ZERO-SEQUENCE BLOCKING TRANSFORMER

Abstract

A zero-sequence blocking transformer includes a first core part, a first pair of windings wound around the first core part, a second core part and a second pair of windings wound around the second core part, the first core and the second core having a geometry to generate a leakage inductance.

Claims

1. A zero-sequence blocking transformer comprising: a first core part; a first pair of windings wound around the first core part; a second core part; and a second pair of windings wound around the second core part, the first core and the second core having a geometry to generate a leakage inductance.

2. A zero-sequence blocking transformer as claimed in claim 1, wherein the first core part and the second core part combine to form a toroidal core defining a central space.

3. A zero-sequence blocking transformer as claimed in claim 1, wherein the first core part and the second core part are first and second legs of an EE core geometry.

4. A zero-sequence blocking transformer as claimed in claim 3, further comprising a third core part as a third leg of the transformer, and a third pair of windings formed on the third leg.

5. A zero-sequence blocking transformer as claimed in claim 4, further comprising a fourth core part as a fourth leg of the transformer, and a fourth pair of windings formed on the fourth leg.

6. A zero-sequence blocking transformer according to claim 1, further comprising a supplemental core part to create an additional leakage flux path therethrough, providing an additional leakage inductance.

7. A zero-sequence blocking transformer as claimed in claim 6, where the supplemental core part comprises an additional magnetic component without a winding.

8. A zero-sequence blocking transformer as claimed in claim 6, wherein the first core part and the second core part combine to form a toroidal core defining a central space, and wherein the supplemental core part comprises a rod of magnetic material fitted into the central space between the four windings to create the additional leakage flux path.

9. A zero-sequence blocking transformer according to claim 6, wherein the supplemental core part is a third leg and wherein the third leg is a middle leg between the first and second legs or wherein one of the first and second legs is a middle leg formed between the other of the first and second legs and the third leg.

10. A multi-phase auto-transformer rectifier unit comprising: a plurality of diode bridge rectifiers connected in parallel; a DC-link capacitor between the rectifiers and a load to be driven, in use, by the unit; and a zero-sequence blocking transformer as claimed in claim 1 between the rectifiers and the DC-link capacitor.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0016] FIG. 1 is a schematic circuit view of a 12-pulse ATRU with IPT architecture.

[0017] FIG. 2 shows the structures of the IPTs of FIG. 1.

[0018] FIG. 3 is a schematic circuit for a 12-pulse ATRU with ZSBT.

[0019] FIG. 4A shows an example of a toroidal core used in a known ZSBT.

[0020] FIG. 4B is the equivalent circuit of the core of FIG. 4A.

[0021] FIG. 5 shows an example of a toroidal core modified according to this disclosure and its equivalent circuit.

[0022] FIG. 6 shows an example of a further modified toroidal core for a 12-pulse ATRU according to this disclosure, and its equivalent circuit.

[0023] FIGS. 7A and 7B show alternative examples of an EE core modified according to this disclosure.

[0024] FIG. 8 is a schematic circuit for a 12-pulse ATRU according to the disclosure.

[0025] FIG. 9 is a schematic circuit for an 18-pulse ATRU according to the disclosure.

[0026] FIG. 10 is a schematic circuit for a 24-pulse ATRU according to the disclosure.

[0027] FIG. 11 shows an example of a core for ZSBT in an 18-pulse ATRU modified according to this disclosure.

[0028] FIG. 12 shows an example of a core for ZSBT in a 24-pulse ATRU modified according to this disclosure.

[0029] FIG. 13 shows an example of an alternative core structure for ZSBT in an 18-pulse ATRU modified according to this disclosure.

[0030] FIG. 14 shows an example of an alternative core structure for ZSBT in a 24-pulse ATRU modified according to this disclosure.

DETAILED DESCRIPTION

[0031] The described embodiments are by way of example only. The scope of this disclosure is limited only by the claims.

[0032] The use of IPTs and ZSBTs in ATRUs will be briefly described for background, with reference to FIGS. 1 to 4.

[0033] ATRUs are commonly used in medium to high power AC-DC power conversion systems used in e.g. aerospace applications. FIGS. 1 and 3 show examples of 12-pulse ATRUs. Other winding schemes and topologies are also known, e.g. 18-pulse, 24-pulse.

[0034] As described above, to improve performance of the ATRU, IPTs or ZSBTs are connected between the outputs of the diode bridge rectifiers and the DC-link capacitor.

[0035] FIG. 1 shows a 12-pulse ATRU having a three-phase supply 1, an input filter 2, a 12-pulse ATU 3, two diode bridge rectifiers 4a and 4b, DC-link capacitor 6, load 7 and IPTs 5a and 5b between the rectifiers and the DC-link capacitor. For a 12-pulse ATRU three phases are input to the ATRU which provides six outputs so two rectifier bridges are needed. An IPT is provided for each rectifier—i.e. for the six outputs of the 12-pulse ATRU, two IPTs are required.

[0036] As seen in FIG. 2, the IPT has two windings A+, B+; A−, B−, wound on a magnetic core 10 with a small air gap g. The small air gap prevents the core being saturated from the net flux imbalance generated by the zero-sequence currents circulating between the outputs of the two diode bridges.

[0037] As an alternative to IPTs, the zero-sequence currents can be cancelled by zero-sequence blocking transformers as mentioned above.

[0038] FIG. 3 shows a 12-pulse ATRU with ZBSTs. The ATRU has a three-phase supply 11, an input filter 12, a 12-pulse ATU 13, two diode bridge rectifiers 14a and 14b, DC-link capacitor 16, load 17 and ZSBTs 15a and 15b between the rectifiers and the DC-link capacitor.

[0039] As seen in FIG. 4A, the ZSBT has two windings A+, A−, wound on a toroidal core 20. The main magnetic fluxes generated by the positive and negative currents are usually equal and cancel each other out. This is seen in the equivalent circuit of FIG. 4B. ZSBTs have leakage inductances Lleak and magnetizing inductances Lmag as shown in the equivalent circuit in FIG. 4B. Only the leakage inductance is important in limiting zero-sequence currents between the outputs of the diode bridges as well as minimizing the output ripple currents.

[0040] For both of the above mentioned solutions, for a 12-pulse ATRU, two IPT or ZSBT units (5a, 5b; 15a, 15b) are required. The same principle applies for higher pulse ATRUs—two IPT or ZSBT units are required for each multiple of 12 pulses. For an 18-pulse ATRU, two IPTs or three ZSBTs would be required, for a 24-pulse ATRU, four ZSBTs would be required etc.

[0041] As mentioned above, each of these units can, particularly for low permeability core materials, become large, bulky and heavy due to the number of turns of the windings and the size of the core required to achieve the necessary self-inductance to limit the zero-sequence currents.

[0042] The aim of the present disclosure is to reduce the overall size of the ZSBT solution for 12-pulse ATRUs or higher.

[0043] The solution according to tis disclosure is an integrated magnetic core ZSBT design in which, for a 12-pulse ATRU, the four coils of the ZSBT are wound onto a single core rather than two separate cores as in the conventional designs. This means that for a 12-pulse ATRU, only one ZSBT unit is required to cancel the zero-sequence currents of two rectifiers. For ATRUs with higher numbers of pulses, for each set of twelve pulses, a single ZSBT unit is required, rather than two. Therefore, for a 24-pulse ATRU, only two ZSBT cores are required instead of four. For an 18-pulse ATRU, two ZSBT cores are provided instead of three (one, instead of two, for 12 outputs and another for the other six outputs).

[0044] FIG. 5 shows a ZSBT design according to the disclosure for a 12-pulse ATRU. Here, four windings A+, A−, B+, B−, are provided on a single core 30. The windings are arranged as shown such that the flux produced by the + and − current winding pairs is cancelled out—i.e. ΦA+=ΦA− and ΦB+=ΦB− and only the net flux Φnet is left circulating inside the core. The net flux is produced by the zero-sequence current. No additional external power is required for the system to function properly.

[0045] The same concept can apply to an E-core design, whereby two coils are provided on each leg of the core (not shown in its simplest form, but shown with a further modification as described below).

[0046] If it is necessary or desired to further increase or control the leakage inductance of the ZSBT, the design can be further modified using the concepts described in European patent application EP-A-3876249, by inserting an additional inductance path. The leakage inductance of a ZSBT is a product of that leakage flux that does not flow from one winding to another—here, the net flux not flowing from windings A to windings B. B inserting a magnetic rod across a toroidal core (as shown in FIG. 6) or adding an extra leg to an E-core as shown in FIGS. 7A and 7B, flux can be diverted from the main path as leakage flux allowing the leakage inductance to be controlled.

[0047] By providing four windings on a common coil, according to this disclosure, the number of ZSBT units required in an ATRU can be reduced. This can be seen for different ATRUs with toroidal cores with reference to FIGS. 8 to 10.

[0048] For a 12-pulse ATRU (FIG. 8) it can be seen that, compared to FIG. 3, only one ZBST 15 unit is required instead of two (15a, 15b in FIG. 3). The other parts of the system are the same as in FIG. 3 and the same reference numerals are used for those parts.

[0049] FIG. 9 shows the solution for an 18-pulse ATRU which, again has a three-phase supply 11, input filter 12 and, here, an 18-pulse ATRU 23. A balancing resistor 24 is provided and three diode bridge rectifiers 25a, 25b and 25c, a DC capacitor 27 and load 28. Conventionally, for three diode bridge rectifiers, three ZSBT units would be required. With the modification of this disclosure, only two units 26a, 26b are required.

[0050] FIG. 10 shows the solution for a 24-pulse ATRU which, again has a three-phase supply 11, input filter 12 and, here, a 24-pulse ATRU 33. Here, the system requires four diode bridge rectifiers 34a, 34b, 34c and 34d, a DC capacitor 36 and load 37. Conventionally, for four diode bridge rectifiers, four ZSBT units would be required. With the modification of this disclosure, only two units 35a and 35b are required.

[0051] The principle can be applied for any greater number of pulse ATRUs. For any even number of diode bridges (12-pulse, 24-pulse, 36 pulse etc.) the number of ZSBTs is, therefore halved. For odd numbers of diode bridges, the number of ZSBTs is also reduced in that for each pair of bridges, only one ZSBT is needed instead of one.

[0052] FIGS. 11 to 14 show possible monolithic core designs using the above concept and, as a preferred feature to add further leakage inductance control, with an additional leakage path. For E-core designs, all of the windings for the ZSBT can be provided onto a single unit in having one core leg for each pair of windings and, if preferred, the additional flux path. Therefore, regardless of the number of pulses and, hence, diode bridges, the ZSBT solution can be provided as a single unit, with one core leg for each pair of coils—i.e. one core leg for each six pulses.

[0053] FIG. 11 shows a core design for an 18-pulse ATRU which two windings A+, A−; B+, B−, C+, C− on each core leg 40, 50, 60 and with the additional inductance path 70.

[0054] FIG. 12 shows the corresponding design for a 24-pulse ATRU with coil pairs A+, A−; B+, B−; C+, C−; D+, D− on legs 41, 51, 61, 71 and the extra path 81.

[0055] Alternatively, the cores can be designed with a symmetrical structure as shown in FIGS. 13 and 14, with the core legs, each having a pair of windings, extending from a central point, and at equal angles from each other, with the additional inductance path, if required, at the central point. For an 18-pulse ATRU, for example, as shown in FIG. 13, three legs are spaced 120 degrees apart. For a 24-pulse ATRU, four legs are spaced 90 degrees apart.

[0056] The ZSBT designs according to this disclosure provide a simpler, smaller and lighter zero-sequencing current solution to ATRUs of any size.