Patents Assigned to Turbodyne Systems, Inc.
  • Patent number: 5841649
    Abstract: Six sets of parallel-connected MOSFETs are gated to provide a 3-phase output. At least one of the MOSFETs in each of three sets of the six sets has a separately metallized current-sensing pad. The output from this pad represents the phase current. When phase current reaches a maximum permissible level, this signal controls the MOSFET gates to limit current.
    Type: Grant
    Filed: January 10, 1997
    Date of Patent: November 24, 1998
    Assignee: Turbodyne Systems, Inc.
    Inventors: David T. Willett, Edward M. Halimi
  • Patent number: 5823149
    Abstract: NOx emissions from gasoline engines are reduced by mixing water in the gasoline to reduce combustion temperatures. The water is dispersed in the gasoline as the gasoline is delivered to the cylinders. When the engine is not operating, the water separates from the gasoline and causes rusting. In accordance with this invention, the mixing of water into the gasoline is terminated before the engine is shut off so as to purge the system of the water/gasoline dispersion so that there no longer is water in the fuel supply system by the time the engine is stopped.
    Type: Grant
    Filed: July 24, 1996
    Date of Patent: October 20, 1998
    Assignee: Turbodyne Systems, Inc.
    Inventors: Anatoly D. Mezheritsky, Edward M. Halimi
  • Patent number: 5787711
    Abstract: An internal combustion engine cooling system incorporating a motor-assisted turbofan is disclosed. The turbine-driven fan is increased in rotational speed by energizing a motor attached to the turbine fan shaft from an outside power source to provide required cooling air flow. The cooling air system of the invention also includes a ducted fan for supplying cooling air for one or more heat exchangers, and is controlled via inputs from an engine speed sensor for providing a motor operating signal, a flow sensor downstream of the heat exchangers for providing a motor operating signal, and temperature sensors located throughout the cooling circuits.
    Type: Grant
    Filed: September 16, 1996
    Date of Patent: August 4, 1998
    Assignee: Turbodyne Systems, Inc.
    Inventors: William E. Woollenweber, Edward M. Halimi
  • Patent number: 5771868
    Abstract: Systems with exhaust gas recirculation and two-stage charge air compression include an internal combustion engine having an exhaust manifold and an intake manifold; a turbocharger with an exhaust gas turbine and a compressor, each having an inlet and an outlet; a first exhaust gas conduit connecting the exhaust gas turbine inlet with the exhaust manifold; a charge air conduit connecting the turbocharger compressor outlet with the intake manifold; a motor-driven compressor having an inlet and an outlet, with the outlet connected with the inlet of the turbocharger compressor; a two-input proportioning gas control valve having a first inlet open to atmosphere and a second inlet connected with an EGR conduit connected with the flow of exhaust gas from the internal combustion engine, and an outlet to deliver a mixture of air and exhaust gas to the inlet of the motor-driven charge air compressor; and a control operating the two-input proportioning gas control valve to mix in controlled proportions, air from atmosph
    Type: Grant
    Filed: July 3, 1997
    Date of Patent: June 30, 1998
    Assignee: Turbodyne Systems, Inc.
    Inventor: Magdi K. Khair
  • Patent number: 5605045
    Abstract: An exhaust gas-driven turbine drives a compressor to charge an internal combustion engine. An integral motor is positioned on the connecting shaft to add power to the turbocharging shaft, especially at low exhaust gas volume. Cooling for this motor includes circulation of engine oil therearound and may include insulation to limit heat inflow from the turbine and may include air flow through the motor to carry away heat inflow from the turbine.
    Type: Grant
    Filed: September 18, 1995
    Date of Patent: February 25, 1997
    Assignee: Turbodyne Systems, Inc.
    Inventors: Edward M. Halimi, Ralph P. Maloof, William E. Woollenweber