NASA NTRS · 19990045905
Load Distribution in Transmissions "Split"
Abstract
The transmission system of a helicopter must meet particularly critical requirements. It must transmit engine power to the rotor, at the same time ensuring a typical speed reduction of 60 to 1. It must also be safe, reliable, light, and reach a high level of performance while, at the same time, it must produce few vibrations and little noise. Helicopter transmissions have achieved high-level performances thanks to the combination of analyses, experiments, and the application of practical field experience. However, the new generation of helicopters will require transmission systems that are even safer, lighter, less noisy, and more reliable.
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Krantz, Timothy L., Delgado, Irebert R.. 1998-01-01. Load Distribution in Transmissions "Split". https://ntrs.nasa.gov/citations/19990045905
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