Technology Impact on Helicopter, Tilt Rotor, and Tilt Fold Rotor Concepts

VFS-F40-1158

5/16/1984

Authors
Abstract
Content

This paper initially presents historical weight trends of the major subsystems of helicopters that also apply to tilt rotor and tilt fold rotor aircraft. These data reveal that the helicopter industry is responding to customer requirements for a faster, smoother rotorcraft and is building a lighter weight, lower cost aircraft with higher productivity. Implementation of emerging technology in the major subsystems of the helicopter indicates that this trend will continue into the next decade. The impact of this technology on total aircraft productivity is then presented. In addition, it is shown that advanced rotorcraft concepts like the tilt rotor and the tilt fold rotor will benefit even more from emerging technology than the conventional helicopter.

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DOI
https://doi.org/10.4050/VFS-F40-1158
Citation
Matthys, C. and Scroggs Jr., E., "Technology Impact on Helicopter, Tilt Rotor, and Tilt Fold Rotor Concepts," Forum 40 - Arlington, VA 1984, Arlington, VA, May 16, 1984, https://doi.org/10.4050/VFS-F40-1158.
Additional Details
Publisher
Published
5/16/1984
Product Code
VFS-F40-1158
Content Type
Technical Paper
Language
English