NPC T Type Vienna rectifier

Validation of the reliability of NPC T Type Vienna rectifiers in shoot-through conditions.

Introduction

There is an increasing demand from the aeronautics industry for highly efficient, compact, and reliable three-phase rectifiers. The conventional rectifiers employed in today's aircrafts rely on passive solutions which are extremely robust, but are also heavy and bulky. The active rectifiers employ semiconductors that switch at high frequencies in order to provide control to the rectifier variables, reduce the size of magnetic components, and increase efficiency. The most popular among them is the bidirectional three-phase boost rectifier. The main drawback of this rectifier is poor tolerance to shoot-through of the rectifier bridge leg, which would cause the DC bus to short circuit and a complete failure of the system. The Vienna rectifier is immune to shoot-through of the one switch in the leg due to the inclusion of protective diodes. In this application, a three-phase Vienna rectifier is implemented using three NPC T type leg components from the Converters Library. The application demonstrates the high reliability of the Vienna rectifier in two main aspects:

  • it maintains the constant output voltage in asymmetric load conditions
  • it is immune to a short-circuit on the output voltage in case of control errors (switch faults)

Model description

The Vienna rectifier topology is shown in Figure 1. For example, if the switch Qa is off and the phase current iA is positive, the phase leg A is clamped to the positive DC link, and therefore, Voltage from phase A to neutral (VAN) is equal to Vdc/2. Similarly, if Qa is off and iA is negative, then VAN will be −Vdc/2. If the Qa is on, phase leg A will be clamped to the DC link neutral point and the VAN will be zero, regardless of iA polarity. The same operation principle applies to both phase B and phase C. This topology is implemented using the NPC T-type inverter legs shown in the Figure 2. There are two pairs of complementary switches. Switches S2 and S3 perform the equivalent function of the Q switch, while switches S1 and S4 improve the shape of input currents.

Figure 1: Vienna rectifier topology



Figure 2: NPC T-type leg topology



The electrical part of the model is shown in Figure 3. The inverter uses an ideal DC source for powering the DC link. The Vienna rectifier is specific for its two capacitors on the DC side and voltage balancing. Each of the output capacitors is chosen to be 100 µF in order to allow a slow output voltage loop. The grid-side connection of the inverter is implemented using a LC filter. The suggested parameters of the filter for this model are Ci= 3.09 µF, L=30 mH, Cd=7.73 µF, and Rd=13.68 Ω (theses parameters are set in the Model Initialization panel).

Figure 3: Typhoon HIL schematic of a three-phase Vienna rectifier



The control part, shown in Figure 4, consists of voltage (top center) and current regulation loops (center). DC link balancing is also demonstrated (top right).

Figure 4: Current and voltage loop



Typically, the outer (voltage) loop is designed for DC link voltage regulation, while the inner (current) loop is used to control the AC input current. The DC link voltage error is fed to a proportional and integral (PI) regulator, and the output of the PI regulator is fed to the inner current loop as the D-channel current reference (Id_ref). For the unity power factor case, the Q-channel current reference is set to 0. For the three-level neutral point clamping topology, an additional DC voltage balance control loop is required, because, in this case, there are two capacitors at the output and it is important that the output voltage is evenly distributed.
Table 1. HIL device resource utilization
No. of processing cores 1
Max. matrix memory utilization 90.19%
Max. time slot utilization 85.33%
Simulation step, electrical 1µs
Execution rate, signal processing 100µs

Simulation

Figure 5: Vienna rectifier SCADA panel



This rectifier is designed so that the voltage on the DC link remains constant regardless of the applied load, in this case 800V. The simulation starts with a 200 Ω resistive load (R4). Seeing that the control is stable and the output voltage is 800V, a 300Ω resistor (R15) can be connected in parallel by checking the Load Step 1 checkbox. After a transient dip of about 2s, the voltage at the DC link returns to 800V, as can be seen in Figure 6. The DC link voltage also remains 800V during asymmetrical loading. If we close the S3 contactor using the “Load Step 2” checkbox, which adds a 150 Ω resistor (R16) model-wise in parallel with C17 output capacitor, the DC link remains relatively close within the 800V range (+/-4V). This is shown in Figure 7 .

Figure 6: DC voltage dip with an increased input currents with a symmetrical load



Figure 7: DC voltage dip and input currents with an asymmetrical load



The DC link voltage also remains at 800V if one of the switches (S1 or S4) is closed, but the current waveform is deformed. This case is shown in Figure 8.

Figure 8: DC voltage and input currents with a switch fault scenario



Table 2. Minimum requirements
Files
Typhoon HIL files

examples\models\aerospace\npc t-type vienna rectifier

npc t-type vienna rectifier.tse,

npc t-type vienna rectifier.cus

TyphoonTest IDE script examples\tests\103_npc_t_type_vienna_rectifier

test_npc_t_type_vienna_rectifier.py

Minimum hardware requirements
No. of HIL devices 1
HIL device model HIL402
Device configuration 1