Patent Document

The present application is a continuation-in-part of U.S. patent application Ser. No. 11/275,814, filed Jan. 30, 2006. U.S. patent application Ser. No. 11/275,814, filed Jan. 30, 2006, is hereby incorporated by reference. 

   BACKGROUND 
   The present invention pertains to actuators for heating, ventilation and air conditioning systems, and particularly to actuator controls. 
   SUMMARY 
   The invention is a system for maintaining desired actuator control in the event of a power disruption despite the amount of the duration of the disruption, and in the event of slow voltage rise. 

   
     BRIEF DESCRIPTION OF THE DRAWING 
       FIG. 1  is a diagram of a damper with an actuator which a latch and related circuitry may control; 
       FIG. 2  is a block diagram of the latch and related circuitry; 
       FIGS. 3   a  and  3   b  are graphs of drive signals to an actuator; 
       FIG. 4  is a truth table of the latch; 
       FIG. 5  is a block diagram of the latch and actuator arrangement; 
       FIG. 6  is a schematic of a slow voltage rise detector, reset device and latch logic; 
       FIG. 6   a  is a graph of the voltage on the capacitor of the reset circuit; 
       FIG. 7  is a schematic of an oscillator and actuator control device; 
       FIG. 8  is a schematic of a motion sensor and related circuitry; 
       FIG. 9  is a schematic of a current overload detection circuit; 
       FIG. 10  is a schematic of a high temperature detection circuit; 
       FIG. 11  is a schematic of power supply circuitry; and 
       FIG. 12  is a schematic of motor interface circuitry. 
   

   DESCRIPTION 
   An item of concern is the control of a smoke and fire actuator  17  ( FIG. 1 ) connected to, for an illustrative example, to a damper  18  (actuable mechanism) of an HVAC (heating, ventilation and air conditioning) system of a building. The actuator  17  may have two different modes, run (i.e., drive) and hold. Actuator  17  may be regarded as, for instance, a motor, solenoid, and the like, and be connected with a mechanical linkage  60  ( FIG. 2 ) to the damper  18  in a vent  27  of the HVAC system for flow  26  control. Here, an instance of the actuator  17  may be a motor. The terms “actuator” and “motor” may be used herein interchangeably. 
     FIG. 2  is a block diagram of the present system  10  incorporating an RS latch integrated AC detect reset and slow voltage rise compensating mechanisms having an application to actuators. The system is for maintaining desired actuator control in the event of a power disruption despite the amount of the duration of the disruption, and in the event of slow voltage rise. The blocks or modules and their interconnections in  FIG. 2  are illustrated in the other Figures discussed herein. There may be a slow voltage rise (voltage change) detector  13  and a power supply  12  having an indicator tied in with ultimately an R input  14  of an RS latch logic device  11  (NOR gates  41  and  42  of latch mechanism  40  in  FIG. 6 ). There is an actuation sensor  16 , which may include a Hall sensor  52  ( FIG. 8 ), for indicating movement of the motor or actuator  17 , connected to the S input  14  of latch  11 . The actuator  17  may be mechanically linked via connection  60  to the damper  18 . The actuator  17  or damper  18  may be spring loaded to close the damper when there is no other force acting on the damper, such as that of the actuator  17  operating to open it or hold it open. 
   The actuator  17  may be operated with a pulse width modulated (PWM) or varied pulse width electrical power drive signal. An example actuator  17  may be a motor. The motor may be a brushed D.C. type of device. During a run or drive mode, the actuator or motor  17  may be fed a high duty ratio (i.e., a large pulse width) drive signal to open the damper  18 . During the hold mode, the motor  17  may be fed a low duty ratio (i.e., a small pulse width) drive signal which needs to be only sufficient to hold the damper  18  in its position against the tension of, for instance, an actuator spring acting to close the damper. The low duty ratio signal may be used to conserve energy, and to lengthen the life of the actuator  17  by eliminating excessive stress on it. 
   The output of the logic device  11  may be a logic 1 or a logic 0. The logic 0 is a signal for a run mode pulse width waveform module  21  for a driver or oscillator  23  to provide the respective run signal to the motor or actuator  17 . The logic 1 is a signal for a hold mode pulse width waveform module  22  for oscillator  23  to provide the respective hold drive signal to the motor or actuator  17 . Modules  21  and  22 , and oscillator  23  may constitute oscillator module  49 . The output of the module  21  may select a 60 percent duty cycle of a signal  24  and the output of the module  22  may select a 20 percent duty cycle of a signal  25 , as shown in  FIGS. 3   a  and  3   b,  respectively. These are examples since the duty cycles may be of other percentages. A run drive signal may be defined as having a duty cycle greater than about forty percent and a hold drive signal may be defined as having a duty cycle less than about forty percent. The frequency of signals  24  and  25  may be about 20 KHz or another value. 
   The module  21  may output the run mode signal to the oscillator  23 , which in turn can output a 60 percent or so duty cycle drive signal to the actuator  17 . Actuator  17  may rotate the damper  18 , if closed, about 90 degrees for a full open position. Then a signal from the actuation sensor  16 , which senses actuator  17  motion, may indicate that the actuator  17  has stopped. Then a signal, indicating no motion of the actuator  17 , may go to the S input  15  of the RS latch logic device  11 . Device  11  may output a logic 1 signal indicating a hold to module  22  which indicates oscillator  23  to provide the  20  or so percent duty cycle drive signal to the actuator  17 . This drive signal may provide just enough amount of signal to the actuator  17  to hold the damper  18  open. The weaker 20 percent duty cycle drive signal to the actuator  17  may be provided in lieu of the 60 percent duty cycle drive signal to avoid unneeded stress on the actuator, to extend the life of the motor or actuator, and to save power. 
   If power is lost to an overall system of which the actuator and damper are a part, then the damper  18  will close because of no hold or drive signal being provided to the actuator  17 . The actuator  17  or damper  18  may have a spring-loaded tension applied to the damper  18  to cause the damper to close and remain closed when no drive signals are applied to the actuator  17 . This characteristic is for safety reasons, among other reasons, such as, for example in the event of a fire, to prevent movement of smoke along with air  26  ( FIG. 1 ) in the vent passages  27  to various spaces of the building, including those spaces with personnel still in them. 
     FIG. 5  is a block diagram of components of the system  10  incorporating the present invention. The components and their interconnections are described herein. The Figure shows an overview of a circuit  150  which may include a voltage change detector, slow voltage rise detector or AC detect circuit  13 , a reset circuit  53 , a latch  40 , a driver or oscillator  49  and an actuator control module  56 . Circuits  13  and  53  may be quite integrated with overlap having an appearance of one circuit in some implementing designs. Circuits  13  and  53  may be regarded as a detect and reset circuit  149 . 
   The present circuit may have an RS latch  40  as shown in  FIGS. 1 and 6 . This latch is to prevent actuator  17  from going back into a run mode after stalling, thus preventing oscillation. 
   An issue is that, when power is taken away, energy has to dissipate from the circuit before the latch  40  can be reset properly and the actuator  17  can return to the run mode so as to drive the damper  18  back open. If power is removed from the actuator  17  after it has reached a hold mode and then is powered shortly after (within 2 seconds), the actuator will return to the hold mode. During the power-off time, the actuator  17  spring returns a short distance of a stroke to put the damper  18  in a partially closed position. Since the actuator  17  comes back into the hold mode, the damper  18  may remain in the partially closed position. Such successive power interruptions will cause the actuator  17  to eventually let the damper  18  close all the way. This action may be a major issue in the field because when customers test their backup power generators, they may remove power from the actuator system for about one second or less. However, the related art actuator literature for this configuration appears to say to remove power for more than two seconds to reset the actuator properly. The present system  10  may have the actuator reset virtually immediately after removing power and to remove this power removal duration requirement. 
   Another issue is when voltage to the actuator  17  rises slowly, the actuator may enter the hold mode before it is able to drive open the damper  18  and thus the damper remains closed. This can be a significant cause of customer complaints in the field relating to normal behavior of the actuator  17 . The invention is a system for solving these issues so that the actuator and damper arrangement of this configuration can compete better in the field and keep customers satisfied. Upon a return of power, the present system  10  permits the actuator  17  to open the damper  18  before the actuator enters the hold mode. Also, the period of time between the moment of detecting a loss of power in the system  10  and a moment of detecting a return of power in the system may range from about a millisecond to greater than five minutes, while still permitting system to operate appropriately as indicated herein. 
   The present system may begin to solve the latch  40  reset problem by detecting a loss in AC, if the primary source of power, or DC if not, which occurs upon a power loss to the system. Upon the loss of power, an AC-detect or voltage change circuit  13  may reset the RS latch  40  before the energy is dissipated from the system circuit, which puts the actuator  17  back into the run mode. Energy during a dissipation period after the power loss for circuit operation may be provided by a large capacitor (e.g., capacitor  109  of  FIG. 11 ) across the system circuit power supply terminals. The actuator  17  in the run mode may provide the correct initial condition for the circuit when power is restored whether there is still electrical energy or not in the circuit. The slow voltage rise problem may be solved by keeping the actuator  17  in a run mode at lower voltage levels. When the voltage is below the level for the actuator to operate, the AC-detect circuit  13  keeps the actuator  17  in the run mode upon a power return thereby preventing it from latching prematurely into a hold position. Once the voltage reaches a certain level, the actuator or motor  17  begins to turn the damper  18 . For an intermediate voltage, both the AC-detect circuit  13  and the reset circuit  53  keep the actuator  17  in a run mode. As the voltage to the actuator  17  continues to increase, the AC-detect circuit  13  cuts out of the system control circuit, allowing the circuit to latch into the hold state once the actuator drives the damper  18  to its fully open position. The period of energy dissipation of the system circuit may be extended in time with a more substantially sized capacitor across the system circuit power supply terminals  51  and  47 . 
   The slow voltage rise, voltage change or AC detect circuit  13  and reset circuit  53  may consist of an op-amp used as a comparator  31 , an inverter  32 , six resistors  33 ,  34 ,  35 ,  36 ,  37  and  38 , and a ten microfarad capacitor  39  feeding via the inverter  32  into the R input  14  of an RS-latch  40  ( FIG. 6 ). Latch  40  may have two NOR gates  41  and  42  interconnected in a latch-like fashion (i.e., the output of each gate connected to an input of the other gate). Upon a loss of power, the voltage across a resistor divider of resistors  33  and  34  may decrease. Resistors  33  and  34  may be 100K ohms and 15K ohms, respectively. Resistor  33  has one end connected to one end of resistor  34 , and another end connected to an output line  51  of the power supply circuit  12  for the system ( FIG. 11 ). The other end of resistor  34  may be connected to ground  47 . The voltage at the common connection of resistors  33  and  34  may be fed into the non-inverting terminal  44  of the comparator  31 . The voltage at terminal  44  may hit or go below a certain predetermined level, which is the level of the voltage at the inverting terminal  45  of the comparator  31 . The voltage at the inverting terminal  45  may be provided by a voltage divider of resistors  35  and  36  connected in series across Vcc  46  and ground  47 . Resistors  35  and  36  may each be 10K ohms. The voltage at the inverting terminal  45  may be relatively fixed. Since it has a smaller rail, input  45  reaches its fixed voltage before the non-inverting input  44  reaches its voltage.  FIG. 6   a  shows the voltage on capacitor  39  versus time. When a voltage at the non-inverting input  44  is the same or less than the voltage at the inverting input  45 , then a comparator  31  output  43  may have a low impedance and thus rapidly discharge the capacitor  39  (as shown by curve  151  in  FIG. 6   a ) to provide a logic 0 via a 909 ohm resistor  37  at one end of capacitor  39  to the input of inverter  32 . The other end of capacitor  39  may be connected to ground  47 . Inverter  32  may have an output  14  that provides a logic one to the R input  14  of latch  40 . 
   Dimension  153  of  FIG. 6   a  represents the period of disruption of power to the system. Once power is restored to the system, the voltage across a divider having resistors  33  and  34  may increase and be present at the non-inverting input  44 . This voltage may eventually become higher than the voltage at the inverting terminal  45 , which results in an open-collector output  43  at the comparator  31 . Output  43  then presents a high impedance and does not affect the charge on the capacitor  39 . Capacitor  39  may be charged up by current through a 100K ohm resistor  38  from Vcc  46  (as shown by curve  152  in  FIG. 6   a ). But before capacitor  39  is charged and Vcc  46  is on or up to its normal voltage, the input to inverter  32  is low and the inverter&#39;s output to the R input is a logic high or one. Then the output  48  of latch  40  would be a logic low or zero indicating a run mode. The RC time constant of resistor  38  and capacitor  39  provides an appropriate amount of time due to charging so that the actuator  17  may be in the run mode for that period of time which is until the actuator reaches the end of the stroke and before a logic zero is fed from inverter  32  to the R input  14 . 
     FIG. 4  shows a truth table of the RS latch  40  for the R input  14 , the S input  15  and the Q output  48 . The row where R=1 and S=0, Q is 0 for a drive at start-up. The row where R=0 and S=0, Q is Q in that Q=Q′=0 for a drive. The row where R=0 and S=1, Q is 1 for a hold. The row where R=1 and S=1, Q is 0 for a drive. 
     FIG. 7  shows an oscillator and associated circuitry  49 . The oscillator  49  may have an output  55  that proceeds to a motor or actuator control device or module  56  that is connected via line  61  to one side of the actuator  17  where it is connected to a ground  47  with the FET switch  57 . The ground  47  connection may have a 0.33 ohm resistor  62  for current sensing. The other end of the resistor  62 , connected to the source of FET  57 , may be connected to a current sensor  58  ( FIG. 9 ) via a line  59 . Output  55  is connected to the gate of FET  57 . The drain of the FET is connected to the actuator  17  via a line  61 . Signals such as the 60 percent duty cycle signal  24  and the 20 percent duty cycle signal  25  may be applied from oscillator output  55  to actuator  17  via module  56 . 
     FIG. 8  shows a schematic of a module  16  with a motion or actuation sensor  52  and related circuitry. Sensor  52  may be a Hall effect sensor model SS443A by Honeywell International Inc. Power may be applied to the sensor  52  via line  51  from module  12  ( FIG. 11 ). An output from the actuation sensor module  16  may be connected via a line  15  to the S input of NOR gate  42  of latch  40  ( FIG. 6 ). 
   For further detail of actuation sensor module  16  in  FIG. 8 , line  51  may provide power through a 909 ohm resistor  114  to the sensor  52 . The sensor is also connected to ground  47 . A zener diode (1N5254B)  116  may be connected across the power input terminals of sensor  52  with the anode to ground  47 . A sensor signal output  115  may be connected to one end of a 10K ohm resistor  117  and one end of a 0.1 microfarad capacitor  118 . The other end of capacitor  118  may be connected to one end of a 100K ohm resistor  119  and to a cathode of diode (1N4148)  120 . The anode of diode  120  may be connected to ground  47 . The other end of resistor  117  may be connected to Vcc  46 . The other end of resistor  119  may be connected to a base of transistor  121  and to one end of a 100K ohm resistor  122 . The other end of resistor  122  may be connected to ground  47 . The collector of transistor  121  may be connected through a 150K ohm resistor  123  to Vcc  46 . The collector of transistor  121  may also be connected to one end of a ten microfarad capacitor  124  and to line  15 . The other end of capacitor  124  and the emitter of transistor  121  may be connected to ground  47 . 
     FIG. 9  is a diagram of the current sensor module  58  which may be presented with a voltage drop across resistor  62  of actuator control module  56  ( FIG. 7 ) via line  59  to an inverting input of comparator  63 . A voltage from the mid-point of a voltage divider with 10K and 976 ohm resistors  64  and  65 , respectively, connected in series from Vcc  46  to ground  47 , may be provided to a non-inverting input of comparator  63 . If there is an amount of current through resistor  62  in module  56  that is determined to be excessive for the actuator  17 , then the voltage drop to the inverting input of comparator  63 , when compared to the voltage drop across resistor  65 , may cause an output on line  66  to go from a logic high to a logic low indicating a current overload through actuator  17 . Line  66  may be connected to an input of a NOR gate  67  in the temperature sensor module  68  of  FIG. 10 . 
   A ten microfarad capacitor  125  may be connected across the resistor  65 . The output of comparator  63  may be connected through a 100K ohm resistor  126  to Vcc  46 . Also, the output of comparator  63  may be connected through a 0.001 microfarad capacitor  127  to ground  47 . 
     FIG. 12  is a diagram of a circuit  130  for application with an actuator  17  which may generate back EMF when running backwards upon a deenergizing of the actuator. A power connection to actuator  17  may be lines  61  and  51 . A 0.01 microfarad capacitor  135  may be connected across lines  51  and  61 . The actuator  17  may for example be a brush D.C. motor that drives an actuable mechanism  18  ( FIG. 1 ). Actuator  17  may be caused to run backwards by a spring on the actuator  17  or mechanism  18 , and return it to its normal position during a deenergized state of the actuator. The circuit  130  may reduce the speed of the actuator  17  and mechanism  18  while returning to its normal position while in the deenergized state, with current returning through a diode  131 , having a cathode connected to an anode of zener diode  132 , and presenting a voltage across the zener diodes (1N5917B)  132 ,  133  and  134  which are connected in series with the anode of diode  134  connected to line  51  and the anode of diode  131  connected to line  61 . Current may flow through a P-channel FET  136 , which has a drain connected to line  51  and a source connected to the cathode of diode  131 . The gate of transistor  136  may be connected through a 20K ohm resistor  137  to a collector of an NPN transistor  138 . The gate of transistor  136  may also be connected through a 10K ohm resistor  139  to the cathode of diode  131 . The emitter of transistor  138  may be connected to the ground  47 . The base of transistor  138  may be connected through a 40.2K ohm resistor  141  to Vcc  46 , and the base may also be connected through a 10K ohm resistor  140  to ground  47 . 
     FIG. 10  shows a temperature sensitive resistor  69  that may change in resistance relative to temperature variation. Resistor  69  may be proximate to the actuator  17  for purposes of detecting an overheating situation within the actuator. The resistor  69  may be a part of a voltage divider with resistor  69  connected to Vcc  46  and a resistor  71  connected to ground  47 . The midpoint or connection of resistors  69  and  71  may be connected to an input of an inverter  72  via a 10K ohm resistor  73 . Resistors  69  and  71  may have nominal values of 47K and 3.740K ohms, respectively. An output from inverter  72  may go via a line  74  to an input of an inverter  75  and an input of a NOR gate  76 . An output of inverter  75  may be connected through a 100K ohm resistor  77  to the input of inverter  72 . The output of inverter  75  may also be connected to an input of NOR gate  67 . 
   An output of NOR gate  67  may be connected via a 100K ohm resistor  78  to a base of an NPN transistor  79 . The emitter of transistor  79  may be connected to ground  47  and the collector may be connected via a line  81  to oscillator module  49  ( FIG. 7 ). The output  48  of latch  40  ( FIG. 6 ) may be connected to an input of NOR gate  76 . An output of gate  76  may go via a 100K ohm resistor  82  to a base of an NPN transistor  83 . The emitter of transistor  83  may be connected to ground  47  and the collector may be connected via a line  84  to the oscillator module  49  of  FIG. 7 . 
   The output  48  from the latch  40  ( FIG. 6 ) may be connected through a 10K ohm resistor  85  to a base of an NPN transistor  86  ( FIG. 7 ). The collector of transistor  86  may be connected to a cathode of a diode  87 , and the anode of the diode  87  may be connected through a 6.040K ohm resistor  88  to a terminal  89 . The emitter of transistor  86  may be connected to an anode of a diode  91 . The cathode of diode  91  may be connected through a 43.2K ohm resistor  92  to the terminal  89 . The emitter of transistor  86  may be connected through a 130K ohm resistor  93  to the terminal  89 . The emitter of transistor  86  may also be connected through a 10K ohm resistor  94  to an input of an inverter  95 . Line  84  from the collector of transistor  83  in  FIG. 10  may be connected to the input of inverter  95 . The output  55  of inverter  95  and of the oscillator  49  may be connected to the gate of FET  57 . The emitter of transistor  86  may also be connected to an input of an inverter  96 . The output of inverter  96  may be connected to one end of a 0.001 microfarad capacitor  97 . The other end of capacitor  97  may be connected to terminal  89 . Terminal  89  may be connected through a 10K resistor  98  to an input of an inverter  99 . Also, line  81  from the collector of transistor  79  ( FIG. 10 ) may be connected to the input of inverter  99 . The output of inverter  99  is connected to the input of inverter  96 . 
     FIG. 11  is a diagram of the rectifier, filter and regulator module  12 . A power source module  54  may provide a  24  volt AC supply via lines  155  and  156  to module  12 . A 0.10 microfarad capacitor  101  may be connected across lines  155  and  156 . Another 0.10 microfarad capacitor  102  may be connected between line  156  and a ground  103 . Ground  103  is different from and isolated from the ground  47  of the system. The power on lines  155  and  156  may go through a full-wave rectifier  104 . Diode  105  may have a cathode connected to a cathode of a diode  106 . Diode  106  may have an anode connected to a cathode of diode  107 . Diode  107  may have an anode connected to an anode of diode  108 . The cathode of diode  108  and the anode of diode  105  may be connected to line  155 . The anode of diode  106  and the cathode of  107  may be connected to line  156 . The cathodes of diodes  105  and  106  may be connected to line  51 . The anodes of diodes  107  and  108  may be connected to ground  47 . Thus, a full-wave rectification of the voltage signal from the source  54  may be present across line  51  and ground  47 . Various other approaches, such as other rectification or direct current schemes, with other kinds of components, half-wave, or just a plain DC voltage from the power source module  54 , may be utilized for providing the power to lines  51  and  47 . A 1000 microfarad capacitor  109  and a 0.1 microfarad capacitor  110  may be connected across the power output line or terminal  51  and ground  47 . Capacitors  109  and  110  may provide filtering for the output from rectifier  104 . Capacitor  109  may provide some sustaining reserve power for a brief period of time to system  10  upon a disruption of power to the system. About a 5.1 volt zener diode  111  may have an anode connected to ground  47  and a cathode connected through a 2K ohm resistor  112  to line  51 . A 0.1 microfarad capacitor  113  may be connected across the zener diode  111 . The connection between the cathode of diode  111  and resistor  112  may be the Vcc supply terminal  46 . The five or so volts at terminal  46  may be regarded as regulated. 
   In the present specification, some of the matter may be of a hypothetical or prophetic nature although stated in another manner or tense. 
   Although the invention has been described with respect to at least one illustrative example, many variations and modifications will become apparent to those skilled in the art upon reading the present specification. It is therefore the intention that the appended claims be interpreted as broadly as possible in view of the prior art to include all such variations and modifications.

Technology Category: 5