1995-05-01

A Candidate Electrical Power System for Next Generation Military Aircraft 951425

An electrical system composed of an integral main engine electrical starter/generator and a power management and distribution system for a high performance more electric airplane is presented. The paper emphasizes the fault tolerance and high reliability requirements and discusses the necessary architecture to satisfy them. A number of critical technical issues associated with the more electric airplane, such as severe EMI environment, regenerative power, and system integration and stability are discussed.

SAE MOBILUS

Subscribers can view annotate, and download all of SAE's content. Learn More »

Access SAE MOBILUS »

Members save up to 18% off list price.
Login to see discount.
Special Offer: Download multiple Technical Papers each year? TechSelect is a cost-effective subscription option to select and download 12-100 full-text Technical Papers per year. Find more information here.
We also recommend:
TECHNICAL PAPER

Power Management and Distribution System for a More-Electric Aircraft (MADMEL) - Program Status

1999-01-2547

View Details

TECHNICAL PAPER

Comparison of All-Electric Secondary Power Systems for Civil Transport

929493

View Details

TECHNICAL PAPER

Study on Main Engine Start for More Electric Architecture Aircraft

2006-01-3071

View Details

X