with an equal number of parts in the batch being higher and lower than the average part size. Thus, the parts could be "matched," i.e., a Part Acould be matched with a Part B so that a very small clearance is achieved when assembled. While in theory this should result in little wasted material and involve only the physical process of identifying parts that should be joined together, for partsrequiring a very low clearance this process is costly, inefficient, and is not always successful in achieving the desired clearance.
Manufacturers have sought more efficient and effective processes to achieve low clearance matching parts with limited success. Processors have attempted to specify the limits of geometric error on the two parts, thus establishing a maximumclearance amount. However, this methodology does not guarantee that the two parts will fit together, for example, if a Part A is at the upper limit of its geometric tolerance Part A may not fit together with a Part B at the lower end of its geometrictolerance. In addition, the parts may not fit together with a sufficiently low clearance. For example, if both Part A and Part B are at the low end of their respective geometric tolerance ranges, the clearance between the two parts may be higher thandesired. Further, to ensure the desired clearance is achieved and to reduce assembly costs, Parts A and B must generally be manufactured to a high degree of precision to reduce the amount of variation, which increases manufacturing costs considerably. Given these constraints, previous manufacturing techniques that were capable of rapid throughput, i.e., less than 10 minute production times, were generally only able to achieve clearance tolerances of approximately 0.0011 inch.
The complexity and difficulty in manufacturing low clearance mated parts is exacerbated when attempting to create a set of mated parts when, for instance, Part A has a shape that includes two or more diameters, e.g., a first diameter extendingfor a certain portion of Part A and a second diameter extending for another portion of Part A. Multiple diameter parts pose challenges to manufacturers because Part A generally needs to mate with Part B at a low clearance at both diameters. However, thefirst diameter portion of Part A may end up at a certain tolerance and the second diameter portion of Part A may have a different tolerance. Thus, typically attempts to mate Part A with Part B require a compromise between the clearance at the firstdiameter portion and the clearance at the second diameter portion, resulting in a set of parts without an overall desired clearance value.
In addition, the aforementioned processes and others known in the art do not account for the challenges that arise when parts are treated to increase hardness. For example, hardcoat anodizing is a process that is generally used to increase thewear and corrosion resistance of the natural oxide layer on the surface of aluminum parts. A typical hardcoat anodizing application will add several thousandths of an inch to the surface of a part. However, the process typically does not provide arepeatable thickness from part to part and thus the tolerance range on a batch of parts achieved during the original machining process may be lost. While some manufacturers will machine the hardcoated part in order to return a part to within requiredtolerances, machining the hardcoated part is not only an extra, costly process, it can damage the hardcoat, thus limiting its effectiveness.
The present disclosure describes a device, system and method for generating low clearance slidably mated parts. In an exemplary embodiment, a measurement device is described that measures edge data associated with a first part and processes thedata to determine the size and the geometric errors associated with the first part. Additionally, a processing machine may be instructed by the measurement device to remove material from a second part so that the first part and the second part whenmated together have a clearance tolerance of less than about 0.00005 inch.
In one exemplary embodiment, a measurement device includes a non-contact micrometer, an air bearing rotary table, an air bearing linear slide, and a holding device for holding the first part by its base on the air bearing rotary table. Wheninserting a first part into the holding device, the operator may generally induce tilt and position error relative to the non-contact micrometer. The non-contact micrometer transmits light across the first part to a receiver, thus illuminating theopposed edges associated with the first part. Two sets of edge data are stored by a control system, a first set representing the difference between the one edge of the first part and a reference point and the second set representing the distance betweenthe two opposed edges. The first part is then rotated by the air bearing rotary table by a defined increment and the opposed edge data of the first part is captured again. Once edge data has been taken around the circumference of the first part, theair bearing linear slide moves the non-contact micrometer to another plane substantially orthogonal to the longitudinal axis of the first part. Edge data around the circumference is then taken at the new plane as before. The process is repeated for theremainder of the first part. The two sets of data are analyzed and from one or both of them the size and geometric errors associated with the first part are deduced. The size and geometric errors associated with the first part provide the dimensionalinformation necessary to instruct the processing machine. An amount of as little as 0.00005 inch may be added to the dimensional information in order to provide the clearance necessary between the two parts.
In another exemplary embodiment, the processing machine includes plural lateral slides, a rotary table, a minilathe, a boring bar, a probe, and a centering chuck. The second part is placed into the centering chuck and the probe aids,intermittently, in centering the boring bar with the center of the second part. The minilathe and boring bar are moved horizontally by the plural lateral slides so that the boring bar is positioned to remove material from the second part based on theinstructions from the measurement device. The end result is that the first part and the second part fit together with a clearance tolerance of less than about 0.00005 inch.
Generally, low clearance machined part mating system 100 is suitable for the volume manufacture of mating parts that slidably engage one another at precise clearances. As will be discussed more fully below, an exemplary embodiment of lowclearance machined part mating system 100 contemporaneously obtains measurements sufficient to calculate the size of and the geometric errors associated with a first part and then uses the calculations to create a second part. The resulting slidableclearance tolerance, i.e., proximity to the desired clearance, between the two parts may be consistently as little as 0.00005 inch, or even less in some cases, which may be considered a reduction of more than 20 times the clearance tolerance levelsachievable using prior art techniques. Less precise clearance tolerances are also obtainable with system 100.
In one embodiment of the present disclosure, the process by which mating parts are made can be performed in less than about 9 minutes. However, more or less time may be taken depending on various circumstances, e.g., the precision required orthe length of the part to be measured and machined. In another embodiment of the present disclosure, the process may be performed in less than about 2 minutes with the resulting clearance tolerance between the two mated parts being about 0.00005 inch.
Referring first to FIG. 1, there is illustrated an example of a low clearance machined part mating system 100 in accordance with an exemplary embodiment of the present invention. System 100 typically includes a measurement device 104, a controlsystem 108, and a processing machine 112. Measurement device 104 is generally capable of measuring, contemporaneously and to a high degree of accuracy, a plurality of parameters of a first part 116. In an exemplary embodiment, first part 116 isgenerally cylindrical. However, as those skilled in the art will readily appreciate, first part 116 may embody many other shapes, configurations, and dimensions. In any event, measuring system 100 is not intended to be limited by the shape of firstpart 116 as described herein.
Generally, the parameters that measurement device 104 may measure include the radius from a theoretical reference point or geometric axis of a first part 116 and the diameter of the first part, but other parameters may be measured as well, asdesired. Measurement device 104 may determine the parameters from edge data measurements taken in increments or continuously around the circumference of first part 116 and at selected planes spaced along the longitudinal axis of the first part. Controlsystem 108 receives data determined by measurement device 104, processes the data as described below to determine the size of and geometric errors associated with first part 116, and then transforms these calculations into instructions for processingmachine 112. Processing machine 112 is typically operated to remove material from a second part 120 so that first part 116 and the second part fit together with a very small clearance. Measurement device 104, control system 108, and processing machine112 may communicate in an integrated fashion through a known data transfer mechanisms as may be devised by a person of ordinary skill in the art.
FIG. 2 shows an exemplary measurement apparatus 200 suitable for use as, or as a part of, measurement device 104. Measurement apparatus 200 may include a base 202, movement devices, e.g., a linear slide 204 and a rotary table 208, a holdingdevice, e.g., chuck 212, a non-contact micrometer 216, and a display device 220.
Base 202 is generally sized and dimensioned so as to provide support for the other components of measurement apparatus 200 and to minimize outside disturbances during the measurement operation. Base 202 may be made of materials that provide astable measurement surface and is typically, but not necessarily, sized to accommodate the rest of measurement apparatus 200. In an exemplary embodiment, base 202 is natural solid granite base with bored holes and threaded inserts on steel welded framesand includes adjustable leveling feet. As an additional precaution against vibration, base 202 may include components for vibration isolation (not shown).
Linear slide 204 generally moves along the longitudinal axis of first part 116. Linear slide 204 may move in response to instructions from control system 108, on instructions from an external source such as a machine operator work station, orbased on predefined inputs to measurement apparatus 200. In any event, linear slide 204 should be capable of very accurate linear movements, e.g., precision linear movement of twenty micro inches in six inches of travel, and should have a straightnessof about 0.00003 inch in about one inch of linear travel or approximately 0.0002 inch in about eight inches of travel, although the precision and straightness of linear slide 204 will vary as a function of the intended application of low clearancemachined part mating system 100. In an exemplary embodiment, linear slide 204 includes air bearing slide 224. Air bearing slide 224 may be of any number of constructions known in the art. For example, air bearing slide 224 may be a constrained box waydesign (not shown) that provides a fully preloaded air bearing carriage for high stiffness and resistance to off-set loading. In this example, high accuracy is generally achieved through tight form geometry control of the linear box rails and centralplacement of the linear drive which minimizes offset errors (not shown). Also included in a typical motorized air bearing slide 224 are brushless DC linear motors, high resolution encoders, and amplifiers, (not shown) although manual operation is alsopossible. Those skilled in the art will readily identify other suitable means, such as the use of hydrostatic linear slides or linear guide bearing slides, for accurately moving linear slide 204. In one implementation, linear slide 204 is a verticallypositioned air bearing slide 224 that has a straightness of about 0.00003 inch in about one inch of linear travel or approximately 0.0002 inch in about eight inches of travel.
Linear slide 204 may be coupleable with non-contact micrometer 216. Non-contact micrometer 216 is generally capable of identifying the edge characteristics of first part 116 without physically touching the first part. Non-contact micrometer216 may, in one embodiment, be designed to determine the edge characteristics of opposed points on first part 116. In an exemplary embodiment, non-contact micrometer 216 includes a light-emitting diode (LED)/charged-coupled device (CCD) opticalmicrometer, although as will be readily apparent to one skilled in the art, other non-contact micrometers are available such as laser micrometers or CCD laser micrometers. In any event, non-contact micrometer 216 is capable of measuring first part 116at least at two places simultaneously. When non-contact micrometer 216 is implemented as a LED/CCD optical micrometer, the non-contact micrometer sends a plurality of light from LED emitter 228 across first part 116 to CCD receiver 232. In thisconfiguration, the plurality of light emitted from LED emitter 228 may create a shadow of first part 116 on CCD receiver 232 that indicates two opposed edges of the first part.
Rotary table 208 is generally capable of rotating first part 116 around its longitudinal axis. Rotary table 208 may move incrementally or continuously in response to instructions from control system 108, on instructions from an external sourcesuch as a machine operator, or based on predefined inputs to measurement apparatus 200. In any event, rotary table 208 should be capable of accurate rotational movements. Rotary table 208 may be a rotary index table, a precision spin table, or otherhigh precision apparatus with rotational capabilities. Although rotary table 208 may be manually or mechanically operated, a suitable rotary table 208 may include air bearings, DC motors, digital drives and rotary encoders (not shown), although othercomponents known to those skilled in the art may be included and/or substituted. In an exemplary embodiment, rotary table 208 is a rotary air bearing table, however, those skilled in the art will readily identify other suitable means for accuratelyrotating first part 116 such as hydrostatic rotary tables or spindle bearing tables. In one implementation, rotary table 208 has a radial and axial accuracy of about five micro inches. In an alternative embodiment, rotary table 208 may be integratedwith linear slide 204 and thus may be suitable for rotating first part 116 as well as moving the first part past non-contact micrometer 216.
Chuck 212, a type of holding device, may be coupled with rotary table 208 and is generally sized and dimensioned to hold first part 116. Generally, chuck 212 holds first part 116 in an offset and tilted position, i.e., with the longitudinalaxis of first part 116 being non-parallel to the axis of rotation of rotary table 208 and with the center of first part 116 being offset from the center of rotary table 208, but as those skilled in the art will readily identify, chuck 212 may be designedto hold first part 116 in any suitable orientation.
Optionally, display device 220 may be coupled to vertical movement component 204. Generally, display device 220 is suitable for presenting the measurement results of non-contact micrometer 216 and the movements of rotary table 208 and linearslide 204. Display device 220 may also include a user interface that enables an operator to manipulate the components of measurement device 200. In certain embodiments, display device 220 may be integrated with control system 108.
In an alternative embodiment, measurement device 200 may be configured so that non-contact micrometer 216 rotates around a stationary first part 116 (not shown). In this embodiment, non-contact micrometer 216 may be coupled with rotary table208. First part 116 may be held by chuck 212, which may be coupled to linear slide 204. Linear slide 204 may move first part 116 so as to place different planes that are substantially orthogonal to the longitudinal axis of first part 116 in view ofnon-contact micrometer 216 for measurement. In yet another alternative embodiment of measurement device 200, non-contact micrometer 216 may be coupled with both rotary table 208 and linear slide 204, or the rotary table and the linear slide may beintegrated into the same device, so that the non-contact micrometer may move both rotationally and longitudinally about first part 116. A person of ordinary skill in the art will readily recognize that other various assemblies of the aforementionedcomponents are possible that allow for contemporaneous measurement of opposed points around and along the longitudinal axis of first part 116.
In yet another embodiment, measurement device 200 may be configured so that several non-contact micrometers 216 may be assembled in a stacked arrangement, e.g., one on top of the other or side-by-side, to take multiple measurements along thelongitudinal axis of first part 116 at the same time.
FIG. 3 shows an exemplary processing apparatus 300 suitable for use as, or as a part of, processing machine 112. Processing apparatus 300 typically includes a base 302, a centering chuck 304, a spindle 306, a removal tool 308, a probe 312, anda plurality of lateral slides 316.
Processing apparatus 300 is suitable for facilitating removal of material from second part 120 so as to create the appropriate clearance between first part 116 and the second part. Those skilled in the art will readily appreciate that there areseveral types of processing apparatus 300 that may be suitable for removing material from second part 120. Typically, processing apparatus includes a removal tool 308, such as a drill bit for a drill or a honing stone for a honer that makes contact withsecond part 120, for removing material from second part 120. Examples of removal tool 308 include, but are not limited to, boring bars, drills, reamers, grinders, and honers. In an exemplary embodiment, processing apparatus 300 is a minilathe that usesa boring bar to remove material from second part 120.
Base 302 is generally sized and dimensioned so as to provide support for the other components of process apparatus 300 and to minimize outside disturbances during the processing of second part 120. Base 302 may be made of many materialsrecognized in the art as providing a stable processing environment and may be sized to accommodate processing apparatus 300. In an exemplary embodiment, base 302 is natural solid granite base with bored holes and threaded inserts on steel welded framesand includes adjustable leveling feet. As an additional precaution against vibration, base 302 may include components for vibration isolation.
Centering chuck 304 is generally a removable fixture on processing apparatus 300 that centers and constrains the movement of second part 120. Centering chuck 304 may be sized and dimensioned to hold second part 120 and provide sufficientrestraint on the movement of second part 120 during the machining process. As movement during the machining process may induce deviations in second part 120, centering chuck 304 typically, although not necessary, is sized and dimensioned to hold onlycertain sizes of second part 120. For example, second parts 120 falling within a first size range may be held by a centering chuck 304 of a first size, and second parts 120 falling within a second size range may be held by a centering chuck 304 of asecond size, and so on. In an exemplary embodiment, centering chuck 304 is a diaphragm chuck having a plurality of circumferentially spaced jaws mounted on a diaphragm.
Centering chuck 304 may be combined with spindle 306 so that second part 120 may be rotated during the machining process. Generally, spindle 306 is similar to rotary table 208 described above, although as shown in FIG. 3, spindle 306 ispositioned so that the longitudinal axis of second part 120 is generally parallel to a major surface 307 of base 302. In an exemplary embodiment, spindle 306 is a rotary air bearing spindle having a radial and axial accuracy of about five micro inches.
Probe 312 generally serves to help center removal tool 308 with respect to the center of second part 120. Probe 312, in an exemplary embodiment, may contact removal tool 308 temporarily, at, for instance when removal tool 308 is a boring bar,the tip of the boring bar. Probe 312 is designed to communicate to control system 108 the position in two dimensional space of the tip of removal tool 308 (x and z directions, as shown on FIG. 3). Using a reference point and probe 312, removal tool 308may be positioned in substantially the center of second part 120 in the x direction (as seen on FIG. 3). Probe 312 may then be removed from removal tool 308 so that it does not interfere with material removal from second part 120. In one embodiment,the location of removal tool 308 relative to the center of second part 120 is periodically checked using probe 312. In another exemplary embodiment, probe 312 is a linear variable differential transducer (LVDT) probe attached to or near spindle 306. Aswould be readily apparent to one skilled in the art other probe types or more than one probe may be used to center removal tool 308. For instance, in another embodiment of probe 312, the probe is designed and configured, with the use of one or moreprobes, to give the three dimensional location of removal tool 308.
Lateral slides 316 are generally coupled to base 302 and to removal tool 308. Lateral movement devices 316 are capable of very precise lateral movements and in general, may be of similar construction to linear slide 204. In an exemplaryembodiment, lateral slides 316 are horizontally positioned air bearing slides 316A-B that have a straightness of approximately 0.00003 inch in about one inch of linear travel or approximately 0.0002 inch in about eight inches of travel. Air bearingslides 316A-B may also have, in another exemplary embodiment, a precision linear movement to a desired location of about twenty micro inches in six inches of travel. In this two air bearing slide embodiment, air bearing slide 316A may move removal tool308 in one direction along a horizontal plane parallel to surface 307 of base 302 while air bearing slide 316B may move removal tool 308 in another direction along the same horizontal plane. When configured this way, air bearing slides 316A-B mayselectively and precisely position removal tool 308 in a desired location in the horizontal plane so as to remove material from second part 120 per the instructions of control system 108. In another embodiment, a third air bearing slide (not shown), orsimilar structure, may be provided to allow for a third direction of movement.
It is to be noted that one or more of the aspects and embodiments described herein may be conveniently implemented using a machine (e.g., a computing device) programmed and communicating with other specialized components according to theteachings of the present specification, as will be apparent to those of ordinary skill in the art. Appropriate software coding can readily be prepared by persons skilled in the art based on the teachings of the present disclosure, as will be apparent tothose of ordinary skill.
Such software may be a computer program product that employs a machine-readable medium. A machine-readable medium may be any medium that is capable of storing and/or encoding a sequence of instructions for execution by a machine (e.g., acomputing device) and that causes the machine to perform any one of the methodologies and/or embodiments described herein. Examples of a machine-readable medium include, but are not limited to, a magnetic disk (e.g., a conventional floppy disk, a harddrive disk), an optical disk (e.g., a compact disk "CD", such as a readable, writeable, and/or re-writable CD; a digital video disk "DVD", such as a readable, writeable, and/or rewritable DVD), a magneto-optical disk, a read-only memory "ROM" device, arandom access memory "RAM" device, a magnetic card, an optical card, a solid-state memory device (e.g., a flash memory), an EPROM, an EEPROM, and any combinations thereof. A machine-readable medium, as used herein, is intended to include a single mediumas well as the possibility of including a collection of physically separate media, such as, for example, a collection of compact disks or one or more hard disk drives in combination with a computer memory.
FIG. 4 shows a diagrammatic representation of one implementation of a machine/computing device in the exemplary form of a control system 108 within which a set of instructions for causing the device to perform any one or more of the aspectsand/or methodologies of the present disclosure may be executed. Control system 108 includes a processor 405 and a memory 410 that communicate with each other, and with other components, such as measurement device 104 and processing machine 112 via a bus414. Bus 414 may include any of several types of communication structures including, but not limited to, a memory bus, a memory controller, a peripheral bus, a local bus, and any combinations thereof, using any of a variety of architectures.
Memory 410 may include various components (e.g., machine readable media) including, but not limited to, a random access memory component (e.g., a static RAM "SRAM", a dynamic RAM "DRAM", etc.), a read only component, and any combinationsthereof. In one example, a basic input/output system 420 (BIOS), including basic routines that help to transfer information between elements within control system 108, such as during start-up, may be stored in memory 410. Memory 410 may also include(e.g., stored on one or more machine-readable media) instructions (e.g., software) 425 embodying any one or more of the aspects and/or methodologies of the present disclosure. In another example, memory 410 may further include any number of programmodules including, but not limited to, an operating system, one or more application programs, other program modules, program data, and any combinations thereof.
Control system 108 may also include a storage device 430. Examples of a storage device (e.g., storage device 430) include, but are not limited to, a hard disk drive for reading from and/or writing to a hard disk, a magnetic disk drive forreading from and/or writing to a removable magnetic disk, an optical disk drive for reading from and/or writing to an optical media (e.g., a CD, a DVD, etc.), a solid-state memory device, and any combinations thereof. Storage device 430 may be connectedto bus 414 by an appropriate interface (not shown). Example interfaces include, but are not limited to, SCSI, advanced technology attachment (ATA), serial ATA, universal serial bus (USB), IEEE 1395 (FIREWIRE), and any combinations thereof. In oneexample, storage device 430 may be removably interfaced with control system 108 (e.g., via an external port connector (not shown)). Particularly, storage device 430 and an associated machine-readable medium 435 may provide nonvolatile and/or volatilestorage of machine-readable instructions, data structures, program modules, and/or other data for control system 108. In one example, instructions 425 may reside, completely or partially, within machine-readable medium 435. In another example,instructions 425 may reside, completely or partially, within processor 405.
Control system 108 may also include a connection to measurement device 104. Measurement device 104 may be interfaced to bus 414 via any of a variety of interfaces (not shown) including, but not limited to, a serial interface, a parallelinterface, a game port, a USB interface, a FIREWIRE interface, a direct connection to bus 414, and any combinations thereof. Alternatively, in one example, a user of control system 108 may enter commands and/or other information into control system 108via an input device (not shown). Examples of an input device include, but are not limited to, an alpha-numeric input device (e.g., a keyboard), a pointing device, a joystick, a gamepad, an audio input device (e.g., a microphone, a voice response system,etc.), a cursor control device (e.g., a mouse), a touchpad, an optical scanner, a video capture device (e.g., a still camera, a video camera), touchscreen, and any combinations thereof.
A user may also input commands and/or other information to control system 108 via storage device 430 (e.g., a removable disk drive, a flash drive, etc.) and/or a network interface device 445. A network interface device, such as networkinterface device 445 may be utilized for connecting control system 108 to one or more of a variety of networks, such as network 450, and one or more remote devices 455 connected thereto. Examples of a network interface device include, but are notlimited to, a network interface card, a modem, and any combination thereof. Examples of a network include, but are not limited to, a wide area network (e.g., the Internet, an enterprise network), a local area network (e.g., a network associated with anoffice, a building, a campus or other relatively small geographic space), a telephone network, a direct connection between two computing devices, and any combinations thereof. A network, such as network 450, may employ a wired and/or a wireless mode ofcommunication. In general, any network topology may be used. Information (e.g., data, instructions 425, etc.) may be communicated to and/or from control system 108 via network interface device 455.
Control system 108 may further include a video display adapter 460 for communicating a displayable image to a display device 465, such as display device 220. Examples of a display device 465 include, but are not limited to, a liquid crystaldisplay (LCD), a cathode ray tube (CRT), a plasma display, and any combinations thereof.
In addition to display device 465, control system 108 may include a connection to processing machine 112 or one or more other peripheral output devices including, but not limited to, an audio speaker, a printer, and any combinations thereof. Processing machine 112 or other peripheral output devices may be connected to bus 414 via a peripheral interface 470. Examples of a peripheral interface include, but are not limited to, a serial port, a USB connection, a FIREWIRE connection, a parallelconnection, a wireless connection, and any combinations thereof.
Turning now to an exemplary operation of mating system 100 and with reference to exemplary embodiments shown in FIGS. 2 and 3 and in addition with reference to FIG. 5, first part 116 is typically manufactured at the beginning of a measurementprocess 500 to a predetermined tolerance at step 504. Typically, the acceptable tolerance level of first part 116 would be dependent upon several factors including, but not limited to, the cost of higher tolerance levels, the time required to improvethe tolerance levels, and/or if first part 116 would receive any further treatments, e.g., anodizing. In an exemplary embodiment, first part 116 is manufactured to a fairly wide tolerance level, e.g., a level of about +/-0.002 inches. Optionally, firstpart 116 may be coated, e.g., anodized (either Type II or Type III), after manufacture with a material designed to modify the properties of the first part. Typically, such coating will harden the outer surface of first part 116, although other surfacemodifications are encompassed by the present invention.
First part 116 is then measured by measuring device 104 at step 508. As shown in FIG. 5, measurement of first part 116 begins at a first position, i.e., X=1, and at a first cross-sectional plane, i.e., P=1. As discussed more fully below,measurements may be taken around first part 116, i.e., from X=1 to X=N, at multiple planes, i.e., P=1 to P=M, in order to sufficiently characterize the surface features and size of the first part.
Typically, first part 116 is secured to measuring device 104 via chuck 212. As will be described more fully below, it may be advantageous to secure first part 116 into chuck 212 in such a way so as to induce position errors. This may beachieved by either manual positioning of first part 116 in an off-center, tilted position, by designing chuck 212 so that first part 116 will be in an off-center, tilted position when secured into chuck 212, or by other means known by a person ofordinary skill in the art.
Once secured, a plurality of parameters, e.g., the edge data of first part 116, are measured by measuring device 104 at step 512. Parameters determined by non-contact micrometer 216 may be stored in storage device 430 by control system 108 astwo or more data sets at step 514. In an exemplary embodiment, first data set 516 may represent the distance between an edge of first part 116 and a reference point in the cross-section or plane of measurement, typically inside the boundaries of firstpart, that is substantially orthogonal to the longitudinal axis of the first part so as to generate edge datum, i.e., a theoretical radius of the first part. Second data set 518 may represent the distance between the opposed edges of first part 116,i.e., the diameter of the first part at the point of measurement. Additional data sets may be included for other features of first part 116 or to segment of the first part. For example, if first part 116 is a spool valve with three concentric lands ofdifferent diameters, (as shown in FIG. 7 (described below), lands 704, 708, and 712), data sets may be devised such that edge data sets, both first and second data sets 516, 518, respectively, as previously described, are determined for each land. Inany event, measuring device 104 is not intended to be limited by delineation of data sets as described herein, as data sets may be created as necessary to measure the appropriate features of first part 116.
Control system 108 then determines whether first part 116 should be rotated at step 520 by evaluating whether the first part has been measured at all the predefined places around the circumference of the part in a given plane of measurement. Iffirst part 116 has not been measured at all predefined places and so should be rotated further, the method proceeds to step 524 where control system 108 instructs rotary table 208 to rotate first part 116. Once rotated, non-contact micrometer 216determines the edge data of first part 116, which is then stored by control system 108 in for example, storage device 430. In an exemplary embodiment, control system 108 instructs rotary table 208 to continuously rotate first part 116 and to enable tothe capture of edge data each time rotary table 208 has moved approximately 10 degrees, thus enabling the capture of edge data at thirty-six locations around circumference of first part 116. In an alternative embodiment, control system 108 instructsrotary table 208 to rotate first part 116 in 10 degree increments within a given plane of measurement and rotates the part a total of thirty-five times, thus also enabling the capture of edge data at thirty-six locations around circumference of firstpart 116.
First part 116 may be rotated more or less than about thirty-five times depending on the degree of accuracy sought regarding the surface characteristics of first part 116. Typically, the number of measurements may also be limited by timeallotted for measuring. The degree of accuracy obtained per unit time can be referred to as the characterization efficiency, which represents the number of measurements per unit time to achieve a clearance tolerance level corresponding to a certainlength of first part 116. When maximized, this parameter generally represents the minimum number of measurements of first part 116 allowable to achieve a minimal clearance tolerance range and meet processing time requirements. In an exemplaryembodiment, measurement device 104 has a characterization efficiency upper limit of about 72. In a further refined embodiment, the characterization efficiency has a value of about 36, although depending upon design parameters in particular applicationsa characterization efficiency of between about 18 to 54 may be found useful.
It is also understood that there is some redundancy in rotating first part 116 thirty-five times given that non-contact micrometer 216 takes edge data at opposed locations. This redundancy may be necessary to ensure consistent measurement ofthe radius of first part 116 as the reference point in the cross-section or plane of measurement that is substantially orthogonal to the longitudinal axis that includes the edge datum may not be the actual center of the cross-section or plane. Thisredundancy may also be used to correct for errors in second data set 518. For example, if the diameter of first part 116 is measured twice per revolution the diameter should be the same when measured at 10.degree. and 190.degree.. If thesemeasurements do not match, the data can be corrected or first part 116 can be remeasured.
If control system 108 determines that first part 116 should no longer be rotated within the current plane of measurement (e.g., first part 116 has been rotated thirty-five times, equals a predefined specification, or if upon assessing thepredefined increment, control system 108 calculates that the part has been rotated 360 degrees), control system 108 then resolves whether linear slide 204 should move non-contact micrometer 216 to another plane along the longitudinal axis of first part116 at step 528. In an exemplary embodiment, measurement device 104 repeats steps 512, 516, 520, and 524 along the longitudinal axis of first part 116 at any desired increment, for instance, each 0.1 inch. In alternative embodiments, measurement device104 may measure at larger or smaller increments depending upon the accuracy required for machining second part 120 and the dimensions of first part 116. For example, if first part 116 is a valve spool with multiple lands having concentric diameters asseen in FIG. 7, measurement device 104 may not necessarily measure the space between the lands, e.g., between first land 704 and second land 708, as this may not have an impact on the instructions to processing machine 112.
If no further movement along the longitudinal axis of first part 116 is necessary, for example, the number of increments previously measured equals a predefined specification or if upon assessing the predefined increment, control system 108determines, based on the total length of the first part, that the part has measured the length of the first part, the control system, via processor 405, a program module in storage device 430, or other means known in the art, initiates an error and sizedetermination, at step 536, calculating the geometric errors and size associated with first part 116. An exemplary embodiment of an error and size determination process 536 is diagramed below in connection with FIG. 6.
At step 604 of process step 536, control system 108 may retrieve stored first data set 516 from storage device 430 or other storage location in control system 108. Error and size determination process 536 then may begin the process ofdetermining the roundness of first part 116 at a given plane using first data set 516.
In some cases, artifacts may exist in the data in first data set 516. If artifacts exist in first data set 516 and are to be removed before the roundness of first part 116 is determined, the first step may be to eliminate artifacts from thefirst data set. Artifacts may be microscopic dust, debris, or other removable particles of matter that obscure the feature being measured, e.g., the edge or diameter of first part 116. These artifacts may affect the measurements taken by measurementdevice 104 by increasing the value of measurement, e.g., a larger diameter or radius is measured at a given point of measurement, and in some cases may need to be removed in order to more accurately ascertain the surface characteristics of first part116. Artifacts may be removed in a process which generally includes removing outliers in both the positive and negative directions that exceed a certain amount and/or removing outliers that exceed excursions of a certain, predefined amount. In anexemplary embodiment, artifacts are identified by reviewing the measured data as a sequence and noting deviant data points that diverge significantly from the data point before and after the deviant data point. The deviant data points may then bealtered or corrected by various methods, including, but not limited to, remeasuring first part 116 or approximating a value for the deviant data point that may more closely represent the true value.
A second error removal step may be the removal of position error, i.e., offset of the center of first part 116 from the axis of rotation of measurement device 104, at step 612. Position error may caused by the general imprecision that comeswith mounting first part 116 into chuck 212 or it may be purposefully induced. Although it is theoretically possible to position first part 116 so that the first part's axis of rotation is centered in measurement device 104, there are methodologies thatexist in the art to remove errors that may come from improper mounting. In fact, it may be advantageous to induce position error either through manual, mechanical, or other means in order to make the position error easier to identify and to make themeasurement process quicker and less costly, e.g., less time is taken to align the part and special tools are unnecessary to ensure positioning. In an exemplary embodiment, position error is removed from first data set 516 by identifying a 1 Hz harmonicin the first data set, including its phase angle, amplitude, and offset and then subtracting the amplitude value of the harmonic at the appropriate phase angles. The correlation between a pure first order harmonic and the harmonic identified in firstdata set 516 may be used as a guide as to when the phase angle, amplitude, and offset have been sufficiently delineated. In an exemplary embodiment, the correlation between the pure harmonic and the harmonic identified in first data set 516 is greaterthan 95%. Greater or less correlation between the pure harmonic and the harmonic identified in first data set 516 may be desirable when it is desired that the mating parts have consistently improved or lower quality clearances, respectively.
A third error removal step may include the removal of Abbe error, e.g., chucking tilt angle of first part 116, at step 616. Abbe error is generally the linear positional error caused by the combination of the axes of measurement being offsetfrom the plane of motion and an angular error in that motion. Abbe error may be calculated by methods readily known in the art, which may include comparing the data taken at two different planes along first part 116. In an exemplary embodiment, Abbeerror is calculated after the removal of the first order harmonic, i.e., step 612. As mentioned previously with regards to position error, it may be advantageous to induce Abbe error while securing first part 116 to chuck 212 in order to more easilyidentify the error and to lower operational costs.
A fourth error removal step may include the removal of tilt error resulting from the mispositioning of first part 116 in chuck 212. Although it is theoretically possible to position first part 116 so that it is perfectly perpendicularly placedin measurement device 104, there are methodologies that exist in the art to remove errors that may come from improper mounting. As with position error and Abbe error it may be advantageous to induce the error, in this case tilt error, either throughmanual, mechanical, or other means in order to make the tilt error easier to identify and to make the measurement process quicker and less costly, e.g., less time is take to align the part and special tools are unnecessary to ensure proper positioning. The process for removing tilt error is generally the same as that for removing position error except that instead of identifying a first order harmonic, first data set 516 is evaluated for a second order harmonic. In an exemplary embodiment, tilt erroris removed from first data set 516 by identifying a 2 Hz harmonic in the first data set, including its phase angle, amplitude, and offset and then subtracting the amplitude value of the harmonic at the appropriate phase angles. The correlation between apure second order harmonic and the harmonic identified in first data set 516 may be used as a guide as to when the phase angle, amplitude, and offset have been sufficiently delineated. In an exemplary embodiment, the correlation between the pureharmonic and the harmonic identified in first data set 516 is greater than 95%. Greater or less correlation between the pure harmonic and the harmonic identified in first data set 516 may be desirable when it is desired that the mating parts haveconsistently improved or lower quality clearances, respectively.
As shown by exemplary process 600, after the removal of errors from first data set 516, several geometric errors may be calculated. For example, roundness error of first part 116 may be determined step 624. Generally, roundness error isconsidered the difference between the actual surface of first part 116 and a circle having a constant radius. There are several methodologies used for determining roundness error known in the art. Several methods are described in ANSI B 89.3.1: 1972Measurement of Out-of-Roundness, which is incorporated herein by reference in its entirety. In an exemplary embodiment of process 600, roundness error is calculated using the least squares circle method (LSC). The LSC generates a reference circle sizedso that the sum of the area between the circle and the surface of first part 116 inside the circle equals the sum of the area between the circle and the surface of first part 116 outside the circle. The roundness error then can be determined as thedifference between the maximum and minimum distance from this reference circle, i.e., the difference between the shortest and longest radius from the center of the reference circle. Once roundness error is calculated at a given plane, the processproceeds to step 628 at which point the determination is made whether or not the process has determined roundness error at all the planes of first part 116 included in first data set 516. If not, the process returns to step 608 so that the roundnesserror at the remaining planes along first part 116 may be determined. It would be readily apparent to a person skilled in the art that other methods exist by which to determine roundness error, some of which are described in ANSI B 89.3.1: 1972, whichis referenced above.
In some applications it may be desired that concentricity error also be determined using first data set 516, at step 634. Concentricity error is generally considered the condition in which all the cross-sectional elements of a cylinder orcylinders have common axes. In an exemplary embodiment of process 600, when first part 116 is generally cylindrical, each respective center of the substantially circular planes previously measured by measurement device 104, as shown in steps 632 and633, may be determined from first data set 516. The center of each plane may be determined by correcting for position and tilt as described previously. The concentricity error may then be determined at step 634 by assessing the variation in thelocation of the centers along the longitudinal axis of first part 116. Notably, although concentricity error may be determined using first data set 516, as will be discussed further below, it may be preferable to use second data set 518. As illustratedin FIG. 6, concentricity error of first part 116 is determined in parallel with determining the roundness of the first part at steps 624 and 628 and cylindricity error at steps 636, 637, and 638 of the first part. Alternatively, concentricity error maybe determined before or after roundness error and/or cylindricity error are determined.
Another geometric error that may be determined, if desired, is cylindricity error at step 636. Cylindricity error is typically considered the three-dimensional geometric difference between the cylindricity of an item from a reference cylinder. In an exemplary embodiment, cylindricity error is determined by using an LSC approach, whereby, a reference cylinder is sized so that the sum of the area between the cylinder and the surface of first part 116 inside the cylinder equals the sum of thearea between the cylinder and the surface of first part 116 outside the cylinder. The cylindricity error then can be determined as the difference between the maximum and minimum distance from this reference cylinder. As illustrated in FIG. 6,cylindricity error of first part 116 is determined in parallel with determining the roundness error of the first part at steps 624 and 628 and concentricity error of the first part at steps 634, 633, and 634. Alternatively, cylindricity error may bedetermined before or after roundness error and/or concentricity error are determined.
Process 600 may also include error removal and analysis of second data set 518, beginning at step 640. In this regard, process 600 removes the various errors and imperfections previously described, e.g., artifacts (step 644), position error(step 648), Abbe error (step 652), and tilt error (step 656). After the desired errors and artifacts are removed, geometric errors may be determined from second data set 518 in a similar manner as previously described or via other methodologiesrecognizable to those skilled in the art. In addition, the size of first part 116 may be determined at step 660. In an exemplary embodiment, the size of first part 116 would be determined by finding the minimum circumscribed circle (MCC), as defined inANSI B 89.3.1: 1972 Measurement of Out-of-Roundness, which is incorporated herein by reference in its entirety, at each plane of first part 116. The MCC is determined, in one exemplary embodiment, by iteratively adjusting the center at a plane of firstpart 116 so that a circle can be determined that is the smallest circle that encapsulates the entire surface of first part 116. This process is repeated at all planes, i.e., step 662, for which data was taken in measurement process 500. The largest MCCdetermined from an analysis of all planes indicates the minimum opening in second part 120 that would allow entry by first part 116.
In an exemplary embodiment of process 600, process 600 may additionally include a threshold exceed step 670, which determines whether any of the aforementioned errors, i.e., roundness, concentricity, or cylindricity, if determined, exceed acorresponding predetermined threshold error value. If one or more of the errors exceed a corresponding predetermined threshold value, the process does not proceed to step 664. Instead, the process ends. If, however, none of the errors exceed acorresponding predetermined threshold value, the process continues to step 664, where the size of the opening in second part 120 is determined.
In an alternative embodiment of process 600, process 600 may be configured to assess a first part with multiple features, e.g., multiple design diameters, as shown in FIG. 7. FIG. 7 shows a first part 116 with a first diameter 704, a seconddiameter 708, and a third diameter 712. In order to make a low clearance matching set between first part 116 and second part 120, process 600 may be designed to conduct the aforementioned steps on first diameter 704, second diameter 708, and thirddiameter 712. For instance, after measurement apparatus has measured first part 116 at all desired planes and at all desired locations around the first part, process 600 may determine the size and geometric errors for first diameter 704, then maydetermine the size and geometric errors for second diameter 708, and then may determine the size and geometric errors for third diameter 712. The size and geometric errors may be determined by the methods previously described or by other means known inthe art. The geometric errors may be compared against corresponding predetermined threshold values and if not exceeded, may be used to determine the size of the opening in second part 120 for each of the aforementioned diameters.
Concentricity error may also be determined at step 634 from the results of the MCC analysis. As the MCC analysis results in a circle being defined at each plane of data on first part 116, the centers of each of these circles can be compared forvariability along the axis resulting in a concentricity error determination.
Notably, the size of first part 116 as determined by the process described above may need to take into consideration other geometric errors, such as cylindricity error, at step 664. For example, if first part 116 is shaped like a banana, thelargest MCC may be smaller than necessary for first part 116 to slide into second part 120. Cylindricity error may be combined with the size determination to adjust the "effective size" of first part 116, that is, the smallest size of first part 116that will fit into second part 120.
With the calculation of the size and geometric errors of first part 116 completed, the manufacture of second part 120 may be performed. Typically, control system 108 develops a set of instructions for processing machine 112, which are derivedfrom process 600 that describes the dimensions of second part 120. As a final optional step, a clearance amount that adds additional space between the surfaces of first part 116 and second part 120 may be included in the determination of the necessaryopening size of second part 120. A clearance amount may be added to allow for easier mating of the two parts. In an exemplary embodiment, generally, the opening in second part 120 is enlarged by a small value, typically about 0.00005 inch. Any suchincrease in the opening size of second part 120 will vary as a function of the context in which the first part 116 and second part 120 will be used, desired ease of mating of the two parts, and other factors.
Referring again to FIG. 5, and specifically to step 540, the manufacture of second part 120 takes place on processing machine 112. Second part 120 is precisely hollowed out according to the instructions of control system 108 by, for example,removal tool 308. Hole enlarger is moved by lateral slides 316A-B and second part 120 is rotated by spindle 306, thus in combination, the movements allow for removal of material around the entire inner circumference of the opening of second part 120 andalong the longitudinal axis of second part 120. In an exemplary embodiment, removal tool 308 is capable of movement in two directions in the coordinate plane. However, in alternative embodiments processing machine 112 may be designed and configured sothat removal tool 308 is capable of movement in all three directions of the coordinate plane such that various shapes may be hollowed out of second part 120.
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