Powertrain system in plug-in electric vehicles

Patent metadata

Field	Value
Publication number	US-9878635-B1
Application number	US-201514618696-A
Country	US
Kind code	B1
Filing date	Feb 10, 2015
Priority date	Feb 13, 2013
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

A powertrain system for plug-in electric vehicles (PEVs) includes one or a number of Energy Storage Sub-Systems (ESSs), and a plurality of Propulsion Machine-Inverter Groups, operatively coupled to the ESSs for being powered in accordance with power requirements of the Propulsion Machines (PMs). Various interface configurations between the ESS(s) and Propulsion Machines are contemplated for the subject powertrain. Some ESSs are coupled to respective PMs (via a common DC Link or a number of independent DC Links) directly, and some through power converters, which may be DC-to-DC, DC-to-AC, AC-to-DC, bi-directional, single input-single output, multiple input-single output, or multiple input-multiple output converters. A Supervisory Energy Management Sub-System cooperates with a Maximum Efficiency Tracker to dynamically control energy distribution in the system based on power requirements of the PMs through control of Propulsion Inverters and/or power converters to dynamically adjust the power level output by the ESSs to the DC Links' voltage variations.

First claim

What is claimed is:

1. A powertrain system in plug-in electric vehicles (PEVs), comprising:
at least one Energy Storage Sub-System (ESS) having opposite first and second terminals,
a plurality of Propulsion Machine-Inverter Groups, each composed of a Propulsion Machine and a Propulsion Inverter coupled to an input of said Propulsion Machine, said plurality of Propulsion Machine-Inverter Groups being operatively coupled to said at least one ESS for being powered in accordance with power requirements of said Propulsion Machines,
at least one common Direct Current (DC) Link operatively coupled between said at least one ESS and at least one of said plurality of Propulsion Machine-Inverter Groups, and
at least one power converter operatively coupled between said at least one ESS and said common DC link, wherein said power converter includes:
main switches S 1 , S 2 , S 3 , and S 4 coupled sequentially between said opposite first and second terminals of said at least one ESS, wherein said main switches S 2 and S 3 are coupled each to the other,
a first zero-voltage switching (ZVS) circuit coupled to said first terminal of said at least ESS between said main switches S 1 and S 2 , said first ZVS circuit being configured to substantially eliminate switching losses in main switches S 1 and S 2 , thereby attaining an increased switching frequency for said main switches S 1 and S 2 , and
a second zero-voltage switching (ZVS) circuit coupled to said second terminal of said at least one ESS between said main switches S 3 and S 4 , said second ZVS circuit being configured to substantially eliminate switching losses in said main switches S 3 and S 4 , thereby attaining an increased switching frequency for said main switches S 3 and S 4 ,
wherein each of said main switches S 1 -S 4 includes a solid state switch.

2. The powertrain system of claim 1 , further comprising a Maximum Efficiency Tracker Sub-System operatively coupled to the Propulsion Machine in at least one of said plurality of Propulsion Machine-Inverter Groups to dynamically track operational power requirements of said Propulsion Machine, and an Inverter Controller Sub-System operatively coupled to said Maximum Efficiency Tracker Sub-System and said Propulsion Inverter in said at least one Propulsion Machine-Inverter Group, wherein said Inverter Controller Sub-system is configured to control said Propulsion Inverter to split power outputted from said at least one ESS in correspondence with said Propulsion Machine operational power requirements.

3. The powertrain system of claim 1 , wherein said at least one power converter operates to dynamically adjust the power level outputted by said at least one ESS to said common DC Link's voltage variations.

4. The powertrain system of claim 3 , further comprising a plurality of ESSs composed of a first group of ESSs and a second group of ESSs, and a plurality of said power converters operatively coupled between said second group of ESSs and said common DC Link, wherein at least one ESS in said first group thereof is directly coupled to said common DC Link, and wherein each ESS of said second group of ESSs is coupled to said common DC Link through a respective one of said plurality of power converters.

5. The powertrain system of claim 4 , further comprising a plurality of power converter's controllers, each controller being operatively coupled to a respective one of said plurality of power converters, and a Supervisory Energy Management Sub-System coupled to said power converters' controllers and said Maximum Efficiency Tracker Sub-System, wherein said Supervisory Energy Management Sub-System is configured to supply required power signals to said power converters' controllers responsive to the readings of the Maximum Efficiency Tracker Sub-System, thereby affecting the splitting of power among said plurality of ESS as required by the operational power requirements of said plurality of Propulsion Machines.

6. The powertrain system of claim 3 , wherein said power converter is selected from a group consisting of: DC-to-DC converter, AC-to-DC converter, and DC-to-AC converter.

7. The powertrain system of claim 3 , further comprising a plurality of ESSs, and a plurality of power converters, wherein each ESS of said plurality thereof is operatively coupled to said common DC Link through a respective one of said plurality of said power converters.

8. The powertrain system of claim 3 , wherein said power converter is a single input-single output converter.

9. The powertrain system of claim 3 , wherein said power converter is a multi-input-single output converter, further comprising a plurality of ESSs composed of a first group of ESSs and a second group of ESSs, wherein said ESSs in said second group thereof are coupled to said common DC Link through said multi input-single output converter.

10. The powertrain system of claim 9 , further comprising a second group of power converters, wherein each power converter in said second group thereof is coupled between respective two of said plurality of ESSs.

11. The powertrain system of claim 9 , wherein at least one ESS in said first group of the ESSs is directly coupled to said common DC Link.

12. The powertrain system of claim 11 , further comprising a second group of power converters, wherein each power converter in said second group thereof is coupled between respective two of said plurality of ESSs.

13. The powertrain system of claim 1 , further comprising a multi input-multi output power converter, a plurality of ESSs, and a plurality of said DC Links, wherein each Propulsion Machine-Inverter Group in said plurality thereof is coupled to a respective one of a plurality of outputs of said multi input-multi output power converter through a respective one of said plurality of DC links, and wherein each of said plurality of ESSs is coupled to a respective input of said multi input-multi output power converter.

14. The powertrain system of claim 13 , further comprising a second group of power converters, wherein each power converter in said second group thereof is coupled between respective two of said plurality of ESSs.

15. The powertrain system of claim 14 , wherein said plurality of ESSs further comprises a second group of ESSs, wherein each ESS in said second group thereof is connected to a respective Propulsion Machine-inverter Group through a respective one of said plurality of DC Links, and wherein said each power converter in said second group thereof is coupled between respective two of said ESSs in said second group thereof.

16. The powertrain system of claim 1 , further comprising a plurality of ESSs, a plurality of said DC Links, and a plurality of power converters, wherein each power converter in said plurality thereof is coupled to a respective one of said plurality of ESSs, and wherein each of said plurality of Propulsion Machine-Inverter Groups is coupled to a respective one of said plurality of power converters through a corresponding one of said plurality of DC Links.

17. The powertrain system of claim 16 , further comprising a second group of power converters, wherein each power converters in said second group thereof is coupled between respective two of said plurality of ESSs.

18. The powertrain system of claim 1 , further comprising a plurality of ESSs composed of a first group of ESSs and a second group of ESSs, a plurality of said DC Links, and a plurality of single input-single output power converters,
wherein at least one ESS in said first group of ESSs is coupled to a respective Propulsion Machine-Inverter

Assignees

• Khaligh Alireza
• Dusmez Serkan
• Univ Maryland

Inventors

• Khaligh Alireza
• Dusmez Serkan

Classifications

• B60L11/1868 Primary

  Operations & Transport · mapped topic

• Y10S903/904

  Component specially adapted for hev · CPC title

• B60L11/1803

  Operations & Transport · mapped topic

• B60L3/12 Primary

  Recording operating variables {; Monitoring of operating variables} · CPC title

• H02M1/0058

  by employing soft switching techniques, i.e. commutation of transistors when applied voltage is zero or when current flow is zero (using an auxiliary actively switched resonant commutation circuit connected to an intermediate DC voltage or between two push-pull branches of an inverter bridge H02M7/4811; in resonant inverters H02M7/4815; in inverters operating from a resonant DC source H02M7/4826) · CPC title