Patent Publication Number: US-6984897-B2

Title: Electro-mechanical energy conversion system having a permanent magnet machine with stator, resonant transfer link and energy converter controls

Description:
CROSS REFERENCE APPLICATION 
     This is a non-provisional patent application of provisional patent application Ser. No. 60/442,633 filed Jan. 23, 2003. 
    
    
     This invention was made with Government support under Contract NO. DE-FG36-03G013138 awarded by the Department of Energy. The Government has certain rights in this invention. 
    
    
     BACKGROUND OF THE INVENTION 
     1. Field of the Invention 
     An electro-mechanical energy conversion system including a permanent magnet induction machine to selectively convert and transfer energy from an energy source and an energy load. 
     2. Description of the Prior Art 
     Seemingly limitless electro-mechanical systems and devices have been devised to convert electrical energy to mechanical energy or vice versa. 
     In efforts to reduce dependency on fossil fuels, countless generator systems to convert mechanical to electrical energy including various wind power systems or wind turbines have been developed. Such systems generally include a shaft-mounted turbine to drive an electrical generator. To operate the generator at optimum speed for maximum power output, the wind turbine must produce a relatively constant torque or speed despite changes in wind speed and wind direction. Generally, the pitch of the turbine blades is varied to regulate the torque or resultant speed. Unfortunately, such pitch angle control mechanisms are complex and costly to manufacture, maintain and repair. 
     Moreover, such energy conversion systems using variable speed wind turbine generators to provide the source of energy to utility power grids require a matched constant output frequency at preferably optimum power output. Thus, the variable frequency AC from such turbine generators must be converted to a constant frequency AC for use by the utility power grid. Generally, this conversion can be accomplished through an intermediate conversion to DC by a rectifier and subsequent inversion to fixed-frequency AC by means of an inverter. Unfortunately, such systems are inefficient, relatively expensive, difficult to maintain operation and relatively unreliable as an electricity source. 
     U.S. Pat. No. 5,028,804 discloses an energy conversion generation system to receive energy from a resource and convert the energy into electrical power for supply to a polyphase electrical power grid operating at a system frequency. The controller establishes a reference signal, then processes the sensor signal with the reference signal to produce a controller signal. The converter produces the excitation power at an excitation frequency in response to the controller signal so as to increase the ratio of the electrical power output to the resource energy power input received by the prime mover. 
     U.S. Pat. No. 4,490,093 describes a windpower system comprising a support and a turbine having a shaft rotatively mounted to the support. The turbine has variable pitch blades controlled by the differential motion of a rotary control shaft coaxial with the turbine shaft and the turbine shaft so that the blade pitch can be varied by a stationary motor without requiring any slip rings or other such wear-prone couplings. In the event of a power failure, rotary motion of the control shaft is prevented so that the turbine blades are feathered solely due to the force developed by the rotating turbine. When the turbine is used to generate electrical power an induction generator is coupled to the turbine shaft. The shaft speed is indicative of generator output power. Thus, generator speed is monitored and used to control the pitch of the turbine blades so as to maintain generator output power at the maximum value when wind speed is below the machine&#39;s rated wind speed and no more than rated output power when wind speed exceeds rated wind speed. 
     U.S. Pat. No. 4,426,192 teaches a method and apparatus for controlling windmill blade pitch. The pitch of the turbine blades is based on a dual-deadband control strategy. If the current turbine speed is determined to be outside of a relatively wide deadband, action is taken to correct the speed by changing blade pitch. If the current speed is within the relatively wide deadband, then the average of the turbine speed over an interval is compared with a relatively narrow deadband within the wider deadband. Action is then taken to change the blade pitch if the average speed is outside the narrow deadband. In this way, wide excursions of turbine speed are corrected promptly, but the frequency of control actions is minimized by requiring only the average speed to be kept within tight limits. 
     U.S. Pat. No. 6,137,187 relates to a variable speed system such as a wind turbine comprising a wound rotor induction generator, a torque controller and a proportional, integral derivative (PID) pitch controller. The torque controller controls generator torque using field oriented control, and the PID controller performs pitch regulation based on generator rotor speed 
     U.S. Pat. No. 5,225,712 shows a wind turbine power converter that smooths the output power from a variable speed wind turbine to reduce or eliminate substantial power fluctuations on the output line. The power converter has an AC-to-DC converter connected to a variable speed generator that converts wind energy to electric energy, a DC-to-AC inverter connected to a utility grid, and DC voltage link connected to an electrical energy storage device such as a battery or a fuel cell. An apparatus and method for controlling the instantaneous current flowing through the active switches at the line side inverter to supply reactive power to the utility grid is also disclosed. The inverter can control reactive power output as a power factor angle, or directly as a number of VARs independent of the real power. Reactive power can be controlled in an operating mode when the wind turbine is generating power, or in a static VAR mode when the wind turbine is not operating to produce real power. To control the reactive power, a voltage waveform is used as a reference to form a current control waveform for each output phase. The current control waveform for each phase is applied to a current regulator which regulates the drive circuit that controls the currents for each phase of the inverter. Means for controlling the charge/discharge ratio and the regulating the voltage on the DC voltage link is also disclosed. 
     U.S. Pat. No. 5,028,804 relates to an energy conversion generation system to receive energy from a resource and convert the energy into electrical power for supply to a polyphase electric power grid operating at a system frequency. A prime mover driven by the resource energy and a converter such as a power electronic converter produces excitation power from power received from a converter power source. A brushless doubly-fed generator having a rotor with rotor windings and a stator with stator windings comprises a first and second polyphase stator system. The rotor is driven by the prime mover. The first stator system supplies the electrical power to the grid, and the second stator system receives the excitation power from the converter. A sensor senses a parameter of the electrical power output supplied to the grid and produces a sensor signal corresponding to the sensed parameter. A controller controls the converter in response to the sensor signal. 
     U.S. Pat. No. 4,523,269 discloses a DC to N phase AC converter, a DC source having first and second terminals for deriving equal amplitude opposite polarity DC voltages, a series resonant circuit, and N output terminals, one for each phase of the converter. The series resonant circuit is selectively connected in series with the first and second terminals and the N output terminals for an interval equal to one half cycle of the resonant circuit resonant frequency, so that current flows between a selected one of the first and second terminals and the resonant circuit and a selected one of the N output terminals during the interval. The resonant circuit current is zero at the beginning and end of the interval. A capacitor shunting each of the output terminals has a value relative to the capacitance of the series resonant circuit such that the voltage across each output terminal remains approximately constant between adjacent exchanges of energy between the resonant circuit and the output terminal. The selective connection is in response to a comparison of the actual voltage across each of the N output terminals and a reference voltage for each of the N output terminals. The comparison controls when the flow of current between the selected first and second terminals and the selected output terminal via the resonant circuit begins. The frequency of the AC voltage developed across the N output terminals is much less than the resonant frequency of the circuit. 
     Despite these systems, there remains a need for an efficient, reliable variable speed energy conversion system. 
     SUMMARY OF THE INVENTION 
     The present invention relates to an electro-mechanical energy conversion system to selectively convert and transfer energy from an energy source to an energy load and an energy transfer multiplexer to selectively control the direction of power or energy flow through the energy transfer multiplexer to control the operation of the electro-mechanical energy conversion system. 
     The electro-mechanical energy conversion system may comprise a motor to drive a pump, fly wheel, or other such device or a generator to power an electrical power grid or an electrical load. 
     For example, the electro-mechanical energy conversion system of the present invention comprises a permanent magnet induction machine to convert wind energy into an electrical power output to a polyphase electric power grid operating at a system frequency comprising a variable speed generation system such as a turbine for converting the wind energy into mechanical energy and a generator coupled to the turbine to drive the rotor to create power in the stator to supply electrical power to the power grid. The generation system also includes control means for varying the rotor speed in response to the power output and the wind energy to increase the ratio of the electrical output power to the wind energy input. 
     The electro-mechanical energy conversion system operates at high efficiency regardless of variable resource conditions by controlling the rotor speed. Thus, the electro-mechanical energy conversion system can operate at substantially reduced rating. Thus, the equipment and operating costs are significantly lower than those of existing systems. 
     These and other objects, features and advantages of the present invention will become apparent to those skilled in the art from the following description and drawings. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       For a fuller understanding of the nature and object of the invention, reference should be had to the following detailed description taken in connection with the accompanying drawings in which: 
         FIG. 1A  is a block diagram of the energy transfer multiplexer of the present invention. 
         FIG. 1B  is a block diagram of the electro-mechanical energy conversion system of the present invention. 
         FIG. 2A  is a rotor voltage/rotor frequency curve for the electro-mechanical energy conversion system for the present invention controlling a doubly fed induction machine. 
         FIG. 2B  is a mechanical input power/rotation rate curve for the electro-mechanical energy conversion system of the present invention controlling a doubly fed induction machine. 
         FIG. 2C  is a rotor power/rotation rate curve for the electro-mechanical energy conversion system of the present invention controlling a doubly fed induction machine. 
         FIG. 3A  is a block diagram of the electro-mechanical energy conversion system of the present invention implemented with a doubly fed induction machine and mechanical energy source. 
         FIG. 3B  is a block diagram of the electro mechanical energy conversion system of the present invention implemented with a permanent magnet generator or machine and mechanical energy source. 
         FIG. 3C  is a block diagram of an electrical to electrical energy conversion system of the present invention. 
         FIG. 4  is a topological schematic of the energy transfer multiplexer or energy transfer section of the electro-mechanical energy conversion system of the present invention implemented with IGBT switches. 
         FIG. 5  is a circuit diagram of the energy transfer multiplexer or energy transfer section of the electro mechanical-energy conversion system of the present invention implemented with IGBT switches. 
         FIG. 6  is a schematic of the drivers or controlled power switches of the energy transfer section of the electro-mechanical energy conversion system of the present invention implemented with IGBT switches. 
         FIG. 7  is a schematic of the sensors of the energy transfer multiplexer or energy transfer section of the electro-mechanical energy conversion system of the present invention implemented with IGBT switches. 
         FIG. 8  is a schematic the drivers or controlled power switches of the energy transfer multiplexer or energy transfer section of the electro-mechanical energy conversion system of the present invention implemented with SCR switches. 
         FIG. 9  shows an IGBT power switch or driver of the electro-mechanical energy conversion system of the present invention for the IGBT switches. 
         FIG. 10  shows a SCR power switch or driver of the electro-mechanical energy conversion system of the present invention for the SCR switches. 
         FIG. 11  shows the initial or starting polarity and the final polarity of the capacitor potential for the plurality of switches or control points of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention and the associated plurality of the differential voltage,  I Δ O  between the input E 1  and output E 0  potential. 
         FIG. 12  depicts various electrical charge states on the bi-directional resonant link of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention. 
         FIG. 13  shows the informational or decision flow and control logic for switching states of the first and second plurality of switches or energy transfer control points of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention. 
         FIG. 14  shows a sinusoidal energy reference curve of the electro-mechanical energy conversion system of the present invention. 
         FIGS. 15 through 17A  and  17 B show the process of pre-charging the shuttle or resonant capacitor of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention. 
         FIG. 18  shows the energy transfer through the bi-directional resonant transfer link of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention where the current flow or charge transfer is from E 1  to E 0  (left to right) equation. 
         FIG. 19  shows the energy transfer through the bi-directional resonant transfer link of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention transferring energy from the load to the source and equation where the current flow or charge transfer is from −E 0  to −E 1  (right to left). 
         FIG. 20  continues and completes the family of equations deriving the quantity of current transferred between the rotor and stator of the electro-mechanical energy conversion system of the present invention. 
         FIG. 21  is a graphic depiction of the energy or power transfer of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention. 
         FIG. 22  is another graphic depiction of the energy or power transfer of the energy transfer multiplexer or electro-mechanical energy conversion system of the present invention. 
     
    
    
     Similar reference characters refer to similar parts throughout the several views of the drawings. 
     DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT 
     The present invention relates to an electro-mechanical energy conversion system including a permanent magnet induction machine to selectively convert and transfer energy from an energy source to an energy load and an energy transfer multiplexer to selectively control the flow of energy from an energy source to an energy load. 
     The electro-mechanical energy conversion system of the present invention may be configured to operate as a generator or motor. As a generator, the electro-mechanical energy conversion system can convert mechanical energy from wind turbines, hydro turbines, steam turbines, internal combustion engineers, fly wheels and the like to generate electrical energy to power an electrical power grid, rural power, electric boats, industrial pumps and the like. 
     The electrical energy can also be converted and stored in the form of hydrogen storage, batteries or compressed air for future use. Likewise, as a motor, the electro-mechanical energy conversion system can convert electrical energy from an electrical power source to power a wide range of mechanically driven or powered devices or systems such as electric boat drives, traction drives, pumps and fans. Of course, there is no known limit as to the application of the electro-mechanical energy conversion system either as a generator or motor. 
     The present invention can include a selectively controlled bi-directional inverter and an energy converter device comprising the permanent magnet induction machine to create a sinusoidal current source/sink. 
     When the electro-mechanical energy conversion system operates with a doubly fed induction generator, a variable frequency/amplifier 3 phase AC excitation current is fed to the rotor winding to generate a rotor electrical excitation frequency. Power is selectively fed to or from the rotor windings to transfer substantially constant frequency, constant amplitude power through the air gap to the stator windings. Specifically, rotor electrical excitation frequency is either added to or subtracted from the rotor mechanical (shaft speed): frequency to generate a substantial constant 3 phase AC power output on the stator winding. 
     Since the bi-directional inverter operates either as a sinusoidal current source or as a sinusoidal current sink, the electro-mechanical energy conversion system as described more fully hereinafter generates a sinusoidal current at the desired frequency or accepts a sinusoidal current at a given frequency thereby selectively transferring energy in either direction. This significantly expands the stability of the operating region of a doubly fed induction machine with a substantial 30% to 45% reduction in the required power level at the rotor winding as compared to equivalent pulse width modulation devices. This power reduction coupled with the reduction in the need for additional harmonic filtering reduces the cost of bi-directional compared to an equivalent PWM converter by about 1 cent per watt of delivered grid power; i.e. $30,000 for a 3×10 6  watt system. In other words, the increased stability of the induction machine and increased operating frequency range allows a lower converter maximum power level with attendant reduced costs. 
     In addition, by utilizing a bi-directional sinusoidal current, the increased stability coupled with the removal of the “PWM required” filter, improves on the design requirements for the mechanical components by reducing the number of components required or by decreasing the ratings of some of the components. The faster operating response improves the elasticity of the mechanical generator drive train. This increased compliance, coupled with sinusoidal current waveform reducing torque ripple prolongs the operating life of the various mechanical components. 
     Moreover, the increased stability on the system also permits a change in the gear ratio and therefore the rotor frequency band above and below the 60 Hertz operating point from ±20 Hertz to +32 Hertz, −8 Hertz. This reduces the required power level of the energy converter and permits additional mechanical power source capture and improved generator performance at the high frequency high power point. Thus the maximum mechanical power input occurs at 68 Hertz reduced from 80 Hertz associated with typical variable speed input energy sources. As a result, the present invention can be effectively implemented with a four pole configuration rather than a six pole configuration with an attendant reduction in generator cost of about 30%. 
     Further, this 12 Hertz or 720 revolutions per minute reduction in the rate of rotor rotation reduces not only the mechanical stress but also increases maximum power available from the generator. 
     These aspects of the present invention provide substantial design and operational flexibility with attendant fabrication and operating savings. 
     As shown in  FIG. 1A , the energy transfer multiplexer comprising a bi-directional resonant inverter generally indicated as  2  including a first bank or plurality of switches or energy transfer control points generally indicated as  4  and a second bank or plurality of switches or energy transfer control points generally indicated as  6  operatively coupled by a series resonant transfer link generally indicated as  8  to selectively control the direction of power or energy flow between the first and second bank or plurality of switches or energy transfer control points  4  and  6  to control the operation of an electro-mechanical energy conversion system in response to a plurality of predetermined conditions or parameters as described more fully hereinafter. Although the operation of the energy transfer multiplexer  2  is described in association with the electro-mechanical conversion system  10 , the energy transfer multiplexer  2  is useful in other applications. 
     As shown in  FIG. 1B , the electro-mechanical energy conversion system  10  comprises an energy converter device such as a permanent magnet induction machine or doubly fed induction machine as described more fully hereinafter coupled between an energy source  12  and the energy load  14  to convert the energy from the energy source  12  and an transfer the converted energy to the energy load  14 . 
     As shown in  FIG. 3A , the electro-mechanical energy conversion system  10  comprises an energy converter device generally indicated as  16  coupled between the input energy source  12  and the output energy load  14  to convert the energy from the input energy source  12  from one form of energy to another and to transfer the converted energy to the output energy load  14  and an energy conversion and transfer control  18  to selectively control the energy converted from the input energy source  12  and transferred to the output energy load  14  in response to a plurality of predetermined conditions or parameters. 
     As shown in  FIG. 3A , the energy converter device  16  includes an energy converter section or device  20  comprising a doubly fed induction machine having a rotor  22  and stator  24  to selectively convert the energy from the input energy source  12  and to selectively transfer the converted energy to the output energy load  14  and an energy transfer section or energy transfer multiplexer  26  coupled to the energy conversion section or device  20  comprising the doubly fed induction machine to selectively transfer energy between the rotor  22  and the stator  24  and to feed the converted energy to the output energy load  14  as described more fully hereinafter. 
     The energy conversion and transfer control or energy management system  18  comprises an energy converter control  28  to control the operation of the energy transfer device or energy transfer multiplexer  26  and a source/load control  30  to control the operation of the input energy source  12  and output energy load  14  with respect to the energy converter device  16 . 
       FIG. 3A  depicts the electro-mechanical energy conversion system  101  as generator with a wind turbine device as the input energy source  12 . As described more fully hereinafter, since the wind turbine device is a variable speed energy source, the energy transfer device  26  and energy converter control  28  of the energy conversion and transfer control  18  control the electrical excitation of the windings of the rotor  22  of the doubly fed induction machine  20  to generate three phase power on the stator  24  matching the frequency of the three phase power of the stator  24  with the AC frequency of the output energy load  14 . 
       FIG. 3B  depicts the electro-mechanical energy conversion system  10  wherein the energy converter section or device  20  comprises a permanent magnet induction machine in place of the doubly fed induction machine  20  depicted in FIG.  3 A. Otherwise, the various components of the electro-mechanical energy conversion system  10  are virtually the same. 
       FIG. 3C  depicts an electrical to electrical energy conversion system  10  using electrical power as the input energy source  12 . The energy transfer multi-plexer shown in  FIGS. 3A ,  3 B and  3 C respectively are similar in function and operation as described hereinafter 
       FIGS. 4 through 7  show the energy transfer device or energy transfer multiplexer  26  implemented through the use of IGBT switches; while,  FIG. 8  shows the energy transfer device  26  implemented through the use of SCR switches. 
     As best shown in  FIGS. 4 and 5 , the energy transfer device  26  comprises a plurality of rotor energy transfer control elements or switches generally indicated as  102  and a plurality of stator energy transfer control elements or switches generally indicated as  104  operatively coupled in energy transfer relationship by a bi-directional resonant transfer link generally indicated as  106  and an isolation element or component generally indicated as  108 . 
     The energy transfer multiplexer  26  may include the isolation element or component  108  as shown in  FIGS. 4 through 8  or may be implemented without the isolation element or component  108  are shown in FIG.  1 A. For example, when the energy transfer multiplexer  26  is used with a doubly fed induction machine the rotor winding is already isolated from the stator winding obviating the necessity of an isolation transformer. 
     The plurality of rotor energy transfer control elements or switches  102  comprises an IGBT switch  110  coupled to each phase A, B, C of the rotor  22  of the doubly fed induction machine by a corresponding conductor or line  112  shunted to ground by a corresponding shunt capacitor  114 . Similarly, the plurality of stator energy transfer control elements or switches  104  comprises an IGBT switch  116  coupled to each phase a, b, c of the stator  24  of the doubly fed induction machine  20  by a corresponding conductor or line  118  connected to corresponding slip rings  119  and shunted to ground by a corresponding shunt capacitor  120 . The bi-directional resonant transfer link  106  comprises a series resonant inductor  122  and resonant capacitor  124 ; while, the isolation element or component  108  comprises a transformer generally indicated as  126  coupled between the bi-directional resonant transfer link  106  and the plurality of energy transfer control elements or switches  104 . 
     The energy transfer device  26  further includes a first local ground energy transfer control element or switch  128  coupled or connected between one side of the resonant link  8  to ground and a second local ground energy transfer control element or switch  130  coupled or connected between the opposite side of the resonant link  8  and ground  12 . 
     As shown in  FIG. 6 , the operation in energy transfer control elements or IGBT switches  110 ,  116 ,  128  and  130  are controlled by a corresponding driver  132  coupled to the energy conversion and transfer control  18  by a corresponding driver conductor or line  134 . Energy transfer control elements or IGBT switches  110 ,  116 ,  128  and  130  and driver  132  connections are shown in detail in FIG.  9 . 
       FIG. 7  shows a plurality of operating parameters or condition sensors to sense and feed real time current and voltage values or data to the energy converter control  28  of the energy conversion and transfer control  18 . 
     Specifically, the rotor phase current for each phase A, B, C of the rotor  22  of the doubly fed induction machine  20  is monitored or sensed at corresponding sensor point  136  on corresponding conductors or lines  112  and fed to the energy converter control  28  of the energy conversion and transfer control  18  by corresponding conductors or lines  137 ; while, the stator phase current for each phase a, b, c of the stator  24  of the doubly fed induction machine  20  are monitored or sensed by a corresponding current sensor  138  and fed to the energy converter control  28  of the energy conversion and transfer control  18  by corresponding conductors or lines  139 . Current through the primary and secondary windings of the transformer  126  are monitored or sensed by at corresponding sensor points  140  and  142  respectively and fed to the energy converter control  28  of the energy conversion and transfer control  18  by corresponding conductors or lines  141  and  143  respectively. In the event no transformer  126  or isolation device is used, the line current is monitored or sensed. 
     The rotor phase voltage for each phase A, B, C of the rotor  22  of the doubly fed induction machine  20  is monitored or sensed at sensor points  138  on corresponding conductors or lines  112  and fed to the energy converter control  28  of the energy conversion and transfer control  18  by corresponding conductors or lines  144 ; while, the stator phase voltage for each phase a, b, c of the stator  24  of the induction machine  20  are monitored or sensed at corresponding sensor points  138  or equivalent on corresponding conductors or lines  118  and fed to the energy converter control  28  of the energy conversion and transfer control  18  by corresponding conductors or lines  146 . The stator common voltage and the fundamental resonant capacitor voltages on opposite sides of the resonant choke  122  and the resonant capacitor  124  are monitored or sensed at corresponding sensor points  148 ,  150  and  152  respectively and fed to the energy converter control  28  of the energy conversion and transfer control  18  by corresponding conductors or lines  154 ,  156  and  158  respectively. 
     The energy transfer device  26  implemented with SCR switches is similar in topology, sensing and control. As shown in  FIG. 8 , the energy transfer device  26  using the SCR switches comprises a plurality of rotor energy transfer control elements or switches generally indicated as  202  and a plurality of stator energy transfer control elements or switches generally indicated as  204  operatively coupled in energy transfer relationship by a bi-directional resonant transfer link generally indicated as  206  and an isolation element or component generally indicated as  208 . The plurality of rotor energy transfer control elements or switches  202  comprises an SCR switch  210  coupled to each phase A, B, C of the rotor  22  of the doubly fed induction machine  20  by a corresponding conductor or line  212  shunted to ground by a corresponding shunt capacitor (not shown). Similarly, the plurality of stator connected energy transfer control elements or switches  204  comprises an SCR switch  216  coupled to each phase a, b, c of the stator windings  24  of the doubly fed induction machine  20  by a corresponding conductor or line  218  shunted to ground by a corresponding shunt capacitor (not shown). The bi-directional resonant transfer link  206  comprises a series resonant inductor  222  and resonant capacitor  224 ; while, the isolation element or component  208  comprises a transformer generally indicated as  226  coupled between the bi-directional resonant transfer link  206  and the plurality of rotor energy transfer control elements or switches  204 . The energy transfer device  26  further includes a first local ground energy transfer control element or switch  228  and a second local ground energy transfer control element or switch  230  coupled between ground and opposite sides of the bi-directional resonant transfer link  206 . A reset control comprising an IGBT switch  231  coupled to the resonant inductor  222  by a secondary winding  233  is used to reset the SCR switches  210  and switch  216  as described more fully hereinafter. 
     As shown in  FIG. 8 , the operation of the SCR switch energy transfer inverter is controlled by the energy transfer control elements or SCR switches  210 ,  216 ,  228  and  230  and the commutating switch  231  are turned on by drivers  232  controlled through lines  234  from controller  28  and commutated off by the reset control IGBT switch  231  controlled by a corresponding driver  132  coupled to the controller  28  of the energy conversion and transfer control  18  by a corresponding driver conductor or line  134 . 
     A plurality of operating parameters or condition sensors used to sense and feed real time current and voltage values or data to the energy converter control  28  of the energy conversion and transfer control  18  for the SCR switch implementation is virtually the same as that shown in  FIG. 7  for the IGBT switches implementation except for the SCR reset switch  231  to reset the SCRs after each energy transfer. 
     As previously mentioned, the electro-mechanical energy conversion system  10  can operate with various prime movers as a generator. Such prime movers require resource energy adjustment means responsive to a controller signal for controlling or limiting the resource energy from the input energy source  12  to the stator  24  of the electro-mechanical energy conversion system  10 . For example, a hydro turbine generally has a hydro inlet and gate means such as a gate for closing the hydro inlet in response to a gate position signal. Similarly, a steam turbine generally has variable position inlet gate valves that open and close to control the amount of steam received by the turbine. Wind turbines typically have adjustable blades with an adjustable pitch angle that is varied to control the force of the wind received by the turbine blades. Solar energy power generation systems generally have adjustable solar panels or mirrors, which may be adjusted to vary the angle of incidence of the solar rays on the panels or mirrors. 
     More particularly, when used with a hydro turbine, the resource energy adjustment comprises a gate means for dosing the hydro inlet of the hydro turbine in response to the turbine controller signal. The turbine controller signal comprises a gate position signal. A turbine efficiency maximizer means receives and processes the head sensor signal and the gate position signal to produce the hydro turbine efficiency output signal. U.S. Pat. No. 5,028,804 discloses such a generator control system. For a wind turbine, a turbine controller produces a wind turbine controller signal that comprises a blade pitch adjustment signal. A wind turbine including adjustable blade with variable pitch angles, the resource energy adjustment means comprising means for adjusting the pitch angle of the blades in response to the blade pitch adjustment signal. A wind turbine efficiency maximizer receives and processes the wind speed sensor signal and the blade pitch adjustment signal to produce a wind turbine efficiency output signal U.S. Pat. No. 6,137,187 shows such a variable speed wind turbine generator control system. 
     As previously stated,  FIG. 3A  depicts the implementation of the electro-mechanical energy conversion system  10  using wind power as the input energy source  12  to generate electrical energy transferred to an output energy load on grid  14 . When operating as a wind powered generator, the input energy source  12  comprises a wind driven propeller  310  coupled to the rotor  22  through a gear assembly or other mechanical coupling mechanism  312  and an output shaft  314 . As described hereinafter, the energy converter control  28  of the electro-mechanical energy conversion system  10  compensates for changing wind speed and direction to supply power to the output energy load or power grid  14  at a substantially constant 60 Hertz output from the stator  24 . This is accomplished by electrically exciting the rotor windings such that the rotor mechanical frequency and rotor electrical excitation frequency are theoretically equal to substantially 60 Hertz. The resultant 60 Hertz energy or power on the rotor  22  is transferred across the air gap of the doubly fed induction machine  20  to the stator  24  to be supplied to the grid  14  at substantially 60 Hertz through a switch  316 . While a three phase grid is shown, the electro-mechanical energy conversion system  10  may be implemented for use with a single phase load. 
     The operation of the energy transfer multiplexer  26  as described hereinafter with either a doubly fed induction machine or a permanent magnetic induction machine is essentially the same. However, as show in  FIG. 3A , when used with a doubly fed induction machine, the energy transfer multiplexer  26  is coupled between the windings of the wound motor  22  and energy converter section or device  20  and the stator  24  of the energy converter section or device  20  and the energy load  14  to transfer energy bi-directionally through the energy transfer multiplexer  26  to compensate for variations in the input energy source  12  to create or generate a virtual rotor frequency of 60 Hertz. On the other hand, as shown in  FIG. 3B , when used with a permanent magnetic induction machine, the energy transfer multiplexer  26 , isolated from the energy source  12 , is coupled between the stator  24  of the energy converter section or device  20  (permanent magnet) and the load  14  to transfer the variable energy supply from the energy source  12  through the rotor  22  and stator  24  of the energy converter section or device  20  to the load. The energy transfer multiplexer  26  receives variable frequency energy signals from the stator  24  and compensates for these varying frequency energy signals to feed a substantially constant frequency of 60 Hertz. In short, in the doubly fed induction machine, the input or output frequency of the rotor windings or the rotor  22  of the energy transfer multiplexer  26  is variable and the output frequency of the stator  24  of the energy converter section or device  20  is substantially constant. In comparison, in the permanent magnet induction machine, the output frequency of the stator  24  of the energy converter section of device  20  fed to the energy transfer multiplexer  26  is variable; while the output for the energy transfer multiplexer  26  fed to the energy load  14  is substantially constant. 
     The energy transfer multiplexer  26 , when used to control a variable speed permanent magnetic generator, has numerous operational and cost advantages. 
     Specifically, a permanent magnetic generator powered by a wind turbine at variable rotational speed outputs electrical energy with a sinusoidal wave form that varies in both frequency and voltage amplitude. Accordingly, for a 3 phase permanent magnetic generator, the energy transfer multiplexer electrical configuration has four input switches, 3 phase switches and an input ground switch, connected through a series resonant circuit to four output phase switches, 3 output switches and an output ground switch. Operation of the input phase switch in conjunction with the output ground switch allows the energy transfer multiplexer to function as a “charge pump” thereby allowing electrical charge to be transferred from a lower voltage to a higher voltage. 
     In contrast, pulse width modulation requires massive, expensive, low frequency DC inductors to obtain significant voltage gain. 
     Another advantage is the ability to actively, selectively and simultaneous control both the input and output power factor. 
     The energy transfer multiplexer selectively controls the four input and four output switches to allow varying size packets of charge to be transferred from the variable time varying input phase voltage to the variable time varying output phases. Accordingly, greater current flow for leading power factor or smaller current flow for lagging power factor can be obtained at a given value voltage of the AC waveforms. 
     In addition, the energy transfer multiplexer  26  is a bi-directional power flow allowing wind turbines to spin-up or start at very low wind speed by transferring power from the 3 phase grid to the permanent magnet generator as a permanent magnet motor. 
     The energy transfer multiplexer  26  is a symmetrical network that selectively processes power flow in either direction. 
     An advantage of electro-mechanical energy conversion system  10  with the energy transfer multiplexer  26  as opposed to pulse width modulation (PWM) power conversion, for wind turbines for both permanent magnet generators and doubly fed wound rotor machines is the large system bandwidth. The energy transfer multiplexer allows direct AC to AC conversion without utilizing an intermediate DC link; the benefits of energy transfer multiplexer resonant link for direct AC to AC conversion without a DC link include:
         System soft-start with current in rush control, when the permanent magnet machine is operating as a generator or as a motor.   Very low windspeed start-up because of the energy transfer multiplexer property of variable voltage gain   The energy transfer multiplexer symmetrical configuration allows the permanent magnet generator to spin-up the windturbine at zero windspeed utilizing the grid power.   Rapid transient response allowing improved system stability; energy transfer multiplexer does not require high current-low frequency chokes that cause time delay in the in the system response.   Rapid, almost instantaneous, shut-down because both the input and output phase switches are opened after each charge transfer at zero current and if not reclosed constitute an automatic shutdown.   Improved system compliance because as the rapid transient response, soft-start and substantially instantaneous shut-down.       

     Finally, the compact design of permanent magnet generators allows relatively higher speed operation. The AC to DC rectification required for the PWM DC link is limited by inductance at high power levels at higher generator frequencies. With no requirement for a DC link, energy transfer multiplexers samples the AC sinusoidal wafeform with discrete small-duration (typically 20 ms-40 ms) time intervals that with optimum phase to ground by pass capacitors allow the generator to, operate with low distortion sinusoidal current and voltage waveforms at near unity power factor. 
     The eight switch symmetrical (4 switch resonant link) configuration includes a maximum of power processing system functionality; high gain, high bandwidth, high frequency, high efficiency, bi-directional power processing with soft-start, rapid shut-down and dual PF control. Further, the energy transfer multiplexer low distortion sinusoidal waveform operation inherently minimizes EMI, physical size and weight because unlike PWM, large high current low frequency DC magnetic filters are not required in energy transfer multiplexer power processors. Lastly, the energy transfer multiplexer symmetrical 8-switch power network, operating by transferring individual packets of electrical charge, represents a digitally controlled generic power processor applicable to all types of rotating electromagnetic machines. 
     In summary, a comparison of pulse width modulation and energy transfer multiplexer configurations and operating parameters shows that the solid state components, semiconductors and diodes, with other electrostatic and resistive components are roughly equivalent. Even the heat sinks (efficiency) and wiring requirements are about the same complexity. The unique advantage of energy transfer multiplexer in wind turbine power processing relates to:
         size—energy transfer multiplexer do not require large expensive robust magnetic filters;   weight—no magnetic filters;   performance
           a) high speed more compact generator,   b) low windspeed power through-put (constant conversion efficiency)   c) broad speed (operational frequency) range with sufficient voltage gain at the lower end of the frequency range   
           soft-start;   rapid shut-down, no stored energy   wide bandwidth, transient control       

     For wind turbines with permanent magnet generator energy transfer multiplexer, the reduction in annual cost of power (a function of annual average wind speed) may be 10% to 40%. 
     For wind turbines with DFIM (large turgines) with energy transfer multiplexer, the initial cost of the power electronics is calculated to be reduced by 20% to 50% relative to pulse width modulation implementation. 
     As described in U.S. Pat. No. 6,137,187, various operating parameters or conditions associated with the input energy source  12  such as wind conditions, blade pitch, blade rotational speed and torque may be supplied to or calculated by the source/load control  30  to control the operation of the mechanical input such as blade pitch through feed back loops depicted generally as  318 . Control signals and sensor signals are fed between energy converter control  28  and source/load control  30  through cable or lines  320  and between energy transfer device  26  and energy converter control  28  through cables or lines  322 . 
     The energy converter control  28  controls the operation of the energy transfer device  26  to maintain the effective frequency of the rotor  22 , mechanical frequency plus or minus winding excitation frequency, at substantially 60 Hertz through the operation of the bi-directional resonant transfer link  106  by selecting the switching states of the rotor energy transfer control elements or IGBT switches  102  or SCR switches  202  and the stator energy transfer control elements or IGBT switches  104  or SCR switches  204  to control the transfer of excitation energy to and from the rotor windings. 
     The switching states of IGBT switches  110 ,  116 ,  128  and  130  or SCR switches  210 ,  216 ,  118  and  230  and IGBT switch  231  of the corresponding energy transfer device  26  are selectively controlled by the converter transfer control logic of the micro-controller or microprocessor in the energy converter control  28  of the energy conversion and transfer control  18  to adjust excitation of the rotor windings of the doubly fed induction machine  20  through three phase slip rings generally indicated as  324  to compensate for changes or variations in the mechanical input conditions such as frequency and power level. 
     The various system currents and voltages previously described are sensed and fed to the energy converter control  28 . At the same time, the mechanical rotor speed or rotational rate is measured. If the mechanical rotor speed or rotational rate is substantially 60 Hertz, power or excitation energy is neither added to nor subtracted from the rotor windings. However, if the mechanical rotor speed or rotation rate is greater than or less than substantially 60 Hertz, power or excitation energy is subtracted from or added to the rotor windings. 
     As shown in  FIG. 2A , when the mechanical rotor speed or rotation rate of the rotor  22  is greater than substantially 60 Hertz, the doubly fed induction machine  20  operates as a current sink drawing power from the rotor windings to compensate for the mechanical rotation over-speed of the rotor  22  to generate a magnetic stator (output) frequency of substantially 60 Hertz; the mechanical rotor speed (frequency) less rotor winding excitation frequency at the correct corresponding voltage, amplitude form a straight line curve shown on the right side of FIG.  2 A. Conversely, when the mechanical rotor speed or rotational rate of the rotor  22  is less than substantially 60 Hertz, the doubly fed induction machine  20  requires as a current source feeding power into the rotor winding to compensate for the mechanical rotational under-speed of the rotor  22  to create a effective rotor speed (frequency) of substantially 60 Hertz; the mechanical rotor speed (frequency) plus rotor winding excitation magnetic frequency, at the corresponding voltage amplitude, also form the straight line phase curve shown on the left of FIG.  2 A. 
     The micro-controller or microprocessor of the energy converter control  28  generates reference curves corresponding to the compensating rotor pulse repetition frequency and corresponding power amplitude of the power transferred between the rotor  22  and stator  24  to maintain the effective rotational rate of the rotor  22  at substantially 60 Hertz. The electro-mechanical energy conversion system power output is shown in  FIGS. 2B and 2C . 
       FIG. 11  shows the various possible switching configurations of the rotor switches  102  or  202  and the stator switches  104  or  204 . Specifically, any one of the three phase rotor switches  110  or  210  or the first ground switch  128  or  228  can be closed or actuated at the same time with any one of the stator switches  116  or  216  or the second ground energy transfer control element or switch  130  or  230  to control the transfer energy between the rotor  22  and the stator  24  as represented in FIG.  12 . 
     As stated, the microprocessor or micro-controller of the electro-mechanical energy conversion system  10  generates a reference curve or sine wave for each phase of the doubly fed induction machine  20  as shown in  FIG. 14  in accordance with the substantially linear relationship between the mechanical rotor speed or frequency and voltage or amplitude of the energy converter device  16  whether operating as a current source, 40 Hertz to 60 Hertz, or a current sink, 60 Hertz to 80 Hertz as shown in FIG.  2 A. The various values of the stator and rotor currents and voltages are sensed and fed to the micro-controller. The capacitor voltage are also sensed and fed to the microprocessor. These operating parameters or conditions are compared with reference appropriate curve dictated by the mechanical rotor speed and grid power demands to generate control signals to control drivers to actuate or enable switches  102  and  104  or  202  and  204 . In addition, the SCRs are self commutative by the reset control IGBT switch  231 . 
     The energy management system of the present invention comprises the energy transfer multiplexer  2  coupled to the energy source  12  to receive energy therefrom and to the energy load  14  to feed energy thereto and a system control coupled to the energy transfer multiplexer  2  to control the flow power to the energy load  14 . As previously described, the energy transfer multiplexer  2  power comprises the first plurality of switches or control points  4  coupled to the energy source  12  to receive energy therefrom and a second plurality of switches or control points  6  coupled to the energy load  14  to feed energy thereto coupled by the resonant link  8  to transfer unrectified A/C signals therebetween and the system control comprising the plurality of sensors to monitor operating conditions of the signal processing to control the operation of the energy transfer multiplexer in response to the operating conditions wherein the plurality of sensors coupled between the logic section and the first plurality of switches or control points, the second plurality of switches or control points and the resonant link to sense the voltage levels of each of the first plurality of switches or control points and each of the second plurality of switches or control points and the voltage level across the capacitor and to generate voltage level signals corresponding to each voltage level and to feed the voltage level signals corresponding to each voltage level and to feed the voltage level signals to the logic section for processing and generate control signals fed to the switches or control points or sites as shown in FIG.  13 . The entire signal processing and signal generation is time dependent. 
     The energy management system or signal processing section comprises power/phase management section, a polarity management section, a voltage management section and a switch management section to receive operating voltage signals, compare the operating voltage signals with predetermined voltage references and generate control signals when the operating voltage signals exceed the predetermined voltage reference to control the transfer of energy through the energy transfer multiplexer  26 . 
     Specifically, the voltage for each switch  110  and  116  or  210  and  216  is sampled or interrogated to determine whether or not potential for phase A, B, C on the rotor  22  and for phase a, b, c on the stator  24  are within a predetermined range or band on either side of the appropriate voltage reference curve exemplified in FIG.  14 . The actual voltages measured as the various phases are compared in the power/phase management section to determine if the corresponding phase voltage is within the predetermined reference-band. If-so, no-power is transferred into or out of the rotor  22  for the time increment and phase sampled. 
     The operation of the energy transfer multiplexer  26  as depicted in  FIGS. 4 and 8 , is best understood with reference to FIG.  13 . In particular, if energy transfer is required, the polarity of charge across the resonant capacitor  124 ,  224  is sensed by polarity management section and corrected or reversed if necessary. To correct the polarity of the charge on the resonant capacitor  124 ,  224 , if necessary, both sides of the resonant link  106 / 206  are connected or coupled simultaneously to local ground by the first ground switch  128 / 228  and second ground energy transfer control element or switch  130 / 230  for one-half cycle of the resonant frequency. With the correct polarity for the output phase connection request, the resonant capacitor  124 ,  224  is connected between the selected input switch  110 ,  210  phase A,B,C, or ground switch  128 ,  228  and the selected output switch  116 ,  216  on phase a,b,c. 
     The voltage management section calculates and compares the final change V CF  on the resonant capacitor  124 / 224  with a first predetermined voltage value such as three times the capacitor break down voltage  3  E MAX  if the final charge V CF  is equal to or greater than the first predetermined voltage, then the resonant link  106 / 206  is connected to ground through ground switch  128 / 228  and to the selected phase switch  116 / 216  (indicated on  FIG. 13  as G I -E O ) to discharge the stored energy on resonant capacitors  124 / 224  to provide a safety margin to prevent the voltage across the resonant capacitor  124 / 224  from exceeding the breakdown voltage. If the final charge V CF  is less than the first predetermined, the initial charge V cs  on the resonant capacitor  124 / 224  is compared to a second predetermined voltage value such as 1.5 times the output voltage E O . If the initial charge V CS  is equal to or greater than the second predetermined voltage, then the resonant link  106 / 206  is connected to ground though ground switch  128 / 228  and the selected output phase switch  116 / 216  ( FIG. 13  as G I -E O ). If the initial charge V CS  is less than the second predetermined voltage, the sum of the selected input voltage E I  and the initial charge V CS  is compared to the output voltage E O . If the sum of the input voltage E I  and initial charge V CS  is equal to or less than the output voltage E O , then the resonant link  116 / 216  is connected between selected input switch  110 / 210  and ground switch  130 / 230  to increase the entire charge V CS . If the sum of the input voltage E I  and initial charge V CS  is greater than the output voltage E O , then the resonant link  116 / 216  is connected between E I  and E O  to complete the energy transfer between the energy source  12  and the energy load  14 . 
     The switch management section generates output for resonance wait or delay time. 
     In other words, with the correct polarity across the resonant capacitor  124 / 224 , when the V CF  is less than a predetermined multiple of E MAX  and V CS  is less than a predetermined multiple of E O  and the sum of E I  and V C  is greater than E O , the poled input phase E I  supplies power or energy to the poled output phase E O  by closing the corresponding switches; the resonance wait or delay time is to allow time for the resonant transfer before re-triggering the system. 
     On the other hand, with the correct polarity across the resonant capacitor  124 / 224 , when the V CF  is less than a predetermined multiple of E MAX  and V CS  is less than a predetermined multiple of E O  and the sum of E I  and V c  is less than E O  the poled input phase E I  is connected to G O  to increase the charge on the resonant capacitor  124 / 224 ; this sequence may be repeated as indicated in  FIGS. 15 and 16B . 
     With the correct polarity across the resonant capacitor  124 ,  224 , when the V CS  is greater than a predetermined multiple of E MAX  or the V CF  is greater than a predetermined multiple of E O , the poled output phase E O  is connected to G I  to discharge. 
     It will thus be seen that the objects set forth above, among those made apparent from the preceding description are efficiently attained and since certain changes may be made in the above construction without departing from the scope of the invention, it is intended that all matter contained in the above description or shown in the accompanying drawing shall be interpreted as illustrative and not in a limiting sense. 
     It is also to be understood that the following claims are intended to cover all of the generic and specific features of the invention herein described, and all statements of the scope of the invention that, as a matter of language, might be said to fall therebetween.