Virtual electronic circuit breaker
View Patent ↗A virtual electronic circuit breaker having an electrical relay and a control circuit, the control circuit including a load and wire protection (“OC”) detection unit, a microprocessor and a driver. The OC detection unit is configured to monitor a power flow and the electrical relay is effective to control it. The driver is effective to cause the relay to stop the power flow upon receipt of a deactivation command. The OC detection unit is effective to cause the driver to receive a deactivation command if the OC detection unit senses that a short circuit condition or an overload condition exists. The microprocessor of the control unit is configured so as to be capable of, at least, receiving input from the OC detection unit and sending output to the driver.
1. A circuit breaker, comprising:
an electrical relay effective to control an amount of power flow;
a control circuit, the control circuit having an OC detection unit, a microprocessor, a driver;
said driver effective to cause said relay to stop said power flow upon receipt by the driver of a deactivation command;
said OC detection unit configured to monitor said power flow; said OC detection unit being connected to the driver and being effective to cause said driver to receive a deactivation command if said OC detection unit senses that an overload condition exists; and
said microprocessor configured to be capable of receiving input from said OC detection unit and sending output to said driver; and,
a redundant source of power connected to the electrical relay and to the control circuit effective to allow the control circuit and the relay to operate while only receiving power from said redundant source of power;
wherein said circuit breaker is located on an aircraft and said microprocessor is adapted to receive at least one of “reset,” “collar,” “on,” or “off” commands from a control panel in said aircraft; the circuit breaker is characterized in that the OC detection unit is directly connected to the driver.
2. The circuit breaker of claim 1 wherein said power flow is selected from the group consisting of 1-phase alternating current (AC), 3-phase AC and direct current (DC).
3. The circuit breaker of claim 2 wherein said power flow is 1-phase AC.
4. The circuit breaker of claim 1 wherein said microprocessor is effective to send to outside said control circuit an amount of indication and status information.
5. The circuit breaker of claim 1 wherein said microprocessor is effective to cause said driver to receive a deactivation command upon receipt by the microprocessor of an “off” command.
6. The circuit breaker of claim 1 wherein said microprocessor is effective to communicate with a programming and test bus.
7. The circuit breaker of claim 1 further comprising a ground fault interruption (GFI) detection unit, wherein said GFI detection unit is integrated with said control circuit.
8. The circuit breaker of claim 7 wherein said GFI detection unit is effective to, when the GFI detection unit senses that a ground fault condition has occurred, communicate to said microprocessor that a ground fault condition has occurred.
9. An electrical system for an aircraft, comprising:
a source of limited power;
a load, drawing an amount of power flow from said source of limited power; and
a circuit breaker in accordance with claim 1 .
10. The electrical system of claim 9 , wherein said source of limited power is an aircraft engine.
11. The electrical system of claim 10 , wherein said load is the actuator mechanism of an aircraft control surface.
12. A method of protecting an electronic circuit, comprising the steps of:
providing a power flow;
providing a circuit breaker in accordance with claim 1 ;
said microprocessor receiving input from said OC detection unit and sending output to said driver,
monitoring said power flow utilizing said OC detection unit; and
causing said driver to receive from said OC detection unit a deactivation command when an overload condition is sensed.