Power rectifier circuit and systems, associated method, and aircraft comprising such a circuit or systems

• US 8,467,206 B2
• Filed: 01/21/2009
• Issued: 06/18/2013
• Est. Priority Date: 01/31/2008
• Status: Active Grant

• Current Assignee: Centre National De La Recherche Scientifique, Airbus Operations (European Aeronautic Defence and Space Company EADS NV), Institut National Polytechnique de Toulouse
• Original Assignee: Airbus Operations SAS (Airbus SE), Centre National De La Recherche Scientifique, Institut National Polytechnique de Toulouse
• Inventors: Iturriz, Marcelo Fernando, Richardeau, Frederic, Meynard, Thierry, Helali, Hassan
• Primary Examiner(s): Berhane, Adolf
• Assistant Examiner(s): Jackson, Lakaisha
• Application Number:
  US12/865,575
• Publication Number:
  US 20110002148A1
• Time in Patent Office: 1,609 Days
• Field of Search: 363/17, 363/53, 363/54, 363/56.02, 363/56.05, 363/67, 363/69, 363/70, 363/71, 363/89, 363/98, 363/126, 363/128, 363/132, 363/127
• US Class Current: 363/70
• CPC Class Codes: H02M 7/10 arranged for operation in series, e.g. for multiplication of voltage
• CPC Class Codes: H02M 7/25 arranged for operation in series, e.g. for multiplication of voltage

Abstract

A power rectifying circuit for an electric current signal supplied by an alternating power source, which includes: two separate switching assemblies adapted to be connected to a power terminal of the source, wherein at least one switching assembly includes a plurality of boost cells in cascade, each boost cell including a diode, a switch mechanism and a capacitor, the capacitors of the two terminal boost cells of the switching assemblies having one terminal in common. The circuit may include two assemblies of boost cells, and can be used in electric systems onboard aircrafts.

Claims

1. A power rectifying circuit for electrical current delivered by an alternating current source, comprising:

two separate commutation assemblies arranged to be connected to a supply terminal of a source, at least one commutation assembly comprising a plurality of commutation boost cells in cascade;

each boost cell comprising a diode connected between a first input terminal and a first output terminal of the cell, a switch means connected between a second input terminal and a second output terminal of the cell, and a capacitor connected between the two output terminals of the cell,

the plurality of commutation boost cells of at least one of the commutation assemblies being arranged in cascade so that the first and second output terminals of one boost cell are connected respectively to the first and second input terminals of the following boost cell,

the capacitors of the two terminal boost cells of the commutation assemblies having one terminal in common,

wherein the power rectifying circuit further comprises blocking means for blocking all the switch means of the circuit in case of detection of a low-impedance fault in one of the boost cells, and

the power rectifying circuit further comprises means for detecting a low-impedance fault in a boost cell arranged to detect a voltage at terminals of the switch means of the cell during a predetermined time interval following a control signal to start the switch means to detect a fault of the boost diode of the cell or following a control signal to block the switch means to detect a fault of the switch means.

2. The power rectifying circuit according to claim 1, wherein each commutation assembly comprises two boost cells.

3. The power rectifying circuit according to claim 1, further comprising a pair of rectifying means arranged to be connected between the supply terminal and respectively each of the commutation assemblies, so as to rectify a low-frequency input current.

4. The power rectifying circuit according to claim 3, wherein each power rectifying means comprises a diode.

5. The power rectifying circuit according to claim 3, wherein the power rectifying means are in series with a same forward direction as the diodes of the commutation assembly to which the power rectifying means are connected.

6. A power rectifying system for electrical current delivered by a multi-phase alternating current supply source, comprising:

a plurality of power rectifying circuits each according to claim 1, arranged such that each can be connected to a supply terminal connected to respectively each of phases of the multi-phase current, and in which the circuits share the capacitors of the final boost cells.

7. The power rectifying system according to claim 6, wherein a cell of one of the rectifying circuits and the corresponding cell in the other circuit share the same capacitor.

8. A power rectifying system for the electrical current delivered by an alternating current supply source, comprising:

two power rectifying circuits each according to claim 1, arranged to be connected respectively to each of terminals of the supply source, and in which the circuits share the capacitors of the final boost cells.

9. The power rectifying system according to claim 8, in which the two circuits are combined to exclusion of rectifying means provided between each of the terminals of the source and each input of the two commutation assemblies, the rectifying means connected to a given commutation assembly being exclusive, in opposite directions of current flow.

10. The power rectifying circuit according to claim 1, wherein the switch means comprises controlled transistors.

11. The power rectifying circuit according to claim 1, wherein the means for detecting a low impedance fault comprises a transistor controller that is coupled to a voltage detector.

12. An aircraft comprising a power rectifying circuit according to claim 1.

13. A power rectifying method for an electrical current signal delivered by an alternating current supply source, the method being achieved by a rectifying circuit comprising:

two separate commutation assemblies arranged to be connected to a supply terminal of the source, at least one commutation assembly comprising a plurality of commutation boost cells in cascade,

each boost cell comprising a diode connected between a first input terminal and a first output terminal of the cell, a switch means connected between a second input terminal and a second output terminal of the cell, and a capacitor connected between the two output terminals of the cell,

the boost cells of at least one of the commutation assemblies being arranged in cascade so that the first and second output terminals of a boost cell are connected respectively to the first and second input terminals of the following boost cell, and

the capacitors of the two terminal boost cells of the assemblies having one common terminal,

the method comprising sequential control of each of the switch means so as to deliver DC voltages to the terminals of the terminal capacitors,

the method comprising blocking all the switch means of the circuit in case of detection of a low-impedance fault in one of the boost cells, and

the method comprising detecting a low-impedance fault in a boost cell arranged to detect a voltage at terminals of the switch means of the cell during a predetermined time interval following a control signal to start the switch means to detect a fault of the boost diode of the cell or following a control signal to block the switch means to detect a fault of the switch means.

14. The method according to claim 13, further comprising sensing a low impedance fault in at least one of the boost cells, and following the sensing, blocking the switching means in the boost cells.

15. The method according to claim 13, further comprising forcing the switching means of a commutation assembly to be in a forward state when the other commutation assembly is active during an alternation of an input current.