RANDOM VIBRATION GENERATING APPARATUS

Abstract: A shaker table (10) for testing and quality control of devices attached to the table is shown. The mounting table has pneumatic exciters (50) attached thereto. The mounting table (20) provides uniform distribution of forces applied by the pneumatic exciters (50). The forces are evenly distributed in all directions from the impact of the exciters on the mounting table. The mounting table (20) is supported on a foundation (2) by adjustable supports (4). The exciters are supplied with pressurized air from a source (12) through an airline (14).

Description: RANDOM VIBRATION GENERATING APPARATUS CROSS REFERENCE TO RELATED APPLICATION The present application is a continuation and part of United States Patent Application 07/487,457, filed March 1, 1990, for Method and Apparatus for Generating Substantially Uniform, Randomly Oriented Vibrations in a Shaker Table. Both applications are in the name of applicant herein. BACKGROUND OF THE INVENTION Field of the Invention The present invention relates generally to the shaker tables to which manufactured devices are mounted for vibrational testing. More particularly, the present invention relates to a specific mounting table and to the exciters or vibrators mounted thereto. Description of the Prior Art Shaker tables for testing the reliability of manufactured devices are well known. Such shaker tables are used either under laboratory conditions or in conjunction with an assembly line. Often, shaker tables are mounted within thermal chambers, which gives the added flexibility of testing for defects in the manufactured product which may be exposed by elevated temperature or temperature cycling. The shaker tables typically include a platform or mounting table upon which a device to be tested is mounted. Exciters or vibrators are attached to the mounting table to vibrate, the device. It is necessary to provide an even distribution of the vibration amplitude, magnitude, direction and frequency in a range. Typical of such arrangements is U.S. Patent No. 4,735,089 issued to Richard L. Baker, et aJL. That patent and others attempt to establish a uniform amplitude to the mounting table from the exciters over the range of frequencies generated. The Baker patent identifies a problem with rigid shaker tables in achieving the objective of creating random vibration of substantially equal amplitude over the range of frequencies in a multi-axial direction. Baker does so by use of a flexible shaker table that is said to resolve potential resonance problems normally inherent in rigid mounting tables. The end result of this multi-axial excitation is a relatively complex mounting table or platform, having multiple layers, multiple connectors and multiple potential wear points. My co-pending application discloses and claims a honeycomb table structure which achieves random vibration in multi-axial directions in a relatively rigid table. The present invention is a improvement of the table disclosed in my pending application. It is also inherent in the manufacture and use of shaker tables that energy, in the form of compressed air to operate the exciters, will be required. Heretofore, the exciters that have incorporated resilient polymeric materials in the piston portion of the cylinder piston combination of the exciter, have been unable to cycle at higher rates for a given air pressure. None of these pistons have been cooled by the operating air pressure. The rapid movements of the piston in the cylinder have generated heat that melted the materials from the thermal environment in which they were placed or which they internally generated. A prior art vibrator is shown in U.S. Patent No. 3,376,790. There has never been a pneumatic exciter specifically made for the requirements of shaker tables. Specifically, exciters which individually vary the impact cycle rate between the piston and cylinder of the exciter have not been known. SUMMARY OF THE INVENTION It is the principle object of the present invention to provide a rigid mounting table of a shaker table which randomly disburses any given force applied to the shaker table by an exciter in a multi-axial direction and in a substantially uniform matter. It is a related object of the present invention to provide an exciter for a shaker table which uses a resilient programmer. It is still another object of the present invention to provide a variable rate exciter for a shaker table. Accordingly, the present invention is directed to a shaker apparatus with a mounting table made of a cored or honeycomb structure in such a way that the mounting table, together with any device or manufactured product attached thereto, when vibrated by an exciter, will provide multi-axial random or quasi-random vibrations, even if the excitations are delivered to the table in only one axial direction, due to the dispersive effects of the cored or honeycomb structures and the mode of construction of the mounting table or platform. Manufactured or test devices are connected to the mounting table, which can be supported on the mounting system within a test chamber. This invention is also directed to a method of changing the distribution of relative magnitudes of the x, y, z, and rotational components of the vibrations by manipulation or arrangement of the exciters which impart excitations to the shaker table. A section of aluminum honeycomb assembly has been tested by placing a triaxial set of accelerometers thereto. A modal hammer was used to excite the assembly normal to the assembly and then in the planes of the assembly and the responses were measured in each case. Regardless of the axis of excitation, responses in all axes were observed. Subsequent theoretical analysis of the reason for this behavior led to the conclusion that stress wave propagation scattering (or deflection from its path) was due to the stress wave encountering a junction of the honeycomb assembly. A "junction" is an intersection of the top or bottom face sheets with the assembly, the intersection of a common interlayer sheet with a honeycomb structure, or the intersection of a honeycomb structure with another honeycomb structure oriented in a different direction within the same layer. The junctions deflect energy from one direction into energy in directions other than the direction of the arriving elastic wave. This effect generates a response in all directions after multiple refractions and reflections of the stress wave within the honeycomb assembly. This physical phenomena allows the operation of this invention wherein the elastic wave scattering will help generate multi-axial vibration with only a limited number of exciters. A similar effect occurs in the cored structure which is more detailed herein. In an alternative embodiment, the mounting table includes a central core of homogeneous material having a preselected area and thickness. A mounting surface covers one or more surfaces of the central core. Mounting holes are formed in the mounting surface. A bottom surface of the central core has a plurality of cavities formed therein along predefined or perpendicularly intersecting rows and columns, defining a junction of the intersection. The bottom surface is covered with an adhesive layer and an aluminum sheet, covering the open cavities. In addition to the mounting table construction, multi-axial vibration is enhanced by vectoring of the exciters. Variations in the line spectra of the excitations from the exciters may be accomplished by modulating the air pressure imparted to the exciters or emanating from the exciters. This modulation can be accomplished by using the exhaust of a rotary ball vibrator as the input to one or more linear exciters. The exhaust pressure from the rotary ball vibrator is modulated in an irregular but cyclical fashion as the ball rotates and passes an exhaust port. The rotary vibrator can be used to add low frequency excitation to the mounting table. Modulation can also be accomplished by varying the exhaust backpressure on the linear exciters in order to control the cycle rate of the impacts. Another modulation method is to pressurize an accumulator and exhaust the air to the exciters while holding the accumulator input closed, allowing the pressure to decrease as the exciters use the air. This will sweep the line spectra generated by the exciters. After the air pressure has dropped to some desired pressure, the inlet of the accumulator is opened and the air pressure is thereby increased, again sweeping the cycle rate of the exciters. This is repeated as necessary. A combination of accumulators can also be used as an extension of this technique. Also, the exhaust from the linear exciters can be throttled or restricted to control the excitation frequency. An analog voltage controlled pressure regulator can also be used to control inlet pressure which is modulated over time to attain the desired spectrum smearing. Any combination of the foregoing modulation methods together with other methods detailed herein can be used without departing from the scope and spirit of the invention. A tunable dampening device is shown to dampen the vibrations in the table in one axial direction, with the extent of dampening capable of being easily adjusted. The exciters are attached to the mounting table through attachment holes. The exciters include an outer cylinder to which an air inlet is connected. A hollow interior of the cylinder receives a piston assembly comprised of an outer body and a resilient programmer connected thereto. The programmer reciprocates within the cylinder and strikes a rebound surface near the position at which the exciter is connected to the mounting table. The piston assembly goes through a thrust stroke and a rebound stroke in completing a cycle. Inlet passageways in air fluid communication with the air inlet means direct pressurized air through the outer body of the piston and into an interior thrust chamber of the cylinder. The piston assembly moves toward the rebound surface of the cylinder where a rebound chamber is defined, exhausting air through the exhaust port and striking the rebound surface of the cylinder with the programmer of the piston assembly. In the rebound stroke the air inlet means supplies air to the programmer, which programmer, through cooling passageways, pressurizes the rebound chamber and moves the piston assembly away from the rebound chamber and toward the thrust chamber. In an alternative embodiment of the exciter, the piston assembly includes means for rotating a piston in the cylinder. As the piston rotates the stroke length varies. The size of the inlet through which pressurized air from the air inlet means is received by the piston, and/or the size of the exhaust port, change as the piston is randomly rotated. This varies the pressure in the thrust chamber and, correspondingly, the speed and force with which the piston strikes the rebound surface. This invention meets the need for a rigid shaker apparatus which accurately translates intended vibrations to a device to be tested without encountering local resonance peaks, and it solves the resonance problem without using elastomeric or other damping means. The apparatus relies on the elastic wave scattering effects of the cored, honeycomb or cavity filled structure. Since damping techni-ques are not used, the desired multi-axial vibrations can be generated using only a 5 limited number of exciters, and only a limited amount of excitation. Other aspects, features and details of the present invention can be more completely understood by reference to the following detail description of a preferred 10 embodiment, taken in conjunction with the drawings, and from the appended claim. BRIEF DESCRIPTION OF THE DRAWINGS Fig. 1 is a perspective view of the entire shaker apparatus. 15 Fig. 2 is a perspective view of one embodiment of the invention. Fig. 3A is an exploded diagrammatic side view of one embodiment of a mounting table of Fig. 1 using a honeycomb assembly. 20 Fig. 3B is a top view in enlarged scale of the honeycomb structure used in the embodiment of the mounting table. Fig. 3C is an exploded diagrammatic perspective view of an embodiment of the honeycomb assembly where a 25 plurality of honeycomb layers are combined in a vertical array to form the shaker table of the invention. Fig. 3D is an exploded diagrammatic perspective view of another embodiment of the honeycomb assembly where a plurality of honeycomb layers are combined in a planar 30 array to form the shaker table of the invention. Fig. 4 is a perspective view of one embodiment of the table of Fig. 1 using a cored configuration. Fig. 5A is a graph depicting the x versus y directional response in a test device used in the shaker 35. apparatus depicted in Fig. 1 indicating that the various axial directions are incoherent relative to one another. Fig. 5B is a graph depicting the x versus z directional response in a test device used in the shaker apparatus depicted in Fig. 1 indicating that the various axial directions are incoherent relative to one another. Fig. 5C is a graph depicting the y versus z directional response in a test device used in the shaker apparatus depicted in Fig. 1 indicating that the various axial directions are incoherent relative to one another. Fig. 5D is a graph depicting the vibrational response in the x direction of a test device used in the invention. Fig. 5E is a graph depicting the vibrational response in the y direction of a test device used in the invention. Fig. 5F is a graph depicting the vibrational response in the z direction of a test device used in the invention. Fig. 6A is a diagrammatic depiction of an embodiment of the invention wherein a wedge-shaped support is provided for vectoring the excitations. Fig. 6B is a diagrammatic depiction of another embodiment of the invention wherein air pressure to the exciter is modulated by a rotary vibrator. Fig. 6C is a diagrammatic depiction of yet another embodiment of the invention wherein air pressure to the exciter is modulated by an accumulator. Fig. 6D is a diagrammatic depiction of yet another embodiment of the invention wherein air pressure to the exciter is modulated by an analog valve. Fig. 6E is a diagrammatic depiction of yet another embodiment of the invention wherein pressure to a second exciter is modulated to output from a first exciter. Fig. 6F is a diagrammatic depiction of yet another embodiment of the invention wherein air pressure to each of several exciters is- modulated by feeding each exciter with air through a single manifold. Fig. 6G is a diagrammatic depiction of yet another embodiment of the invention showing a combination of throttling, use of several exciters being fed by one line, and use of large and small exciters. Fig. 7A is a diagrammatic depiction of yet another embodiment of the invention wherein air pressure in the exciter is modulated by valving on the exciter exhaust. Fig. 7B is a diagrammatic depiction of yet another embodiment of the invention wherein the input of several exciters receive air from a single manifold which in turn receives modulated air pressure from the exhaust of a rotary ball vibrator. Fig. 7C is diagrammatic depiction of yet another embodiment of the invention wherein air pressure from exhaust of the exciter is restricted. Fig. 8 is a diagrammatic depiction of a tunable damper for notching the vibration spectrum. Fig. 9 is a front elevational view of yet another embodiment a shaker table fabricated in accordance with the invention. Fig. 10 is a bottom plan view of the invention. Fig. 11 is a fragmentary enlarged sectional view taken in the plane of line 11-11 of Fig. 10. Fig. 12 is an enlarged exploded perspective view of a mounting table of the invention. Fig. 13 is a bottom plan view of a central core of the mounting table shown in Fig 12. Fig. 14 is an enlarged fragmentary sectional view taken in the plane of line 14-14 of Fig. 13. Fig. 15 is a fragmentary enlarged sectional view taken in the plane of line 15-15 of Fig. 13. Fig. 16 is a fragmentary enlarged sectional view taken in the plane of line 16-16 of Fig. 11. Fig. 17 is a fragmentary enlarged sectional view taken in the plane of line 17-17 of Fig. 10. Fig. 18 is a fragmentary enlarged sectional view taken in the plane of line 18-18 of Fig. 17. Fig. 19 is an enlarged sectional view taken in the plane of line 19-19 of Fig. 17. Fig. 20 is an exploded perspective view of an exciter used in conjunction with the invention. Fig. 21 is an enlarged sectional view of another embodiment of the exciter of the invention. Fig. 22 is a sectional view taken in the plane of line 22-22 of Fig. 21. Fig. 23 is a sectional view taken in the plane of line 23-23 of Fig. 21. Fig. 24 is a sectional view taken in the plane of line 24-24 of Fig. 21. Fig. 25 is an exploded perspective view of the exciter shown in Fig. 21. Fig. 26 is an exploded perspective view of another embodiment of the exciter of the invention. DESCRIPTION OF THE PREFERRED EMBODIMENTS A shaker apparatus 10 includes a platform or mounting table 20 attached to isolating supports 4 and one or more exciters 50. A device or manufactured product 6 to be tested is coupled or fixed to the mounting 20 table and the exciters 50 operated to shake the shaker apparatus 10 and the attached device. A dispersive layer within the table structure and manipulation and arrangement of the exciters 50 allow the device to be subjected to randomly distributed multiaxial and multirotational, incoherent vibrations with a limited number of exciters 50 oriented in one or a limited number of directions and without the need for damping or complex shaker table construction. Turn now to Fig. 1. The shaker apparatus comprises the mounting table 20 mounted to a foundation 2 by at least three of the supports 4, two of which are shown in Figure 1. The foundation 2 is an essentially vibration-free support for the shaker apparatus 10. Although shown as being supported from below, the apparatus can also be supported from any direction. The device 6 to be tested is securely fastened to the mounting table 20. Preferred methods of fastening include a bolting device 6 into inserts in the mounting table 20 with bolt 8 (as shown in Fig. 1) , clamping the device 6 onto the top surface of the mounting table 20, creating a vacuum between the device 6 and the surface of table 20 or using magnetic forces to attach device 6 to the top surface of the mounting table 20. The mounting table 20 is mounted on the foundation 2 by a plurality of the supports 4, which supports 4 isolate the motion of the mounts table 20 from the foundation 2. At least three of the supports 4 are required. The suppcts 4 are attached to the mounting table 20 through load spreaders or inserts disposed into table 20 to reinforce table 20 at points of high local loading. One or more of the exciters 50 are attached to the mounting table 20. The exciters 50 are mounted to the mounting table 20 by vector supports 10. To a substantial degree only the vibrational energy generated by exciter 20 is coupled to the device 6 and all other extrinsic sources of energy or vibration are isolated therefrom. The exciters 50 each impart excitations to the mounting table 20 along only one direction although this may, as discussed below, result in excitations appearing at the device 6 in any or all the six possible degrees of freedom of motion. An air source 12 is connected to an airline 14 which is, in turn, connected to the input of the exciters 50. This air source 12 supplies the air pressure which drives the exciters 50 to generate and impart vibrational energy to the mounting table 20. The exciter 50 can be any device which imparts excitation to table 20. Preferably, the exciter 50 is a pneumatic air operated vibrator. The exciters 50 may be attached to any part of the mounting table 20. If more than one of the exciters 50 are used, they should ideally be positioned to impart orthogonal excitations with respect to one another. In addition to being attached to the outside surface of the mounting table 20 (as shown in Fig. 1) , the exciters 50 can be attached to the inside surface of or disposed within the mounting table 20 as shown in Fig. 2. This uniquely constructed mounting table 20 is constructed as a hollow or partially hollow cube or body. Since the exciters 50 are mounted inside the mounting table 20, more space is available on its outside surface for mounting the device 6. Any number of the exciters 50 may be used, but the attributes of the table and several methods of vectoring and modulating the excitations discussed below require only a limited number of the exciters 50 to impart multiaxial vibrations to the device 6. Referring to Fig. 3A, one embodiment of the mounting table 20 is constructed of honeycomb material. The mounting table 20 comprises a honeycomb assembly 30 sandwiched between a top surface sheet 32 and a bottom surface sheet 34. The honeycomb assembly 30 is attached at multiple points of contact to the top surface sheet 32 and the bottom surface sheet 34. The surface sheets 32 and 34 are constructed of plastic, metal or a composite material. The methods of attaching the surface sheets 32 and 34 to the honeycomb assembly 30 are preferably by adhesive bonding, diffusion bonding, welding or brazing. The honeycomb assembly 30 comprises at least one layer 36 of honeycomb structure formed from undulating walls 38 which extend between the top and bottom surface sheets 32 and 34 in a first direction. The walls 38 define within the layer 36 of honeycomb structure an axis of maximum stiffness. Additional of the layers 36 of honeycomb structure, if present, are disposed in a second and third direction which may be perpendicular to the first direction. Other angles of orientation may be used in order to attain the desired mechanical properties. As best seen in the top sectional view in enlarged scale in Fig. 3B as seen in Fig. 1, the layer 36 of the honeycomb assembly 30 is formed from the corrugated walls 38, which comprise thin vertically oriented metallic strips, e.g., of aluminum, which are bonded together at contacting surfaces 40 to form a hexagonal matrix of open ended cells. The layer 36 utilizes a conventional internal honeycomb structure and therefore has nonisotropic stiffness. Due to the internal welding and periodic double wall structure where the strips attach one to the other, the layer 36 is stiffer in one direction than in the orthogonal direction. The honeycomb assembly 30 may be comprised of the single layer 36 of honeycomb. It is preferred that the honeycomb assembly 30 be quite thick, namely one to four inches thick as measured along thickness 31 of Fig. 3A. However, as diagrammatically depicted in Fig. 3A, the honeycomb assembly 30 may also be comprised of a plurality of the identical layers 36. Each of the plurality of the layers 36 can be of identical or different construction in relative thickness, weight, strength or cell size. The thickness 31 then is the cumulative thickness of the plurality of the honeycomb layers 36. In one preferred embodiment, the honeycomb assembly 30 is comprised of a plurality of the honeycomb layers 36, with the stiffer axis of the layers 36 alternately oriented in at least two different directions. The stiff axis is symbolically depicted in Figs. 3A and b by a double-headed arrow. Each of the layers 36 in the plurality which comprises the honeycomb assembly 30 is attached to each of the next adjacent layers 36 by adhesive bonding, diffusion bonding, welding or brazing. A vertically stacked array of the layers 36 is diagrammatically depicted in Fig. 3C wherein each of the layers 36 is disposed above or below the next adjacent layer 36 with its stiffer axis rotated to any arbitrary angle (illustrated in Fig. 3C as a 90-degree angle) relative to the orientation of the stiffer axis of the adjacent layer 36. Fig. 3D diagrammatically depicts a plurality of the layers 36 laid in a planar array wherein each of the layers 36 lies in the same plane of all the other layers 36 in the honeycomb assembly 30, but is arranged so that no two of the layers 36, sharing a common side, have the same spatial orientation in the plane relative to their stiff axes. Although shown in Fig. 3D to be 90 degrees, the angles or orientation may be arbitrarily chosen. In the embodiment shown in Fig. 3A, the honeycomb assembly 30 is two or more of the layers 36 of honeycomb with a common interlayer surface sheet 42 attached between each adjacent pair of the layers 36. The interlayer surface sheets 42 are flat sheets of metal, preferably aluminum, and the method of attaching the interlayer surface sheets 42 to the layers 36 are preferably adhesion bonding, diffusion bonding, welding or brazing at their points of contact. The topmost and bottom-most of the layers 36 as seen in Fig. 3A are attached at their points of contact to the top surface sheet 32 and the bottom surface sheet 34. Another embodiment of the mounting table 20 is shown in Fig. 4. A cored table 44 is a slab of material which has cores 46 formed at various locations along its top or outer surface. The material preferably has a high strength-to-weight ratio and could be titanium, magnesium or a composite of different materials. In Fig. 4, each of the cores 46 has been drilled within approximately one quarter of an inch of each adjacent core 46. The cores 46 perform a similar function as the honeycomb assembly 30 of Fig. 3, in creating multiaxial vibrations from unidirectional excitation by diffusion through the cores 46. In order to preserve strength in the cored table 44 each of the cores 46 is drilled to a depth which is less than the thickness of the slab. Thus, no core 46 is drilled entirely through the slab. In addition, the cored table 44 may have a surface sheet 48 bonded, braised or welded to the open cored surface to increase strength and stiffness. In a second alternative embodiment shown in Fig. 9, the mounting table 20 is formed principally of an aluminum central core 100, an upper surface of which has mounting holes 102 and 104 (Figs. 12-14). The bottom surface has cavities 106 and 108 formed therein through holes 110 formed in the bottom surface. The cavities 106 and 108 are formed by milling or similar machine tooling process. The cavities 106 are smaller than the cavities 108. The cavities 106 are centered about the mounting holes 102. The holes 102 define positions where the exciters 50 are mounted to the bottom surface of the mounting table 20. The cavities 106 are arrayed in patterns of four about the mounting holes 102, leaving a larger area of solid aluminum in the central core 100 about the mounting holes 102. The mounting holes 102 define the center of a four cavity array 112 of the cavities 106 (Fig. 13) . The larger square cavities 108 are formed in perpendicularly intersecting rows 114 and columns 116 between the mounting holes 102. The other mounting holes 104 are likewise used for mounting the manufactured devices 6 (not shown in this embodiment to the mounting table 20. Once the central core 100 is formed, the bottom surface receives a layer of adhesive film 118, such as those made by American Cyanamid Company under the trademark FM300K (Fig. 12) . To that adhesive film 118 an aluminum alloy skin 120 is bonded, covering the mounting holes 104 and aligning with the holes 102. The exciters 50 are mounted through the holes 102 to the mounting table 20. An integral bottom surface of the mounting table 20 is formed. The top surface includes a rubber mounting sheet 122 through which sheet 122 are formed the holes 102 and 104. An insulating layer 123, such as sold under the trademark Zircar Type 100, is disposed between the central core 100 and the mounting sheet 122. As previously mentioned and as is best seen in Fig. 9, the holes 102 are formed at positions in the mounting table 20 where the exciters 50 connect to the bottom surface of the mounting table 20. The remaining holes 104 are more densely spaced among the rows 114 and columns 116 at positions where an exciter 50 is not attached (Fig. 15 and 16) . The construction of the central core 100 with the cavities 106 and 108 allows for uniform dispersion of forces applied by the exciters 50. Therefore, according to the invention the internal structure of the mounting table 20, be it the cored table 44 or the cavities 106 and 108 of the central core 100, is broken up by the multiplicity of walls and cavities which may be regularly disposed and formed from geometric shapes or arrays 112 as illustrated above, or may be arbitrarily shaped and/or randomly distributed throughout the volume of the mounting table 20. A mounting table 20 built up from a lattice of rectangular, triangular or any other shaped grid or complex of connected walls is expressly included within the scope of the invention. The unidirectional excitations from the exciters 50 are randomly dispersed by the mounting table 20 resulting in substantially uniform, randomly oriented vibrations at device 6 in a predetermined spectrum range. Results of testing performed on a workpiece using an embodiment of the apparatus similar to the embodiment shown in Fig. 1, and incorporating one layer of honeycomb between a top and bottom face sheet, clearly indicate the dispersive effects of the honeycomb structure. The testing was performed on a test device weighing 70 pounds, which is considered to be substantially heavier than any electronic equipment which will be screened by the apparatus. The test device was securely fastened to the top surface sheet of the mounting table 20, the mounting table was rectangular and four pneumatic exciters 50 were vertically attached to the top surface sheet with one exciter 50 being attached at each corner. Each exciter 50 was vectored in the z direction and was made to impart vibrational excitations to the table 20. The magnitude of vibrations oriented in the x, y and z directions were measured at the test device. Fig. 5A, 5B and 5C represent results of the above described test performed on the 70 pound test device. Comparisons of measured responses are shown in two directional axes with respect to each other over time. Figures 5D, 5E and 5F are representative of the amplitudinal responses along each axis over a frequency range. As clearly shown, the vibrational responses in the various axial directions are incoherent relative to one another indicating the dispersive effects of the shaker table. Similar results have been measured in experiments using a table incorporating the cored slab shown in Fig. 4 and the central core 100 with cavities 106 and 108 shown in Fig. 9 in lieu of the honeycomb assembly 30. In order to further create multiaxial vibrations in the device 6 to be tested the following describes the manipulation and arrangements of the exciters 50. A vectoring means can be attached to exciter 50 for vectoring the excitations imparted to the shaken table 10 to achieve a desired vibration balance between different axial directions. One such vectoring means is a wedge-shaped piece 11, shown in Fig. 6A. In Fig. 6B the exciter 50 may be comprised of at least one pneumatic vibrator 52 having an input 54 and an output 56, and a modulation means to modulate the air pressure imparted to the input of each of the pneumatic vibrators 52. As seen in Fig. 6B the modulation means is comprised of a rotary ball vibrator 60 having an exhaust output 64 attached to the input 54 of a pneumatic vibrator 52 for imparting modulated air pressure into pneumatic vibrator 52. A source of air pressure 12 is coupled to input 62 of rotary ball vibrator 60 to produce a pulsed output. The pulsed output is generated by the rotation of one or more balls 66 held in a retaining ring 67 which act as vanes in a circular air passage 68. The interruption of air flow as each ball 66 passes output 64 creates a pulsating air pressure to input 54 of vibrator 52. This in turn causes the line spectra output of vibrator 52 to be smeared over a frequency range. Vibrator 60 may also be mechanically attached to table 20. In another embodiment diagrammatically depicted in Fig. 6C the modulation means comprises at least one accumulator 70 having an exhaust output 71 which is attached to input 54 of the pneumatic vibrator 52. Accumulator 70 delivers pressurized air to the input of pneumatic vibrator. An alternating means or solenoid controlled valve 72 is attached to accumulator 70 to alternately start and stop the flow of air through accumulator 70 for supplying a continuously varying air pressure to the pneumatic vibrator 52 from air supply 12. Again, this causes the line spectra output of vibrator 52 to be smeared over a frequency range. In another embodiment shown in Fig. 6D, an analog voltage controlled valve 74 such as manufactured by Norgren under Model Designation 53-5004-00 is used to modulate the inlet air pressure to the vibrators. An analog pressure regulator is used in a closed loop control system to maintain a given average vibration level. The regulator can also provide modulation of the air pressure. In another embodiment shown in Fig. 6E the exhaust of one pneumatic exciter is attached and used to drive a set of one or more of the exciters 50. This provides a varying inlet pressure to the set of exciter(s) and also provides a varying backpressure to the first exciter. The net effect is to smear the line spectra. In another embodiment shown in Fig. 6F, two or more of the exciters 50 are supplied with air from the same manifold 76 or air line 14. The manifold 76 or line pressure of line 14 is not constant due to the pulsing flow as various exciters take in quantities of air from the manifold 76 or line 14. The effect is particularly pronounced if one exciter 50 uses substantially more air per stroke of the cycle than the others. Any combination of the above may be utilized as depicted in Fig. 6G where air line 14 is split into two paths to two large exciters 51. One of the large exciters 51 has its input 54 restricted. Each of the large exciters 51 has its exhaust output 56 connected to input 54 of one or more smaller exciters which in turn are attached to the mounting table 20. This provides a cascading modulation of the vibrations to the table 20. The exciters 51 are usually attached to the fixture, but are shown as detached here. In another embodiment as diagrammatically depicted in Fig. 7A, the modulation means comprises means 78 to throttle or restrict the exhaust from the output 56 of pneumatic exciter 52, changing the repetition or cycle rate of the exciter 52. This method may be used to achieve a different cycle rate of each exciter and smear the vibration spectra experienced by the device 6. In another embodiment diagrammatically depicted in Fig. 7B, a rotary ball vibrator 60 is attached to the mounting table 20. Vibrator 60 has its input 62 supplied with air pressure from source 12 via line 14. The exhaust 64 of vibrator 60 is connected to the inlet of manifold 76 via line 15. Manifold 76 has at ' least two outlets each supplying air pressure via line 14 to a pneumatic vibrator 52 which is attached to table 20. This causes an additional vibrational spread between different axial directions and frequencies. In yet another embodiment depicted in Fig. 7C, a pop-off valve 79 is used to control the air pressure in vibrators 52. Pop-off valve 79 can either be connected to the input 54 of a vibrator 52 (as depicted in the dashed box 1) or to the exhaust output 56 of a vibrator 52 (as depicted in dashed box 3) . In either case, pop— off valve 79 opens according to its design at a given first air pressure and to close at a second lower air pressure. Connection to input 54 of vibrator 52 modulates the pressure into vibrator 52. Connection to output 56 modulates the backpressure to vibrator 52 changing the repetition frequency of vibrator 52 and smearing the line vibration spectrum seen at the device 6. The line spectrum generated by each of the exciters 50 is generated by the cycle rate of the exciter 50. The spectra will contain the fundamental repetition frequency and all harmonics of that rate. The exciter 50 can be made to have different cycle rates even when supplied with the same air pressure by changing either the stroke, piston weight or port timing slightly. To obtain the desired spectrum shape, a tunable damper for notching the vibration spectrum is depicted in Fig. 8. A mass 80 is placed between two progressively wound springs 82. Means 84 for preloading springs 72 is provided to compress the coils and change the spring rate and the natural frequency of the vibration. The means for preloading the springs is adjustable. Any means for spring compression may be utilized, such as a movable pressure plate bearing against one end of the springs and adjusted by a lockable screw drive. This will then generate a user tunable damper for notching the vibration spectrum after the damper is attached to the mounting table 20. Alternatively, adjustable damping is established by throttling air to the mass 80, instead of using the wound springs. Each of the exciters 50 (Figs. 17-20) includes a piston assembly 124 slidable within a cylinder 126. The piston assembly 124 is connected to the mounting table 20 by a piston mounting bolt 128 and washer 130. A pair of titanium spacers 132 and the titanium bolt 128 and washer 130 thermally insulate the exciter 50 from the mounting table 20 (Fig. 9) . The cylinder 126 has a chamfered end 134 and an open end closed by an end cap 136 secured by threaded bolts 138. The piston assembly 124 includes a piston body 140 connected to a resilient programmer 142 (Fig. 20) . The piston assembly 124 slides along the interior of the cylinder 126. The programmer 142 is of resilient polymeric material such as Dupont Delrin 100 while the piston body 140 of the piston assembly 124 is made of steel or aluminum. The piston assembly 124 moves in a reciprocal manner interiorly of the cylinder 126 under the influence of pressurized air admitted to the cylinder 126 through air pressure inlet 144 through fitting 146. The piston assembly 124, with reference to Figs. 17 and 18, moves to the left in a thrust stroke, striking a rebound surface 148 of the cylinder 126 and imparting a force across the chamfered surface 134 to the mounting table 20. The rapid movement of the piston assembly 124 would heat and melt the polymeric material of the programmer 142 absent cooling passageways 150, defining means for cooling the programmer 142. In the thrust stroke, air is admitted through the air pressure inlet 144 to inlet thrust passageway 152 formed in the piston body 140. Air exhausts into a thrust chamber 154 formed interiorly of the cylinder 126. The piston assembly 124 moves toward the rebound surface 148, exhausting air in a rebound chamber 156 through exhaust port 158. At the completion of the thrust stroke, a distribution ring 160 in fluid communication with the air pressure inlet 144 admits pressurized air to a rebound inlet passageway 162 formed in the cylinder 126. The rebound inlet passageway 162 is in fluid communication with a central chamber 164 of the piston body 140 which is in fluid communication with a central passageway 166 of the programmer 142. In turn, the central passageway 166 is in fluid communication with the laterally extending cooling passageways 150. The passageways 150 extend laterally away from the central passageway 166 uniformly around the circumference of the programmer 142. The rebound stroke begins with pressurized air moving from the distribution ring 160, through the inlet passageway 162 and the central chamber 164, through the piston body 140 and into and out of the programmer 142 through the passageways 166 and 150. The rebound chamber 156 is pressurized and the piston assembly 124 moves from the rebound chamber 156 toward the thrust chamber 154. A mounting system 168 (Figs. 9 and 11) includes four hangers 170 secured to walls of a thermal chamber 172, for testing thermal excitations to the device 6. The hangers 172 support springs 174 which allow multi-axial movement of the entire mounting table 20. Standard bolt connections 176 are used to connect the springs 174 to the mounting table 20. The hangers 172 are releasably connected to the walls of the chamber 172. Various attachment positions are provided on the walls so that the vertical position of the mounting table 20 can be changed. This feature permits the chamber volume to be increased or decreased, depending on the size of the device 6. As a result, higher temperatures are realized for a given volume or less power is used to achieve a given temperature. In an alternative embodiment of the exciter 50 shown in Figs. 21 through 26, like parts retaining the numbers used in the preferred embodiment, the exciter 50 includes a piston assembly 176 which reciprocates within a cylinder 178 at a variable cycle rate. The piston assembly 176 includes a tubular inner sleeve 180 fixedly connected to the cylinder 178 and a piston 182, which piston 182 is slidable and randomly rotated within the inner sleeve 180. This variable rate cycle is induced mechanically by varying the inlet port timing during the thrust stroke, and/or the rebound stroke by varying the exhaust port timing. The variable cycle rate of the alternative embodiment of the exciter 50 helps the shaker table 10 deliver multi-axial broadband continuous frequency distribution vibrations to the mounted manufactured device 6. The piston 182 is randomly rotated as part of the variable reciprocation timing. Angling an inlet port 184 of the inner sleeve 180 relative to air received from the air inlet 144 imparts a rotation to the piston 182. The angling is relative to a radius of the cylinder 178 (Fig. 25). With reference to Figs. 21 and 22, the piston 182 is rotated relative to port inlet 184. A programmer 186 is fixedly positioned relative to the cylinder 178 by a set screw. An angular inlet and exhaust port 188 of the piston 182 is variably covered or uncovered relative to the distribution ring 160. A curvilinear surface 196 of the sleeve 180 registers with the distribution ring 160. This structure varies the amount of pressurized air admitted to a thrust passageway 190 of the piston 182, randomly varying the cycle rate of the piston assembly 176. As the angular port 188 reaches the surface 196 the amount of air admitted to the piston 182 for .the thrust stroke is randomly varied, depending on the rotational position of the piston relative to the surface 196. This allows varying amounts of air from the inlet 144 to reach the port 188. The thrust stroke is initiated through the angled air inlet 184, air being directed around distribution ring 160 from the air inlet 144. The angular port 188 of the piston 182 receives the pressurized air from the inlet 184, the amount varying on the rotational position of the piston 182. The thrust passageway 190 of the piston 182 receives the air from the port 188 and is in fluid communication with a thrust chamber 192. The piston 182 moves toward impact with a rebound surface 194 defined by the resilient programmer 186. As the piston 182 moves within the inner sleeve 180, the port 188 uncovers from a second curvilinear surface 197 of the inner sleeve 180. The air is exhausted through the programmer 186, the cooling passageways 150 and central passageway 166 to the exhaust port 158. Just as was the case with the curvilinear surface 196, the amount of air exhausted from the port 188 is altered depending on the extent to which the port 188 is covered or uncovered. This structure enhances the random cycle rate, either alone or in conjunction with the curvilinear surface 196. The rebound stroke is initiated as the piston 182 strikes the rebound surface 194 of the programmer 142. The piston 182 is forced away from the rebound surface 194 and toward the thrust chamber 192, where the thrust stroke is reinitiated. It is appreciated that the length of the stroke varies depending on the amount of air initially supplied in the thrust stroke and/or exhausted in the rebound stroke. A modified piston 183 is randomly rotated by vectored passageways 185 in fluid communication with the thrust passageway 190 is shown in Fig. 26. A cap 187 covers the vectored passageways 185. Notches 189 are formed in the cap 187 so that the exhaust of the piston 183 is directed from the passageway 190 and into the thrust chamber 192. This vectored flow imparts a random rotation to the piston 183 during each thrust stroke. Randomness is imparted, as previously described, by the inlet and exhaust port timing. This construction is in lieu of, or in combination with, the angled inlets 184 shown in Figs 23 and 25. Although the invention has been described with a certain degree of particularity, it is understood that the present disclosure had been made by way of example, and changes in detail or structure may be made without departing from the spirit of the invention, as defined in the appended claims.

Claims: CLAIMS What is claimed is: 1. An improved shaker apparatus of the type having a mounting table for carrying and vibrating a device to be screened, comprising: exciter means secured to said mounting table for imparting excitations thereto; mounting means coupled to said mounting table for mounting said shaker table to a foundation and for substantially isolating vibration of said mounting table from the foundation; and dispersive means for dispersing unidirectional excitations imparted to said table into substantially incoherent multiaxial and multirotational directions. 2. The shaker apparatus of Claim 1 wherein said mounting table has a bottom surface sheet and wherein said dispersive means comprises a dispersive assembly secured on said bottom surface sheet, and a top surface sheet secured on said assembly. 3. The shaker apparatus of Claim 2 wherein said assembly comprises at least one layer of honeycomb structure formed from undulating walls which extend between said top and bottom surface sheets in a first direction and which walls define within said layer of honeycomb structure an axis of maximum stiffness, said layer of honeycomb structure extending in a second and third direction. 4. The shaker apparatus of Claim 3 wherein said assembly comprises a plurality of said layers of honeycomb structure, each of said layers fixed adjacent to at least one other one of said layers, and each of said layers having its axis of maximum stiffness oriented in a direction different than the direction of said corresponding axis of .maximum stiffness of said adjacent layer of honeycomb structure. 5. The shaker apparatus of Claim 3 wherein said honeycomb assembly further comprises at least one common interlayer sheet, said common interlayer sheet fixed to and between two of said layers wherein said layers and said common sheet are alternately stacked with said common interlayer sheet between said layers. 6. The shaker apparatus of Claim 4 wherein said honeycomb assembly further comprises a plurality of interlayer sheets, said interlayer sheets equal in number to one less than the number of said layers, each of said interlayer sheets fixed to and between two of said layers so that said layers and said interlayer sheets are alternately stacked with one of said common sheets between each adjacent pair of said layers. 7. The shaker apparatus of Claim 1 wherein said dispersive means comprises a substantially solid block of material having a plurality of cores predrilled therein. 8. The shaker apparatus of Claim 7 wherein said mounting table further comprises a top face sheet attached to said block of cored material so that said surface sheet covers said plurality of cores. 9. The shaker apparatus of Claim 1 wherein said dispersive means comprises a three dimensional lattice of connecting walls defining a multiplicity of spaces within said dispersive means. 10. The shaker apparatus of Claim 1 wherein said dispersive means comprises: a central core having a plurality of cavities formed from one surface into said central core, said cavities of two types, one type uniformly distributed in arrays about mounting holes for connection of an exciter to the mounting table and a second type mounted in rows and columns between said mounting arrays, said mounting arrays and rows and columns of said first and second type of cavities defining .a geometric pattern of cavities throughout the surface of said central core; and a sheet connected to the surface of the center core in which said cavities are formed. 11. The invention as defined in Claim 10 wherein said array of cavities comprise cavities of generally pentagon shaped plan views. 12. The invention as defined in Claim 10 wherein said cavities of the second type are of generally square geometric plan view. 13. The invention as defined in Claim 10 wherein said array of cavities include four cavities of the first type separated from horizontally and vertically adjacent arrays by single rows and columns of cavities of the second type. 14. The invention as defined in Claim 10 wherein a rubber mounting layer is bonded to the other surface of said central core. 15. The invention as defined in Claim 14 wherein an insulating layer is disposed between the mounting layer and the central core. 16. The shaker apparatus of Claim 1 wherein said dispensive means comprises a central core having a plurality of cavities formed in one surface thereof. 17. The shaker apparatus of Claim 16 wherein the one surface is coved by a homogenous sheet of material. 18. The shaker apparatus of Claim 16 wherein another surface of said central core has an insulating layer and a mounting layer laminated thereto. 19. The shaker apparatus of Claim 1 wherein said table has a interior which is at least in part hollow, and an inside and outside surface; and wherein said exciter means is attached to said inside surface of said table so that more of the outside surface of said table is available for attachment to said device. 20. The shaker apparatus of Claim 1 wherein vectoring means is attached to said exciter means for vectoring the excitations imparted to said. achine to achieve a desired vibration balance between different directions. 21. The shaker apparatus of Claim 1 wherein said exciter means comprises: at least a first pneumatic vibrator having an input and an output; an air source coupled to said vibrator input for supplying air pressure to said input of said vibrator; and input modulation means to modulate the air pressure supplied to said input of said pneumatic vibrator. 22. The shaker apparatus of Claim 21 wherein said input modulation means comprises a rotary ball vibrator having an exhaust output attached to said input of said pneumatic vibrator for imparting modulated air pressure into said pneumatic vibrator, and said rotary ball vibrator having an input coupled to said air source. 23. The shaker apparatus of Claim 21 wherein said input modulation means comprises: at least one accumulator having an exhaust output, attached to said input of at least one of said first set of at least one of said pneumatic vibrator, for imparting pressurized air to said pneumatic vibrator; said accumulator having an input coupled to said air source; and alternating means attached to said accumulator to alternately start and stop the flow of air through said accumulator for supplying a continuously varying air pressure to said pneumatic vibrator. 24. The shaker apparatus of Claim 21 wherein said input modulation means comprises an analog voltage controlled pressure regulator, attached to said input of said pneumatic vibrator. 25. The shaker apparatus of Claim 21 wherein said input modulation means comprises: at least a second pneumatic vibrator having an input and output, εaid output of said second pneumatic vibrator attached to said input of said first pneumatic vibrator, and said input of said second vibrator being coupled to said air source. 26. The shaker apparatus of Claim 21 wherein said input modulation means comprises a manifold having an input and a plurality of outputs, and wherein said apparatus further comprises a plurality of said first vibrators, each of said outputs of said manifold coupled to an input of one of said plurality of said first pneumatic vibrators. 27. The shaker apparatus of Claim 21 wherein said input modulation means comprise at least one pop-off valve having an output attached to said input of said first pneumatic vibrator, said pop-off valve characterized by a pressure hystersis. 28. The shaker apparatus of Claim 1 wherein said exciter means comprises: at least one pneumatic vibrator having an input and an output; an air source coupled to said inputs for supplying air pressure to said vibrators; and throttle means connected to the output of said at least one pneumatic vibrator for restricting the exhaust of said vibrator, whereby the repetition rate of the vibrator is changed. 29. The shaker apparatus of Claim 1 wherein said exciter means comprises: at least one pneumatic vibrator having an input and an output, said input of said pneumatic vibrator supplied with air pressure; and a pop-off valve attached to said output of said pneumatic vibrator. 30. The shaker apparatus of Claim 1 wherein said exciter means comprises a plurality of vibrators being supplied with air pressure and each coupled to said apparatus, each of said vibrators having different stroke rates relative to each other. 31. The shaker apparatus of Claim 1 wherein said exciter means comprises a plurality of vibrators being supplied with air pressure and each coupled to said apparatus, each of said vibrators having different piston weights, different strokes or different port timing relative to each other. 32. An improvement in a method of generating a substantially randomly oriented, incoherent, multi-axial vibration spectrum to a workpiece comprising the steps of: generating excitations of a predetermined line spectrum; coupling said excitations to a dispersive layer, said excitations being directed in a single predetermined direction; and dispersing said excitations in said dispersive layer into incoherent multiaxial and multirotational directions, whereby said substantially randomly oriented multi-axial and multirotational vibration spectrum is provided at said work piece coupled to said dispersive layer. 33. The improvement of Claim 32 wherein said step of generating line spectrum comprises the steps of providing a pneumatic exciter coupled to said dispersive layer and modulating input air pressure to said pneumatic exciter to smear said line spectrum. 34. The improvement of Claim 32 wherein said step of generating line spectrum comprises the steps of providing a pneumatic exciter coupled to said dispersive layer and modulating output air pressure from said pneumatic exciter to smear said line spectrum. 35. The improvement of Claim 32 wherein said step of generating line spectrum comprises the steps of providing a plurality of pneumatic exciters coupled to said dispersive layer, each pneumatic exciter having an input and an output, and selectively modulating air pressure flowing through said plurality of pneumatic exciters by selectively coupling said inputs and outputs of said pneumatic exciters in parallel and/or series to each other according to a predetermined configuration to smear said line spectra generated by said plurality of exciters. 36. A tunable dampening apparatus comprising: a mass having a left side and a right side; and a first progressively wound coil having a first end coupled to the left side of said mass; and a second progressively wound coil having a first end coupled to the right side of said mass and a second end coupled to an object having vibrations to be dampened, the axial line of said coils defining a dampened direction; loading means coupled to a second end of said first coil for compressing said first and second progressively wound coils to a desired load; and adjusting means attached to said loading means for adjusting the load exerted on said coils by said compression. 37. A method of tunably dampening an object's vibration in one axial direction comprising: attaching one end of a first progressively wound coil to the left side of a mass; attaching the other end of said first coil to said object; said right side opposing said left side, the axial line of said coils defining a dampened direction; compressing the other end of said second coil to a desired load; and adjusting the load exerted on said coils. 38. A tunable dampening apparatus for a shaker apparatus wherein a mass is movable in a housing by throttling air to the housing. 39. An exciter for a shaker table comprising in combination: a cylinder having a substantially cylindrical interior; a piston slidable in said cylindrical interior of said cylinder; air inlet and exhaust means for admitting and exhausting pressurized air to and from the interior of said cylinder and moving said piston in thrust and rebound strokes along said cylindrical interior; and a resilient programmer aligned with said piston and defining a rebound surface for said piston, said programmer in fluid communication with said air inlet means. 40. The invention as defined in Claim 39 wherein said air inlet means is in fluid communication with a distribution ring formed about said cylindrical interior, said ring registering with a thrust passageway of said piston to initiate said thrust stroke. 41. The invention as defined in Claim 40 wherein the thrust passageway exhausts into a thrust chamber of the cylinder, moving the piston assembly toward a rebound chamber of the cylinder, an exhaust port formed through the cylinder for allowing air flow to exhaust from said rebound chamber upon movement of said piston toward said rebound chamber. 42. The invention as defined in Claim 40 wherein said distribution ring is in fluid communication with a passageway in the piston whereby upon completion of the thrust stroke air is admitted along the passageway to the piston body and then through a second passageway to the programmer, exiting said programmer through cooling passageways of the cooling means. 43. The invention as defined in claim 39 further including: means for randomly rotating said piston in said cylinder; and port means for varying the amount of air admitted to move said piston, dependent upon the rotational position of the piston relative to the cylinder. 44. The invention as defined in Claim 44 wherein said port means further includes means for varying the amount of air exhausted from said cylinder as the piston moves within said cylinder dependent upon the rotational position of the piston relative to the cylinder. 45. An exciter for a shaker table comprising in combination: a cylinder having a substantially cylindrical interior; a piston slidable in said cylindrical interior of said cylinder; means for randomly rotating said piston in said cylinder; and means for admitting and exhausting air to and from the cylindrical interior in an amount dependent on the rotational position of said piston. 46. The invention as defined in Claim 45 wherein the stroke of said piston varies as the amount of air admitted and exhausted to said cylinder from said means for admitting and exhausting air. 47. The invention as defined in Claim 45 wherein said means for rotating said piston is an angular air inlet formed in said cylinder. 48. The invention as defined in Claim 45 wherein said means for rotating said piston is a vectored passageway formed in said piston in fluid flow communication with said means for admitting air to said cylinder. 49. The invention as defined in Claim 45 wherein said means for admitting air to said cylinder is a cylindrical sleeve having a curvilinear surface which covers a portion of an inlet port of said piston depending on the rotational position of said piston relative to said cylinder, said inlet port in air flow communication with a thrust passageway passing through said piston and into a thrust chamber of said cylinder. 50. The invention as defined in Claim 49 wherein said means for exhausting air from said cylinder includes a second curvilinear surface which covers a portion of an exhaust port of said piston as said piston moves toward a rebound chamber of said cylinder.

Inventors: HOBBS GREGG K, HOBBS, GREGG, K.
Applicants: HOBBS GREGG K, HOBBS, GREGG, K.
Application year: 1991
Main classification: F16F7
IPC codes: G01M7