Fault Tolerant Power Supply for Aircraft Store Interface

Harminder Singh Johar; Abhijit Bhattacharyya; Srinivas Rao S

doi:10.14429/dsj.72.17737

Harminder Singh Johar DRDO - Research Centre Imarat, Hyderabad - 500 069, India https://orcid.org/0000-0001-6716-1843
Abhijit Bhattacharyya DRDO - Defence Research and Development Laboratory, Hyderabad – 500 058, India
Srinivas Rao S Electrical Engg. Deptt. NIT, Warangal, Telangana - 506 004, India https://orcid.org/0000-0003-2777-7429

DOI: https://doi.org/10.14429/dsj.72.17737

Keywords: Hold-up capacitor, MIL-STD-704F, GOST-19705-89, MIL-STD-461F, MIL-STD-810G

Abstract

This paper brings out the design of a fault-tolerant power supply unit for the aircraft-store interface. This switched mode power supply provides multiple 30 V regulated and isolated DC outputs required for pre-launch preparations and auto-launch operations of avionic sub-systems in a store. 3Ø-115V-400Hz-AC supply as well as 27V-DC supply are available from a fighter aircraft for powering up of any store. Power (wattage) output from 27V/10A DC is inadequate to power up various onboard avionic sub-systems in guided stores involving seekers and other avionics. Hence, it is planned to convert available high power 3Ø-115V-400Hz-AC supply for applications requiring higher wattages (of the order of 500 watts or more). This power supply provides multiple output options of 30V regulated and isolated DC supply with multiple input supplies from Aircraft, viz. 3Ø-115V-400Hz-AC, 1Ø-115V-400Hz-AC and 27V DC. One of the outputs provided is with hold-up capacitors, to cater for any input power interruptions as per requirements of MIL-STD-704F and GOST-19705-89 standards. This power supply is a ready-to-connect device and essentially consists of housing, components of DC to DC conversions, EMI/EMC filters, solid state power controllers, control switches, and control circuitry for monitoring signals.