Modular Equipment Center Lightning Threat Reduction Architecture

• US 20150102659A1
• Filed: 10/11/2013
• Published: 04/16/2015
• Est. Priority Date: 10/11/2013
• Status: Active Grant

• Current Assignee: The Boeing Co.
• Original Assignee: The Boeing Co.
• Inventors: Liffring, Mark E., Shander, Mark S., Hasenoehrl, Thomas R., Karimi, Kamiar J., Paterson, John T., Whitney, Marvin J., Woods, Ed
• Granted Patent: US 9,561,867 B2
• Time in Patent Office: Days
• US Class Current: 307/9.1
• CPC Class Codes: B60R 16/03 for supply of electrical power to vehicle subsystems or for circuit arrangements for charging batteries H02J7/00
• CPC Class Codes: B64D 2221/00 Electric power distribution systems onboard aircraft
• CPC Class Codes: B64D 45/02 Lightning protectors; Static dischargers in general H01T
• CPC Class Codes: Y10T 29/49117 Conductor or circuit manufacturing

Abstract

A composite vehicle architecture without a current return network for reducing lightning threats. A plurality of modular equipment centers (MECs) are spatially distributed throughout the vehicle. Equipment loads within the vehicle are each serviced by the nearest MEC. Twisted and shielded electrical conductor pairs provide secondary power to the equipment loads to minimize the amount of wire throughout the aircraft as well as the return currents on the aircraft.

Claims

1. A power distribution system for a vehicle, the system comprising:

a plurality of modular equipment centers (MECs) spatially distributed throughout the composite vehicle, the plurality of MECs distributing power to a plurality of equipment loads throughout the composite vehicle, each of the equipment loads within the composite vehicle serviced by a nearest MEC of the plurality of MECs; and

a plurality of multiple conductor cables, each multiple conductor cable comprising multiple electrical power conductors and a neutral conductor wherein the electrical power conductors and the neutral conductor carry substantially equal but opposite currents, wherein each equipment load is coupled to the nearest MEC with one of the multiple conductor cables such that a length of a loop defined by the electrical power conductors and the neutral conductor of each multiple conductor cable between each MEC and associated equipment loads is minimized.

2. The power distribution system of claim 1 wherein each of the plurality of multiple conductor cables is an electrical conductor pair.

3. The power distribution system of claim 2 wherein each of the electrical conductor pairs are twisted electrical conductor pairs.

4. The power distribution system of claim 1 wherein the vehicle comprises a plurality of vehicle sections coupled together and defining section breaks between adjacent vehicle sections, and wherein the vehicle is otherwise free of a current return network extending across section breaks between multiple vehicle sections of the vehicle.

5. The power distribution system of claim 1 wherein the vehicle comprises a plurality of vehicle sections coupled together defining a section break between adjacent vehicle sections, and wherein the multiple conductor cables do not extend across section breaks.

6. The power distribution system of claim 1 further comprising a transorb on power inputs for the one or more MECs within a respective vehicle section.

7. The power distribution system of claim 1 further comprising a safety ground bus coupled between adjacent MECs.

8. The power distribution system of claim 1 wherein the neutral conductor is routed with a three-phase power feeder.

9. The power distribution system of claim 1 wherein the vehicle comprises a composite fuselage skin.

10. A method of reducing lightning threats to a composite vehicle, the method comprising:

spatially distributing modular equipment centers (MECs) throughout the composite vehicle for distributing electrical power to a plurality of equipment loads throughout the composite vehicle; and

coupling each equipment load to the nearest MEC with a conductor pair, each electrical conductor pair comprising an electrical power conductor and a neutral conductor for carrying equal but opposite currents.

11. The method of claim 10 further comprising twisting an electrical power conductor and a neutral conductor together to form the conductor pair.

12. The method of claim 10 further comprising each MEC distributing secondary power only within each respective vehicle section to service associated equipment loads.

13. A system for minimizing return currents and eliminating the need for a dedicated return path in a composite aircraft, the system comprising:

a plurality of modular equipment centers (MECs) spatially distributed throughout the composite aircraft;

a plurality of equipment loads throughout the composite aircraft; and

a plurality of conductor pairs for distributing power from the MECs to the equipment loads, wherein each equipment load is powered by the nearest MEC to minimize a length of each conductor pair between each equipment load and the nearest MEC.

14. The system of claim 13 wherein the composite aircraft comprises a plurality of vehicle sections coupled together defining a body and a section break between adjacent vehicle sections, and wherein conductor pairs from the MECs to the equipment loads do not cross section breaks.

15. The system of claim 13 wherein the conductor pairs are twisted and shielded electrical conductor pairs.

16. The system of claim 13 wherein a length of a loop defined by a electrical power conductor and a neutral conductor of each conductor pair between each MEC and associated equipment loads is minimized.

17. A system of reducing lightning threats to a composite vehicle, the system comprising:

a plurality of modular equipment centers (MECs) spatially distributed throughout the composite vehicle, the plurality of MECs distributing power to a plurality of equipment loads throughout the composite vehicle, each of the equipment loads within the composite vehicle serviced by the nearest MEC; and

a plurality of twisted and shielded electrical conductor pairs, each twisted and shielded electrical conductor pair comprising an electrical power conductor and a neutral conductor wherein the electrical power conductor and the neutral conductor carry equal but opposite currents, wherein each equipment load is coupled to the nearest MEC with one of the twisted and shielded electrical conductor pairs such that a length of a loop defined by the electrical power conductor and the neutral conductor of each twisted and shielded electrical conductor pair between each MEC and associated equipment loads is minimized, wherein the composite vehicle comprises a plurality of vehicle sections coupled together and defining section breaks between adjacent vehicle sections, and wherein the composite vehicle is otherwise free of a current return network extending across section breaks between multiple vehicle sections of the composite vehicle, and wherein the plurality of twisted and shielded electrical conductor pairs do not extend across section breaks.

18. The system of claim 17 wherein each MEC distributes secondary power only within each respective vehicle section to service associated equipment loads.