US3729663A - Actuator systems employing energy recovery techniques - Google Patents

Actuator systems employing energy recovery techniques Download PDF

Info

Publication number
US3729663A
US3729663A US00168102A US3729663DA US3729663A US 3729663 A US3729663 A US 3729663A US 00168102 A US00168102 A US 00168102A US 3729663D A US3729663D A US 3729663DA US 3729663 A US3729663 A US 3729663A
Authority
US
United States
Prior art keywords
actuator
current
storage device
path
energy storage
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00168102A
Other languages
English (en)
Inventor
T Stevenson
G Scarrott
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fujitsu Services Ltd
Original Assignee
Fujitsu Services Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fujitsu Services Ltd filed Critical Fujitsu Services Ltd
Application granted granted Critical
Publication of US3729663A publication Critical patent/US3729663A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/48Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed
    • G11B5/54Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head into or out of its operative position or across tracks
    • G11B5/55Track change, selection or acquisition by displacement of the head

Definitions

  • ABSTRACT A system for accelerating and decelerating a movable element of an actuator includes an inductive energy [30] Foreign Application Priority Data storage means, a circuit for producing a predetermined current condition in the inductor which holds the element in a balanced position and stores energy in the storage means, and switch means for discharging the storage means through the actuator to ac- Sept. 4, 1970 Great Britain ..42,368/74 [52] US. Cl. .1 ....318/135, 318/687, 321/45 lift. (Il. celerate the element.
  • an assisting inductor acts to apply a step function voltage to the recording head and thus reduce the time necessary for the current in the head winding to reach its maximum value
  • the circuit elements must absorb this current upon dissipation of the recording field. Consequently, the electrical power necessary to energize the head winding is not being economically employed as a result of being dissipated in the circuit elements.
  • a system for controlling movement of the movable element of an actuator including an inductive energy storage means, circuit means for producing a predetermined current condition in the storage means to establish a store of energy therein, means for discharging the energy storage means through the actuator to cause the actuator element to accelerate in a desired direction; and means for feeding to the storage means current arising from movement of the element in opposition to current accelerating the element thereby to apply kinetic energy developed by movement of the element to the energy storage means.
  • FIGURE shows in schematic form a system for accelerating and decelerating a movable element of an actuator.
  • a control circuit 12 has a first output connected to the base of a transistor 10 by means of a line 22, and a second output connected to the base ofa transistor 11 by a line 23.
  • An inductor 25 has a core element 20 and associated windings 16 and 17 so that the coils are coupled in a uniform polarized manner. To keep leakage inductance between the windings 16 and 17 to a minimum they may be wound in bifilar arrangement.
  • the positive terminal ofa power source 18 is connected to the negative terminal of a power source 19. Both of these terminals are connected to the same input of an actuator 21.
  • the negative terminal of the source 18 is connected to the upper end of the winding 17 while the positive terminal of the source 19 is connected to the lower end of the winding 16.
  • the lower end of winding 17 is connected through a diode 14 to the collector of the transistor 11 while the upper end of the winding 16 is connected through a diode 15 to the collector of the transistor 10.
  • the other input of the actuator 21 is connected to the emitter electrodes of the transistors 10 and 11.
  • the actuator 21 may, for example, be a linear motor employed in a magnetic disc head positioning system. This motor may be of the moving coil type as described in co-pending U.S. Pat. application Ser. No. 102772, filed Dec. 30, 1970, which application is assigned to the assignees of the present invention.
  • the actuator 21 includes a movable mass which is acted upon by a DC. motor producing a force proportional to the current in the motor.
  • the mass-motor combination has an equivalent circuit whose dominant impedance component is capacitive. Consequently, the equivalent capacitance of the actuator can be regarded as forming part of a tuned circuit with the inductive impedance of the inductor 25 so that the actuator and the inductor can inter-exchange energy.
  • One form of linear motor or actuator is illustrated in U.S. Pat. No. 3,260,870.
  • control circuit 12 is arranged to produce output signals over the lines 22 and 23 to hold both of the transistors 10 and 11 in a conductive condition.
  • the power source 19 can then cause a current i, to flow through the winding 16, the transistor 10 and the actuator 21.
  • the source 18 causes a current i which is arranged to be substantially equal to current I], to flow through the winding 17, the transistor 11 and the actuator.
  • the currents i, and i flow in opposite directions in the actuator and since currents i and i: are substantially equal they effectively cancel one another in the actuator, so that the nett current flow through the actuator 21 is insufficient to energize the actuator to cause operation thereof. Even though the nett current flow through the actuator 21 is zero, the currents i and i will produce a standing current condition in the inductor so that a state of energy corresponding to the sum of i and i is established in the inductor.
  • the control unit 12 may be controlled by a servo system, which forms no part of the present invention, to control the currents i, and i by equal and opposite amounts whilst maintaining the required nett current condition through the actuator 21. Consequently the circuit 12 is able carefully to hold the actuator 21 stationary in the required position by making the appropriate changes in i, and i
  • This mode of operation will, for example, allow a recording head (not shown) to be positioned adjacent to a single track on a mag netic disc (not shown).
  • the balanced current condition in the actuator has to be removed so that the actuator is to be energized. This may be effected by causing the control circuit 12 to pass an output over the line 23 which renders the transistor 11 non-conductive and the output over the line 22 holds the transistor conductive.
  • the current flow i through the series circuit including the coil 17, the diode 14, the power source 18, the actuator 21, and the transistor 11 is interrupted, whilst the current continues to flow through the series circuit including the coil 16, the diode 15, the transistor 10, the actuator 21 and the power source 19;
  • the inductor tries to maintain a total current flow of i plus i through the windings 16, 17 but with the circuit of winding 17 interrupted the current i cannot flow in winding 17 with the result that the inductor causes a current initially equal to current i to be added to the standing current i in winding 16 and therefore a nett current equal to 1', plus i flows through the actuator 21.
  • the actuator On receipt of this combined current i and i the actuator is accelerated in a first direction. During this acceleration energy is withdrawn from the inductor, so that the current component i falls.
  • the movement of the actuator generates a back E.M.F. which produces a current i acting in opposition to the driving current i and i so that at any instant the movement of the actuator is the resultant of the falling magnitude current i;, the current i from the source 19 and the opposing current i arising from the back E.M.F.
  • the control circuit 12 When the inductor has travelled approximately half ofthe required distance through which it is to move the control circuit 12 is operated to reverse the conductive states of the transistors 10 and 11 so that the winding 16 is effectively switched out of circuit and the winding 17 is switched back into circuit.
  • the current arising from the back E.M.F. generated by movement of the actuator 21 will now flow in the winding 17 in the same direction as the initial standing current i and result in building be able to build up the standing current condition in the inductor and the actuator will come to rest with the standing current in the inductor 25 restored to the initial value. That is to say the kinetic energy of the actuator has been applied to the inductor 25 rather than being dissipated in circuit elements such as the transistors 10 and 11.
  • the inductor 25 and the actuator 21 form part of a tuned circuit a clamped resonance condition is produced between the inductor and the actuator which latter acts as a capacitance with respect to the back E.M.F. thereby aiding the required energy transfer.
  • the actuator 21 is decelerated and comes to rest after moving a certain distance X.
  • the distance X of motion of the actuator 21 is dependent upon the parameters ofthe actuator (or linear motor) and inductor 25.
  • the actuator may be moved a shorter distance by causing the control circuit 12 to reverse the connections from the actuator 21 to the inductor 25 before the back E.M.F. causes the current to reach zero.
  • the actuator may be moved a greater distance than distance X by disconnecting the actuator 21 from the inductor 25 for a period after the current has reached zero following acceleration of the actuator from its rest position.
  • the control circuit 12 renders both the transistors 10 and 11 non-conductive. It will be appreciated however that both transistors may be rendered non-conductive simultaneously only when the current is zero, since a large voltage spike, which would damage the transistors 10 and 11, would be produced if the transistors 10 and 11 were open-circuited with a current flowing therethrough.
  • the requirements imposed on the power sources 18 and 19 are lower than if the kinetic energy of actuator 21 were simply dissipated in the circuit components.
  • the power sources 18 and 19 which are of nominally equal voltages, need only be able to produce a current and voltage sufficient to magnetize the inductor 25 and to make up for the resistive losses in the inductor 25 and in the transistors 10 and 11 and actuator 21. Such losses, however, are small in com parison to the total energy returned to the inductor 25 so that the total dissipation of power is kept to an economically low level.
  • the system can be returned to a stationary mode by continue to apply an output signal over the line 23 to hold the transistor 11 conductive and rendering the transistor 10 conductive by operating the control circuit 12 to apply an appropriate output signal over line 22. In this manner, the currents i and i are re-established.
  • the actuator 21 is energized to move in one direction by rendering the transistor 10 fully conductive and the transistor 11 nonconductive.
  • the control circuit 12 may apply output signals to render the transistor 10 non-conductive and transistor 11 conductive to energize the actuator 21 to cause motion in a reverse direction.
  • actuator 21 has been described as a moving coil linear motor, it will be appreciated that other forms of electrical motors may be employed. Thus, rather than moving a coil by a distance X, an armature may be moved by an angle if, for example, a suitable D.C. electric motor is used.
  • the diodes 14 and 15 are provided for the purpose of protecting the transistor 11 and 10 respectively, from back voltages developed by the transformer action between the windings l6 and 17 of the inductor 25.
  • transistor 10 and 11 are employed as switching devices, it will be realized that other semiconductor switching elements or thermionic valves may be employed as well.
  • An actuator driving system including an actuator having an element movable in response to the application of an electric current to the actuator; an inductive energy storage device; first and second electrical power sources connected to the actuator to supply currents subtractively thereto and to the energy storage device to supply currents additively thereto; and control means effective in a first condition to cause the power sources to supply substantially equal currents and in a second condition to supply unequal currents, switching of the control means from the first to the second condition causing energy stored in the energy storage device to be delivered to the actuator.
  • switch means is operative to enable current flow through said selected path and to interrupt current flow in said other path so as to decelerate the element and transfer kinetic energy of the element to the storage device.
  • said inductive energy storage device includes a first winding connected in said first path and a second winding connected in said second path and a magnetic core effective to couple electromagnetically the first and second windings.
  • a system as claimed in claim 2 in which the switch means includes a transistor in each current path, and in which the control means is operable to adjust the conductive states of the transistors to change the conduction condition of the first and second paths.

Landscapes

  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
  • Control Of Linear Motors (AREA)
  • Linear Motors (AREA)
  • Control Of Direct Current Motors (AREA)
US00168102A 1970-09-04 1971-08-02 Actuator systems employing energy recovery techniques Expired - Lifetime US3729663A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4236870 1970-09-04

Publications (1)

Publication Number Publication Date
US3729663A true US3729663A (en) 1973-04-24

Family

ID=10424114

Family Applications (1)

Application Number Title Priority Date Filing Date
US00168102A Expired - Lifetime US3729663A (en) 1970-09-04 1971-08-02 Actuator systems employing energy recovery techniques

Country Status (5)

Country Link
US (1) US3729663A (hu)
DE (1) DE2138611C3 (hu)
GB (1) GB1344627A (hu)
HU (1) HU164251B (hu)
PL (1) PL82216B1 (hu)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2425172A1 (fr) * 1978-05-03 1979-11-30 Bar Maurice Asservissement de l'induction dans un circuit magnetique par decoupage
WO1995012913A1 (en) * 1993-11-05 1995-05-11 Magnetic Bearing Technologies, Inc. Increased stroke force pulsed power linear actuator
US6614195B2 (en) * 2000-05-09 2003-09-02 Tennant Company Linear actuator control structure
US6617712B1 (en) * 1998-10-26 2003-09-09 Marposs, S.P.A. Linear position transducer with primary and secondary windings and a movable induction coupling element
US20100265298A1 (en) * 1998-10-16 2010-10-21 Silverbrook Research Pty Ltd Inkjet printhead with interleaved drive transistors
US8087757B2 (en) 1998-10-16 2012-01-03 Silverbrook Research Pty Ltd Energy control of a nozzle of an inkjet printhead

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3406328A (en) * 1966-04-28 1968-10-15 Borg Warner Static inverter carrier system
US3449654A (en) * 1965-10-11 1969-06-10 Gen Motors Corp Direct current commutation system for brushless electrical motors
US3465233A (en) * 1968-01-10 1969-09-02 Ramsey Controls Inc Self-commutating inverter
US3474322A (en) * 1967-01-24 1969-10-21 Westinghouse Brake & Signal Controllable rectifier circuits providing energy recovery from commutation circuit
US3530347A (en) * 1966-09-22 1970-09-22 Mesur Matic Electronics Corp Energy transfer means for stepping motors
US3560821A (en) * 1969-04-21 1971-02-02 Sigma Instruments Inc Pulse type drive circuit for an inductive load
US3560818A (en) * 1969-02-03 1971-02-02 Ford Motor Co Reluctance motor power circuit using dual energy sources

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3449654A (en) * 1965-10-11 1969-06-10 Gen Motors Corp Direct current commutation system for brushless electrical motors
US3406328A (en) * 1966-04-28 1968-10-15 Borg Warner Static inverter carrier system
US3530347A (en) * 1966-09-22 1970-09-22 Mesur Matic Electronics Corp Energy transfer means for stepping motors
US3474322A (en) * 1967-01-24 1969-10-21 Westinghouse Brake & Signal Controllable rectifier circuits providing energy recovery from commutation circuit
US3465233A (en) * 1968-01-10 1969-09-02 Ramsey Controls Inc Self-commutating inverter
US3560818A (en) * 1969-02-03 1971-02-02 Ford Motor Co Reluctance motor power circuit using dual energy sources
US3560821A (en) * 1969-04-21 1971-02-02 Sigma Instruments Inc Pulse type drive circuit for an inductive load

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2425172A1 (fr) * 1978-05-03 1979-11-30 Bar Maurice Asservissement de l'induction dans un circuit magnetique par decoupage
WO1995012913A1 (en) * 1993-11-05 1995-05-11 Magnetic Bearing Technologies, Inc. Increased stroke force pulsed power linear actuator
US20100265298A1 (en) * 1998-10-16 2010-10-21 Silverbrook Research Pty Ltd Inkjet printhead with interleaved drive transistors
US8011757B2 (en) * 1998-10-16 2011-09-06 Silverbrook Research Pty Ltd Inkjet printhead with interleaved drive transistors
US8087757B2 (en) 1998-10-16 2012-01-03 Silverbrook Research Pty Ltd Energy control of a nozzle of an inkjet printhead
US6617712B1 (en) * 1998-10-26 2003-09-09 Marposs, S.P.A. Linear position transducer with primary and secondary windings and a movable induction coupling element
US6614195B2 (en) * 2000-05-09 2003-09-02 Tennant Company Linear actuator control structure
USRE41036E1 (en) 2000-05-09 2009-12-15 Tennant Company Linear actuator control structure

Also Published As

Publication number Publication date
DE2138611B2 (de) 1979-11-08
GB1344627A (en) 1974-01-23
PL82216B1 (hu) 1975-10-31
DE2138611A1 (de) 1972-03-09
HU164251B (hu) 1974-01-28
DE2138611C3 (de) 1980-07-17

Similar Documents

Publication Publication Date Title
US3372288A (en) Sequential switching with delay for controlled rectifier circuits
US3116445A (en) Single phase induction motors and starting arrangement therefor
US3530347A (en) Energy transfer means for stepping motors
EP0049948B1 (en) Control system for transducer positioning motor
US3629679A (en) Linear motor power failure detection circuit and fail-safe control
US3729663A (en) Actuator systems employing energy recovery techniques
US3876168A (en) Motor control for tape transport system
US3584280A (en) Transistor motor apparatus including current attenuation means
GB841199A (en) Improvements in regenerative electromechanical actuator drive circuits
US4342956A (en) Proportional base drive circuit
US3433207A (en) Electronic control system for fuel injection systems
CA1037556A (en) Driving circuit for printing electromagnet
US3573593A (en) Angular velocity control system for step servo motor system responsive to winding deenergization
GB1073960A (en) Improvements in or relating to the inducing of current flow in superconducting circuits
US3211964A (en) Actuator power supply
GB2095065A (en) Solenoid control circuit
US3374402A (en) Data printing apparatus
US3127522A (en) Time controlled switch using saturable core input
US3449639A (en) Actuator driver circuit
US3714535A (en) Servo displacement limiter with reversing capabilities
GB1428786A (en) Actuator drive circuit
US3803456A (en) Electronic feedback control system for slow-speed operation of electromechanical devices
US3930171A (en) Low power, fast rise time current driver for inductive load
US3678344A (en) Electromagnetic relay operation monitor
US3963967A (en) Contactor interlock circuits