Method for optimising the architecture of the power supply of a load

Patent metadata

Field	Value
Publication number	US-10630093-B2
Application number	US-201415025993-A
Country	US
Kind code	B2
Filing date	Sep 30, 2014
Priority date	Sep 30, 2013
Publication date	Apr 21, 2020
Grant date	Apr 21, 2020

Abstract

A method for optimizing the architecture of the power supply of a load, includes the following steps: determination of a mission profile (16) sizing according to the power required by the load over time; definition of the sources of energy storage for hybridization; association of a characteristic behavior model with each source of energy storage; determination of the couples of sources of energy storage that can generate the mission profile with a minimum mass; and determination, from the potential couples of sources of energy storage, of the couple with the weakest mass.

First claim

The invention claimed is:

1. A method for optimizing the architecture of an electric power supply of a load, comprising:
determining a dimensioning mission profile according to a capacity demand over time of a load;
defining possible energy storage sources for hybridization, among energy storage sources of the battery, super-capacitor or fuel cell type;
associating a characteristic behavior model with each energy storage source;
determining couples of energy storage sources which are capable of generating a mission profile with minimum mass;
determining, among potential couples of energy storage sources, a couple with the lowest mass; and
constructing an electric power supply of a load using said couple with the lowest mass.

2. The method as claimed in claim 1 , wherein each characteristic behavior model corresponds to a Ragone diagram giving the total energy which can be supplied by the energy storage source, according to the capacity delivered per unit of mass of the energy storage source.

3. The method as claimed in claim 2 , wherein said determining couples of energy storage sources which are capable of generating the mission profile with minimum mass comprises: for each possible couple of energy storage sources for hybridization, determining working points on the Ragone diagram for energy storage sources which are capable of generating the mission profile and minimizing the total mass of the two energy storage sources.

4. The method as claimed in claim 3 , further comprising comparing the mass of the couple thus determined with the mass of an energy source in an existing architecture.

5. The method as claimed in claim 3 , further comprising:
defining suitable power converters for hybridization;
determining couples of energy storage sources which are capable of generating the mission profile with minimum mass, as a function of available power converters; and
determining power converters as a function of the couple thus determined.

6. The method as claimed in claim 3 , further comprising further comprising reading-out the energy storage sources in the couple thus determined, and the capacity utilization profiles of the energy storage sources in the couple thus determined.

7. The method as claimed in claim 2 , further comprising comparing the mass of the couple thus determined with the mass of an energy source in an existing architecture.

8. The method as claimed in claim 2 , further comprising:
defining suitable power converters for hybridization;
determining couples of energy storage sources which are capable of generating the mission profile with minimum mass, as a function of available power converters; and
determining power converters as a function of the couple thus determined.

9. The method as claimed in claim 2 , further comprising further comprising reading-out the energy storage sources in the couple thus determined, and the capacity utilization profiles of the energy storage sources in the couple thus determined.

10. The method as claimed in claim 1 , further comprising comparing the mass of the couple thus determined with the mass of an energy source in an existing architecture.

11. The method as claimed in claim 10 , further comprising the following steps:
defining suitable power converters for hybridization;
determining couples of energy storage sources which are capable of generating the mission profile with minimum mass, as a function of available power converters; and
determining power converters as a function of the couple thus determined.

12. The method as claimed in claim 1 , further comprising:
defining suitable power converters for hybridization;
determining couples of energy storage sources which are capable of generating the mission profile with minimum mass, as a function of available power converters; and
determining power converters as a function of the couple thus determined.

13. The method as claimed in claim 12 , further comprising further comprising reading-out the energy storage sources in the couple thus determined, and the capacity utilization profiles of the energy storage sources in the couple thus determined.

14. The method as claimed in claim 1 , further comprising reading-out the energy storage sources in the couple thus determined, and the capacity utilization profiles of the energy storage sources in the couple thus determined.

Assignees

• Airbus Group Sas
• Airbus Defence & Space Sas
• Airbus Helicopters

Inventors

• Fleury Benoit
• Massiot Gregor
• Lancelevee Pierre-Bertrand
• Labbe Julien

Classifications

• B64D2221/00

  Electric power distribution systems onboard aircraft · CPC title

• H02J7/345

  using capacitors as storage or buffering devices · CPC title

• G06F30/20

  Design optimisation, verification or simulation (optimisation, verification or simulation of circuit designs G06F30/30) · CPC title

• G06F17/5009

  Physics · mapped topic

• 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