IP Library Granted Patent US 8,238,130
Granted Patent B2
US 8,238,130 · App. 12/241,683 · Granted Aug 7, 2012

Low-mass, bi-directional DC-AC interface unit

Assignee: General Electric Company
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Quick Facts
Patent No.
US 8,238,130
App. No.
12/241,683
Granted
Aug 7, 2012
Kind
B2
Abstract

A DC-AC converter includes a DC-DC converter providing bi-directional conversion between a first DC power signal and a second DC power signal, the first DC power signal being on a first DC bus and the second DC power signal being on a second DC bus. The DC-AC converter also includes an inverter providing bi-directional DC-AC conversion between a third DC power signal and a first AC power signals the third DC power signal being on the second DC bus and the first AC power signal being on a first AC bus.

Claims (28)

1. A bidirectional DC-AC converter, comprising:

a DC-DC converter providing bi-directional conversion between a first DC power signal and a second DC power signal, the first DC power signal being on a first DC bus and the second DC power signal being on a second DC bus; and

an inverter providing bi-directional DC-AC conversion between a third DC power signal and a first AC power signal, the third DC power signal being on a third DC bus and the first AC power signal being on a first AC bus,

wherein the third DC power signal comprises the first DC power signal biased by the second DC power signal; and

wherein a voltage magnitude of the second DC power signal is inverted with respect to a voltage magnitude of the first DC power signal.

2. The DC-AC converter of claim 1 , further comprising:

an AC filter connected to the first AC bus to filter the first AC power signal.

3. The DC-AC converter of claim 1 , wherein the bi-directional DC-DC circuit comprises a Ćuk converter.

4. The DC-AC converter of claim 1 , wherein the bi-directional DC-DC circuit comprises a buck-boost converter.

5. The DC-AC converter of claim 1 , wherein a rail of the first DC bus is connected to a first rail of the third DC bus and a rail of the second DC bus is connected to a second rail of the third DC bus.

6. The DC-AC converter of claim 5 , wherein a voltage across the third DC bus is between 270 to 540 VDC.

7. The DC-AC converter of claim 1 , further comprising:

a DC filter connected to the first DC bus to obtain the first DC power signal.

8. The DC-AC converter of claim 5 , wherein the first DC power signal is a uni-polar DC signal and the second DC power signal is a bi-polar DC signal.

9. A power conditioning unit for an aircraft, comprising:

a DC-DC converter providing bi-directional conversion between a first DC power signal and a second DC power signal, the first DC power signal being on a first DC bus and the second DC power signal being on a second DC bus;

an inverter providing bi-directional DC-AC conversion between a third DC power signal and a first AC power signal, the third DC power signal being on a third DC bus and the first AC power signal being on a first AC bus; and

a second inverter providing bi-directional AC-DC conversion between a second AC bus and the first DC power signal, the second AC power signal being on a second AC bus;

wherein the third DC power signal comprises the first DC power signal biased by the second DC power signal; and

wherein a voltage magnitude of the second DC power signal is inverted with respect to a voltage magnitude of the first DC power signal.

10. The power conditioning unit for an aircraft of claim 9 , wherein the first DC bus is uni-polar.

11. The power conditioning unit for an aircraft of claim 9 , wherein the second DC bus is bi-polar.

12. The power conditioning unit for an aircraft of claim 9 , wherein the bi-directional DC-DC circuit is a Ćuk converter.

13. The power conditioning unit for an aircraft of claim 9 , wherein the bi-directional DC-DC circuit is a buck-boost converter.

14. The power conditioning unit for an aircraft of claim 9 , wherein a rail of the first DC bus is connected to a first rail of the third DC bus and a rail of the second DC bus is connected to a second rail of the third DC bus.

15. The power conditioning unit for an aircraft of claim 14 , wherein a voltage across the third DC bus is between 270 to 540 VDC.

16. The power conditioning unit for an aircraft of claim 9 , wherein the first DC power signal is a uni-polar DC signal and the second DC power signal is a bi-polar DC signal.

17. The DC-AC converter of claim 1 , wherein the first DC power signal is biased positively, negatively, or neutrally.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 30, 2008
From: WIEGMAN, HERMAN LUCAS NORBERT; CARLSON, WILLIAM EUGENE; PEROZEK, PAUL MICHAEL
To: GENERAL ELECTRIC COMPANY
Reel/Frame 021608/0535 →
Continuity (1)
Related Publication 20100080030A1 · Apr 1, 2010