IP Library › Granted Patent US 12,199,441
Granted Patent B2
US 12,199,441 · App. 18/171,999 · Granted Jan 14, 2025

Apparatus and method for controlling one or more inverters

Inventors: Madhav Manjrekar (Charlotte, NC); Prithwiraj Roy Chowdhury (Charlotte, NC)
Assignee: THE UNIVERSITY OF NORTH CAROLINA AT CHARLOTTE
H02J3/44H02J3/18H02J2203/20
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Quick Facts
Patent No.
US 12,199,441
App. No.
18/171,999
Granted
Jan 14, 2025
Kind
B2
Abstract

An example apparatus for controlling one or more inverters is provided herein. In some embodiments, the apparatus for controlling one or more inverters may include one or more controllers. In some embodiments, each of the one or more inverters is associated with at least one power source. In some embodiments, each of the one or more controllers may configured to provide droop control, voltage magnitude control, phase control, frequency control and inertia control for an associated inverter of the one or more inverters. In some embodiments, each of the one or more controllers comprises a voltage control loop, a virtual inertia control loop, and a droop control loop enabling the power supplies to sync with a power grid and/or other power supplies when the power supply is disconnected from the power grid and/or other power supplies and/or connected to a power supply to the power grid and/or other power supplies.

Claims (25)

1. An apparatus for controlling one or more inverters, the apparatus comprising:

two or more controllers, wherein

each of the two or more controllers is configured to provide droop control, voltage magnitude control, phase control, frequency control, and inertia control for an associated inverter of the one or more inverters,

each of the two or more controllers comprises a voltage control loop, a virtual inertia control loop, and a droop control loop, and

each of the one or more inverters is associated with at least one power source.

2. The apparatus of claim 1 , wherein the droop control loop is associated with a droop control loop input and a droop control loop output, wherein the droop control loop input comprises an active power and a reactive power and the droop control loop output comprises a point of common coupling reference voltage magnitude and a reference frequency.

3. The apparatus of claim 2 , wherein the droop control loop comprises one or more droop coefficients.

4. The apparatus of claim 1 , wherein the virtual inertia control loop is associated with a virtual inertia control loop input and a virtual inertia control loop output, wherein the virtual inertia control loop input comprises an active power and a reference frequency and the virtual inertia control loop output comprises a phase angle and a point of common coupling reference voltage.

5. The apparatus of claim 4 , wherein the virtual inertia control loop comprises one or more inertia coefficients.

6. The apparatus of claim 1 , wherein the voltage control loop is associated with a voltage control loop input and a voltage control loop output, wherein the voltage control loop input comprises a point of common coupling reference voltage and the voltage control loop output comprises an inverter reference voltage.

7. The apparatus of claim 1 , wherein the at least one power source comprises a direct current power source.

8. The apparatus of claim 1 , wherein a first inverter of the one or more inverters comprises a black-start capability.

9. The apparatus of claim 1 , wherein the one or more inverters comprise two or more inverters.

10. The apparatus of claim 9 , wherein a first inverter of the two or more inverters is in parallel with a second inverter of the two or more inverters.

11. The apparatus of claim 1 , wherein a first controller of the two or more controllers comprises an active and reactive power control circuitry.

12. A method of controlling one or more inverters, each of the one or more inverters associated with at least one power source, the method comprising:

providing, using two or more controllers, droop control, voltage magnitude control, phase control, frequency control, and inertia control for the one or more inverters, wherein the two or more controllers comprise a voltage control loop, a virtual inertia control loop, and a droop control loop.

13. The method of claim 12 , wherein the droop control loop is associated with a droop control loop input and a droop control loop output, wherein the droop control loop input comprises an active power and a reactive power and the droop control loop output comprises a point of common coupling reference voltage magnitude and reference frequency.

14. The method of claim 13 , wherein the droop control loop comprises one or more droop coefficients.

15. The method of claim 12 , wherein the virtual inertia control loop is associated with a virtual inertia control loop input and a virtual inertia control loop output, wherein the virtual inertia control loop input comprises an active power and a reference frequency and the virtual inertia control loop output comprises a phase angle and a point of common coupling reference voltage.

16. The method of claim 15 , wherein the virtual inertia control loop comprises one or more inertia coefficients.

17. The method of claim 12 , wherein the voltage control loop is associated with a voltage control loop input and a voltage control loop output, wherein the voltage control loop input comprises a point of common coupling reference voltage and the voltage control loop output comprises an inverter reference voltage.

18. The method of claim 12 , wherein the at least one power source comprises a direct current power source.

19. The method of claim 12 , wherein the one or more inverters comprise two or more inverters.

20. The method of claim 19 , wherein a first inverter of the two or more inverters is in parallel with a second inverter of the two or more inverters.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 22, 2023
From: MANJREKAR, MADHAV; ROY CHOWDHURY, PRITHWIRAJ
To: THE UNIVERSITY OF NORTH CAROLINA AT CHARLOTTE
Reel/Frame 063714/0419 →
Continuity (2)
Provisional Application 63311750 · Feb 18, 2022
Related Publication 20230283083A1 · Sep 7, 2023
References Cited (1)
US 20240136947A1 · Ayai · 2024 [cited by examiner]