This is a compact, 30-V DC, 400-W reference design for avionics applications, accepting main frequencies between 400 Hz and 800 Hz. This design consists of a front-end, two-phase interleaved transition mode (TM) power factor correction (PFC) based on UCC28064A. This minimizes the PFC inductor size and reduces EMI filter requirements. The DC/DC is implemented by employing HB-LLC stage, using UCC256404. For efficiency improvement, synchronous rectification is used at secondary side with FETs driven by UCC24612.
| Output voltage options | PMP30763.1 | PMP30763.2 |
|---|---|---|
| Vin (Min) (V) | 96 | 200 |
| Vin (Max) (V) | 134 | 260 |
| Vout (Nom) (V) | 240 | 30 |
| Iout (Max) (A) | 1.8 | 13.3 |
| Output Power (W) | 432 | 399 |
| Isolated/Non-Isolated | Non-Isolated | Isolated |
| Input Type | AC | DC |
| Topology | PFC- Multiphase | Half Bridge- LLC |
A fully assembled board has been developed for testing and performance validation only, and is not available for sale.
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Test results for the reference design, including efficiency graphs, test prerequisites and more
Detailed schematic diagram for design layout and components
Complete listing of design components, reference designators, and manufacturers/part numbers
Detailed overview of design layout for component placement
Files used for 3D models or 2D drawings of IC components
Design file that contains information on physical board layer of design PCB
PCB layer plot file used for generating PCB design layout
Includes TI products in the design and potential alternatives.
| Type | Title | Date | ||
|---|---|---|---|---|
| * | Test report | 93% Efficiency, 400-W AC/DC Reference Design for Avionics | Mar. 27, 2020 |
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