Stable electrical power system with regulated transformer rectifier unit

Patent metadata

Field	Value
Publication number	US-9762064-B2
Application number	US-201414553520-A
Country	US
Kind code	B2
Filing date	Nov 25, 2014
Priority date	Nov 25, 2014
Publication date	Sep 12, 2017
Grant date	Sep 12, 2017

Abstract

A method and apparatus for providing power stably for direct current loads. A regulated transformer rectifier unit is controlled to provide regulated direct current power for the direct current loads at an output of the regulated transformer rectifier unit from alternating current power provided by an alternating current power source to an input of the regulated transformer rectifier unit. The direct current loads comprise passive direct current loads and active direct current loads comprising active switching power supplies. The direct current loads have at least one of constant power characteristics, resistive power characteristics, inductive power characteristics, and capacitive power characteristics. A source impedance at the output of the regulated transformer rectifier unit is determined based on an aggregate load impedance of the direct current loads and stability criterion.

First claim

What is claimed is:

1. A method of providing power stably for direct current loads, comprising:
controlling a regulated transformer rectifier unit to provide regulated direct current power for the direct current loads at an output of the regulated transformer rectifier unit from alternating current power provided by an alternating current power source to an input of the regulated transformer rectifier unit;
wherein the direct current loads comprise passive direct current loads and active direct current loads comprising active switching power supplies, and have at least one of constant power characteristics, resistive power characteristics, inductive power characteristics, and capacitive power characteristics; and
wherein the regulated transformer rectifier unit has a source impedance at the output determined based on an aggregate load impedance of the direct current loads and stability criterion.

2. The method of claim 1 , wherein the source impedance is within magnitude limits and phase limits determined based on the aggregate load impedance and the stability criterion.

3. The method of claim 1 , wherein the stability criterion comprise Nyquist criterion.

4. The method of claim 1 , wherein the alternating current power provided by the alternating current power source comprises variable frequency alternating current power.

5. The method of claim 4 , wherein a frequency of the variable frequency alternating current power varies from between 350 Hz to 1000 Hz.

6. The method of claim 1 , wherein the alternating current power comprises 100 volts root mean square to 300 volts root mean square and the regulated direct current power comprises a one of 18 volts to 40 volts and 38 volts to 60 volts.

7. The method of claim 1 , wherein:
the regulated transformer rectifier unit comprises a plurality of converter modules connected in parallel between the input and the output, wherein each converter module comprises a transformer rectifier unit; and
controlling the regulated transformer rectifier unit comprises controlling the plurality of converter modules to provide the regulated direct current power at the output.

8. The method of claim 1 , wherein the regulated transformer rectifier unit is on an aircraft and controlling the regulated transformer rectifier unit comprises controlling the regulated transformer rectifier unit to provide regulated direct current power for the direct current loads on the aircraft.

9. A method of providing power stably for direct current loads, comprising:
identifying aggregate load impedance for a plurality of active direct current loads comprising active switching power supplies and having constant power characteristics;
determining a source impedance for an output of a regulated transformer rectifier unit configured to provide regulated direct current power for the direct current loads at the output from alternating current power provided to an input of the regulated transformer rectifier unit, wherein the source impedance is determined based on the aggregate load impedance and stability criterion; and
implementing the regulated transformer rectifier unit having the source impedance in hardware.

10. The method of claim 9 , wherein identifying the aggregate load impedance comprises simulating the plurality of active direct current loads under a plurality of different steady state and transient operating conditions.

11. The method of claim 10 further comprising:
verifying the aggregate load impedance by hardware testing.

12. The method of claim 9 , wherein determining the source impedance comprises determining magnitude limits for the source impedance and phase limits for the source impedance based on the aggregate load impedance and the stability criterion.

13. The method of claim 9 , wherein the stability criterion comprise Nyquist criterion.

14. The method of claim 9 , wherein determining the source impedance further comprises simulating the regulated transformer rectifier unit for a plurality of different frequencies of the alternating current power and a plurality of different direct current loads.

15. The method of claim 9 further comprising:
controlling the regulated transformer rectifier unit on an aircraft to provide the regulated direct current power for the direct current loads on the aircraft.

16. An apparatus, comprising:
a regulated transformer rectifier unit configured to provide regulated direct current power for direct current loads at an output of the regulated transformer rectifier unit from alternating current power provided by an alternating current power source to an input of the regulated transformer rectifier unit;
wherein the direct current loads comprise passive direct current loads and active direct current loads comprising active switching power supplies, and have at least one of constant power characteristics, resistive power characteristics, inductive power characteristics, and capacitive power characteristics; and
wherein the regulated transformer rectifier unit has a source impedance at the output determined based on an aggregate load impedance of the direct current loads and stability criterion.

17. The apparatus of claim 16 , wherein the source impedance is within magnitude limits and phase limits determined based on the aggregate load impedance and the stability criterion.

18. The apparatus of claim 16 , wherein the stability criterion comprise Nyquist criterion.

19. The apparatus of claim 16 , wherein the regulated transformer rectifier unit comprises:
a plurality of converter modules connected in parallel between the input and the output, wherein each converter module comprises a transformer rectifier unit; and
a controller configured to control the plurality of converter modules to provide the regulated direct current power at the output.

20. The apparatus of claim 16 , wherein the regulated transformer rectifier unit is on an aircraft and the regulated transformer rectifier unit is controlled to provide regulated direct current power for the direct current loads on the aircraft.

Assignees

• Boeing Co

Inventors

• Karimi Kamiar J
• Liffring Mark Eugene
• Matheson Evelyn Marie
• Aikens Sheverria Antony
• Solodovnik Eugene V
• Barekatein Mehdy

Classifications

• G06F30/36

  Circuit design at the analogue level · CPC title

• H02J1/14

  Balancing load and power generation in DC networks · CPC title

• G06F2119/06

  Power analysis or power optimisation · CPC title

• H02J1/08

  Three-wire DC power distribution systems; Systems having more than three wires · CPC title

• H02J1/102

  being switching converters (H02J1/108, H02J1/12 take precedence) · CPC title