NOISE TESTING SYSTEM WITH TEMPERATURE RESPONSIVE SENSITIVITY

Abstract: An arrangement for isolating an energy transfer system while it is subjected to a test process for noise. The energy transfer system is of the type having an energy input and at least one energy output, and may be mechanical or electrical. The isolation arrangement has a base that supports the energy transfer system. An isolation support supporting the energy transfer system, yet affords multiple degrees of freedom with respect to the base. The energy transfer system is clamped in a manner that permits at least one degree of freedom with respect to the base, via an engagement arrangement that secures the energy transfer system to the isolation support. When mechanical or electrical energy is applied to the evergy transfer system, acoustic energy in the form of sound and/or vibration is issued by the energy transfer system under test, which acoustic energy is monitored by an acoustic sensor that issues a corresponding electrical signal. The monitored acoustic energy is responsive to a qualitative condition in the energy transfer system under test, and also to a temperature thereof. A thermal sensor monitors a temperature change in the energy transfer system under test, and the resulting temperature-responsive electrical signal is employed to control the sensitivity of the acoustic sensor. Such temperature-responsive control is effected non-linearly in certain embodiments of the invention.

Description: Noise Testing System With Temperature Responsive Sensitivity BACKGROUND OF THE INVENTION FIELD OF THE INVENTION This invention relates generally to systems for testing electrical and mechanical energy transfer systems that exhibit vibratory and other responses to electrical or mechanical input energy, and more particularly, to an arrangement that isolates a mechanical or electrical system under test and produces signals and data corresponding to noise produced by the system under test in response to the input energy, the sensitivity ofthe subsystem(s) that monitor the noise being responsive to a temperature ofthe system under test. DESCRIPTION OF THE RELATED ART Noise testing of gears to date has been attempted by methods that rigidly mount the gear or axle assemblies in one or more planes. Some other previous attempts chose to have one ofthe rigidly mounted planes resonate at a frequency sympathetic to gear noise. None of these methods, or any other rigidly mounted test system has been successful. This is due to the lack of repeatability ofthe previous systems, largely as a result of interacting resonances, and external background noise that is transferred through the rigid mounting system. This is especially true in a production test environment. These deficiencies in the prior art are most evident in the axle industry. At this time, the only widely accepted way of measuring gear noise is to acquire an assembled axle and install it in a test car. A specially trained individual then drives the car over its typical operating range while carefully listening for axle gear noise. The individual rates the quality of axle gear noise on a scale that is typically 0 to 10. Ten is usually a perfect axle, i.e. one that has no gear noise. This method is made difficult by: 1 The lack of available trained noise rating individuals 2 The cost of test cars. 3 The lack of quality roads or test tracks on which to perform a repeatable and accurate test. 4 The time required for each test. 5 The subjectivity that humans bring into the rating system Typically less than a dozen axles can be tested by a major manufacturer in one shift due to all ofthe above complications. This low number is not statistically valid when it is considered that most manufacturers make thousands of axles each day. Even with all ofthe above problems, human testers in cars are the only widely accepted method of axle testing in the industry due to the lack of a better more reliable testing method. This lack of a scientific basis for rating axles and gear systems is made worse when the reader considers that modern cars are extremely quiet, and are evolving to become more quite. This market direction increases the pressure on axle and other gear manufacturers to make their products quieter. There is a need for a system that offers gear and axle manufacturers a repeatable, reliable, accurate and practical way of measuring gear noise in production or laboratory environments. It is, therefore, an object of this invention to provide a system for testing an energy transfer system, such as a vehicle axle, quickly and inexpensively, and achieving repeatable results. SUMMARY OF THE INVENTION The foregoing and other objects are achieved by this invention which provides, in a first apparatus aspect thereof, an arrangement for isolating an energy transfer system while it is subjected to a test process for noise, the energy transfer system being ofthe type having an energy input and at least one energy output. In accordance with the invention, the arrangement is provided with a base for supporting the arrangement and the energy transfer system. An isolation support supports the energy transfer system whereby the energy transfer system is translatable in at least one plane of freedom with respect to the base. Additionally, an engagement arrangement is provided for securing the energy transfer system to the isolation support, the engagement arrangement having a first position with respect to the base wherein the energy transfer system is installable on, and removable from, the isolation support, and a second position wherein the energy transfer system is secured to the isolation support. A first acoustic sensor arranged at a first location in the vicinity of the energy transfer system for producing a first signal responsive substantially to a qualitative condition of the energy transfer system. A thermal sensor produces a thermal signal that is responsive to a temperature ofthe energy transfer system. An acoustic sensor sensitivity control arrangement is responsive to the thermal sensor for controlling the amplitude ofthe first signal in response to temperature. In one embodiment of the invention, the thermal sensor is in the form of an infrared sensor that communicates optically with the energy transfer system. In one specific illustrative embodiment of the invention, the thermal sensor means has a directional characteristic and is directed to a predetermined region ofthe energy transfer system for determining a temperature, or a rate of change of temperature, of the predetermined region with respect to time. The control over the amplitude ofthe noise signal with respect to temperature is performed in accordance with a non-linear amplitude-temperature relationship. In one embodiment, there is further provided an energy supply coupled to the energy transfer system for supplying energy thereto when the engagement arrangement is in the second position. The energy transfer system is, in one embodiment of the arrangement ofthe present invention, a mechanical energy transfer system, and in such an embodiment, the energy supply, which is a part ofthe arrangement ofthe invention, is in the form of a source of rotatory mechanical energy. A rotatory coupler couples the source of rotatory mechanical energy to the energy transfer system. In a highly advantageous embodiment ofthe invention, the mechanical energy transfer system test has forward and reverse directions of operation, and drive and coast modes of operation for each of the forward and reverse directions of operation. The mechanical energy transfer system contains at least a pair of meshed elements, at least one ofthe pair of meshed elements being a gear having a plurality of gear teeth thereon, the gear teeth each having first and second gear tooth surfaces for communicating with the other element of the pair of meshed elements. A mechanical energy transfer communication between the pair of meshed elements is effected primarily via the respective first gear tooth surfaces during forward-drive and reverse-coast modes of operation, and primarily via the respective second gear tooth surfaces during forward-coast and reverse-drive modes of operation. With such a system under test, the arrangement ofthe present invention is provided with a first acoustic sensor arranged at a first location in the vicinity ofthe mechanical energy transfer system for producing a first signal that is responsive substantially to a qualitative condition ofthe first gear tooth surfaces. A second acoustic sensor is arranged at a second location in the vicinity ofthe mechanical energy transfer system, and produces a second signal that is responsive substantially to a qualitative condition ofthe second gear tooth surfaces. The first and second locations are distal from each other on opposite sides of the pair of meshed elements. In a further embodiment ofthe invention, the rotatory coupler is provided with a resilient coupler arrangement that transmits rotatory motion thereacross over a predetermined range of rotatory motion transmission angles. The resilient coupler arrangement is provided with first and second coupler portions, the first and second coupler portions being rigidly coupled rotationally to each other. Additionally, they are axially resiliency coupled to each other, whereby the first and second coupler portions are synchronously rotatable over the predetermined range of rotatory motion transmission angles. In yet a further embodiment ofthe invention, the resilient coupler arrangement is provided with first and second coupler portions, the first and second coupler portions being rigidly coupled rotationally to each other, and radially resiliency coupled to each other. Thus, the first and second coupler portions are synchronously rotatable over a predetermined range of axial displacement. A torque sensor advantageously is interposed, in a highly advantageous embodiment, between the source of rotatory mechanical energy and the energy transfer system. The torque sensor produces a signal that is responsive to a torque applied by the source of rotatory mechanical energy to the energy transfer system. The torque sensor is provided with a torque-transmitting element that has a predetermined deformation characteristic. Thus, the torque-transmitting element becomes deformed in response to the torque that is applied by the source of rotatory mechanical energy to the energy transfer system. In this embodiment of the invention, the torque sensor further is provided with a strain sensor that is coupled to the torque-transmitting element for producing a strain signal responsive to the predetermined deformation characteristic of the torque-transmitting element. The strain signal, therefore, is proportional to the torque. It is very advantageous to determine the residual torque required to initiate motion ofthe system under test. The torque sensor is therefore arranged to produce a static torque signal that is responsive to the magnitude ofthe torque required to initiate rotatory motion in the mechanical energy transfer system. In addition, it is advantageous that the torque sensor be arranged to produce a dynamic torque signal that is responsive to the magnitude of torque required to maintain rotatory motion in the mechanical energy transfer system. In a particularly advantageous embodiment ofthe invention, the energy transfer system under test is an electrical energy transfer system, and the energy supply is provided with a source of electrical energy. In such an embodiment, there is provided an electrical load for receiving an output electrical energy from the energy transfer system when the engagement arrangement is in the second position. A first sensor is arranged to communicate with the energy transfer system for producing an information signal that is responsive to an operating characteristic ofthe energy transfer system in response to the energy supplied by the energy supply. The first sensor is arranged to contact the energy transfer system to produce the signal. Alternatively, the first sensor is arranged to contact the isolation support for producing the information signal. The first sensor is arranged, in one embodiment of the invention, so as to be translatable relative to the energy transfer system. When it is desired to monitor an acoustic energy emitted by the system under test, a microphone is provided for producing a signal that is responsive to an acoustic energy issued by the energy transfer system in response to the energy supplied by the energy supply. A laser sensor may additionally be provided for producing a signal that is responsive to a displacement of the energy transfer system in response to the energy supplied by the energy supply. In still further embodiments, an accelerometer or a velocity sensor is employed. The resilient support element that supports the energy transfer system, in a preferred embodiment ofthe invention, is configured to exclude a natural frequency of any combination of the base, the engagement arrangement, and the energy transfer system. Thus, the vibratory or acoustic energy provided by the system under test constitutes all ofthe energy that would be measured and analyzed, without contribution or modification thereof by the structure ofthe support system. Preferably, the isolation support supports the energy transfer system so that it is translatable in at least a second plane of freedom with respect to the base. In a highly advantageous embodiment of the invention, there is provided an engagement driver that has a first portion that is coupled to the base, and a second end that is coupled to the engagement arrangement. The engagement driver is, in one embodiment, provided in the form of a linear actuator that has a first end coupled to the base, and a second end coupled to the engagement arrangement. The linear actuator is arranged to drive the engagement arrangement between the first and second positions. Moreover, it is decoupled from the engagement arrangement when the engagement arrangement is in the second position. In this arrangement, an engagement coupler is interposed between the engagement arrangement and the engagement driver. The engagement coupler is provided with a support portion installed on the isolation support. First and second engagement arms are pivotally coupled to the support portion. Additionally, first and second articulated members coupled at a pivot point to one another and to the engagement driver, and are pivotally coupled at distal ends thereof to respective ones of the first and second engagement arms. In this manner, the engagement driver urges the pivot point along a predetermined path to a latching position beyond where the first and second articulated members are axially parallel. Such a latching effect is facilitated by a resilient biasing arrangement that is installed on at least one of the first and second engagement arms. The resilient biasing arrangement applies a resilient biasing force to the energy transfer system, which additionally maintains the engagement arrangement in the second position. A displacement sensor is installed on at least one of the first and second engagement arms, and serves to produce a distance signal that is responsive to a distance between the one of the first and second engagement arms on which the displacement sensor is installed and the energy transfer system. In this manner, the distance signal is responsive to a predetermined dimension ofthe energy transfer system. In accordance with a method aspect ofthe invention, there is provided a method of testing a gear assembly of the type having an input and an output. The method includes the steps of: installing the gear assembly on a mounting arrangement that resiliently permits motion of the gear assembly in all directions, and that has a resilient frequency characteristic that excludes all natural frequencies ofthe gear assembly; applying a torque at the input ofthe gear assembly, whereby the gear assembly is rotatably operated; applying a load at the output ofthe gear assembly; sensing a predetermined operating characteristic ofthe gear assembly; and controlling the step of sensing in response to a temperature ofthe gear assembly. In one embodiment of this method aspect ofthe invention, the step of sensing is provided with the step of detecting acoustic energy issued by the gear assembly. Also, the step of detecting acoustic energy issued by the gear assembly is provided with the step of placing a microphone n the vicinity ofthe gear assembly. In a further embodiment, the step of sensing is provided with the step of detecting vibratory displacement energy issued by the gear assembly. The step of detecting vibratory displacement energy issued by the gear assembly is provided with the further step of effecting communication between an accelerometer and the gear assembly, and the step of detecting vibratory displacement energy issued by the gear assembly is provided with the further step of effecting communication between a velocity sensor and the gear assembly. After performing the step installing there is further provided the step of clamping the gear assembly to the mounting arrangement. In an embodiment where the mounting arrangement is installed on a reference base portion, the step of clamping is performed in response to the further step of applying a clamping actuation force to a clamping arrangement with respect to the reference base portion. A clamping actuation force is applied, and the gear arrangement is enabled to move freely independent ofthe reference base portion. In a further embodiment, the step of applying a clamping force is provided with the further step of applying a resilient clamping force to the gear assembly. This step may, in certain embodiments, include the further step of monitoring a predetermined dimension ofthe gear assembly in response to the step of clamping. This is accomplished by use of a sensor that measures distance traveled. Sensing is effected by monitoring a first sensor that receives acoustic energy that is responsive to a qualitative condition ofthe gear assembly in a drive mode of operation. When the drive mode of operation is in a first direction of operation, the qualitative condition of the gear assembly in the drive mode of operation includes a qualitative condition of a first surface ofthe teeth ofthe gear assembly. Also when drive mode of operation is in a first direction of operation, the qualitative condition ofthe gear assembly in the drive mode of operation includes a qualitative condition of a profile of a gear of the gear assembly, and a qualitative condition of the eccentricity of a gear ofthe gear assembly. Additionally, the qualitative condition ofthe gear assembly in the drive mode of operation includes a qualitative condition ofthe angular orientation ofthe gears ofthe gear assembly. In still further embodiments of the method aspect of the invention, wherein the drive mode of operation is in a first direction of operation, the qualitative condition of the gear assembly in the drive mode of operation includes a qualitative condition of a plurality of moving components ofthe gear assembly. In a further embodiment ofthe invention, the step of sensing is provided with the further step of monitoring a second sensor that receives acoustic energy that is responsive to a qualitative condition ofthe gear assembly in a coast mode of operation. The coast mode of operation includes a qualitative condition of a second surface ofthe teeth ofthe gear assembly. When the coast mode of operation is in a first direction of operation, the qualitative condition of the gear assembly in the coast mode of operation includes a qualitative condition of a profile of a gear of the gear assembly. Additionally, the qualitative condition of the gear assembly in the coast mode of operation includes a qualitative condition ofthe eccentricity of a gear ofthe gear assembly, as well as the angular\ orientation ofthe gears ofthe gear assembly. In further embodiments, the coast mode of operation includes a qualitative condition of a plurality of moving components ofthe gear assembly. In accordance with a further embodiment of this method aspect ofthe invention, the drive and coast modes of operation are cyclical over a period that is shorter than a cycle period ofthe input ofthe gear assembly. Conversely, the period can be longer than a cycle period ofthe input ofthe gear assembly. This will depend, to an extent, upon the operating ratios within the system under test. In situations where the system under test is an electrical system, harmonics and signal distortions may affect the apparent cycle period in relation to the cycle period ofthe input energy. In an advantageous embodiment, the first and second sensors are disposed at respective locations that are distal from each other, with the gear assembly interposed therebetween. This enables distinguishing between operating modalities ofthe system under test, as well as facilitating analysis of operating characteristics ofthe system under test that have directional components. BRIEF DESCRIPTION OF THE DRAWING Comprehension ofthe invention is facilitated by reading the following detailed description, in conjunction with the annexed drawing, in which: Fig. 1 is a front plan representation of an arrangement for isolating a system under test, constructed in accordance with the principles ofthe invention; Fig. 2 is a side plan view ofthe embodiment of Fig. 1; Fig. 3 is an exploded plan representation ofthe embodiment of Fig. 1 showing certain drive components; Fig. 4 is a top plan view ofthe embodiment of Fig. 1; Fig. 5 is a partially phantom front plan view of a drive arrangement that supplied rotatory mechanical energy to an isolate mechanical energy transfer system under test; Fig. 6 is side plan view ofthe drive system of Fig. 5; Fig. 7 is a side plan representation of the drive system as shown in Fig. 6, enlarged to show greater detail; Fig. 8 is a side plan view of a coupler that couples the drive system to the mechanical system under test; Fig. 9 is a top plan view of the coupler of Fig. 8 showing therein three engagement surfaces for coupling with the flanks of an hexagonal nut (not shown in this figure) at the rotatory input ofthe mechanical system under test; Fig. 10 is a plan representation of a clamping arrangement constructed in accordance with the principles ofthe invention, the clamping arrangement being shown in two positions; Fig. 11 is a compact drive arrangement constructed in accordance with the invention for coupling the rotatory output of a mechanical energy transfer system under test to a rotatory load; Fig. 12 is a partially cross-sectional side plan view of the compact drive arrangement of Fig. 11 further showing a resilient coupling element; Fig. 13 is a partially phantom enlarged representation of the resilient coupling element shown in Fig. 12; Fig. 14 is an isometric representation of an arrangement for isolating a system under test, constructed in accordance with the principles of the invention, the system under test being an electrical energy transfer device; Fig. 15 is a process diagram of a typical process for conducting an energy analysis; Fig. 16 is a process diagram of a process for conducting an energy analysis in accordance with the principles ofthe present invention; and Fig. 17 is a process diagram of a process for conducting an energy analysis in accordance with the principles ofthe present invention for determining bumps and nicks in a mechanical energy transfer system. DETAILED DESCRIPTION OF THE INVENTION Fig. 1 is a front plan representation of an arrangement for isolating a system under test, constructed in accordance with the principles ofthe invention. As shown in this figure, an isolating arrangement 10 is arranged to support in relative isolation a mechanical drive system in the form of a differential 11. Differential 11 is ofthe type that is conventionally employed in a motor vehicle (not shown) and is intended to be tested for a variety of operating conditions, using isolating arrangement 10. The differential is ofthe type having a rotatory input 13 that receives rotatory mechanical energy from a drive arrangement (not shown in this figure) that will be described below. In addition, differential 11 has rotatory outputs 14 and 15, respectively, that produce rotatory mechanical energy in response to the rotatory input energy received at rotatory input 13. When employed in a motor vehicle (not shown), differential 11 is coupled to the drive shaft (not shown) ofthe vehicle at rotatory input 13, and rotatory outputs 14 and 15 are coupled to the vehicle's drive wheels (not shown). Differential 11 is shown to be supported on a pair of supports 18 and 19 that are installed on a base 20. Each of supports 18 and 19 has installed thereon a respectively associated one of resilient isolating elements 22 and 23. A respective one of engagement arrangements 24 and 25 are installed on resilient isolating elements 22 and 23. The engagement arrangements will be described in detail hereinbelow and serve to couple differential 11 at its rotatory outputs 14 and 15 whereby it is secured with respect to base 20, yet limited motion of differential 11 is permitted relative to base 20. Fig. 1 further shows a pair of load arrangements 28 and 29 that apply a controllable load to respectively associated ones of rotatory outputs 14 and 15. The rotatory outputs are coupled mechanically (coupling not shown in this figure) to load arrangements 28 and 29 in a manner that facilitates limited motion ofthe rotatory outputs with respect to base 20. The permissible displacement of differential 11 in accordance with the present invention is along multiple planes of freedom, and, as will be described hereinbelow, the coupling arrangements (not shown in this figure, between rotatory outputs 14 and 15 and their respective associated load arrangements 28 and 29 permit axial and rotative degrees of freedom of motion. Such couplings will be described with respect to Figs. 9-12. Fig. 2 is a side plan view ofthe embodiment of Fig. 1. This figure is taken along line 2-2 of Fig. 1. In addition to some ofthe structure shown in Fig. 1, Fig. 2 shows a safety cover 30 that protects the user (not shown) of the isolating arrangement in accordance with established safety standards. Elements of structure that correspond to those discussed hereinabove with respect to Fig. 1 are similarly designated. Fig.2 shows engagement arrangement 24 having engagement arms 32 and 33 that are shown in an engaged position around rotatory output 14. As will be described hereinbelow, engagement arms 32 and 33 have engaged and disengaged (not shown) positions in response to actuation of an engagement driver which is shown in this figure in the form of a linear actuator 35. A safety cover 30 is shown to be coupled to a cover hinge 31 , whereby the safety cover is rotatable thereabout in response to actuation of a cover actuator 34. In operation, the safety cover is arranged in the position shown in the figure during performance ofthe testing procedure, and it is raised to a position that is not shown in order to facilitate installation and removal ofthe system under test, i.e., differential 11. Fig. 2 additionally shows a drive motor 40, which in this embodiment, is coupled to a belt pulley 42, shown in Fig. 1. Fig. 3 is an exploded plan representation ofthe embodiment of Fig. 1 showing certain drive components. Elements of structure that have previously been discussed are similarly designated. The drive arrangement, and the manner by which it is coupled to differential 11, will be discussed in detail hereinbelow with respect to Figs. 5-8. Fig. 4 is a top plan view ofthe embodiment of Fig. 1. Elements of structure that have previously been discussed are similarly designated. Moreover, differential 11 has been removed, and therefore, is not visible in this figure. In Fig. 4, each of load arrangements 28 and 29 has associated therewith a respective one of load coupler arrangements 44 and 45, each of which is coupled by a respective load belt 46 and 47 to a respective one of load units 48 and 49. Load arrangement 28 will be described in detail hereinbelow with respect to Fig. 11, and the load coupler arrangements, 44 and 45, will be described in detail with respect to Fig. 12. Referring to Fig. 4, rotatory outputs 14 and 15 (not shown in this figure) are coupled (coupling not shown in this figure) to respectively associated ones of load coupler arrangements 44 and 45 which, as previously noted, provide multiple degrees of freedom of movement. Load units 48 and 49, in this specific illustrative embodiment of the invention, are in the form of electric brakes or electric motors. Of course, other forms of loads can be employed in the practice of the invention. In embodiments of the invention where the load units are in the form of electric motors, such motors can provide simulated braking and driving operations. Thus, in the present embodiment where the isolating arrangement is directed to the testing of a drive component for a vehicle, such as a differential, the load units can be operated in a drag, or generator mode, wherein the differential would be operated in a simulated drive mode. That is, the load is driven by the differential. Alternatively, the load units can be operated in a motor drive mode, wherein the differential is itself driven by the load, i.e., operated in a simulated coast mode. In a highly advantageous embodiment of the invention, the differential can be operated and thereby tested in drive and coast modes of operation in forward and reverse directions. It is to be remembered that during drive and coast modes of operation different gear tooth surfaces (not shown) within the differential are caused to communicate with one another, thereby affording enhanced testing capability. Fig. 5 is a partially phantom front plan view of a drive arrangement that supplies rotatory mechanical energy to an isolated mechanical energy transfer system under test. Elements of structure that have previously been discussed are similarly designated. As shown in this figure, output shafts 52 and 53 are shown protruding from the fragmented representation of rotatory outputs 14 and 15, respectively. The output shafts rotate in response to the application of a rotatory drive at rotatory input 13. Fig. 6 is side plan view ofthe drive system of Fig. 5. The operation ofthe drive arrangement that will supply a rotatory drive to rotatory input 13 of differential 11 is described herein with reference to Figs. 5-9. As stated, drive motor 40 is coupled via a drive belt 41 to belt pulley 42 which is installed on a drive shaft 55 that is shown in the figures to extend axially vertically. Belt pulley 42 contains a torque sensing arrangement (not shown) that provides an electrical signal responsive to torque differential between the belt pulley and drive shaft 55. The electrical signal responsive to torque (not shown) is available at signal output connector 56. In this specific illustrative embodiment of the invention, the torque sensing arrangement contained within belt pulley 42 and its associated signal output connector 56 is in the form of a strain gauge (not shown) installed to respond to the displacement of a web (not shown). That is, in the practice of this aspect ofthe invention, torque is transmitted across a web whereby, for example the torque is applied across the periphery ofthe web, and an output shaft is coupled nearer to the center ofthe web. Of course, these may be reversed. As torque is applied, the web is correspondingly deformed, and a strain gauge installed on the web measures the deformity in the web in response to the applied torque. Over a predetermined range of torque, the deformation ofthe web, as determined by the strain gauge, can be correlated to the magnitude ofthe applied torque. Signal output connector 56, in this specific illustrative embodiment of the invention, additionally contains circuitry (not shown) that is AC coupled to the torque sensing arrangement, and that modulates and demodulates the resulting torque signal. Shaft 55 is shown in Fig. 6 to be supported against axially transverse motion by a pair of journal bearings 58. Drive shaft 55, therefore, rotates about its axis in response to a rotatory drive energy supplied by drive motor 40 and delivered thereto by drive belt 41. A coupling arrangement 60 that is fixed axially onto drive shaft 55 permits resilient axial displacement of a coupling shaft 62 with respect to the axis of drive shaft 55. Coupling arrangement 60 is formed of a flanged member 61 that is coupled to rotate with drive shaft 55. A further flanged member 63 is shown to be engaged with coupling shaft 62. Flanged members 61 and 63 are each provided with respective resilient elements 65 that facilitate the permissible axial displacement of coupling shaft 62 with respect to the central axis defined by drive shaft 55. The rotatory energy is transmitted across intermediate element 67, with which resilient elements 65 communicate. Fig. 7 is a side plan representation of the drive system as shown in Fig. 6, enlarged to show greater detail. As shown in Figs. 6 and 7, the uppermost end of coupling shaft 62 is arranged to be connected to rotatory input 13 of differential 11 (shown in fragmented form in these figures). Differential 11 is ofthe conventional type having an hexagonal nut 69 (Fig. 7) installed at rotatory input 13. Rotatory input 13 is formed as a pinion shaft, and hexagonal nut 13 is threadedly engaged therewith. The application of a high tightening torque to hexagonal nut 13 during assembly of the differential prevents same from loosening during application ofthe rotatory energy via coupling shaft 62. Fig. 7 shows differential 11 in the process of being installed onto coupling shaft 62, and therefore hexagonal nut 69 is shown in two positions, where it is designated 69 and 69', respectively. Upon completion ofthe installation of differential 11, hexagonal nut 69 becomes engaged with a nut driver 70. Nut driver 70 is axially translatable, and therefore is shown in two positions, where it is designated 70 and 70'. Fig. 8 is a side plan view of nut driver 70 that couples the drive system to the mechanical system under test. Fig. 9 is a top plan view of nut driver 70 of Fig. 8 showing therein three engagement surfaces for coupling with the flanks of an hexagonal nut (not shown in this figure) at the rotatory input ofthe mechanical system under test. As shown in Fig. 8 and Fig. 9, nut driver 70 has a tapered outward appearance when viewed from the side (Fig. 8). Internally, nut driver 70 is provided with three engagement surfaces 71. The engagement surfaces engage with the flank surfaces of the nut (not shown) at rotatory input 13 of differential 11. The nut driver is, as previously noted, axially displaceable along the axis of coupling shaft 62, and is urged upward toward the nut at the rotatory input ofthe differential by operation of a resilient spring member 72 (Fig. 6). Thus, the nut driver is urged into communication with the nut by operation ofthe light resilient bias supplied by spring 72, thereby ensuring engagement between nut driver 70 and the hexagonal nut (not shown in Figs. 8 and 9) at the rotatory input of differential 11. It is to be noted that the light axial bias applied by the engagement spring is negligible and affords the differential a degree of freedom of movement in the axial direction. Referring once again to Fig. 7, sensors 73-76 are shown for monitoring various aspects ofthe operation ofthe differential in response to the application ofthe rotatory input. For example, in one embodiment of the invention, the various sensors are configured to monitor angular position ofthe rotatory input, transaxial displacement of the drive shaft, transaxial displacement ofthe differential in response to the application ofthe rotatory input energy, temperature in the region ofthe input bearing (not shown) ofthe differential, acoustic noise, etc. Fig. 10 is a plan representation of a clamping arrangement constructed in accordance with the principles ofthe invention, the clamping arrangement being shown in two positions. Elements of structure that correspond to those previously described are similarly designated. As shown, support 18 is coupled to base 20, illustratively via one or more fasteners 140. In this embodiment, a pair of resilient support elements 141 are disposed on support element 18 and there is supported thereon an isolation support 142. The isolation support has a central V-shaped region 144 in the vicinity of which are installed support bearings 146 and 147. Rotatory output 14 of differential 11 (not shown in this figure) rests on the support bearings. Engagement arms 32 and 33, as previously noted, have first and second positions corresponding to open and closed conditions. Engagement arms 32 and 33 are shown in the closed condition, wherein rotatory output 14 is clamped to support bearings 146 and 147. When the support arms are in the open position, identified as 32' and 33' (shown in phantom), the differential can be removed or installed onto isolation support 142. Actuation of the engagement arms between the open and closed conditions is effected by operation of linear actuator 35 which is coupled to the engagement arms by respectively associated ones of engagement coupler links 148 and 149. Engagement coupler links 148 and 149 are each coupled at a respective first ends thereof to a respectively associated one of engagement arms 32 and 33, and they each are coupled to one another at a central pivot coupling 150. An armature 151 of linear actuator 35 travels vertically to effect clamping and release of rotatory output 14. When armature 151 is extended upward, engagement arms 32 and 33 are urged toward rotatory output 14, whereby spring-loaded contacts 152 and 153 communicate with rotatory output 14. In this embodiment, the spring-loaded contacts exert a resilient biased force against rotatory output 14 facilitating the latching ofthe engagement arms by operation of armature 151. As shown, when the armature is extended fully upward, engagement coupler links 148 and 149 are urged beyond the point where their respective axes are parallel, and therefore, the engagement coupler links are biased against the underside of isolation support 142. It should be noted that the pivot pin (not specifically shown) coupled to armature 151 at pivot coupling 150 has a smaller diameter than the apertures in the engagement coupler links. Thus, during testing ofthe vibration and noise of the differential, armature 151 of linear actuator 35 is essentially decoupled from engagement coupler links 148 and 149 and isolation support 142. When it is desired to remove differential 11 from isolating arrangement 10, armature 151 is withdrawn, whereupon pivot coupling 150 is translated to the location identified as 150'. In this position, the engagement arms are translated to the location shown in phantom as 32' and 33'. In a further embodiment ofthe invention, one or both of spring-loaded contacts 152 and 153 is provided with a displacements sensor 154 that produces an electrical signal, or other indication, responsive to the extent of inward translation ofthe spring- loaded contact. Such an indication would be responsive to the outside dimension ofthe rotatory output of differential 11 , thereby providing a means for determining dimensional variations of the differential housing (not specifically identified in this figure) during a production run. Fig. 11 is a compact drive arrangement constructed in accordance with the invention for coupling the rotatory output of a mechanical energy transfer system under test (not shown in this figure) to a rotatory load, which will be described hereinbelow in the form of an electric rotatory device that is operable in drive and generator modes. As shown in this figure, a load arrangement 80 is provided with a load motor 81 having a belt pulley 82 arranged to rotate with a load motor shaft 83. In this specific embodiment, pulley 82 is coupled to a further belt pulley 85 via a load belt 86. Pulley 85 is coupled to a tubular shaft 89 having a flanged portion 90 that is arranged in axial communication with tubular shaft 89. In a manner similar to that of pulley 46 in Fig. 6, belt pulley 82 in Fig. 11 contains a torque sensing arrangement 87 that provides an electrical signal (not shown) responsive to a torque differential between the belt pulley and load motor shaft 83. The electrical signal responsive to torque is available at signal output connector 84, as described below. In this specific illustrative embodiment of the invention, torque sensing arrangement 87 contained within belt pulley 82 and its associated signal output connector 84 include a strain gauge 88 installed to respond to the displacement of a web 92. That is, in the practice of this aspect of the invention, torque is transmitted across web 92 wherein, for example, the torque is applied across the periphery of the web, and an output shaft 98 is coupled nearer to the center ofthe web. Of course, the application of the torque may be rotationally reversed. As the torque is applied, web 92 is correspond- ingly deformed, and strain gauge 88 installed on the web measures the deformity in the web in response to the applied torque. Over a predetermined range of torque, the deformation of web 92, as determined by measurement ofthe electrical response of strain gauge 88 at signal output connector 84, can be correlated to the magnitude ofthe applied torque. As described hereinabove with respect to signal output connector 56 in Fig. 6, in this specific illustrative embodiment ofthe invention, signal output connector 84 in Fig. 11 additionally contains circuitry (not shown) that is AC coupled to the torque sensing arrangement, and that modulates and demodulates the resulting torque signal. The torque signal will be to a significant extent responsive to the load or drive characteristic of load motor 81 , which is controllable by the application of appropriate electrical signals (not shown) or connection of electrical loads (not shown) at electrical terminals 99 thereof. Tubular shaft 89 is supported rotatably by ball bearings 91. On the other side of pulley 85 is arranged a resilient element 93 that is secured to remain in communication with pulley 85 by operation of an end cap 94. End cap 94 has internally affixed thereto a load shaft 95 that is arranged to extend along the interior length of tubular shaft 89. Thus, notwithstanding that tubular shaft 89 is axially fixed in a support 96, load shaft 95 will rotate with the tubular shaft but can experience displacement transverse to axis of rotation 98. Thus, any rotatory element (not shown in this figure) that would be coupled to load shaft 95 at its associated coupler 97 would be provided with freedom of motion in any direction transverse to the axis of rotation ofthe load shaft, and therefore would not be constrained in the axially transverse direction. Fig. 12 is a partially cross-sectional side plan view of a compact drive arrangement similar in some respects to that of Fig. 11. This figure shows a shaft support system 100 that provides the degree of freedom of motion discussed hereinabove with respect to the embodiment of Fig. 11, and additionally provides axial thrust support. Shaft support system 100 is provided with a pulley 101 that can be coupled to another rotatory element (not shown) via a belt 102. The pulley is fixed to a tubular shaft 104 that is axially fixed in a support 105 by ball bearings 106. At the other end of tubular shaft 104, the tubular shaft is expanded radially to form a shaft portion 108 having a large diameter than the central portion of the tubular shaft. A resilient coupling arrangement that is generally designated as 110 is resiliently coupled to shaft portion 108. Resilient coupling arrangement 110 is provided with an intermediate plate 111 and an end plate 112 that are resiliently coupled to one another whereby they rotate with tubular shaft 104. A central shaft 114 is coupled at its right-most end to end plate 112 so as to be rotatable therewith. The central shaft, however, experiences freedom of movement in all directions transverse to its axis of rotation. Any travel of central shaft 114 toward the right hand side is limited by an end stop 115, which is arranged, in this embodiment, to provide a measure of axial adjustment. The other end of central shaft 114 is coupled to a resilient coupling arrangement which is generally designated as 117. Fig. 13 is a partially phantom enlarged representation ofthe resilient coupling element shown in Fig. 12. Resilient coupling element 117 is shown in this figure in an expanded form to facilitate this detailed description. Central shaft 114 (Fig. 12) has a reduced diameter end portion 120 on which is installed a flanged washer 121 having a reduced diameter portion 122 and a flange 123 formed therearound. A further flanged element 125 is installed on reduced diameter end portion 120 of central shaft 114, a shear pin 127 being disposed between flanged washer 121 and further flanged element 125. In addition, an annular portion 128 is arranged to surround the flanged washer and the further flanged element, and to overlie circumferentially the axial region where resilient element 127 is disposed. All of these elements are secured to reduced diameter end portion 120 of central shaft 114 by a fastener 129 and a washer 130. As shown, fastener 129 is threadedly engaged axially onto the end of central shaft 114. A support portion 132 is fixed onto further flanged element 125 by fasteners 133. Support portion 132 is resiliently coupled to a flanged shaft 135 by means of studs 136. Thus, even though central shaft 114 enjoys freedom of movement transverse to its axis of rotation, resilient coupling arrangement 117 provides yet further freedom of movement in all directions transverse to the axis of rotation for flanged shaft 135. Flanged shaft 135, in one embodiment ofthe invention, is ultimately coupled to a rotatory output, such as rotatory output 15 of Fig. 1. Alternatively, shaft support system 100 can be used in the drive arrangement of Fig. 6 to provide significant degree of motion lateral to the axis of rotation to the drive shaft. Fig. 14 is an isometric representation of an arrangement for isolating a system under test, the isolation system being constructed in accordance with the principles ofthe invention. In this embodiment, the system under test is an electrical energy transfer device. As shown in this figure, an isolation support 160 isolates an electrical energy transfer device, illustratively in the form of an electrical transformer 162. The electrical transformer is secured to an isolation base 164 by operation of a toggle locking device 165. Isolation base 164 is mechanically isolated from a ground surface 166 by a plurality of resilient isolation elements 170. That is, the isolation base is permitted freedom of movement in at least one plane of motion, and preferably a plurality of planes of motion, by operation ofthe resilient isolation elements. In the practice of this specific illustrative embodiment of the invention, the resilient isolation elements have a resilience characteristic that, as previously noted in regard of other embodiments ofthe invention, exclude a natural frequency of isolation support 160 and transformer 162. The motion of the transformer and the isolation support is therefore responsive substantially entirely to the electrical energy that is transferred to or from transformer 162 via its electrical terminals 172. Fig. 15 is a process diagram of a typical process for conducting an energy analysis of a gear system. In this known system, gears under test 180 are driven by a drive 181, the speed of which is controlled by a speed control 183. Information relating to the drive speed is conducted to a digital data storage system 185. Analog sensors 187 obtain analog data from gears under test 180, the analog signals from the sensors being conducted to an A/D converter 188. The A/D converter performs the conversion of the analog signals in response to a clock 190, and the resulting digital data is conducted to digital data storage system 185. Thus, digital data storage system 185 contains the digitized analog signals obtained from sensors 187, which data is correlated to the speed at which gears under test 180 are driven. The digital data of digital data storage system 185 is converted to the frequency domain by subjecting same to a fast Fourier transform at step 193. The resulting frequency components are then ordered at step 194 and analyzed manually at step 195. At this step, the collected data, in the frequency domain, is analyzed in the context of predetermined test criteria. The pass/fail decision is then made at step 197, and if the predetermined criteria is not met, a "fail" indication is produced at step 198. Otherwise, a "pass" indication is issued at step 199. Fig. 16 is a process diagram of a process for conducting an energy analysis in accordance with the principles ofthe present invention. As show in this figure, gears under test 201 are driven into rotation by a drive system 202, which also drives an encoder 204. Encoder 204 delivers signals responsive to the rotation of gears under test 201 to an A/D converter 206. In this embodiment, the signal from encoder 204 serves as a pacing clock for the A/D converter. Information relating to noise and displacement issued by the gears under test is collected by analog sensors 207. The resulting analog signals are conducted to A/D converter 206 where they are converted to digital signals correlated to the rotation of drive system 202. The digital signals from A/D converter 206 are conducted to a digital data store 210 where they are maintained in correlation to the drive information obtained from encoder 204. In this specific illustrative embodiment ofthe invention, the digital data is stored two-dimensionally, wherein sensor signal amplitude is identified with the y-axis, and rotational position is identified with the x-axis. The correlated digital data is subjected to a fast Fourier transform at step 212 wherein the data is converted into its frequency components. Data in the frequency domain is subjected to processing at step 214, where a power spectrum density is created using a data window. The power spectrum density data is then analyzed harmonically at step 215 to determine its relationship with predetermined test criteria. The decision whether the power spectrum density data passes or fails with respect to predetermined test criteria is made at step 216, and the predetermined criteria is not met, a "fail" indication is produced at step 217. Otherwise, a "pass" indication is issued at step 218. Fig. 17 is a diagram of a process for conducting an analysis 230 in accordance with the principles of the present invention for determining bumps and nicks in a mechanical energy transfer system. As show in this figure, gears under test 231 are driven into rotation by a drive system 232, via a torque sensor 234. Torque sensor 234 delivers signals responsive to the rotatory force supplied to gears under test 231 to an A/D converter 236. Information relating to noise and displacement issued by the gears under test is collected by noise sensors 237, which may include velocity sensors (not shown in this figure), accelerometers (not shown in this figure), microphones (not shown in this figure), etc. The resulting noise signals are conducted to A/D converter 236 where they are converted to digital signals correlated to the torque applied by drive system 232 to gears under test 231. The digital signals from A/D converter 236 are conducted to a digital data store 240 where they are maintained in correlation to the drive information obtained from torque sensor 234. In this specific illustrative embodiment ofthe invention, the digital data is stored as two two-dimensional data sets, wherein noise sensor signal amplitude is identified with a first y-axis, and time is identified with the x-axis. The amplitude of the torque signal is identified with a second y-axis, and time is again identified with the x-axis. Correlated data from digital data store 240 is subjected to analysis at step 242, wherein peaks that occur simultaneously in the torque and noise signal waveforms are identified. These peaks are then measured at step 244 to determine whether they exceed predetermined thresholds. Those peaks that exceed the predetermined thresholds are then tested at step 245 against the harmonics of each gear tooth frequency, to determine whether the peaks correspond to anomalous conditions. The decision whether the gears under test pass or fail with respect to predetermined test criteria is made at step 246, and if the predetermined criteria is not met, a "fail" indication is produced at step 247. Otherwise, a "pass" indication is issued at step 248. In some embodiments ofthe invention, a calculation ofthe severity ofthe bumps or nicks that caused the anomalous conditions is calculated at step 249. In one embodiment ofthe process of Fig. 17, analysis is performed using only the torque data derived from torque sensor 234, without correlation to the noise data obtained from noise sensor 237. In this embodiment, therefore, noise sensor 237 need not be provided, as the noise signal therefrom is not used. Thus, torque sensor 234 delivers signals responsive to the rotatory force supplied to gears under test 231 to A/D converter 236, and the digital data is stored as a single two-dimensional data set, wherein the amplitude ofthe torque signal is identified with the y-axis, and time is identified with the x-axis. Peaks in the torque signal are then measured at step 244 to determine whether they exceed a predetermined threshold. Those peaks that exceed the predetermined thresholds are then tested at step 245 against the harmonics of each gear tooth frequency, to determine whether the peaks correspond to anomalous conditions. The decision whether the gears under test pass or fail with respect to predeter- mined test criteria is made at step 246, and if the predetermined criteria is not met, a "fail" indication is produced at step 247. Otherwise, a "pass" indication is issued at step 248. As previously noted, a calculation ofthe severity ofthe bumps or nicks that caused the anomalous condition is calculated at step 249. Although the invention has been described in terms of specific embodiments and applications, persons skilled in the art can, in light of this teaching, generate additional embodiments without exceeding the scope or departing from the spirit of the claimed invention. Accordingly, it is to be understood that the drawing and description in this disclosure are proffered to facilitate comprehension ofthe invention and should not be construed to limit the scope thereof.

Claims: WHAT IS CLAIMED IS: 1. An arrangement for monitoring a noise signal issued by an energy transfer system while it is subjected to a test process for noise, the energy transfer system being of the type having an energy input and at least one energy output, the arrangement comprising: a base for supporting the arrangement and the energy transfer system; isolation support means for supporting the energy transfer system whereby the energy transfer system is translatable in at least one plane of freedom with respect to said base; engagement means for securing the energy transfer system to said isolation support means; a first acoustic sensor arranged at a first location in the vicinity of the energy transfer system for producing a first signal responsive substantially to a qualitative condition ofthe energy transfer system; thermal sensor means for producing a thermal signal responsive to a temperature ofthe energy transfer system.; and acoustic sensor sensitivity control means responsive to said thermal sensor means for controlling the amplitude ofthe first signal in response to temperature. 2. The arrangement of claim 1 , wherein said thermal sensor means comprises an infrared sensor for communicating optically with the energy transfer system. 3. The arrangement of claim 2, wherein said thermal sensor means has a directional characteristic and is directed to a predetermined region ofthe energy transfer system for determining a rate of change of temperature ofthe predetermined region with respect to time. 4. The arrangement of claim 1, wherein the response ofthe variation ofthe amplitude of the noise signal with respect to temperature is in accordance with a non-linear amplitude-temperature relationship. 5. The arrangement of claim 1, wherein there is further provided energy supply means coupled to the energy transfer system for supplying energy thereto. 6. The arrangement of claim 5, wherein the energy transfer system is a mechanical energy transfer system, and said energy supply means comprises a source of rotatory mechanical energy. 7. The arrangement of claim 6, wherein there is further provided rotatory coupling means for coupling said source of rotatory mechanical energy to the energy transfer system. 8. The arrangement of claim 7, wherein said mechanical energy transfer system has forward and reverse directions of operation, and drive and coast modes of operation for each ofthe forward and reverse directions of operation. 9. The arrangement of claim 8, wherein there the mechanical energy transfer system contains at least a pair of meshed elements, at least one of said pair of meshed elements being a gear having a plurality of gear teeth thereon, said gear teeth each having first and second gear tooth surfaces for communicating with the other element of said pair of meshed elements, a mechanical energy transfer communication between the pair of meshed elements being effected primarily via the respective first gear tooth surfaces during forward-drive and reverse-coast modes of operation, and primarily via the respective second gear tooth surfaces during forward-coast and reverse-drive modes of operation. 10. The arrangement of claim 9, wherein said first acoustic sensor is arranged at a first location in the vicinity ofthe mechanical energy transfer system, and the first signal is responsive substantially to a qualitative condition of said first gear tooth surfaces. 11. The arrangement of claim 10, wherein there is further provided a second acoustic sensor arranged at a second location in the vicinity ofthe mechanical energy transfer system for producing a second signal responsive substantially to a qualitative condition of said second gear tooth surfaces, and said acoustic sensor sensitivity control means additionally controls the amplitude ofthe second signal. 12. The arrangement of claim 11, wherein the first and second locations are distal from each other on opposite sides of said pair of meshed elements. 13. The arrangement of claim 5, wherein the energy transfer system is an electrical energy transfer system, and said energy supply means comprises a source of electrical energy. 14. The arrangement of claim 13 , wherein there is further provided electrical load means for receiving an output electrical energy from the energy transfer system when said engagement means is in said second position. 15. The arrangement of claim 5, wherein said first acoustic sensor is arranged to communicate with the energy transfer system and the first signal is responsive to an operating characteristic ofthe energy transfer system in response to the energy supplied by said energy supply means. 16. The arrangement of claim 15, wherein said first acoustic sensor is arranged to contact the energy transfer system. 17. The arrangement of claim 15, wherein said first acoustic sensor is arranged to contact said isolation support means. 18. The arrangement of claim 15, wherein said first sensor is arranged to be translatable relative to the energy transfer system. 19. The arrangement of claim 15, wherein said first acoustic sensor comprises a microphone for producing a signal responsive to an acoustic energy issued by the energy transfer system in response to the energy supplied by said energy supply means. 20. The arrangement of claim 15, wherein said first acoustic sensor comprises a laser sensor for producing a signal responsive to a displacement ofthe energy transfer system in response to the energy supplied by said energy supply means. 21. The arrangement of claim 15, wherein said first acoustic sensor comprises an accelerometer. 22. The arrangement of claim 15, wherein said first acoustic sensor comprises a velocity sensor. 23. The arrangement of claim 1, wherein said isolation support means supports the energy transfer system whereby it is translatable in at least a second plane of freedom with respect to said base. 24. A method of testing a gear assembly ofthe type having an input and an output, the method comprising the steps of: installing the gear assembly on a mounting arrangement that resiliently permits motion of the gear assembly in all directions, and that has a resilient frequency characteristic that excludes all natural frequencies ofthe gear assembly; applying a torque at the input ofthe gear assembly, whereby the gear assembly is rotatably operated; applying a load at the output ofthe gear assembly; sensing a predetermined operating characteristic ofthe gear assembly; and controlling said step of sensing in response to a temperature ofthe gear assembly. 25. The method of claim 24, wherein said step of sensing comprises the step of detecting acoustic energy issued by the gear assembly. 26. The method of claim 25, wherein there is further provided the step of detecting electromagnetic energy issued by the gear assembly. 27. The method of claim 26, wherein said step of detecting electromagnetic energy comprises the further step of directing a thermal energy sensor to monitor the temperature of a predetermined region ofthe gear assembly. 28. The method of claim 27, wherein said predetermined region is a region of a bearing ofthe gear assembly. 29. The method of claim 27, wherein said step of controlling comprises the further step of adjusting the sensitivity of an acoustic energy sensor. 30. The method of claim 28, wherein there is provided the further step of monitoring a variation in temperature over time ofthe region ofthe bearing. 31. The method of claim 30, wherein there is provided the further step of determining a qualitative characteristic of the bearing in response to said step of monitoring a variation in temperature over time ofthe region ofthe bearing. 32. The method of claim 26, wherein there is provided the further step of determining a qualitative characteristic of a lubricant in the gear assembly. 33. The method of claim 26, wherein there is provided the further step of determining a qualitative characteristic of a lubricant in the gear assembly. 34. The method of claim 27, wherein there is provided the further step of correlating a predetermined characteristic of the acoustic energy issued by the gear assembly to the thermal energy issued by the gear assembly. 35. The method of claim 26, wherein there is provided the further step of controlling a sensitivity characteristic of an acoustic sensor system in response to the thermal energy issued by the gear assembly. 36. The method of claim 25, wherein said step of detecting acoustic energy issued by the gear assembly comprises the step of placing a microphone in the vicinity of the gear assembly. 37. The method of claim 24, wherein said step of sensing comprises the step of detecting vibratory displacement energy issued by the gear assembly. 38. The method of claim 37, wherein said step of detecting vibratory displacement energy issued by the gear assembly comprises the further step of effecting communication between an accelerometer and the gear assembly. 39. The method of claim 37, wherein said step of detecting vibratory displacement energy issued by the gear assembly comprises the further step of effecting communication between a velocity sensor and the gear assembly. 40. The method of claim 24, wherein said step of sensing comprises the further step of monitoring a first sensor that receives acoustic energy responsive to a qualitative condition ofthe gear assembly in a drive mode of operation. 41. The method of claim 40, wherein said step of sensing comprises the further step of monitoring a second sensor that receives acoustic energy responsive to a qualitative condition ofthe gear assembly in a coast mode of operation. 42. The method of claim 41, wherein said step of controlling comprises the further step of controlling an output signal from the second sensor in response to the temperature ofthe gear assembly. 43. The method of claim 41 , wherein the first and second sensors are disposed at respective locations that are distal from each other, with the gear assembly interposed therebetween.

Inventors: JURANITCH JAMES C, JURANITCH, JAMES, C.
Applicants: JURANITCH JAMES C, VERI TEK INC, JURANITCH, JAMES, C., VERI-TEK, INC.
Application year: 1999
Main classification: G01M13
IPC codes: G01H3, G01M13