Patents by Inventor Carlisle R. Dolland

Carlisle R. Dolland has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 5323303
    Abstract: An active damper for an L-C filter suppresses transients that appear on the DC link from a power supply. The damper suppresses the transients by filtering the line voltage to obtain its steady-state component and comparing the steady-state voltage to the instantaneous voltage on the DC link. When the two voltages differ, the active damper cancels the transient by dissipating the energy on the DC link and the energy stored in the filter's inductor.
    Type: Grant
    Filed: March 5, 1992
    Date of Patent: June 21, 1994
    Assignee: AlliedSignal Inc.
    Inventor: Carlisle R. Dolland
  • Patent number: 4631474
    Abstract: The switch comprises a circuit from a first output terminal via parallel MOS devices in series with current-sensing resistance to a second output terminal, with alternative high-side and low-side configurations having a load between the second terminal and ground, or the first terminal and the DC supply voltage. An input terminal for a digital control signal is coupled via an input diode and two Schmitt Trigger CMOS inverters to a control lead for the gates of the switch. A current overload or short circuit protection circuit coupled between the current-sensor and the input diode comprises two transistors coupled by a diode. A built-in test circuit for indicating the switch condition (on, off, shorted or open) comprises MOS transistors having their gates connected to voltage dividers at the two output terminals, and their drains connected to discrete indication terminals.
    Type: Grant
    Filed: July 11, 1984
    Date of Patent: December 23, 1986
    Assignee: The United States of America as represented by the Secretary of the Air Force
    Inventor: Carlisle R. Dolland
  • Patent number: 4450443
    Abstract: A position transducer for indicating the position of a core member of a linear variable differential transformer produces DC level output signals proportional to changes occurring in the excitation and core displacement. Pulse signals from a clock source are converted to sinusoidal signals of a predetermined frequency and applied to the transformer. Movement of the core member varies the amplitude of the secondary waveform. To extract the position information the primary and secondary waveforms are applied to sample and hold circuits. These circuits receive gating signals to ensure the outputs of the primary and secondary sample and hold circuits acquire peak values of the sinusoidal input signals. The gating signals are derived by applying the sinusoidal primary waveform to a phase shift network. The resultant waveform is squared and used to trigger a one shot to produce a pulse train whose pulse width is 1/14 the period of excitation frequency.
    Type: Grant
    Filed: March 18, 1982
    Date of Patent: May 22, 1984
    Assignee: The Garrett Corporation
    Inventor: Carlisle R. Dolland
  • Patent number: 4401934
    Abstract: A control system for a permanent-magnet motor (10) driven by a multiphase line-commutated inverter (12) is provided with integrators (24) for integrating the back EMF of each phase of the motor for use in generating system control signals for an inverter gate logic (30) using a sync and firing angle (.alpha.) control generator (26) connected to the outputs of the integrators. A precision full-wave rectifier (16) provides a speed control feedback signal to a phase-delay rectifier (14) via a gain and loop compensation circuit (20) and to the integrators for adaptive control of the attenuation of low frequencies by the integrators as a function of motor speed, whereby as the motor speed increases, the attenuation of low frequency components by the integrators is increased to offset the gain of the integrators to spurious low frequencies. While the attenuation may be a continuous linear function of speed, a switch (Q.sub.1) is employed to provide a step change in attenuation at 40% of speed.
    Type: Grant
    Filed: August 7, 1981
    Date of Patent: August 30, 1983
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Carlisle R. Dolland, David A. Bailey
  • Patent number: 4394610
    Abstract: A control system for a permanent-magnet motor (10) driven by a multiphase line-commutated inverter (12) is provided with integrators (24) for integrating the back EMF of each phase of the motor for use in generating system control signals for an inverter gate logic (30) using a sync and firing angle (.alpha.) control generator (26) connected to the outputs of the integrators. A precision full-wave rectifier (16) provides a speed control feedback signal to a phase-delay rectifier (14) via a gain and loop compensation circuit (20) and to the integrators for adaptive control of the attenuation of low frequencies by the integrators as a function of motor speed, whereby as the motor speed increases, the attenuation of low frequency components by the integrators is increased to offset the gain of the integrators to spurious low frequencies. The .alpha.-control signals are produced by the firing angle control generator by means (48, 50) for combining 120.degree.
    Type: Grant
    Filed: August 7, 1981
    Date of Patent: July 19, 1983
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Carlisle R. Dolland
  • Patent number: 4351022
    Abstract: Control signals for phase-delay rectifiers, which require a variable firing angle that ranges from 0.degree. to 180.degree., are derived from line-to-line 3-phase signals (.phi.A, .phi.B, .phi.C) and both positive and negative firing angle control signals (+.alpha. and -.alpha.) which are generated by comparing (at 20) current command and actual current (sensed at 16). Line-to-line phases are transformed (32) into line-to-neutral phases and integrated (at 34) to produce 90.degree. phase delayed signals (A.phi., B.phi., and C.phi.) that are inverted (at 26a, b, c) to produce three cosine signals (C, A and B RAMP) such that for each its maximum occurs at the intersection of positive half cycles of the other two phases which are inputs to other inverters. At the same time, both positive and negative (inverted) phase sync signals are generated for each phase by comparing (at 27a, b, c) each with the next and producing a squarewave when it is greater.
    Type: Grant
    Filed: June 30, 1981
    Date of Patent: September 21, 1982
    Inventors: Alan M. Administrator of the National Aeronautics and space Administration, with respect to an invention of Lovelace, Carlisle R. Dolland, Daniel W. Trimble