Multi-functional AC/DC converter

• US 6,577,106 B2
• Filed: 10/19/2001
• Issued: 06/10/2003
• Est. Priority Date: 11/30/2000
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Lazarovich, David
• Primary Examiner(s): Tso, Edward H.
• Application Number:
  US10/085,788
• Publication Number:
  US 20020126518A1
• Time in Patent Office: 599 Days
• Field of Search: 320/106, 320/110, 320/125, 320/128, 320/137, 320/160, 320/150, 320/153
• US Class Current: 320/137
• CPC Class Codes: H02J 2310/44 for aircrafts
• CPC Class Codes: H02J 7/007 Regulation of charging or discharging current or voltage
• CPC Class Codes: H02J 7/04 Regulation of charging current or voltage

Abstract

A multi-functional AC to DC converter (100) controls AC to DC conversion as a function of at least one characteristic of a battery (200) connected to a DC power bus (300), such that the voltage output by the converter (100) to the DC power bus (300) is varied to efficiently charge the battery (200). In one implementation of the present invention, a multi-functional AC to DC converter (100) also adjusts the voltage output to the DC power bus based on a starting condition of an auxiliary power unit (400) so that the supplied voltage is suitable for starting the APU (400). The present invention is suitable for implementation in an aircraft power system to maintain the voltage output within the compliance range of the DC power bus (e.g., between 27.5 and 29 Vdc) while adjusting the output voltage to efficiently charge a battery (200) connected to the bus (300) and/or start an APU (400) connected to the bus (300).

Claims

1. A multi-functional apparatus for regulating voltage supplied to electrical loads and delivered to a rechargeable battery via a DC power bus, comprising:

an AC to DC converter receiving an AC supply voltage, converting said AC supply voltage to a regulated DC voltage, and outputting said regulated DC voltage to said DC power bus; and

a power controller controlling conversion performed by said AC to DC converter as a function of a characteristic of said battery.

2. The apparatus according to claim 1, wherein said DC power bus is a power bus of an aerospace power system with electrical load connected thereto.

3. The apparatus according to claim 1, wherein said power controller controls conversion performed by said AC to DC converter so that said AC to DC converter outputs a DC voltage that maintains a constant current flow into said battery from said DC bus during a first control mode.

4. The apparatus according to claim 3, wherein said power controller operates in said first control mode when said battery is in a low charge state.

5. The apparatus according to claim 1, wherein said power controller controls conversion performed by said AC to DC converter so that said AC to DC converter outputs a first constant DC voltage during a second control mode.

6. The apparatus according to claim 5, wherein said power controller operates in said second control mode when said regulated DC voltage output by said AC to DC converter reaches a threshold level.

7. The apparatus according to claim 1, wherein said power controller controls conversion performed by said AC to DC converter so that said AC to DC converter outputs a second constant DC voltage, which is lower than said first constant DC voltage, during a third control mode.

8. The apparatus according to claim 7, wherein said power controller operates in said third control mode when current drawn by said battery drops below a threshold level.

9. The apparatus according to claim 7, wherein said third control mode is a constant potential trickle charge mode.

10. The apparatus according to claim 1, wherein said regulated DC voltage is maintained within a compliance range of said DC power bus.

11. The apparatus according to claim 1, wherein said AC to DC converter includes:

a first AC to DC conversion stage converting said AC supply voltage to an intermediate DC voltage;

a switching module converting said intermediate DC voltage to an intermediate AC voltage;

an output transformer transforming said intermediate AC voltage to a step-down AC voltage; and

a rectifier converting said step-down AC voltage to a DC voltage.

12. The apparatus according to claim 11, wherein said AC to DC converter further includes:

a filter filtering the DC voltage generated by said rectifier and outputting said regulated DC voltage to said DC power bus.

13. The apparatus according to claim 11, wherein said power controller generates a switch gating signal and outputs said switch gating signal to said switching module to control a root-mean-square level of said intermediate AC voltage.

14. The apparatus according to claim 13, wherein said switching module is an H-bridge configuration of transistors, each of which receives said switch gating signal.

15. The apparatus according to claim 13, wherein said power controller generates a pulse width modulated switching signal having a pulse width that varies depending on a recharge state of said battery.

16. The apparatus according to claim 15, wherein said power controller varies the pulse width of said pulse width modulated switching signal as a function of load on said DC power bus.

17. The apparatus according to claim 1, wherein said power controller controls conversion performed by said AC to DC converter as a function of temperature of said battery.

18. The apparatus according to claim 1, wherein said AC/DC converter outputs said regulated DC voltage to an auxiliary power unit via said DC power bus.

19. The apparatus according to claim 18, wherein said power controller further controls conversion performed by said AC to DC converter as a function of current drawn by said auxiliary power unit.

20. The apparatus according to claim 1, wherein said characteristic is the recharge state of said battery.

21. The apparatus according to claim 1, wherein said power controller controls conversion performed by said AC to DC converter as a function of a recharge characteristic of said battery, a temperature characteristic of said battery, and load on said DC power bus.

22. An aerospace DC power supply system, said aerospace DC power supply system utilizing a single AC to DC converter to supply a load connected to a DC power bus and to charge a battery continuously connected to said DC power bus in accordance with a multi-stage battery charging control scheme, wherein said system further utilizes said single AC to DC converter to start an auxiliary power unit connected to said DC power bus.

23. An aerospace DC power supply system, said aerospace DC power supply system utilizing a single AC to DC converter to supply a load connected to a DC power bus and to charge a battery continuously connected to said DC power bus in accordance with a multi-stage battery charging control scheme, wherein said AC to DC converter achieves temperature compensated charging of said battery.