Patent Document

FIELD OF THE INVENTION  
       [0001]     The present invention relates to load frames used for imparting forces to test specimens, and more particularly to an apparatus and method for displaying, in three dimensional form, the forces acting on an alignment specimen being held between a movable member and a fixed member of a load frame, to more easily and accurately enable a technician to align the movable member relative to the fixed member.  
       BACKGROUND OF THE INVENTION  
       [0002]     Load frames are used in a variety of applications, in particular to apply forces to a test specimen. This allows strains to be measured on the test specimen and evaluated to determine if the material of the test specimen will be suitable for an intended application. Prior to analyzing the test specimen, however, the load frame has to be checked and calibrated with an alignment specimen to ensure that the force that will be applied to the test specimen is not angularly or concentrically misaligned with an axial center of the test specimen.  
         [0003]     Alignment of the load frame is accomplished by securing an alignment specimen between an upper head and a lower head of the load frame. The lower head is secured to a load bar which is movable linearly vertically on a pair of parallel rails. The upper head is fixed at a desired position on the load frame, and thereafter cannot move. The alignment specimen is secured at its opposite ends between the upper and lower heads. The alignment specimen typically includes a plurality of strain gages secured to it at spaced apart locations along its length. The strain gages provide indications of the bending force experienced by the alignment specimen at various points along its length as a result of the force applied to it by the lower head. If the lower head is angularly or concentrically misaligned, then the force that is applied by it will not be applied directly along the axial centerline of the alignment specimen. Thus, the alignment specimen will be subjected to bending forces at one or more point(s) along its length. An improperly aligned load frame will produce inconsistent test data when the test specimen is placed in the load frame and is subjected to a controlled force. This can lead operators to improper conclusions about the properties of the materials being tested.  
         [0004]     Presently available load frames are typically adjusted to remove angularity and/or concentricity misalignments of the lower head relative to the upper head by collecting data from the instrumented alignment specimen. The data is then displayed on a graph to aid the operator at making alignment adjustments. Often the graph is an X-Y graph which attempts to represent the bending condition(s) at one or more points along the alignment specimen in two dimensional fashion. Since the adjustments to the load frame are made independent of each other (i.e., concentric and angular adjustments are made independently), a key problem is to determine whether the bending being experienced at a given point on the alignment specimen is due to a concentric or angular misalignment of the lower head relative to the upper head. In practice, adjustments have been made for angular and concentric misalignments by trial and error from information presented on X-Y graphs (i.e., in two dimensional fashion). This is often a time consuming process, and it typically needs to be repeated every time new test hardware is used in a load frame.  
         [0005]     Accordingly, it would be highly desirable to provide an apparatus and method that more easily, and intuitively, allows the operator to determine and correct for angular and concentric misalignment of the lower head of a load frame relative to the upper head.  
       SUMMARY OF THE INVENTION  
       [0006]     The present invention relates to an apparatus and method for more quickly and easily correcting for concentric and angular misalignment of the lower head of a load frame relative to the upper head. In one preferred implementation, an instrumented alignment specimen having a plurality of strain gages at various points along its length is secured between the lower and upper heads of the load frame. The lower head is used to apply a force to the alignment specimen while the strain gage obtains information of the strains experienced at designated points along the alignment specimen. From this information the strain measurements are normalized such that only surface strains at a plurality of points on opposing surfaces of the alignment specimen are obtained. Normalized strain information is used to obtain deflection values at the designated plurality of points on the alignment specimen. The deflection values are scaled and then used to obtain X, Y and Z axis deflection values for each designated point along the alignment specimen. The X, Y and Z-axis values are then used to generate a three dimensional visual display on a display screen. The three dimensional image of the alignment specimen provides a slightly exaggerated representation of the deformation of the alignment specimen. The three dimensional image allows the operator to more quickly and easily make adjustments to the upper head of the load frame to align it such that the force that it produces is directed precisely along the axial center of the alignment specimen. Optionally, one or more two dimensional images of the alignment specimen can also be generated on the display screen.  
         [0007]     The method and apparatus of the present invention thus allows alignment of the lower head, relative to the upper head, of a load frame to be accomplished more quickly, easily and intuitively than would otherwise be possible with only two dimensional information presented in graphical form.  
         [0008]     The features, functions, and advantages can be achieved independently in various embodiments of the present inventions or may be combined in yet other embodiments. 
     
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0009]     The present invention will become more fully understood from the detailed description and the accompanying drawings, wherein:  
         [0010]      FIG. 1  is a perspective view of a conventional load frame with which the apparatus and method of the present invention is used;  
         [0011]      FIG. 2  is a perspective view of a typical alignment specimen incorporating a plurality of strain gages formed thereon that is used in the load frame of  FIG. 1  for alignment purposes;  
         [0012]      FIG. 3  is a side view of a simplified version of the alignment specimen to aid in explaining the formulas used in a preferred implementation of the present invention;  
         [0013]      FIG. 4  is a view of the alignment specimen secured between the upper and lower load heads and illustrating a small degree of angular misalignment of the upper head relative to the lower head; and  
         [0014]      FIG. 5  is a flowchart illustrating a plurality of operations performed in implementing a preferred implementation of the present invention. And  
         [0015]      FIG. 6  is an illustration of the three dimensional image of the alignment specimen showing its deformed shape caused by misalignment forces. 
     
    
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS  
       [0016]     The following description of the preferred embodiment(s) is merely exemplary in nature and is in no way intended to limit the invention, its application, or uses.  
         [0017]     Referring to  FIG. 1 , there is shown a conventional load frame  10  coupled to a conventional SCXI chassis  12 , and a computer system  14 . The computer system  14  is also coupled to a display monitor  16 . The load frame  10  is a well known component that may be purchased from a variety of manufacturers. One such manufacturer is MTS Systems Corporation of Eden Prairie, Minn. The SCXI chassis  12  is commercially available from National Instruments Corporation of Austin, Tex. The computer system  14  is a conventional PC that includes an internal analog-to-digital (A/D) board in communication with an output from the SCXI chassis  12 . Display  14  may be a conventional CRT or LCD panel.  
         [0018]     The load frame  10  generally includes a hydraulic press  18 , a pair of parallel, tubular guide rods  20  and a load bar  22  that is movable vertically along the guide rods  20 . The load bar  22  supports an alignment fixture  24 , a load cell  26  and a fixed upper head  28 . The press  18  supports a movable lower head  30  from a cylindrical member  31 . An instrumented alignment specimen  32  is secured at its opposite ends to the upper and lower heads  28  and  30 , respectively. A linear force is applied to the alignment specimen  32  by the press  18  acting on the movable lower head  30 , in response to signals generated from the computer  14  and the SCXI chassis  12 . Strain information generated by the alignment specimen  32  is then fed back to the computer  14  and displayed on the monitor  16 . It is a principal advantage of the present invention that the angular and concentric misalignment forces acting on the alignment specimen  32  are displayed by a three dimensional representation of the alignment specimen that highlights the deformation it experiences when the load is applied to it. This allows the operator to much more quickly, easily and intuitively apply alignments to the alignment fixture  24  via a plurality of adjustment screws (not shown) on the alignment fixture  24 , such that the upper load head  28  is aligned precisely along an axial centerline of the alignment specimen  32 .  
         [0019]     With brief reference to  FIG. 2 , the alignment specimen  32  can be seen in greater detail. The alignment specimen  32  preferably includes a pair of enlarged thickness end portions  34  separated by a central portion  36 . On the central portion at a plurality of spaced apart locations are a plurality of strain gages  38 . Strain gages  38  are bonded to the surface of portion  36  and coupled to a wire harness  40 , that is in turn coupled to the SCXI chassis  12 . In one preferred implementation eight strain gages are bonded to the central portion  36  of the alignment specimen  32 , however, a greater or lesser plurality of strain gages could be employed depending upon the accuracy that one desires to achieve during the alignment procedure.  
         [0020]     With brief reference to  FIG. 3 , a simplified representation of the two misalignments that need to be corrected for will be described. When the upper head  28  is precisely aligned with the lower head  30 , the lower head  30  will exert an upward force precisely along the axial centerline of the alignment specimen  32 . If the upper head  28  is not perfectly perpendicular to the axial centerline, then the lower head  30  will tend to exert a force at an angle  42 , which is drawn extremely exaggerated in  FIG. 3 . This is termed “angular” misalignment. If the upper head  28  is concentrically misaligned with the axial centerline (i.e., laterally displaced from the axial centerline along axis  43 ), this will also cause the lower head  30  to exert a force that is not applied directly along the axial centerline of the alignment specimen  32 . Accordingly, concentric and axial misalignments both need to be accounted for so that the lower head  30  is applying a force directly along the axial centerline of the alignment specimen  32 . When one or both of axial or concentric misalignments are present, such misalignments influence the strain readings sensed by the instrumented alignment specimen  32 . These misalignments would lead to inaccuracies in test results on an actual test specimen that is placed in the load frame  10 .  
         [0021]     Referring now to  FIGS. 4 and 5 , a system and method for presenting three dimensional alignment information, in accordance with a preferred embodiment of the present invention, will be described. With initial reference to  FIG. 4 , a simplified drawing of the alignment specimen  32  is illustrated to aid in understanding the various formulas employed in connection with implementing the method of the present invention. The alignment specimen  32 ′ has a thickness designated by “2y”. A first pair of strain gages  38  are located at a distance “X 1 ” from the stationary end of the alignment specimen  32 ′. A second pair of strain gages  38  are located at a second distance “X 2 ” from the stationary end of the alignment specimen  32 ′. Since  FIG. 4  shows a simplified version of the alignment specimen  32 ′ the enlarged end portions  34  at the end of alignment specimen  32  have been omitted because of two assumptions: 
        1. the majority of the enlarged portion  34  is gripped in the load frame head (either upper head  28  or lower head  30 ), and therefore restrained from bending; and     2. the end portions  34  are of sufficient thickness that bending at those areas defined by the enlarged ends  34  is significantly less than bending in the central portion  36  of the alignment specimen  32 .        
 
         [0024]     The bending in an alignment specimen can be represented as a cantilever beam held at one end, while loads are applied to the other end. The stationary end represents the upper head of the load frame which is immoveable with respect to the frame. The load M and P applied to the other end of the specimen represent the loads applied by the lower head when the system is out of alignment. When the system is perfectly aligned M and P will both be zero and no bending will occur in the specimen.  
         [0025]     The load case presented in  FIG. 4  is a complex load case represented by the following equations:  
             δ   =           PX   2     ⁡     (       3   ⁢   L     -   X     )       +     3   ⁢     MX   2           6   ⁢   EI               (   1   )               σ   =       M   +       P   ⁡     (     L   -   X     )       ⁢   Y       I             (   2   )             
 
         [0026]     where δ is the deflection away from zero (in the +/−y direction) at any position x along the length of the specimen, L is the length of the specimen, P is the Load from  FIG. 4 , M is the moment from  FIG. 4 , E is the modulus of elasticity of the material the specimen is constructed of, I is the cross-sectional moment of inertia of the specimen and σ is the surface stress at point x. It must be assumed that the width, height and cross-section of the specimen is constant along the entire length L, thus the moment of inertia is a constant I for the entire specimen.  
         [0027]     The strain at four points&#39; ε 1u , ε 1l , ε 2u  and ε 2l  as shown in  FIG. 4  can be calculated directly from the strains measured on the alignment specimen  32 ′. These strains will be normalized by the calculated average axial stress due to loading by the load frame  10 , resulting in the strains ε 1u , ε 1l , ε 2u  and ε 2l  representing only the surface strain due to misalignment of the upper head of the load frame. The subscript letter  u  will be used to arbitrarily designate one side of the specimen, and the subscript letter  l  the other side.  
         [0028]     Using equations (1) and (2) and basic mechanics of materials relating to stress analysis, the following equations can be derived for the bending case of the alignment specimen  32 ′: 
 
 For the upper (u) side:  
                 δ   u     ⁡     (   X   )       =         X   2     ⁡     (         (       ɛ     1   ⁢   u       -     ɛ     2   ⁢   u         )     ⁢   X     -     3   ⁢     (         ɛ     1   ⁢   u       ⁢     X   1       -       ɛ     2   ⁢   u       ⁢     X   2         )         )         6   ⁢     (       X   1     -     X   2       )     ⁢   Y               (   3   )                 M   u     =       EI   ⁡     (       L   ⁡     (       ɛ     1   ⁢   u       -     ɛ     2   ⁢   u         )       -       ɛ     1   ⁢   u       ⁢     X   2       +       ɛ     2   ⁢   u       ⁢     X   1         )           (       X   1     -     X   2       )     ⁢   Y               (   4   )                 P   u     =       -     EI   ⁡     (       ɛ     1   ⁢   u       -     ɛ     2   ⁢   u         )             (       X   1     -     X   2       )     ⁢   Y               (   5   )             
 
 For the (l) lower side:  
                 δ   l     ⁡     (   X   )       =         X   2     ⁡     (         (       ɛ     1   ⁢   l       -     ɛ     2   ⁢   l         )     ⁢   X     -     3   ⁢     (         ɛ     1   ⁢   l       ⁢     X   1       -       ɛ     2   ⁢   l       ⁢     X   2         )         )         6   ⁢     (       X   1     -     X   2       )     ⁢   Y               (   6   )                 M   l     =       EI   ⁡     (       L   ⁡     (       ɛ     1   ⁢   l       -     ɛ     2   ⁢   l         )       -       ɛ     1   ⁢   l       ⁢     X   2       +       ɛ     2   ⁢   l       ⁢     X   1         )           (       X   1     -     X   2       )     ⁢   Y               (   7   )                 P   l     =       -     EI   ⁡     (       ɛ     1   ⁢   l       -     ɛ     2   ⁢   l         )             (       X   1     -     X   2       )     ⁢   Y               (   8   )             
 
         [0029]     Because the alignment specimen is assumed to be symmetrical across the loading axis, the values of δ l  and δ u  will be exactly opposite, while M l  and M u , and P l  and P u  will be identical, within the error introduced to the system from the error in measurement in the strain gages  38 .  
         [0000]     Three-Dimensional Display  
         [0030]     Equations (3) and (6) are used directly to create the three-dimensional display because they represent the deflection of the alignment specimen  32  away from the load axis. Three matrices are constructed such that they define a three dimensional surface and two dimensional projections of this surface. This surface, when graphed using a parametric plot, shows a three-dimensional representation of the specimen, including any bending that occurs due to sensed mis-alignment at those locations where the strain gages  38  are located. The projections of the surface help to emphasize the misalignment of the end user. The matrices are expressed as follows: 
 
 X (1, x )= S *(δ l ( x )+ y ) 
 
 X (2, x )= S *(δ u ( x )− y ) 
 
 X (3, x )= S *(δ u ( x )− y ) 
 
 X (4, x )= S *(δ l ( x )+ y ) 
 
 Y (1, x )=− w/ 2 
 
 Y (2, x )=− w/ 2 
 
 Y (3, x )= w/ 2 
 
 Y (4, x )= w/ 2 
 
 Z (1, x )= x  
 
 Z (2, x )= x  
 
 Z (3, x )= x  
 
 Z (4, x )= x  
 
         [0031]     The term “X” is the parametric x-axis positions, “Y” is the parametric y-axis positions and “Z” is the parametric z-axis positions for all numbers x. The term “S” is a user selectable scale factor which modifies the visualization of the deflection to create a more pronounced (i.e., exaggerated) deflection effect for the user. The projections are made by setting each value of a given axis to zero. For example, for a X-Z projection, X would all be zeros. For a Y-Z projection, Y would be all zeros, and for a X-Y projection Z would be all zeros.  
         [0032]     As the strains measured from the specimen change, the values of δ l (x) and δ u (x) change, thus changing the parametric plot to represent the current bending condition.  
         [0033]     With reference to  FIG. 5 , the operation of one preferred implementation of the method will be outlined. In operation  46 , strain information is obtained at a plurality of locations on the alignment specimen  32 ′, as provided by the strain gages  38 . In operation  48 , the strains are normalized to obtain only surface strain information at a designated plurality of points on opposing surfaces of the alignment specimen  32 ′.  
         [0034]     In operation  50 , the normalized strains are used to obtain deflection values at the designated plurality of points on the alignment specimen  32 ′. In operation  52   a , the deflection values obtained in operation  50  are then used to obtain X, Y and Z axis deflection values for each of the designated points along the alignment specimen  32 . At operation  54   b , a scale factor (e.g., 5, 10, 100, etc.) is applied to the deflector values. This provides a three dimensional representation of the deflection of the alignment specimen at each of the given designated points that is slightly exaggerated to enable an operator to more readily visualize the deformation affecting the alignment specimen. In operation  54 , X, Y and Z axis deflection values for each of the designated points that were determined in operation  52   b  are used in plotting a three dimensional visual representation of the alignment specimen on a display, such as monitor  16  ( FIG. 1 ). The three dimensional display of the alignment specimen includes a slightly exaggerated representation of the deformation of its shape caused by the misalignment forces. Being able to readily see a deformed representation of the alignment specimen  32  enables an operator to more quickly, easily and more intuitively apply adjustments to the adjustment screws on the alignment fixture  24  of the load frame  10 .  
         [0035]     A representation of the deformation of the alignment specimen  32  is illustrated in  FIG. 6 .  FIG. 6  also illustrates a two dimensional projection  32   a  in a Z-Y plane  56  and, a two dimensional projection  32   b  in a Z-X plane  58 . Projection  32   a  represents the deformation obtained by setting the X-axis deformation values in the foregoing formulas to zero. Projection  32   b  represents the deformation obtained by setting the Y-axis deformation values to zero. Optionally, an additional three dimensional projection  60  could be provided to illustrate the relative lateral displacements of various portions of the alignment specimen  32  in only the X-Y plane. In this example, circle  62  corresponds to portion  62   a  on the specimen  32 , circle  64  corresponds to portion  64   b  on the specimen  32 , circle  66  corresponds to portion  66   a  on the specimen  32 , circle  68  corresponds to portion  68   a  on the specimen, and circle  70  corresponds to portion  70   a  on the specimen  70 .  
         [0036]     The system and method of the present invention thus allows an operator to more easily adjust the components of a typical load frame to remove any concentric and/or angular misalignment of the upper head relative to the lower head. By providing a three dimensional display of the alignment specimen with a slightly exaggerated representation of the deformation of the specimen, the operator can more easily and intuitively apply the needed corrections to the load frame even more quickly than with previously developed two dimensional graphical alignment systems. Since the three dimensional display is provided essentially in real time, this further expedites the process of aligning the components of the load frame.  
         [0037]     While various preferred embodiments have been described, those skilled in the art will recognize modifications or variations which might be made without departing from the inventive concept. The examples illustrate the invention and are not intended to limit it. Therefore, the description and claims should be interpreted liberally with only such limitation as is necessary in view of the pertinent prior art.

Technology Category: g