Method, apparatus and article for bi-directional DC/DC power conversion

Information

  • Patent Grant
  • 7362557
  • Patent Number
    7,362,557
  • Date Filed
    Wednesday, March 30, 2005
    19 years ago
  • Date Issued
    Tuesday, April 22, 2008
    16 years ago
Abstract
A controller implements a state machine for operating the bi-directional power converter with a flexible load pattern while maintaining a thermal condition of the power converter within acceptable limits. The state machine implements a wait loop in response to selected conditions to maintain the thermal condition.
Description
BACKGROUND OF THE INVENTION

1. Field of the Invention


This disclosure is generally related to power conversion, and particularly to bi-directional power conversion via a DC/DC switch mode power converter.


2. Description of the Related Art


A variety of applications employ DC/DC power conversion to, for example, step-up and/or step-down voltage. For example, electric drive or hybrid automotive applications may at times provide power from a high voltage DC source, such as one or more fuel cells, to supply low voltage DC loads and/or to recharge one or more batteries and/or ultracapacitors. During other times, a low voltage power source, such as one or more of the batteries and/or ultracapacitors, may provide power to a high voltage DC load, such as an electric traction motor coupled to drive one or more wheels via a drivetrain.


Switch mode converters typically offer higher efficiency than linear regulators, and can step-up or step-down the input voltage. In some embodiments, switch mode converters can even invert the input voltage. A variety of switch mode DC/DC converter topologies and operation of the same are known to those of skill in the art. For example, buck converters for stepping down the input voltage, boost converters for stepping up the input voltage, as well as buck-boost converters and flyback converters for alternatively stepping down and stepping up the input voltage.


DC/DC switch mode converter operation is typically limited by thermal constraints, such as the ability to dissipate heat generated by the conversion process. This may be disadvantageous, particularly where some flexibility is desired in the load pattern during boost mode operation of the DC/DC converter. It would thus be desirable to increase the flexibility of operation of the DC/DC converter, while avoiding thermal damage to the DC/DC converter from excessive accumulation of heat.


BRIEF SUMMARY OF THE INVENTION

A controller implements a state machine for operating the bi-directional power converter with a flexible load pattern while maintaining a thermal condition of the power converter within acceptable limits. The state machine implements a wait loop in response to selected conditions to maintain the thermal condition.


In one embodiment, a method of operating a bi-directional power converter, the method comprises: monitoring command and condition signals; and selectively supplying control signals to cause the bi-directional power converter to cycle between a plurality of operational modes based on the monitored command and condition signals, the plurality of operational modes comprising: a ready mode; a buck mode; a boost mode; a fault mode; and a first wait mode.


In one embodiment, selectively supplying control signals comprises supplying control signals to cause the bi-directional power converter to cycle from the boost mode to the first wait mode based in part on the condition signals. In one embodiment selectively supplying control signals comprises determining whether a thermal condition has been reached based in part on the condition signals. In one embodiment, the condition signals comprise an input current.


In one embodiment, selectively supplying control signals comprises supplying control signals to cause the bi-directional power converter to cycle from the boost mode to the first wait mode when an integrated value of an input current exceeds a threshold input current by a defined value.


In one embodiment, the plurality of operational modes further comprises a second wait mode. In one embodiment, selectively supplying control signals comprises supplying control signals to cause the bi-directional power converter to operate in the first wait mode for a first defined period of time and selectively supplying control signals to cause the bi-directional power converter to operate in the second wait mode for a second defined period of time.


In one embodiment, selectively supplying control signals comprises supplying control signals to cause the bi-directional power converter to operate in the fault mode in response to detection of a fault condition. In one embodiment the method further comprises applying a hardware-based over-protection limit to the operation of the bi-directional power converter. In one embodiment the method further comprises applying a software-based over-protection limit to the operation of the bi-directional power converter.


In one embodiment, a system for controlling a power converter, comprises: a fault detection monitor configured to generate a fault signal in response to a fault condition; a state machine configured to transition between a plurality of states comprising a ready state, a boost state, a buck state, a fault state, a first wait state, and a second wait state, wherein the state machine is configured to transition from the boost state to the first wait state in response to an indication of a thermal condition; and a control signal generator configured to generate control signals for controlling the power converter based on a current state of the state machine.


In one embodiment, the state machine is configured to transition between states in the plurality of states based on a received command and the fault signal. In one embodiment, the indication of a thermal condition is a function of a current level. In one embodiment, the indication of a thermal condition is a function of a current level and time. In one embodiment the indication of a thermal condition is an integrated value of an input current in excess of a threshold input current.


In one embodiment, a system for controller a power converter comprises: means for detecting fault conditions; means for transitioning between a plurality of states comprising a boost state, a first wait state and a second wait state; and means for generating control signals coupled to the means for detecting fault conditions and the means for transitioning between a plurality of states.


In one embodiment, the means for transitioning between a plurality of states comprises a state machine implemented in a computer-readable media. In one embodiment, the plurality of states comprises a buck state and a fault state. In one embodiment, the means for transitioning is configured to transition from the boost state to the first wait state in response to an indication of a thermal condition. In one embodiment, the indication of a thermal condition is a function of an input current.


In one embodiment, a computer-readable memory medium stores instructions for causing a control system to control a power converter by: monitoring command and condition signals; and selectively supplying control signals to cause the power converter to cycle between a plurality of operational modes based on the monitored command and condition signals, the plurality of operational modes comprising: a ready mode; a buck mode; a boost mode; a fault mode; and a first wait mode. In one embodiment, the plurality of operational modes further comprise a second wait mode. In one embodiment, the stored instructions further comprise instructions for causing the control system to control the power converter by: selectively generating control signals to cause the power converter to cycle from the boost mode to the first wait mode; and selectively generating control signals to cause the power converter to cycle from the boost mode to the second wait mode.


In one embodiment, the stored instructions further comprise instructions for causing the control system to control the power converter by: selectively supplying control signals to cause the power converter to cycle from the boost mode to the first wait mode in response to an indication of a thermal condition. In one embodiment, the indication of a thermal condition is a function of an input current.





DEFINITIONS AND BRIEF DESCRIPTION OF THE DRAWINGS

In the drawings, identical reference numbers identify similar elements or acts. The sizes and relative positions of elements in the drawings are not necessarily drawn to scale. For example, the shapes of various elements and angles are not drawn to scale, and some of these elements are arbitrarily enlarged and positioned to improve drawing legibility. Further, the particular shapes of the elements as drawn, are not intended to convey any information regarding the actual shape of the particular elements, and have been solely selected for ease of recognition in the drawings.



FIG. 1 is a schematic diagram of a power system comprising a high voltage power source such as a fuel cell system, a low voltage load and/or power source such as a battery and/or ultracapacitor, a bi-directional power converter operable to transfer power between a high voltage bus and a low voltage bus, and an optional high voltage load such as a traction motor, the power system suitable for a variety of applications, for example, suitable for use in an electric or hybrid vehicle, according to one illustrated embodiment.



FIG. 2 is a top plan view of a low voltage connector suitable for making electrical coupling between the power converter and the low voltage loads and/or low voltage power sources.



FIG. 3 is a graph illustrating a voltage/current characteristic of a power converter operating in a boost mode according to one illustrated embodiment.



FIG. 4 is a graph illustrating a voltage/current characteristic of a power converter operating in a buck mode according to one illustrated embodiment.



FIG. 5 is a graph illustrating an output current versus coolant temperature characteristic of a power converter according to one illustrated embodiment.



FIG. 6 is a schematic diagram of a state machine, illustrating a method of operating the power converter of FIG. 1 according to one illustrated embodiment.



FIG. 7 is schematic diagram of a load pattern for the power converter operating in boost mode according to one illustrated embodiment.



FIG. 8 is a schematic diagram of an estimated ON time curve for operation of the power converter while maintaining a thermal condition of the power converter within acceptable limits.



FIG. 9 is schematic diagram of a load pattern for the power converter operating in boost mode according to another illustrated embodiment, showing the flexibility in operation of the power converter while maintaining a thermal condition of the power converter within acceptable limits.



FIG. 10 is a functional block diagram of a system for controlling a power converter according to one embodiment.





DETAILED DESCRIPTION OF THE INVENTION

In the following description, certain specific details are set forth in order to provide a thorough understanding of various embodiments. However, one skilled in the art will understand that other embodiments may be practiced without these details. In other instances, well-known structures associated with power converters, switched mode power converters, controllers, fuel cell systems, uninterruptible power supplies, batteries and/or ultracapacitors have not been shown or described in detail to avoid unnecessarily obscuring descriptions of the embodiments.


Unless the context requires otherwise, throughout the specification and claims which follow, the word “comprise” and variations thereof, such as, “comprises” and “comprising” are to be construed in an open, inclusive sense, that is as “including, but not limited to.”


Reference throughout this specification to “one embodiment” or “an embodiment” means that a particular feature, structure or characteristic described in connection with the embodiment is included in at least one embodiment. Thus, the appearances of the phrases “in one embodiment” or “in an embodiment” in various places throughout this specification are not necessarily all referring to the same embodiment. Further more, the particular features, structures, or characteristics may be combined in any suitable manner in one or more embodiments.


The headings provided herein are for convenience only and do not interpret the scope or meaning of the claimed invention.



FIG. 1 shows a power system 10 suitable for a variety of applications, for example, for use in an electric or hybrid vehicle, or as an auxiliary power supply such as an uninterruptible power supply (UPS). The power system 10 comprises one or more high voltage DC power sources 12, one or more low voltage DC loads 14, a DC/DC switch mode power converter 16 coupled and operable to transfer DC power between the DC power source 12 and DC loads 14 via a high voltage DC bus (e.g., 200-450V HV-BUS) 18 and a low voltage DC bus (12V LV-Bus) 20. The power system also comprises a controller 22 coupled to control the power converter 16. The power system 10 may further comprise one or more high voltage loads 24.


While FIG. 1 identifies suitable voltages for an automotive application, such voltages are merely exemplary and the power system 10 may employ other voltages and other relative voltage levels for automotive as well as other applications. Thus, as used herein and in the claims, the terms high voltage and low voltage are not intended to denominate any specific voltage or voltage range, but rather are used in a relative sense with respect to one another.


In particular, the high voltage power source 12 may take a variety of forms, for example, a fuel cell stack comprising a plurality of fuel cells, such as proton exchange membrane (PEM) fuel cells. The connection between the high voltage power source 12 and the power converter 16 may take place within a protective housing of the power converter 16.


The low voltage load 14 may take a variety of forms, for example, one or more low voltage devices such as monitoring or control systems for the power system 10 or a device associated with the power system 10, for example an electric or hybrid vehicle. The low voltage load 14 may additionally, or alternatively comprise one or more power storage devices, such as one or more batteries and/or one or more ultracapacitors, which act as low voltage loads while being recharged, and act as low voltage power sources when being discharged.


The high voltage load 24 may take a variety of forms such as a high voltage traction drive motor, and/or one or more high voltage auxiliary drive motors such as a compressor, fan and/or pump associated with the power system 10 and/or a device associated with the power system 10 such as an electric or hybrid vehicle.


The power converter 16 may provide galvanic isolation between the high and low voltage buses 18, 20, respectively, for example via a transformer (not shown). The power converter 16 is operable to adjust voltage output in response to pulse width modulated (PWM) input signals. Thermal cooling may be provided by a glycol electronics cooling loop, for example, with a flow rate of approximately 8 liters/minute. The power converter 16 may also include suitable automatic over load and/or over temperature features for reducing or shedding load and/or heat.


The controller 22 may take a variety of forms such as a programmed or programmable microprocessor, digital signal processor (DSP), application specific integrated circuit (ASIC), and/or discrete circuit. The controller 22 provides control signals to one or more switches in the power converter 16. The controller 22 may receive input signals from one or more sensors and/or devices. For example, the controller 22 may receive high voltage side voltage and/or current measurements from voltage sensor 26a and/or current sensor 26b. Additionally, or alternatively, the controller 22 may receive low voltage side voltage and/or current measurements from voltage sensor 28a and/or current sensor 28b. Additionally or alternatively, the controller 22 may receive signals from actuators or sensors associated with other components of the power system 10, such as pedals, motors, compressors, fans, etcetera.



FIG. 2 shows a 2-pole chassis isolated low voltage connector 30 suitable for connecting the low voltage DC bus 20 to the power converter 16. In particular, the portion of the low voltage load 14 acting as a power source, such as batteries and/or ultracapacitors, may be coupled to a vehicle circuit via a 2-pole connection.


With continuing reference to FIG. 1, the controller 22 can provide control signals to the power converter 16 to operate the power converter 16 in a variety of modes, including a boost mode and a buck mode. In the boost mode, the power converter 16 transfers energy from the low voltage bus 20 (e.g., from the 12V battery) to the high voltage bus 18, for example, to provide power during the start-up process of the high voltage power source 12 (e.g., the fuel cell system). In buck mode, the power converter 16 transfers energy from the high voltage bus 18 to the low voltage bus 20, for example, for continuous operation of all low voltage loads carried by the low voltage bus 20 such as low voltage DC loads of an electric or hybrid vehicle and/or recharging of the 12V battery.


The power system 10 may provide the signals to the controller 22 via a signal interface as set out in Table A, below.











TABLE A






digital (d)/




analog (a)/
input (i)/


Signal
PWM
Output (o)







Enable
d
i


Buck/boost mode
d
i


Rated output voltage command
d
i


Faults
d
o


Power reduction because of over temperature
d
o


Cooling request
d
o


Actual 12 V LV-BUS current
d
o


Actual 12 V LV-BUS voltage
d
o


Actual HV-BUS current
d
o


12 V supply
a
i-Supply


Signal ground
a
i-Supply









Suitable input characteristics for an example power converter 16 operating in boost mode are set out in Table B, below.










TABLE B





Characteristics
Values







Input voltage/
7.0-8.5 V: linearly increase maximum output


Output power:
power from 0 kW to 2.3 kW



8.5-10.5 V: linearly increase maximum output



power from 2.3 kW to 3.0 kW



>10.5 V: maximum output power 3.0 kW


Control voltage:
DC/DC control shall be maintained down to 7.0 V


Maximum input
(16 V for operation and 24 V/1 minute survive


voltage:
without operation).









Suitable output characteristics for an example power converter 16 operating in boost mode are set out in Table C, below.










TABLE C





Characteristics
Values







Output voltage during
From 0 V to maximum stabilized output


start-up:
voltage in ≦0.6 seconds under start-up load



condition


Start-up load condition:
C = 13 mF, R = 1.7 kΩ (total HV bus



discharge resistance)









Stabilized output voltage
Input Voltage
Output Voltage


range:
8.5 V-11 V
From 250 V ± 2%




to 424.8 V ± 2%,




derated by the power



 11 V-13 V
250 V ± 2%-424.8 V ± 2%



 13 V-16 V
300 V ± 2%-424.8 V ± 2%








Overvoltage protection:
426.8 V ± 2% (Overvoltage protection is



2 V over max. stabilized output voltage)


Redundant overvoltage
440.6 V ± 1%


protection:


Max. voltage overshot at
 5 V


load dump:


Maximum output voltage:
450 V


Maximum output power:
 3 kW


Load Pattern
See FIGS. 7-9










FIG. 3 shows a line 32 illustrating a boost mode regulated voltage/current characteristic of the power converter 16 operating at 3 kW according to one illustrated embodiment.


Suitable input characteristics for an example power converter 16 operating in buck mode are set out in Table D, below.












TABLE D







Characteristics
Values









Input voltage/
200-230 V: Approximately linearly



Output current:
increase max output current from




120 A at 200 V to 150 A at 230 V.




230-440 V: maximum output




current 150 A



Transients and spikes:
The DC/DC delivers stabilized output




voltage and current characteristics




during the FCS flow switch condition,




thus a voltage drop will occur.










Suitable output characteristics for an example power converter 16 operating in buck mode are set out in Table E, below.










TABLE E





Characteristics
Values







Stabilized output voltage
13.3 V ± 2% to 14.4 V ± 2% with input


range:
voltage >250 V.


Reduced stabilized
Approximately linearly increase output


output voltage:
voltage from 11 to 13.3 V as input



voltage increases 200-250 V.


Maximum output current:
(At high load the DC/DC should hold



the max. current of 150 A down to 8.5 V,



then approximately linear reduction from



150 A at 8.5 V to 0 A at 7 V)


Maximum output power:
2 kW


Load pattern:
Continuously


High Temperature Buck
With coolant inlet temperature above 72° C.,


Mode Operation:
output current should be derated



approximately linearly (see FIG. 5).










FIG. 4 shows a line 34 of a voltage/current characteristic for the power converter 16 operating in buck mode according to one illustrated embodiment.



FIG. 5 shows a line 36 illustrating an output current versus coolant temperature characteristic of the power converter 16 according to one illustrated embodiment.



FIG. 6 shows a state machine 40 implemented by the controller 22 (FIG. 1) in controlling the power converter 16.


The state machine 40 comprises a number of distinct states including: a ready state 42a, buck state 42b, boost state 42c, faulted state 42d, short wait state (e.g., wait 5 seconds) 42e, long wait state (e.g., wait 60 seconds) 42f, the order of the states being denominated in the circles representing the states as 0-5, respectively. The state machine 40 comprises a number of transitions defined between the states, the transitions illustrated by arrows 44a-44u, the order of the transitions being denominated between the head and tail of the arrows as 1-21, respectively. The transition order implies precedence. Thus, for example, if the state is Boost 42c, the condition for the transition 44m to the state Wait 60 seconds 42f is checked first, and if the condition is TRUE the state transition is made without checking any other conditions.


Outputs are persistent, thus if no action is taken to change any of the outputs during a given execution of the state machine 40, the last values for all of the outputs will be used. If none of the conditions for state transition are met, the state does not change, and no actions are taken. Only one state transition occurs per execution of the state machine 40. An appropriate fault bit is set if, and when, a fault occurs. A hardware, software or EPO fault detected by the power converter 16 or an integrated power train is identified as a DC_DC_FAULT.


Table F shows a number of suitable values for a pair of operating parameters for an example power converter 16, that may be calibrated.












TABLE F





Calibratable

Nominal



Parameter Name
Description (Units)
value
Range







DC_HVOV
Threshold HV
440.6
RANGE_V



voltage above



which the DC/DC



converter is



disabled


DC_MIN_OFF_TIME
Minimum time that
2 seconds



the DC/DC



converter is



disabled before



re-enabling.



(Seconds)









The operation of the state machine 40 is set out in Table G, immediately below.













TABLE G






Starting
Ending




Transition #
State
State
Conditions to Transit
Actions at the Transition



















1
READY
READY
TIMER_MODE <
If TIMER_MODE <= DC_MIN_OFF_TIME





DC_MIN_OFF_TIME
Then





or DC/DC Disabled commanded
Increment TIMER_MODE






End


2
READY
FAULTED
Hardware or software fault
Set Disable DC/DC






Set CAN bit or bytes associated to the fault


3
READY
BUCK
DC/DC Enabled commanded
Set DC_DC_MODE to Buck





and Buck Mode selected
Enable DC/DC






Set TIMER_MODE = 0






Set CAN bit DCLV buck on = 1


4
READY
BOOST
DC/DC Enabled Commanded
Set DC_DC_MODE to Boost





and Boost Mode selected
Enable DC/DC






If TIMER_WAIT>=60






Then






Set DCLV 3 times enabled = 0






End






If TIMER_WAIT >= 5






Then






Set CAN Bit DCLV break = 0






Set CAN Bit DCLV 90% I2t = 0






Set I 2t= 0






End






Set TIMER_MODE = 0






Set CAN bit DCLV Boost on = 1


5
FAULTED
READY
Auto-resume fault cleared
Clear CAN bit or bytes associated to the fault





or DC/DC Disabled commanded


6
BUCK
FAULTED
Hardware or software fault
Disable DC/DC






Set CAN bit or bytes associated to the fault






Set CAN bit DCLV buck on = 0


7
BUCK
READY
DC/DC Disabled commanded
Set Disable DC/DC





or Boost Mode selected
Set TIMER_MODE = 0






Set CAN bit DCLV buck on = 0


8
BUCK
BUCK

Detect Hardware fault






or power reduction


9
BOOST
FAULTED
Hardware or software fault
Disable DC/DC






Set CAN bit DCLV Boost on = 0






Set CAN bit or bytes associated to the fault


10
BOOST
READY
DC/DC Disabled commanded
Disable DC/DC





or Buck Mode selected
Set TIMER_MODE = 0






Set CAN bit DCLV Boost on = 0


11
BOOST
BOOST
(I2t < 2,450,000 A2sec
If LV I > 150 A





and igbt_temp <=0)
Then





or
Increment I2t by ∫idt





(I2t < 612,500 A2sec
 If (I2t > 2,450,000 A2sec * 90% and





and igbt_temp > 0)
 igbt_temp <=0) or (I2t > 612,500 A2sec






 * 90% and igbt_temp > 0)






 Then






 Set DCLV 90% I2t






 End






End






Detect Hardware fault






or power reduction


12
BOOST
WAIT 5S
COUNT < 3
Disable DC/DC






Increment COUNT






Set TIMER_WAIT = 0






Set CAN bit DCLV break = 1






Set CAN bit DCLV Boost on = 0


13
BOOST
WAIT 60S
COUNT >= 3
Disable DC/DC






Set COUNT = 0






Set TIMER_WAIT = 0






Set CAN bit DCLV 3 times enabled = 1






Set CAN bit DCLV Boost on = 0


14
WAIT 5S
WAIT 5S
TIMER_WAIT < 5 seconds
Increment TIMER_WAIT


15
WAIT 5S
FAULTED
Hardware or software fault
Disable DC/DC






Set CAN bit or bytes associated to the fault


16
WAIT 5S
READY
DC/DC Disabled commanded





or Buck Mode selected


17
WAIT 5S
BOOST
TIMER_WAIT >= 5 seconds
Enable DC/DC






Set I2t= 0






Set TIMER_WAIT = 0






Set CAN Bit DCLV 90% I2t = 0






Set CAN Bit DCLV break = 0






Set CAN bit DCLV Boost on = 1


18
WAIT 60S
WAIT 60S
TIMER_WAIT < 60 seconds
Increment TIMER_WAIT


19
WAIT 60S
FAULTED
Hardware or software fault
Disable DC/DC






Set CAN bit or bytes associated to the fault


20
WAIT 60S
READY
DC/DC Disabled commanded





or Buck Mode selected


21
WAIT 60S
BOOST
TIMER_WAIT >= 60 seconds
Enable DC/DC






Set I2t= 0






Set TIMER_WAIT = 0






Set TIMER_HW = 0






Set CAN bit DCLV 90% I2t = 0






Set CAN bit DCLV 3 times enabled = 0






Set CAN bit DCLV Boost on = 1









When operating In boost mode, some exemplary efficiencies for the power converter 16 are: 1) greater than 80% from 30% Pmax to Pmax (8.5V<ULV<11V); and 2) greater than 85% from 30% Pmax to Pmax (ULV equal to or greater than 11V). When operating in buck mode some exemplary efficiencies for the power converter 16 are: 1) greater than 85% from 30% Pmax to Pmax (UHV equal to or greater than 350V); and 2) greater than 88% from 30% Pmax to Pmax (250V<UHV<350V).


In some embodiments, the output voltage may vary by approximately 2% from the rated voltage in both boost and buck modes. An AC overlay in the load circuit may be lower than 3% TRMS against the average value.


Table H shows a number of example fault conditions, with corresponding variable names, data types, error types, reset values, and comments.













TABLE H







Error




Variables
Datatype
Type
Reset/Clear Conditions
Comments







DCLV
bit
C3/C4
The general error is reset if all
The general error is set if one of the following


general error


errors are cleared
errors occurs:






DCLV CAN Error, DCLV HV bus over current,






DCLV HV bus over voltage buck, DCLV LV bus






over current buck, DCLV LV bus under voltage,






DCLV LV bus over voltage, DCLV LV over current






boost, DCLV over temperature, DCLV LV






Measurement Error, DCLV InterlockSignal Error,






DCLV HV bus undervoltage and DCLV HW error.






It is also set, if an error occurs which is not






displayed. It could be the case in boost mode for:






DCLV HVOV_BST






(HV V < HV cmd - 30 V) or (HV V <220 V) for






more than 1 s






When the VSC enables the boost mode but HV






V - 10 V > HV cmd






if boost mode is enabled and the corresponding






Siadis bit is not set


DCLV CAN
bit
C3
Set conditions:
The error is active at “CAN timeout” and


Error


According CAN class C
“CAN bus off”.





Specification, chapter “monitoring





of incoming messages” and





“Behavior - Bus off”





Reset conditions:





The DC/DC is re-enabled as soon





as a fault condition is cleared


DCLV HV bus
bit
C4
Disable and re-enable the DC/DC
The absolute value of HV current was more than


over current


and the absolute value of HV
15 A in boost mode, 10 A in buck mode





current should be less than the





specified limit


DCLV HV bus
bit
C3
The HV voltage should be less
The HV voltage was more than 445 V ±2% (HW


over voltage


than the set condition minus 3 V
limit) or 440 V ±1% (SW limit)


buck


DCLV LV bus
bit
C4
Disable and re-enable the DC/DC
The LV current was more than 170 A.


over current


and the LV current should be less


buck


than the specified limit


DCLV LV bus
bit
C4
Disable and re-enable the DC/DC
The LV voltage was less than 6.3 V


under voltage


and the LV voltage should be





more than the specified limit


DCLV LV bus
bit
C3
The LV voltage should be less
The LV voltage was more than 16 V


over voltage


than 15.3 V


DCLV LV
bit
C4
Disable and re-enable the DC/DC
The LV current was more than 370 A


over current


and the LV current should be less


boost


than the specified limit


DCLV over
bit
C4
Disable and re-enable the DC/DC
The coldplate temperature was more than 85 deg C.


temperature


and temperature has to be less





than 83 deg C.


DCLV
bit
C1
The temperature should be less
The coldplate temperature was more than 75 deg C.


temperature


than 74 deg C.


reduction


active


DCLV buck
bit
n/a
Set to 0 if the DC/DC state is
Set to 1 if the DC/DC state is “Buck”


on


different from set condition


DCLV boost
bit
n/a
Set to 0 if the DC/DC state is
Set to 1 if the DC/DC state is “Boost” or “Wait 5 s”


on


different from set condition
or “Wait 60 s”


DCLV
bit
C2
The HV has to be more than 235 V
The DC/DC is enabled and the HV voltage is less


reduction



230 V. The DC/DC can not provide the maximum


buck



output power if required


DCLV
bit
C2
The LV has to be more than 9 V
The DC/DC is enabled and the LV voltage is less


reduction



8.5 V. The DC/DC can not provide the maximum


power boost



output power if required


DCLV LV
bit
C3
The difference between the LV
active, if a difference >2 V between IPT LV


Measurement


voltage has to be less than 1.5 V
measuring and DC/DC LV measuring for t > 1 sec


Error



occurs (auto resume) Hysteresis: active >2 V,






inactive <1.5 V


DCLV
bit
C4
Disable and re-enable the DC/DC
The interlock signal is the same than in the


InterlockSignal


and the interlock signal has to be
message 278(h)


Error


detected


DCLV 90%
bit
n/a
After 5 sec break (respective
Shows that 90% of the actual I2t value is reached


I2t


60 sec), if the DC/DC is not





enabled once more at break


DCLV break
bit
n/a
After 5 sec break (respective
Shows that the DC/DC reached the actual I2t value





60 sec), if the DC/DC is not
and is in a 5 sec break (if 3 times enabled in a





enabled once more at break
60 sec break instead of 5 sec)


DCLV 3 times
bit
n/a
After 60 sec break, if the DC/DC is
Shows that the DC/DC is enabled 3 times


enabled


not enabled once more at break


DCLV > 0° C.
bit
n/a
The IGBT temperature is less than
The IGBT temperature is more than 1 deg C. and





0 deg C. and because of that the I2t
because of that the I2t value is 612,500 A2sec





value is 2,450,000 A2sec


DCLV HV bus
bit
C3
The bit is cleared if (HV voltage >203 V)
The bit is set if (HV voltage <200 V) AND (Buck On


undervoltage


OR (CAN Bit ECU_DcLvEn = 0)
or Boost On) AND (timer >2 sec)


DCLV HW
bit
C3
The bit is cleared if (Buck AND
The bit is set if [ (ECU_DcLvMode=0 AND (LV V


error


(LV V measured > LV V cmd -
measured < LV V cmd - 1 V threshold) AND





0.7 V threshold) OR HV V <200 V)
HV i < 0.1 A AND HV V >203 V) OR





or (Boost AND (HV V measured > HV V
(ECU_DcLvMode=1 AND (HV V





cmd - 20 V threshold)
measured < HV V cmd - 30 V






threshold) AND HV i < 0.1 A) ] AND






[ECU_DcLvEn = 1]






AND [timer >1 second]


DCLV error
bit
n/a
Clear error store
Indicates that an error (only DCLV) has occurred


exits in error



sometime in the past and is stored in the IPT non


store



volatile memory. This is just a status information






for the VCU





Remarks:


C1: Active output power reduction from the DC/DC


C2: Passive output power reduction due to external condition


C3: DC/DC is disabled. It is re-enabled as soon as the fault condition is cleared.


C4: DC/DC is faulted and then shuts down. It can be disabled to clear the fault.







FIG. 7 shows one load pattern 50 for a power converter 16 operating in boost mode. In particular, the power converter 16 is alternatingly switched between an ON state for 5 seconds and an OFF state for 5 seconds, which is repeated three times and followed by a 1 minute break, where the coolant is at approximately 72° C. at a flow rate of 8 liters/minute. A more flexible approach may be desirable.


In an ideal case, the boost mode would be able to run forever, at least until the low voltage power source (e.g., 12V battery and/or ultracapacitors) are discharged. Of course, some power converter 16 designs will overheat if forced to operate essentially continuously, due, for example, to thermal limitations which may exist where the thermal design was primarily based on the load pattern illustrated in FIG. 7.


The load pattern may be changed in a flexible manner, instead of a fixed load pattern 50, while maintaining a thermal condition equivalent to that of the load pattern of FIG. 7. For example, if the low voltage input current is 150 A or less, the power converter 16 operating in boost mode is capable of running continuously, because the thermal condition in this case is equivalent to the thermal condition in buck mode operation. Thus, an indication of the thermal condition may be a function of an input current.


It is however, difficult to predict the boost mode ON time precisely, particularly since it is related to many factors, such as coolant temperature, coolant flow rate, operating history, power level and duration. Using I2t-criteria as an indication of the thermal condition may be useful.


In one embodiment, 350 A with 5 second duration would have an I2t value of 612,500 A2S. If the input current reduced in half, the boost mode ON time can be extended as long as 20 seconds to allow the same amount of I2t pass through. Using the same method, results in a boost mode ON time estimation curve 52 are illustrated in FIG. 8.


The proposed load pattern change would, instead of setting a 5 second fixed boost mode ON time, would allow the integrated powertrain (IPT) software to calculate the ON time based on the low voltage input I2t. Once the low voltage input I2t reaches the 612,500 A2S, the IPT software disables boost mode, sending a message back to a vehicle controller indicating that the power converter boost mode goes into a 5 second break period. After the 5 second break, the vehicle controller may enable the power converter boost mode again. If the vehicle controller enables the power converter boost mode during the 5 second break period, the IPT controller will hold the command until the 5 second break period ends.


In reality the low voltage input current LV_I is not constant, thus the controller may employ an integral operation (e.g., ∫I2dt) to accumulate the total I2t. Since the boost mode can run continuously at 150 A or less, the integral only counts when the low voltage input current LV_I is greater than 150 A.



FIG. 9 shows a proposed boost mode load pattern 54.


In boost mode in some embodiments, if the battery voltage is over, for example, 13V for a short period of time, there will be no problem. Where the low voltage power source is a battery, the battery terminal voltage will drop under 13V once the battery is loaded.


In one embodiment, the start-up load condition in boost mode is 1.7 kOhm/13 mF, in which 1.7 kOhm is the total bleeding resistance, and the 13 mF is the total HV bus capacitance. It is possible to loosen the capacitance limitation if this requirement does not completely reflect a real situation, such as that for a vehicle. It is also possible to implement a high voltage capacitance in power system 10, for example a high voltage capacitance of between 8.4 mF and 13 mF. In such a case, an additional bleeding resistance, other than 2.5K inside the integrated power train, should be added to make sure boost operation starts up properly, because the DC/DC in boost mode takes advantage of the 1.7 kOhm bleeding resistor for a minimum load. If the command voltage in boost mode is higher than 250V, the resistance could be higher than 1.7 kOhm to keep the same minimum load. Table I, below, shows the total resistance and the additional resistance at different voltages. If the commanded high voltage is higher than 310V, no extra resistance is needed.











TABLE I









HV CMD Voltage (V)















250
260
270
280
290
300
310


















Total resistance
1700
1839
1983
2133
2288
2448
2614


(Ohm)


Additional
5315
6955
9592
14519
26955
118421


parallel


resistance


(Ohm)









The power system 10 may employ a number of hardware and/or software implemented protections. For example, a first hardware implemented overvoltage protection scheme may limit high voltage in buck mode to 445V while a second hardware implemented overvoltage protection scheme limits high voltage in boost mode to 426.8V. Additionally, or alternatively, a software implemented overvoltage protection scheme may limit high voltage to 440V.



FIG. 10 shows a functional block diagram of an embodiment of system 100 for controlling a power converter. The system 100 comprises a controller 102. In the embodiment illustrated in FIG. 10, the controller 102 comprises a processor 104, a memory 106, a fault detection module 108, a state machine 110, a control signal generator 112, an I/O module 114 and a controller system bus 116. The control system bus 116 may comprise a power bus, control bus, and status signal bus in addition to a data bus. For the sake of clarity, however, the various control system buses are illustrated in FIG. 10 as the controller system bus 116.


The controller 102 may be implemented in a variety of ways, including as separate subsystems. The controller 102 may be implemented as a microprocessor, a digital signal processor (DSP), an application-specific integrated circuit (ASIC), a gate-driver board, or the like, or as a series of instructions stored in a memory, such as the memory 106 and executed by a processor, such as the processor 104, or various combinations of the above. Thus, software modifications to existing hardware may allow the implementation of the controller 102. Various modules, such as the state machine 110, are identified as separate blocks in the functional block diagram of FIG. 10 because they perform specific functions that will be described in more detail below. These modules may not be discrete units but may be functions of a software routine, which will probably, but not necessarily, be separately callable and hence identifiable elements. The various modules may be combined. For example, all or portions of the fault detection module 108 may be integrated into the state machine 110, which in turn may be integrated into the control signal generator 112.


While the illustrated embodiment denotes a single processor 104, other embodiments may comprise multiple processors. The memory 106 may comprise, for example, registers, read only memory (“ROM”), random access memory (“RAM”), flash memory and/or electronically erasable programmable read only memory (“EEPROM”), and may provide instructions and data for use by the controller 102.


The fault detection module 108 determines whether conditions exist indicating a system fault and generates fault signals in response thereto. For example, the fault detection module may monitor system conditions as indicated by sensors 26a, 26b, 28a, 28b and control signals to determine whether a fault condition exists such as the fault conditions set forth in Table H. In response to detection of a fault condition, the fault detection module may generate fault signals.


The state machine 110 comprises a number of distinct states, such as those described above with respect to FIG. 6 and Table G. The control signal generator 112 may generate control signals for controller a power converter (such as the converter 16 illustrated in FIG. 1) based on a state of the state machine 110 and any fault signals generated by the fault detection module 108. The I/O module 114 facilitates reception and transmission of signals, such as data and control signals, by the controller 102.


Those skilled in the relevant art can readily create source code based on the Tables, Figures and the detailed description provided herein.


The term “computer-readable medium” as used herein refers to any medium that participates in providing instructions to a system or a processor for execution. Such a medium may take many forms, including but not limited to, non-volatile media, volatile media, and transmission media. Non-volatile media includes, for example, hard, optical or magnetic disks. Volatile media includes dynamic memory. Transmission media includes coaxial cables, copper wire and fiber optics. Transmission media can also take the form of acoustic or light waves, such as those generated during radio wave and infrared data communications.


Common forms of computer-readable media include, for example, a floppy disk, a flexible disk, hard disk, magnetic tape, or any other magnetic medium, a CD-ROM, any other optical medium, punch cards, paper tape, any other physical medium with patterns of holes, a RAM, a PROM, EPROM and an EEPROM, a FLASH-EPROM, any other memory chip or cartridge, a carrier wave, or any other medium from which a computer can read.


Various forms of computer readable media may be involved in carrying one or more sequences of one or more instructions to a processor for execution. For example, the instructions may initially be carried on a magnetic disk of a remote computer. The remote computer can load the instructions into its dynamic memory and send the instructions over a telephone line using a modem. A modem local to computer system can receive the data on the telephone line and use an infrared transmitter to convert the data to an infrared signal. An infrared detector coupled to a system bus can receive the data carried in the infrared signal and place the data on system bus. The system bus carries the data to system memory, from which a processor retrieves and executes the instructions. The instructions received by system memory may optionally be stored on storage device either before or after execution by the processor.


Although specific embodiments of, and examples for, the apparatus and method of bi-directional power conversion are described herein for illustrative purposes, various equivalent modifications can be made without departing from the spirit and scope of the disclosure, as will be recognized by those skilled in the relevant art. The teachings provided herein can be applied to other power systems, not necessarily the exemplary electric or hybrid vehicle based system generally described above. Likewise, the teachings provided herein can be applied to other power sources, not necessarily the exemplary fuel cell system, battery and/or ultracapacitors based power sources generally described above.


The various embodiments described above can be combined to provide further embodiments. All of the U.S. patents, U.S. patent application publications, U.S. patent applications, foreign patents, foreign patent applications and non-patent publications referred to in this specification and/or listed in the Application Data Sheet, including but not limited to patents U.S. Pat. No. 5,402,059, issued Mar. 28, 1995; U.S. Pat. No. 6,646,837, issued Nov. 11, 2003; U.S. Pat. No. 6,452,815, issued Sep. 17, 2002; and U.S. Pat. No. 6,587,356, issued Jul. 1, 2003; U.S. application Ser. No. 10/658,559, filed Sep. 8, 2003; Ser. No. 09/683,317, filed Dec. 13, 2001; Ser. No. 10/118,659, filed Apr. 8, 2002; Ser. No. 09/848,482, filed May 3, 2001; Ser. No. 10/345,894, filed Jan. 15, 2003; Ser. No. 10/346,561, filed Jan. 16, 2003; Ser. No. 10/360,832, filed Feb. 7, 2003; and Ser. No. 10/298,473, filed Nov. 18, 2002; and U.S. Provisional Application Ser. No. 60/246,273, filed Nov. 6, 2000; Ser. No. 60/255,371, filed Dec. 13, 2000; Ser. No. 60/270,703, filed Feb. 22, 2001; Ser. No. 60/271,184, filed Feb. 23, 2001; Ser. No. 60/319,070, filed Jan. 16, 2002; Ser, No. 60/319,071, filed Jan. 16, 2002; and Sere. No. 60/319,116, filed Feb. 20, 2002; are incorporated herein by reference, in their entirety. Aspects of the disclosure can be modified, if necessary, to employ systems, circuits and concepts of the various patents, applications and publications to provide yet further embodiments.


These and other changes can be made to the disclosed embodiments in light of the above-detailed description. In general, in the following claims, the terms used should not be construed to limit the disclosure to the specific embodiments disclosed in the specification and the claims, but should be construed to include bi-directional power converter based systems and methods operate in accordance with the claims. Accordingly, the disclosure is not limited by the embodiments, but instead its scope is to be determined entirely by the following claims.

Claims
  • 1. A computer-readable memory medium storing instructions for causing a control system to control a power converter by: monitoring command and condition signals; andselectively supplying control signals to cause the power converter to cycle between a plurality of operational modes based on the monitored command and condition signals, the plurality of operational modes comprising:a ready mode;a buck mode;a boost mode;a fault mode;a first wait mode during which power transfer is disabled; anda second wait mode comprising a duration different than the first wait mode during which power transfer is disabled.
  • 2. The computer-readable memory medium of claim 1, wherein the stored instructions further comprise instructions for causing the control system to control the power converter by: selectively generating control signals to cause the power converter to cycle from the boost mode to the first wait mode; andselectively generating control signals to cause the power converter to cycle from the boost mode to the second wait mode.
  • 3. The computer-readable memory medium of claim 1 wherein the stored instructions further comprise instructions for causing the control system to control the power converter by: selectively supplying control signals to cause the power converter to cycle from the boost mode to the first wait mode in response to an indication of a thermal condition.
  • 4. The computer-readable memory medium of claim 3 wherein the indication of a thermal condition is a function of an input current.
  • 5. The computer-readable memory medium of claim 1, wherein the stored instructions include instructions for causing the control system to supply control signals to cause the power converter to cycle from the boost mode to the first wait mode when an integrated value of an input current exceeds a threshold input current by a defined value.
  • 6. The computer-readable memory medium of claim 1, wherein the stored instructions include instructions for causing the control system to supply control signals to cause the power converter to operate in the fault mode in response to detection of a fault condition.
  • 7. The computer-readable memory medium of claim 1, wherein the stored instructions include instructions for causing the control system to supply control signals to cause the power converter to operate in the first wait mode for a first defined period of time and selectively supplying control signals to cause the bi-directional power converter to operate in the second wait mode for a second defined period of time.
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Related Publications (1)
Number Date Country
20050254273 A1 Nov 2005 US
Provisional Applications (1)
Number Date Country
60558521 Mar 2004 US