Electrical power distribution system with localized distribution conversion units

Patent metadata

Field	Value
Publication number	US-2016122033-A1
Application number	US-201414528698-A
Country	US
Kind code	A1
Filing date	Oct 30, 2014
Priority date	Oct 30, 2014
Publication date	May 5, 2016
Grant date	—

Abstract

An electrical power distribution system for converting and distributing electrical power to local loads within a vehicle is disclosed. The electrical power distribution system includes at least one generator providing high voltage AC (HVAC) power, a primary power panel for receiving the HVAC power from the generator, and a plurality of distribution conversion units located throughout the vehicle. The plurality of distribution conversion units convert the HVAC power from the primary power panel into medium voltage AC (MVAC) power and low voltage DC (LVDC) power for consumption by the local loads within the vehicle. The electrical power distribution system also includes a plurality of HVAC distribution feeder lines. Each HVAC distribution feeder line connects the primary power panel to one of the plurality of distribution conversion units.

First claim

What is claimed is:

1 . An electrical power distribution system for converting and distributing electrical power to local loads within a vehicle, comprising:
at least one generator providing high voltage AC (HVAC) power; a primary power panel for receiving the HVAC power from the generator; a plurality of distribution conversion units located throughout the vehicle, wherein the plurality of distribution conversion units convert the HVAC power from the primary power panel into medium voltage AC (MVAC) power and low voltage DC (LVDC) power for consumption by the local loads within the vehicle; and a plurality of HVAC distribution feeder lines, wherein each HVAC distribution feeder line connects the primary power panel to one of the plurality of distribution conversion units.

2 . The electrical power distribution system of claim 1 , comprising a plurality of remote power distribution units (RPDUs) located throughout the vehicle to distribute both the MVAC power and the LVDC power to the local loads.

3 . The electrical power distribution system of claim 2 , comprising a plurality of MVAC load feeders connecting a respective one of the plurality of distribution conversion units with a respective one of the plurality of RPDUs.

4 . The electrical power distribution system of claim 2 , comprising a plurality of LVDC load feeders connecting a respective one of the plurality of distribution conversion units with a respective one of the plurality of RPDUs.

5 . The electrical power distribution system of claim 1 , wherein the HVAC power is a voltage value above about 150 VAC.

6 . The electrical power distribution system of claim 1 , wherein the MVAC power ranges from over about 80 VAC to under about 150 VAC.

7 . The electrical power distribution system of claim 1 , wherein the LVDC power is under about 70 VDC.

8 . The electrical power distribution system of claim 1 , comprising at least one auxiliary power unit (APU) and an APU generator driven by the APU.

9 . The electrical power distribution system of claim 1 , comprising an energy storage device for providing power to critical DC loads within the vehicle if there is a total loss of generator power.

10 . An electrical power distribution system for converting and distributing electrical power to localized loads within an aircraft, comprising:
a plurality of main engines; a plurality of generators providing high voltage AC (HVAC) power, wherein each of the plurality of generators is driven by one of the plurality of main engines; a plurality of primary power panels, wherein each primary power panel receives the HVAC power from a respective one of the plurality of generators; a plurality of distribution conversion units located throughout the aircraft, wherein the plurality of distribution conversion units convert the HVAC power received from one of the plurality of primary power panels into medium voltage AC (MVAC) power and low voltage DC (LVDC) power for consumption by local loads within the aircraft; and a plurality of HVAC distribution feeder lines, wherein each HVAC distribution feeder line connects the one of the plurality of primary power panels to one of the plurality of distribution conversion units.

11 . The electrical power distribution system of claim 10 , comprising a plurality of remote power distribution units (RPDUs) located throughout the aircraft to distribute both the MVAC power and the LVDC power to the local loads.

12 . The electrical power distribution system of claim 11 , comprising a plurality of MVAC load feeders connecting a respective one of the plurality of distribution conversion units with a respective one of the plurality of RPDUs.

13 . The electrical power distribution system of claim 11 , comprising a plurality of LVDC load feeders connecting a respective one of the plurality of distribution conversion units with a respective one of the plurality of RPDUs.

14 . The electrical power distribution system of claim 10 , wherein the HVAC power is a voltage value above about 150 VAC.

15 . The electrical power distribution system of claim 10 , wherein the MVAC power ranges from over about 80 VAC to under about 150 VAC.

16 . The electrical power distribution system of claim 10 , wherein the LVDC power is under about 70 VDC.

17 . The electrical power distribution system of claim 10 , comprising at least one auxiliary power unit (APU) and an APU generator driven by the APU within the aircraft.

18 . A method of converting and distributing electrical power to localized loads within an aircraft, comprising:
creating high voltage AC (HVAC) power by a plurality of generators, wherein each of the plurality of generators is driven by one of a plurality of main engines; sending the HVAC power from the plurality of generators to respective primary power panels; sending the HVAC power from the respective primary power panels to a plurality of distribution conversion units located throughout the aircraft; and converting the HVAC power from the primary power panel into medium voltage AC (MVAC) power and low voltage DC (LVDC) power for consumption by local loads within the aircraft by the plurality of distribution conversion units.

19 . The method as recited in claim 18 , comprising distributing both the MVAC power and the LVDC power to the local loads by a plurality of remote power distribution units (RPDUs) located throughout the aircraft.

20 . The method as recited in claim 18 , wherein the HVAC power is any voltage value above about 150 VAC, the MVAC power ranges from under about 150 VAC to over about 80 VAC, and the LVDC power is under about 70 VDC.

Assignees

• Boeing Co

Inventors

• Liffring Mark Eugene
• Karimi Kamiar J

Classifications

• H02J4/00 Primary

  Circuit arrangements for mains or distribution networks not specified as AC or DC; Circuit arrangements for mains or distribution networks combining AC and DC sections or sub-networks (arrangements using intermediate DC-AC-DC conversion H02J1/002; arrangements using high-voltage DC [HVDC] links H02J3/36) · CPC title

• B64D41/00 Primary

  Power installations for auxiliary purposes · CPC title

• B64D2221/00

  Electric power distribution systems onboard aircraft · CPC title

• H02J3/00

  Circuit arrangements for AC mains or AC distribution networks · CPC title

• H02J2105/32

  for aircrafts · CPC title