Aircraft power system engineering

High power density aerospace grade battery systems.

Back fit Lithium Iron Phosphate batteries system that are:

  • Designed for starting turbine engines where high currents are needed for a few minutes or less.
  • Designed for 28 volt DC with 20, 40 or 60 AMP hours capacity.
  • Incorporate a battery management system (BMS) is scalable to 1000 Amps and 1000 Volts
  • Reduce battery weight by 60%
  • Provide lower starting temperatures
  • Provide more start cycles between replacement    

 

Retrofit of legacy aircraft power and control systems with high reliability, light weight, solid state components

Providing engineered solutions to address your legacy parts reliability / availably issues:

  • Replacement of reverse current relays with schottky diodes
  • Retrofit mechanical relays with power MOSFETS
  • Replacement of speed (dropping) resistors with PWM controllers