Turbocharger control system

• US 4,174,617 A
• Filed: 08/08/1977
• Issued: 11/20/1979
• Est. Priority Date: 08/08/1977
• Status: Expired due to Term

• Current Assignee: Mir Javid Jalali-Karchay
• Original Assignee: Mir Javid Jalali-Karchay
• Inventors: Jalali-Karchay, Mir Javid
• Primary Examiner(s): Croyle, Carlton R.
• Assistant Examiner(s): Koczo, Jr., Michael
• Application Number:
  US05/822,394
• Time in Patent Office: 834 Days
• Field of Search: 60/600, 60/602, 60/603, 60/605, 60/611, 318/293, 318/295, 318/481
• US Class Current: 60/602
• CPC Class Codes: F02B 37/186 Arrangements of actuators or linkage for bypass valves
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

By comparing with the magnitude of a sea-level reference parameter, an electrical parameter in a pressure-temperature sensor or sensors coupled to the air induction system of an internal combustion engine, particularly a turbocharged engine, a control signal may be derived which will automatically adjust the flow of exhaust gas to the turbocharger and will automatically result in constant engine power from sea level to a critical altitude.

Claims

1. A turbocharger control system for an internal combustion engine having a throttle, an intake manifold and an exhaust manifold, including:

a pressure sensor coupled to said intake manifold and responsive to changes in the air pressure therein to produce a change in a first electrical parameter;

variable electrical means coupled mechanically to said throttle and responsive to the setting of said throttle to set a second electrical parameter of the same type as first electrical parameter;

a comparator circuit including balanced means for comparing the respective total magnitudes of said first and second parameters and trigger means responsive to any imbalance between said total magnitudes of said first and second parameters for producing a correctional output voltage having a polarity indicative of the relative sizes of said total magnitudes of said first and second parameters, respectively;

a gas-driven turbine;

an exhaust gas duct adapted to be coupled at one end to said exhaust manifold and at the other end to said turbine;

an air duct coupled to said intake manifold;

an air compressor;

coupling means for mechanically coupling said air compressor to said turbine, said air compressor being pneumatically coupled to said air duct for the flow of air therebetween;

a by-pass duct coupled to said exhaust-gas duct between said exhaust manifold and said turbine for by-passing exhaust gas around said turbine;

a wastegate adjustably mounted in said by-pass duct for controlling the extent of the by-passing of exhaust gas around said turbine;

a reversible electrical motor having electrical terminals;

driving means coupling said motor to said wastegate; and

,

electrical means coupling said terminals of motor to said comparator circuit for operating said motor, in response to said correctional output voltage, in such a direction that said wastegate is positioned to cause the restoration of the balance between the total magnitudes of said first and second parameters, respectively.

2. A system according to claim 1 which includes, in addition, a temperature sensor coupled to said intake manifold and responsive to changes in air temperature therein to produce a change in a third electrical parameter of the same type as said first parameter;

a comparator circuit including balanced means for comparing the total magnitude of said first and third parameters with the magnitude of said second parameter.

3. A system according to claim 2 in which said pressure and temperature sensors are combined in a unitary device.

4. A system according to claim 3 in which said unitary device is an aneroid chamber containing gas at a predetermined pressure for a given ambient temperature.

5. A system according to claim 2 in which said temperature sensor is a thermistor.

6. A system according to claim 2 in which said first, second and third electrical parameters are electrical resistance.

7. A system according to claim 1 in which said trigger means includes complementary transistors connected in Schmitt configuration.

8. A system according to claim 1 in which said balanced means includes a balanced d.c. power supply having positive, negative and common terminals and positive and negative buses connected to said positive and negative terminals, said first and second parameters, respectively, appearing in series electrical connection between said positive and negative buses.

9. A system according to claim 1 in which said electrical means includes a pair of normally open, single-pole, double-throw relays.

10. A system according to claim 1 in which said coupling means includes a worm gear-worm combination.