The operating conditions of many structures are inherently thermo-mechanical in nature, the change in temperature with time results in thermally induced stresses due to temperature gradients over the component during heating and cooling as well as thermal expansion mismatch between different materials in components and systems. This complexity is exacerbated for structural components that experience mechanically induced stress superimposed over thermally induced stress.
Thermo-mechanical testing is considerably more complex than isothermal mechanical testing. A major difficulty arises in controlling the temperature as a function of time so that thermal gradients on the test specimen are sufficiently small to guarantee continuum volume assumptions, and so that accurate and repeatable mechanical strains may be applied and controlled. In actual practice, because it is so difficult to achieve adequate control over gradients and heat up and cool down rates, the cycle times are slowed and become quite long, on the order of several minutes per heat up and cool down cycle.
Currently two major problems arise in the conduct of thermo-mechanical fatigue (hereinafter “TMF”) testing. They can be categorized as follows: (1) thermal management, and (2) length of test cycle time.
Thermal Management
Thermal gradients and their management play an important role in ensuring that continuum volume element assumptions—uniform volume, temperature and stress—hold true for the test. The main concerns are axial and radial gradients. Axial thermal gradients that vary during thermal cycling induce forces and unintentional strains on the test specimen. Radial thermal gradients that vary during thermal cycling induce cyclic internal stresses that cannot be measured axially. The photo of the specimen 1020 on the right in
There are many adjustments that must be made in order to obtain satisfactory dynamic thermal gradients: very often, the experimentalist is faced with the prospect of accommodating gradients at one end of the temperature cycle at the expense of the other end, and must adjust the coils to center the difference, accepting the gradients as they are present. This is due to a variety of factors, including: differences in heat conduction at either specimen end, differences in coil geometry at either specimen end, and the change in absolute position of the test section of the specimen as a function of temperature due to thermal expansion. Additional movement is experienced under the further application of mechanical strain.
Another problem arises from the movement of the radio frequency heating coils, which heat the specimen, with the rate of power application. A rapid change in flux often results in movement of the coil assembly. If the leads from the furnace/work station are long, and are part of the coil itself, considerable coil deflection occurs relative to the test section with high rates of power application.
TMF Cycle Time Optimization/Reduction
The need to keep thermal gradients minimized has the consequential effect of generally lengthening TMF heating/cooling cycle times. The actual cycle time is largely dominated by the cooling rate achievable on a given test apparatus.
A typical prior art testing fixture is shown in
Each coil 1001 is mounted on a separate adjustment assembly 1002, which is electrically insulated from the load frame by a dielectric block 1003, each assembly 1002 giving axial and concentricity control. Setscrews 1004 are used to lock a given assembly in place once a workable configuration is found. All coils 1001 are electrically in series, and act as one coil, as seen by the RF furnace. This fixture has been successfully employed in TMF testing.
A prior art improvement involving a cooling chamber device, as shown in FIG. 5, facilitates active cooling of the specimen, thus shortening test cycle time. The principle features of this cooling system are: (1) the cooling air impinges on the test specimen 1005 through an array of axial air jets (not shown) at 90 degrees around the specimen 1005 from a constant pressure source; (2) the array of axial jets provides relatively even specimen cooling; (3) the heating coil 1008, inside the cooling chamber 1006, does not interfere with air flow; and (4) an access port (not shown) allows an extensometer to be positioned out of the air flow.
This prior art device still presents a number of problems: (1) the device is quite noisy during operation due to the large flows of air; (2) despite the access port, the cooling chamber still presents an obstacle to access by the extensometer; (3) mounting the chamber itself is difficult and thus time-consuming; (4) the use of nozzles to direct cooling air at the specimen produces poor gradient performance; (5) the maximum temperature capability is too low for duplicating appropriate turbine airfoil temperatures; (6) it is very difficult to adjust the coil positions since they are located inside the chamber, and (7) the device is not easily adaptable to an alternate load frame and specimen mounting configuration that has a requirement of periodic specimen surface inspection during the test.
A thermo-mechanical testing apparatus is disclosed that improves existing thermo-mechanical testing techniques in numerous ways, including: (1) one embodiment facilitates the controlled movement of each coil section separately, thus providing the ability to actively alter the axial position of the RF induction coil with precision and repeatability; (2) another embodiment integrates moveable coil heating and active cooling controls; (3) another embodiment refines the coil device design by providing galvanic isolation from the load frame to minimize the possibility of RF arcing; (4) another embodiment may incorporate an extensometer into the cooling device design; (5) another embodiment improves the fixture design by enabling appropriate adjustment of the cooling device with respect to the test specimen, providing an alternate cooling approach that improves cooling and gradient control; (6) this embodiment radically reduces the operating noise level; (7) all embodiments dramatically improve thermal management and cycle time optimization; and (8) all embodiments enable line of sight access to the specimen test section for inspection during test cycling.
In one embodiment according to the invention, an improved adjustable heating coil support assembly for use in strain-controlled, thermo-mechanical fatigue testing of a specimen is disclosed. The assembly comprises a heating coil fixedly mounted to a moveable stage assembly that is slideably mounted to a slide affixed parallel to the axis of the specimen, and an individual stepper motor mounted to a ball-screw stage affixed to the moveable stage assembly, together with suitable controls. This assembly provides the ability to alter the axial position of the RF induction coil by controlled movement with precision and repeatability. The assembly can support up to a three-zone coil configuration (upper and lower coils, plus a middle coil).
In another embodiment according to the invention, an improved cooling apparatus for use in strain-controlled, thermo-mechanical fatigue testing of a specimen is disclosed. The apparatus comprises: a toroid-like shaped plenum comprised of two fastened, spaced apart components, a body and a cap, having a continuous sidewall around a hollow central bore, wherein the sidewall includes a continuous hollow channel running throughout the periphery of the cooling plenum, said cooling plenum surrounding the specimen, which is suspended within the hollow central bore of the cooling plenum at approximately its central axis, at a section along the specimen's length, wherein the interior side of the plenum sidewall is shaped so as to substantially conform to the cross-sectional shape of the specimen at the section and, in the direction of the specimen, shaped so as to cause pressurized air received at an inlet port in the plenum from a conduit to flow through the hollow channel and exit through the opening between the body and the cap onto the specimen surface at the section; and a flow valve situated in the conduit for controlling the flow of pressurized cooling air through the conduit to the cooling plenum.
In another embodiment according to the invention, an improvement to the cooling apparatus for use in strain-controlled, thermo-mechanical fatigue testing of a specimen is disclosed. The improvement comprises the toroid-like shaped plenum wherein the interior side of the plenum sidewall is shaped so as to substantially conform to the cross-sectional shape of the specimen at the section and, in the direction of the specimen, emulates a curved surface so as to cause pressurized air received at an inlet port in the plenum from a conduit to flow through the hollow channel and exit through the opening between the body and the cap and comprise a fluid jet adhering to the interior side of the plenum sidewall, entraining additional air via the Coanda effect, and directing the fluid jet of pressurized air and entrained air onto the specimen surface at the section.
In another embodiment according to the invention, an improvement to the adjustable heating coil support assembly for use in strain-controlled, thermo-mechanical fatigue testing of a specimen is disclosed as an adjustable heating coil and cooling plenum support assembly. The assembly comprises a heating coil and a cooling plenum each fixedly mounted to a moveable stage assembly that is slideably mounted to a slide affixed parallel to the specimen, and an individual stepper motor mounted to a ball-screw stage affixed to the moveable stage assembly, together with suitable controls. This assembly provides the ability to alter the axial position of the RF induction coil and the cooling plenum by controlled movement with precision and repeatability. The assembly can support up to a three-zone coil configuration (upper and lower coils, plus a middle coil).
In another embodiment according to the invention, an integrated heating coil and cooling apparatus for use in strain-controlled, thermo-mechanical fatigue testing of a specimen is disclosed. The apparatus comprises: a toroid-like shaped plenum; a moveable metallic heating coil comprised of a plurality of windings of a tube for placement within said central bore, such that the heating coil may be located substantially between the top and bottom surfaces of the plenum, surrounding the section of the specimen, the heating coil having an inlet and an outlet comprised of metallic tubing, wherein the inlet includes a first end and the outlet includes a second end, both of which are suitable for connection to a radio frequency induction furnace, wherein the cooling plenum and the heating coil are slideably mounted to a moveable slide-carriage assembly so as to facilitate synchronized movement of the heating coils and the cooling plenum; and a flow valve situated in the conduit for controlling the flow of pressurized cooling air through the conduit to the plenum. The moveable slide-carriage assembly may comprise a dielectric block slideably connected to a slide, which operates along the longitudinal direction of the specimen, and an individual stepper motor mounted to a ball-screw stage affixed to the slide-carriage assembly, together with suitable controls.
In another embodiment according to the invention, the flow valve may comprise a servo-proportional valve.
In yet another embodiment according to the invention, the moveable slide-carriage assembly may also include a sensor, such as an optical sensor, mounted so as to facilitate fine, repeatable positioning of the carriage anywhere along the slide.
In yet another embodiment according to the invention, the heating coils may be comprised of tubing having a substantially square cross section.
In yet another embodiment according to the invention, there is disclosed a method for setting up a thermo-mechanical fatigue test of a specimen. The method comprises: placing first and second heating coils around a specimen together with a cooling plenum; placing the specimen in a load frame suspended between two hydraulic collet grips or similar restraints that provide a constant adjustable gripping force (if the specimen is ceramic, a susceptor must be placed around the specimen or a flux concentrator must be used); placing first and second heating coils transverse to the specimen such that an extremity of each heating coil is positioned at approximately a first and second shoulder of the specimen; adjusting the heating coils about the specimen such that they are generally concentric with the diameter of the specimen; providing a radio frequency induction furnace; bringing the test specimen to test temperature by powering the RF coils; observing temperature readings at first and second ends of specimen gage position and at center of gage position; adjusting overall axial position of the heating coil as a unit such that the temperatures at first and second gage positions reasonably conform to each other; adjusting the spacing between the first and second heating coils along the axis of the specimen such that the temperature at the center of the specimen reasonably corresponds to the temperatures at the first and second specimen gage positions; recording positions of heating coils; proceeding to the next test temperature and repeating the process; repeating the process for each temperature to be tested; and selecting the coil positioning that provides the most favorable thermal gradient for the test.
In yet another embodiment according to the invention, there is disclosed a method for setting up a thermo-mechanical fatigue test of a metal or ceramic specimen with cooling. The method comprises: performing the steps in the preceding paragraph; positioning the cooling plenums such that the central axis of the heating coils and the specimen are generally coaxial with the central axis of a hollow bore of each cooling plenum providing a source of pressurized cooling air.
In yet another embodiment according to the invention, there is disclosed a method for setting up a strain-controlled, thermo-mechanical fatigue test of a ceramic or other non-metallic specimen. The method comprises: surrounding the specimen with a susceptor along the length of the specimen; and then following the steps for setting up a thermo-mechanical fatigue test of a metal specimen, as set forth above. The susceptor may be placed in contact with the specimen, in which case the heating coils will heat the susceptor, which will transfer that heat to the specimen by means of conduction. The susceptor may also be placed about the specimen with an air gap between the susceptor and the specimen, in which case the specimen will be heated by means of infrared thermal radiation from the susceptor. In lieu of a susceptor, a flux concentrator may be mechanically affixed to the heating coil so as to concentrate the magnetic flux from the coil onto the specimen.
A first embodiment of the present invention will be described hereinafter with reference to the drawings. Referring to
The moveable stage 57 includes a dielectric block 55, preferably comprised of a phenolic block, fixedly attached to sides 56A, 56B, preferably also of phenolic material, the combination of which is slideably attached to the stage assembly 53. The dielectric block 55 and sides 56A and 56B may be of unitary construction, such as a milled dielectric block. The moveable stage 57 may be translated along the stage assembly 53 via the ball screw 52, which is driven by the stepper motor 51. The dielectric block 55 and sides 56A and 56B include two elongated slots 58 and 59 milled in a direction normal to the direction of the stage assembly 53 opposite the stage assembly 53, along the first face 60. Two heating coil connection blocks 61 and 62 are slideably mounted into elongated slots 58 and 59. Each heating coil connection block 61, 62 includes a hollow conduit 63, 64 running through the blocks 61, 62 in a direction normal to the stage assembly 53 and parallel to elongated slots 58, 59, and further includes a connection fitting 65, 66 connected to a first end 73 of each conduit 63, 64 for connecting to a lead 67, 68 from a heating coil (not shown) and a connection fitting 69, 70 connected to a second end 74 of each conduit 63, 64 for connection to a lead (not shown) from a radio frequency induction furnace or other type of heating source (not shown). The heating coil connection blocks 61, 62 are preferably comprised of stainless steel. The heating coil connection blocks 61, 62 are fastened to the connection fittings 65, 66 and 69, 70 to facilitate uninterrupted flow, such as by threading the connection fittings 65, 66 and 69, 70 into the heating coil connection blocks 61, 62. Once the heating coil connection blocks 61, 62 are slideably positioned in the elongated slots 58, 59, and an appropriate position for a particular testing apparatus setup has been achieved (as discussed below), the heating coil connection blocks 61, 62 may be fixedly mounted into the dielectric block 55 via thumbscrews (socket head cap screws) 71, 72 or similar fasteners. It is also possible to place both hollow conduits 63, 64 in a single heating coil connection block 61 in a single elongated slot 58, although accuracy of placement of the heating coil may be adversely affected. And the hollow conduits 63, 64 may also be placed on opposite faces of the dielectric block 55 and sides 56A, 56B.
The stepper motor 51 in combination with the ball screw 52 facilitates precise altering of the position of the moveable stage 57 along the stage assembly 53 and thus precise positioning of the heating coil (not shown) both in the direction of the elongated slots 58, 59 attached to the moveable stage 57, and in the direction along the stage assembly 53. Preferably, the combination of the stepper motor 51, ball screw 52, moveable stage 57, and stage assembly 53 should perform controlled movements with extremely fine precision and good repeatability. In lieu of a stepper motor 51, a servomotor may also be capable of providing extremely fine precision and good repeatability. Preferably, the combination of the stepper motor 51, ball screw 52, moveable stage 57, and stage assembly 53 should produce positional accuracy of 0.0001 inch, with bidirectional repeatability of up to 50 micro-inches. Each stepper motor 51 is preferably equipped with a drive (not shown) that permits micro-stepping such that each rotation preferably can be controlled up to a resolution of 1 part in 51,200, with a ball screw lead of 0.1 inch per revolution, and preferably is capable of static holding torque of at least 48 oz.-in.
As shown in
In addition to the combination of a stepper motor 51, ball screw 52, moveable stage 57, and stage assembly 53, other fine adjustment devices with controlled movement, fine precision and good repeatability would also work for adjusting the position of the heating coil. An overall ability to make fine, repeatable adjustments in three independent modes of motion together with an ability to fix in place each of these modes once the proper location has been determined permits a much closer control of temperature gradients than had been available previously. A motor that rotates in small, fixed increments, such as a stepper motor or servomotor is required in order to obtain the fine adjustments needed for proper control of temperature gradients.
Referring to
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When the cap 102 and the body 101 are fastened together, the cooling effect is most pronounced with a space of between one thousandths of an inch (0.002″) and four thousandths of an inch (0.004″) at the interface between the two where interior surface 106 meets interior surface 162, to allow the air to flow from the continuous hollow channel 165 out through the interface where interior surface 106 meets interior surface 162. This may be achieved by the manner in which the body and cap are milled, or spacers or shims may be employed to provide the appropriate space.
The flow of cooling air to the cooling plenum 100 preferably is controlled with a servo proportional valve (not shown), which exhibits smooth and continuous control in the near closed region. A solenoid valve or other type of proportional valve may also be used to control the flow of cooling air.
Referring to
Other than the improvements discussed in the preceding paragraph, the two cooling plenums discussed herein are the substantially the same.
The diameter (169 as shown in
The height of the cooling plenum 100 or improved cooling plenum 200, i.e., the distance between surface 107 and surface 163 in cooling plenum 100, is selected to be as small as possible in order to minimize the obstructions to viewing the specimen during a test and also to permit room for an extensometer (not shown). The limiting factors are the need to deliver compressed air at up to 120 PSI, which effects the strength of the cooling plenum 100 or improved cooling plenum 200 needed for safe operation, and the length of the internal surface (106 plus 162) of the sidewall (105 and 160) needed to initiate the Coanda effect. Below a certain thickness, the Coanda effect is unlikely to arise, as there is not enough length of a body over which the air can flow to induce it. Above a certain size viewing room becomes very cramped. Regarding the plenum angles 270, 271, 272 (in
Many of the specimens tested today have cross-sections that are round, but not all. In accordance with the invention herein, the central bore 104 of the cooling plenum 100 or improved cooling plenum 200 is intended to conform to the cross sectional shape of the specimen 99, such that there is a generally uniform distance between the specimen 99 and the interior surface (106 plus 162) of the sidewall (105 and 160) around the entire specimen 99.
Referring to
A heating coil 98 is shown in
The diameters of the heating coil 98 and leads 109, 110 are specific to a user's needs. The heating coil 98 tubing diameter controls how many turns per linear length can be made, and therefore, the flux intensity. More flux means greater heating effect. The heating coil 98 tubing diameter also controls how much flux is delivered. As the heating coil 98 tubing diameter increases, the heating efficiency drops, but the temperature uniformity improves. As the heating coil 98 tubing diameter decreases, approaching the outer diameter of the specimen, heating efficiency increases, but the temperature uniformity degrades. If the heating coil 98 is too close to the specimen, it is not possible to keep the coil material cool enough. Maximum flux for heating purposes is delivered to the specimen 99 using tubing with a diameter of one-eighth inch, because it allows the largest number of turns per linear length of specimen. While round section tubing is most readily available and thus may be the tubing of choice, square section tubing enhances the flux patterns, improving heating efficiency, and thus is preferable.
The heating coil 98 is mounted to the dielectric block 55 as described in connection with
Thus, both the cooling plenum 100 and the improved cooling plenum 200 may be positioned together with the heating coil 98, and because the tube arm 111 goes through the dielectric block 55, it is electrically isolated. The cooling air supply is attached to the end of the copper tube arm 111 that emerges from the back of the dielectric block 55, and which is attached via clamp 55A and screw 55E. Preferably, the cooling air supply is fed via a flexible hose (not shown) to allow free movement of the cooling plenum 100 or improved cooling plenum 200 with respect to the cooling air supply.
In the embodiment of
In the embodiment of
In step 413 the lab assistant observes temperature readings at first and second gage positions 514, 515, i.e., at the outer edges of the section 514A of the specimen 99 that is being tested, i.e., the portion of the specimen on which the actual test will be conducted, and at the center gage position 515A, i.e., the midpoint between gage positions 514 and 515 along the test section 514A. The temperature readings may be obtained from thermocouples, an optical pyrometer, or a thermal imager (none of which are shown, but with which persons of skill in the art of thermal-mechanical testing apparatus will be familiar). In step 416, the lab assistant adjusts the overall axial position of the heating coils 98, 98A, such that the temperatures at first and second gage positions 514, 515 reasonably conform to each other. Upon making this adjustment, the temperature readings will likely show that the temperatures at the first and second gage positions 514, 515 will be either greater or less than the reading at the center of the gage length. If greater, heating coils 98 and 98A are too far apart and must be moved closer together along the axis of the specimen 99, by moving the moveable stage 57 along the stage assembly 53 employing the stepper motor 51. If less, heating coils 98 and 98A are too close together and must be moved further apart, again by moving the moveable stage 57 along the stage assembly 53 employing the stepper motor 51. In step 417, the lab assistant adjusts heating coils 98 and 98A so that they are closer together along the axis of the specimen 99. In step 418, the lab assistant adjusts heating coils 98 and 98A so that they are further apart. All such adjustments of the heating coils are made with the integrated adjustable heating coil 98/cooling plenum 100 (or 200) support assembly 53, which includes a stepper motor 51/ball screw 52/moveable stage 57/stage assembly 53 arrangement, as discussed above.
The purpose of the adjustments is to arrange spacing between the heating coils 98, 98A and a third heating coil (if used), such that the temperatures at the first and second gage positions 514 and 515 and the temperature at the center point of the gage position 515A reasonably conform to one another. This may take several repetitions until the temperatures reasonably conform. In step 419, the lab assistant records the positions of the heating coils 98, 98A, and a third heating coil (if used) for the test temperature, employing the method described above in connection with
While the foregoing has described what is considered to be the best mode and, where appropriate, other modes of performing the invention, the invention should not be limited to specific apparatus configurations or method steps disclosed in this description of the preferred embodiment. Those skilled in the art will also recognize that the invention has a broad range of applications, and that the embodiments admit of a wide range of modifications without departing from the inventive concepts.
This application claims priority to Provisional Application Ser. No. 61/813,963, filed on Apr. 19, 2013, the entire disclosure of which is incorporated herein by reference.