AC/AC power converter for aircraft

• US 7,906,866 B2
• Filed: 04/11/2008
• Issued: 03/15/2011
• Est. Priority Date: 04/11/2008
• Status: Expired due to Fees

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Xu, Mingzhou, Anghel, Cristian E.
• Primary Examiner(s): Fureman; Jared J
• Assistant Examiner(s): Fauth; Justen
• Application Number:
  US12/101,864
• Publication Number:
  US 20090256419A1
• Time in Patent Office: 1,068 Days
• Field of Search: None
• US Class Current: 307/9.1
• CPC Class Codes: B60L 1/003 to auxiliary motors, e.g. for pumps, compressors
• CPC Class Codes: B60L 15/007 Physical arrangements or structures of drive train converters specially adapted for the propulsion motors of electric vehicles
• CPC Class Codes: B60L 2200/10 Air crafts
• CPC Class Codes: B60L 2210/20 AC to AC converters
• CPC Class Codes: B60L 50/61 by batteries charged by engine-driven generators, e.g. series hybrid electric vehicles
• CPC Class Codes: F02N 11/04 the motors being associated with current generators
• CPC Class Codes: F02N 11/0859 specially adapted to the type of the starter motor or integrated into it
• CPC Class Codes: F02N 11/0866 comprising several power sources, e.g. battery and capacitor or two batteries
• CPC Class Codes: F02N 2011/0885 Capacitors, e.g. for additional power supply
• CPC Class Codes: F02N 2011/0896 Inverters for electric machines, e.g. starter-generators
• CPC Class Codes: Y02T 10/62 Hybrid vehicles
• CPC Class Codes: Y02T 10/64 Electric machine technologies in electromobility
• CPC Class Codes: Y02T 10/70 Energy storage systems for electromobility, e.g. batteries
• CPC Class Codes: Y02T 10/7072 Electromobility specific charging systems or methods for batteries, ultracapacitors, supercapacitors or double-layer capacitors
• CPC Class Codes: Y02T 10/72 Electric energy management in electromobility

Abstract

A matrix converter circuit having two AC/AC matrix converters coupled in parallel in a first mode to power a starter and decoupled in a second mode to each power separate functions used in aircraft power applications. Three common functional modes include 1) start mode with two matrix converters operating in parallel powering the starter, 2) a motor mode where one matrix converter powers a motor, and 3) a constant frequency power mode where the other matrix converter provides constant frequency AC power.

Claims

1. An electric power circuit for converting variable or constant frequency power in an aircraft, comprising:

a starter/generator of the aircraft;

two bidirectional AC/AC matrix converters selectively coupled together in parallel with contactors to receive power flow from a power supply in a forward direction, said matrix converters delivering controlled frequency power to the starter/generator to operate said starter/generator as a starter;

the contactors providing for selective decoupling of the two matrix converters; and

the two decoupled matrix converters simultaneously receive power flow from the starter/generator operating as a generator providing power in a reverse direction, with one matrix converter delivering constant frequency power for constant frequency electrical loads in the aircraft and the other matrix converter delivering controlled, variable frequency power for controlled, variable frequency electrical loads in the aircraft.

2. The circuit of claim 1, further comprising:

three inputs carrying a three-phase power input, each input including an inductor circuit for filtering out frequency components on the input of each of the matrix converter; and

a capacitor coupled in parallel linking two of each of the three inputs, one capacitor coupled between each pair of inputs, and filtering out components on the inputs of each of the matrix converters.

3. The circuit of claim 2, further comprising:

three capacitors coupled in a triangular array, each one of the three inputs connected to one of three apex formed by connecting the triangular array, and filtering frequency components on the inputs.

4. The circuit of claim 1, further comprising:

an array of bidirectional switches.

5. The circuit of claim 1, further comprising:

three outputs from each of the two matrix converters carrying a pulse width modulated power output, each output including an inductor circuit for filtering out frequency components on the output of each of the matrix converters; and

three capacitors coupled in a triangular array, each of the three outputs connected to an apex formed by connecting the triangular array, and filtering frequency components on the outputs.

6. The circuit of claim 1, further comprising:

a power output of controlled frequency power flow from one of the matrix converters providing a constant frequency 400 Hz power load or a controlled frequency power load for powering a motor.

7. A matrix converter circuit producing power in an aircraft, comprising:

a starter/generator of the aircraft;

a first bidirectional matrix converter for providing AC/AC conversion of variable or constant frequency power delivered by the starter/generator functioning as a generator in a first mode to deliver constant frequency power for first electrical loads of the aircraft;

a second bidirectional matrix converter, acting simultaneously with the first matrix converter, for providing AC/AC conversion of variable or constant frequency power delivered by said starter/generator functioning as a generator in a first mode to deliver controlled frequency power for second loads of the aircraft;

the first and second matrix converter for providing AC/AC conversion of power from an external power supply in a second mode to deliver controlled frequency power to said starter/generator functioning as a starter, the first and second matrix converter coupled in parallel to deliver said power; and

wherein the AC/AC conversion does not comprise AC/DC conversion or DC/AC conversion.

8. The matrix converter circuit of claim 7, further comprising:

three inputs to each of the first matrix converters and the second matrix converter carrying a three-phase power signal, each input including an inductor circuit for filtering out frequency components of the power signal to each of the matrix converters; and

at least one capacitor filter coupled in parallel to each of the three inputs filtering out components to each of the matrix converters.

9. The matrix converter circuit of claim 7, further comprising:

the first matrix converter and the second matrix converter includes an array of bidirectional switches.

10. The matrix converter circuit of claim 7, further comprising:

three outputs from each of the first matrix converter and the second matrix converter carrying a controlled frequency pulse width modulated power signal output, each output including an inductor circuit for filtering out frequency components on the output of the matrix converters; and

at least one capacitor filter coupled in parallel to each of the three outputs filtering out frequency components on the outputs of each of the matrix converter circuits.

11. The matrix converter circuit of claim 7, wherein the first matrix converter powers a motor in the first mode and the second matrix converter powers an electronic component in the first mode.