MULTI-STAGE POWER CONVERSION AND DISTRIBUTION

• US 20080030077A1
• Filed: 09/05/2006
• Published: 02/07/2008
• Est. Priority Date: 06/29/2006
• Status: Abandoned Application

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Tiry, Dennis M., Bier, Nelson M., Smith, Grant L.
• Application Number:
  US11/470,035
• Publication Number:
  US 20080030077A1
• Time in Patent Office: Days
• US Class Current: 307/43
• CPC Class Codes: B64G 1/428 Power distribution and management
• CPC Class Codes: H02M 1/007 Plural converter units in cascade push-pull DC/DC converters with pre-regulator H02M3/3374; DC-AC converters following a DC-DC stage including a high frequency transformer H02M7/4807; DC-AC converters following a DC-DC conversion stage generating periodically varying voltages H02M7/4826
• CPC Class Codes: H02M 1/008 Plural converter units for generating at two or more independent and non-parallel outputs, e.g. systems with plural point of load switching regulators

Abstract

A multi-stage power converter is disclosed. The multi-stage power converter includes at least one power source and at least one intermediate down-converter, the at least one intermediate down-converter configured to down convert a voltage output from the at least one power source to an intermediate voltage. The multi-stage power converter further includes one or more point of load converters configured to further convert the intermediate voltage to one or more component voltages applicable to one or more sets of processing components.

Claims

1. A multi-stage power converter, comprising:

at least one power source;

at least one intermediate down-converter configured to down convert a voltage output from the at least one power source to an intermediate voltage; and

one or more point of load converters configured to further convert the intermediate voltage to one or more component voltages applicable to one or more sets of processing components.

2. The converter of claim 1, wherein the at least one power source comprises a primary power source.

3. The converter of claim 1, wherein the at least one intermediate down-converter further comprises at least one intermediate voltage bus.

4. The converter of claim 3, wherein the at least one intermediate voltage bus further comprises at least one power switch between the at least one intermediate down-converter and the one or more point of load converters.

5. The converter of claim 1, wherein the one or more point of load converters and the one or more sets of processing components are mounted on a single processing assembly.

6. The converter of claim 5, wherein the single processing assembly is a radiation-hardened processing assembly.

7. A method for supplying power to one or more radiation-hardened electronic computing elements, the method comprising:

at a first stage, converting at least one input voltage to an intermediate voltage;

distributing the intermediate voltage to one or more point of load converters; and

at a second stage, converting the intermediate voltage into a plurality of voltages applicable for each of the one or more radiation-hardened electronic computing elements.

8. The method of claim 7, wherein converting the at least one input voltage further comprises maintaining a power distribution efficiency level of at least 90%.

9. The method of claim 7, wherein distributing the intermediate voltage further comprises supplying the intermediate voltage to the one or more point of load converters on at least one intermediate voltage bus.

10. The method of claim 7, wherein distributing the intermediate voltage further comprises switching between at least one primary power source and at least one secondary (redundant) power source.

11. The method of claim 7, wherein converting the intermediate voltage further comprises:

regulating the plurality of voltages for each of the one or more radiation-hardened electronic computing elements; and

reducing current levels on the plurality of voltages by at least a factor of 5.

12. A system, comprising:

at least one space device; and

a payload processing subsystem within the at least one space device, the payload processing subsystem including;

one or more power sources,

one or more payload processing assemblies within the payload processing subsystem, and

at least one multi-stage power converter coupled to the one or more power sources, the at least one multi-stage power converter operating at an efficiency level above 90%.

13. The system of claim 12, wherein the at least one space device comprises a radiation-hardened space device.

14. The system of claim 12, wherein the payload processing subsystem further comprises at least one intermediate power bus coupled to the at least one multi-stage power converter.

15. The system of claim 12, wherein the payload processing subsystem further comprises:

at least one primary power supply;

at least one secondary (redundant) power supply;

at least one primary power bus coupled to the at least one primary power supply; and

at least one secondary power bus coupled to the at least one secondary (redundant) power supply.

16. The system of claim 12, wherein the one or more payload processing assemblies further comprise:

at least one set of payload processing components; and

one or more point of load converters coupled to the at least one set of payload processing components.

17. The system of claim 16, wherein each of the one or more point of load converters down converts an intermediate voltage to one or more component voltages applicable for the at least one set of payload processing components.

18. The system of claim 16, wherein each of the one or more point of load converters and the at least one set of payload processing components are mounted on a single printed wiring board assembly.

19. The system of claim 16, wherein the one or more payload processing assemblies further include at least one set of power switches between the at least one multi-stage power converter and the one or more point of load converters.

20. The system of claim 19, wherein the at least one set of power switches comprise a set of single n-channel power MOSFETs.