DESIGN OF AIRCRAFT ELECTRIC POWER SUPPLY SYSTEMS
Abstract
The report describes the possible variations of aircraft electric power systems. It discusses the merits and faults of types of current, generators, equipment, conductors, drives. Numerous circuit diagrams show how to avoid catastrophy in case of failure of individual power sources, lines, convertors, etc. The most promising types and systems are recommended. An example of a draft of an airplane's power system is given.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 06, 1969
- Accession Number
- AD0697985
Entities
People
- G. D. Vlasov
Organizations
- United States Army Foreign Science and Technology Center