A thesis submitted to the Faculty of Engineering, University of the
Witwatersrand, Johannesburg, in fulfillment of the requirements for the
degree of Master of Science in Engineering. / The use of advanced composite materials in helicopter rotor systems offers
opportunities for improvements in aerodynamic geometry, performance,
weight, damage tolerarice, maintenance and operating costs. Technical aspects
of the design and analysis and the-practical aspects of the manufacture of a
composite rotor system are discussed herein. The rotor system was compared
to an existing conventional teetering rotor system, in order to establish the
viability of the new composite rotor system,
This rotor system reduced the number of components by 55% and the manufacturing time by half, due to the simplicity of the design and lay up procedure, thus
making the system economically more viable. The mass was predicted to within
1% of that achieved in practice and gave a mass advantage of 50.5% over the
conventional rotor. Static tests identified the failure modes and stress concentration
points, while. the comparative hover tests showed the system to have
±20% less drag. [Abbreviated Abstract. Open document to view full version] / AC2017
| Identifer | oai:union.ndltd.org:netd.ac.za/oai:union.ndltd.org:wits/oai:wiredspace.wits.ac.za:10539/22844 |
| Date | January 1991 |
| Creators | Cohen, Gary, M |
| Source Sets | South African National ETD Portal |
| Language | English |
| Detected Language | English |
| Type | Thesis |
| Format | Online resource (265 leaves), application/pdf |
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