Aircraft starting and generating system

Patent metadata

Field	Value
Publication number	US-10260471-B2
Application number	US-201515549177-A
Country	US
Kind code	B2
Filing date	Feb 18, 2015
Priority date	Feb 18, 2015
Publication date	Apr 16, 2019
Grant date	Apr 16, 2019

Abstract

An aircraft starting and generating system includes a starter/generator that includes a main machine, an exciter, and a permanent magnet generator. The system also includes an inverter/converter/controller that is connected to the starter/generator and that generates AC power to drive the starter/generator in a start mode for starting a prime mover of the aircraft, and that converts AC power, obtained from the starter/generator after the prime mover have been started, to DC power in a generate mode of the. A load-leveling unit (LLU) is selectively coupled with a DC power output from the starter/generator and has an inverter/converter/controller (ICC) with an LLU metal oxide semiconductor field effect transistor (MOSFET)-based bridge configuration that supplies DC power to the DC power output in a supply mode, and that receives DC power from the DC power output, in a receive mode. A LLU bridge gate driver is configured to drive the LLU MOSFET-based bridge during a supply mode and a receive mode using bi-polar pulse width modulation (PWM).

First claim

What is claimed is:

1. An aircraft starting and generating system, comprising:
a starter/generator that includes a main machine, an exciter, and a permanent magnet generator;
a direct current power output from the starter/generator;
a load-leveling unit selectively coupled with the direct current power output and having an inverter/converter/controller having a load-leveling unit metal oxide semiconductor field effect transistor-based bridge configuration and that supplies direct current power to the direct current power output in a supply mode, and that receives direct current power from the direct current power output, in a receive mode; and
a load-leveling unit bridge gate driver configured to drive the load-leveling unit metal oxide semiconductor field effect transistor-based bridge;
wherein the load-leveling unit bridge gate driver operates to drive the load-leveling unit metal oxide semiconductor field effect transistor-based bridge during the supply mode and the receive mode using bi-polar pulse width modulation.

2. The aircraft starting and generating system of claim 1 wherein the load-leveling unit further comprises a power storage device.

3. The aircraft starting and generating system of claim 2 wherein the power storage device comprises at least one of a battery, a fuel cell, or an ultracapacitor.

4. The aircraft starting and generating system of claim 2 wherein the power storage device is configured to discharge power to the inverter/converter/controller during the supply mode and absorb power from the inverter/converter/controller during the receive mode.

5. The aircraft starting and generating system of claim 3 wherein the power storage device is configured to discharge power simultaneously and in parallel with the starter/generator during periods of peak power requirements.

6. The aircraft starting and generating system of claim 1 wherein the load-leveling unit metal oxide semiconductor field effect transistor-based bridge further comprises at least one of a silicon carbide-based bridge or Gallium Nitride-based bridge.

7. The aircraft starting and generating system of claim 1 , further comprising a main machine metal oxide semiconductor field effect transistor-based bridge that is connected to a stator of the main machine, and a main machine bridge gate driver configured to drive the main machine metal oxide semiconductor field effect transistor-based bridge.

8. The aircraft starting and generating system of claim 7 wherein the main machine comprises a main machine metal oxide semiconductor field effect transistor-based bridge configuration that absorbs excess power of the system in a regeneration mode by storing the excess power in the kinetic energy of the prime mover of the aircraft, and wherein the main machine bridge gate driver operates to drive the main machine metal oxide semiconductor field effect transistor-based bridge during regeneration mode using Space Vector Pulse Width Modulation.

9. The aircraft starting and generating system of claim 8 wherein the main machine metal oxide semiconductor field effect transistor-based bridge further comprises at least one of a silicon carbide-based bridge or Gallium Nitride-based bridge.

10. The aircraft starting and generating system of claim 1 wherein the load-leveling unit metal oxide semiconductor field effect transistor-based bridge further comprises an array of individually-controllable metal oxide semiconductor field effect transistors.

11. The aircraft starting and generating system of claim 10 wherein the load-leveling unit bridge gate driver operates to drive each individually-controllable metal oxide semiconductor field effect transistor.

12. The aircraft starting and generating system of claim 1 wherein the load-leveling unit metal oxide semiconductor field effect transistor-based bridge further comprises individually-controllable wide bandgap device metal oxide semiconductor field effect transistors.

13. The aircraft starting and generating system of claim 12 wherein the metal oxide semiconductor field effect transistors further comprise external diodes configured across a body diode of the metal oxide semiconductor field effect transistors.

14. A method of controlling an aircraft starting and generating system having a starter/generator that includes a main machine having a direct current power output, an exciter, and a permanent magnet generator, a load leveling unit selectively coupled with the direct current power output and having an inverter/converter/controller having a metal oxide semiconductor field effect transistor-based bridge configuration, and a load-leveling unit bridge gate driver configured to drive the metal oxide semiconductor field effect transistor-based bridge, the method comprising:
if in supply mode, selectively coupling the direct current power output with the metal oxide semiconductor field effect transistor-based bridge and supplying power to the direct current power output from the metal oxide semiconductor field effect transistor-based bridge by driving the metal oxide semiconductor field effect transistor-based bridge during supply mode using bi-polar Pulse Width Modulation; and
if in receive mode, selectively coupling the direct current power output with the metal oxide semiconductor field effect transistor-based bridge and receiving power from the direct current power output to the metal oxide semiconductor field effect transistor-based bridge by driving the metal oxide semiconductor field effect transistor-based bridge using bi-polar pulse width modulation.

15. The method of claim 14 wherein, if in the supply mode, the supplying power from the metal oxide semiconductor field effect transistor-based bridge further comprises supplying power from a power storage device to the metal oxide semiconductor field effect transistor-based bridge.

16. The method of claim 15 wherein supplying power from a power storage device further comprises discharging at least a portion of at least one of a battery, a fuel cell, or an ultracapacitor.

17. The method of claim 14 , further comprising, if in start mode, selectively coupling the direct current power output with the metal oxide semiconductor field effect transistor-based bridge and supplying power from the metal oxide semiconductor field effect transistor-based bridge and driving the metal oxide semiconductor field effect transistor-based bridge during start mode using bi-polar pulse width modulation, and wherein the driving the main metal oxide semiconductor field effect transistor-based bridge during start mode starts a prime mover of the aircraft.

18. The method of claim 17 wherein the supplying power from the metal oxide semiconductor field effect transistor-based bridge further comprises supplying power from a power storage device to the metal oxide semiconductor field effect transistor-based bridge.

19. The method of claim 14 , further comprising selectively switching between the supply mode and the receive mode.

20. An aircraft comprising:
an engine;
a starter/generator connected to the engine, and having a main machine, an exciter, and a permanent magnet generator;
a direct current power output from the starter/generator;
a load-leveling unit selectively coupled with the direct current power output and having an inverter/converter/controller with a load-leveling unit metal oxide semiconductor field effect transistor-based bridge configuration and that supplies direct current power to the direct current power output in a supply mode, and that receives direct

Assignees

• Ge Aviation Systems Llc

Inventors

• Huang Hao

Classifications

• H02J2105/32

  for aircrafts · CPC title

• H02J2101/30

  Fuel cells · CPC title

• F02N11/0862

  characterised by the electrical power supply means, e.g. battery · CPC title

• F02N2011/0896

  Inverters for electric machines, e.g. starter-generators · CPC title

• H02M3/1584

  with a plurality of power processing stages connected in parallel · CPC title