Integrated control system and method for controlling mode, synchronization, power factor, and utility outage ride-through for micropower generation systems

• US 6,072,302 A
• Filed: 08/26/1998
• Issued: 06/06/2000
• Est. Priority Date: 08/26/1998
• Status: Expired due to Term

• Current Assignee: Perfect Galaxy International Limited
• Original Assignee: Northrop Grumman Corporation
• Inventors: Hall, William B., Matty, Thomas C., Underwood, Thomas C.
• Primary Examiner(s): Ponomarenko, Nicholas
• Application Number:
  US09/140,391
• Time in Patent Office: 650 Days
• Field of Search: 290/1 A, 290/2, 290/7, 290/52, 322/17, 322/25, 322/28, 322/44, 322/45
• US Class Current: 322/17
• CPC Class Codes: H02J 3/38 Arrangements for parallely feeding a single network by two or more generators, converters or transformers
• CPC Class Codes: H02J 3/40 Synchronising a generator for connection to a network or to another generator

Abstract

An integrated system for comprehensive control of an electric power generation system utilizes state machine control having particularly defined control states and permitted control state transitions. In this way, accurate, dependable and safe control of the electric power generation system is provided. Several of these control states may be utilized in conjunction with a utility outage ride-through technique that compensates for a utility outage by predictably controlling the system to bring the system off-line and to bring the system back on-line when the utility returns. Furthermore, a line synchronization technique synchronizes the generated power with the power on the grid when coming back on-line. The line synchronization technique limits the rate of synchronization to permit undesired transient voltages. The line synchronization technique operates in either a stand-alone mode wherein the line frequency is synthesized or in a connected mode which sensed the grid frequency and synchronizes the generated power to this senses grid frequency. The system also includes power factor control via the line synchronization technique or via an alternative power factor control technique. The result is an integrated system providing a high degree of control for an electric power generation system.

Claims

1. A power generation control system having a plurality of control states for electric power transformation having a full wave rectifier connected to a generator, a DC bus connected to the output of the full wave rectifier, an inverter connected to the DC bus, an inductor unit connected to the output of the inverter, a first contactor unit connecting and disconnecting the inductor unit to and from a grid, and a precharge circuit connected to the DC bus;

the power generation control system comprising;

an initialization state for initializing the state machine;

a first neutral state for idling the state machine while monitoring commands and system parameters;

a pre-charge state for enabling and monitoring the precharge circuit to pre-charge the DC bus to a pre-charge DC voltage;

a second neutral state for disabling the pre-charge circuit and closing the first contactor;

an engine start state for verifying DC link voltage, sending a speed command to the start inverter unit, enabling the start inverter, updating the speed command being sent to the start inverter unit, and determining successful engine start;

a power on-line state for enabling a current mode in said inverter and controlling the inverter to deliver power at a level determined by a power level command;

a power off-line state for opening the first contactor, switching the inverter to a voltage mode, and setting the power level command to a nominal power level;

a shutdown state for disabling the inverter, opening the first contactor after waiting for a cool-down time period, and reinitializing the state machine,

a state controller for controlling the following permitted transitions between said control states;

said initialization state →

said first neutral state ←

→

said pre-charge state →

said second neutral state ←

→

said start engine state ←

→

said power on-line state →

said power off-line state →

said shutdown state.

2. The power generation control system according to claim 1, further comprising:

a third neutral state for receiving a command including the power level command and a shutdown command;

said state controller permitting the following additional state transitions;

said start engine state →

said third neutral state ←

→

said power on-line state.

3. The power generation control system according to claim 1, said state controller permitting the following additional state transitions:

neutral state →

pre-charge state upon receiving a pre-charge start command;

precharge state →

neutral state when a pre-charge rate at which said pre-charge circuit charges the DC bus is not within tolerance values or when the DC bus voltage does not achieve the pre-charge DC voltage.

4. The power generation control system according to claim 1, said state controller permitting the following additional state transitions:

pre-charge state →

start engine state upon successfully achieving the precharge DC voltage on the DC bus and receipt of a start engine command.

5. The power generation control system according to claim 1, said state controller permitting the following additional state transitions:

start engine state →

third neutral state upon receiving a zero power level command,

third neutral state →

power on-line state upon successful engine start and receiving a nonzero power level command,

power on-line state →

power off-line state upon receipt of an off-line command or upon a failed diagnostic test or a grid outage,

power off-line →

third neutral state upon successful diagnostic tests for a predetermined time period,

third neutral state →

shutdown upon receiving a shutdown command,

shutdown state →

said first neutral state upon receiving restart command, and

said second neutral →

shutdown state upon a fault condition or shutdown command.

6. The power generation control system according to claim 1, the device further including an emergency stop input,

said state machine controller opening the first contactor unit and switching the control state to said shutdown state upon receipt of an emergency stop signal from the emergency stop input.

7. The power generation control system according to claim 1,

said pre-charge state and said start engine state respectively returning to said first and second neutral states upon failure of a pre-charge cycle and a start engine cycle.

8. The power generation control system according to claim 2,

said power on-line state returning to said third neutral step when the power level command indicates zero requested power.

9. The power generation control system according to claim 1,

wherein said initialization, pre-charge, power on-line, power off-line, and/or shutdown states perform diagnostic tests on the device,

said state controller controlling state transitions based on results of the diagnostic tests.

10. The power generation control system according to claim 1, the device further including an engine for driving said generator, an engine control unit connected to said engine, and a start inverter connected to the DC bus and to said generator, said engine control unit controlling said engine ignition and fuel for the engine, said engine start state controlling said start inverter to drive the generator as a motor to thereby spin the engine and permit starting thereof, said engine start state also sending an engine start command to the engine control unit.

11. The power generation control system according to claim 10,

wherein said initialization, pre-charge, power on-line, power off-line, and/or shutdown states monitor the engine,

said state controller controlling state transitions based on results of the diagnostic tests.

12. The power generation control system according to claim 1,

said pre-charge state also diagnosing the inverter,

said state controller controlling state transitions based on results of the diagnostic tests.

13. The power generation control system according to claim 1,

said engine start state determining successful engine start by monitoring current drawn from the DC bus by the start inverter and engine speed wherein if the current drawn falls below a current limit value and an engine speed exceeds a speed limit then engine start is successful.