PMP31164

100-W CCM PFC boost reference design for avionics

PMP31164

Design files

Overview

This board is a compact, 360VDC, 100W reference design for avionics applications, working with mains voltage range 90VAC to 130VAC and frequency range 400Hz to 800Hz. A single-phase continuous conduction mode (CCM) power factor correction (PFC) based on the UCC28180 is used to correct power factor and at the same time to minimize harmonic content of input current.

Features
  • Simple single-phase PFC Boost with UCC28180         
  • Designed for avionics applications         
  • Covers 400Hz to 800Hz range         
  • 118.75mm × 47.63mm PCB     
Output voltage options PMP31164.1
Vin (Min) (V) 90
Vin (Max) (V) 130
Vout (Nom) (V) 360
Iout (Max) (A) .28
Output Power (W) 100.8
Isolated/Non-Isolated Non-Isolated
Input Type AC
Topology Boost- PFC^PFC- Boost
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A fully assembled board has been developed for testing and performance validation only, and is not available for sale.

Design files & products

Design files

Download ready-to-use system files to speed your design process.

PDF | HTML
TIDT378.PDF (1192 K)

Test results for the reference design, including efficiency graphs, test prerequisites and more

TIDMCM3.PDF (188 K)

Detailed schematic diagram for design layout and components

TIDMCM4.PDF (235 K)

Complete listing of design components, reference designators, and manufacturers/part numbers

TIDMCM5.PDF (164 K)

Detailed overview of design layout for component placement

TIDMCM7.ZIP (553 K)

Files used for 3D models or 2D drawings of IC components

TIDCGM8.ZIP (99 K)

Design file that contains information on physical board layer of design PCB

TIDMCM6.PDF (594 K)

PCB layer plot file used for generating PCB design layout

Products

Includes TI products in the design and potential alternatives.

AC/DC & DC/DC controllers (external FET)

UCC2818018-kHz-250-kHz CCM PFC controller with enhanced startup & transient response

Data sheet: PDF | HTML

Technical documentation

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Type Title Date
Test report 100W CCM PFC Boost Converter Reference Design for Avionics PDF | HTML Feb. 12, 2024

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