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Determination of the Operational Environment of the Propeller Blades on Beech 1900D Aircraft
Technical Paper
2008-01-2226
ISSN: 0148-7191, e-ISSN: 2688-3627
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Language:
English
Abstract
Data obtained from digital flight data recorders are used to assess the actual operational environment of propellers on a fleet of Beech 1900D aircraft in commuter role. Information is given on various aerodynamic parameters as well as those pertaining to engine and propeller usage. The takeoff rotation has been identified as the most demanding phase of flight in terms of unsteady loads exerted on the propeller blades. Special attention is paid to ground operations.
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Authors
Citation
Dorfling, J., Kliment, L., Rokhsaz, K., DeFiore, T. et al., "Determination of the Operational Environment of the Propeller Blades on Beech 1900D Aircraft," SAE Technical Paper 2008-01-2226, 2008, https://doi.org/10.4271/2008-01-2226.Also In
References
- “Survey of Causes and Damage Leading to Cracks in Propeller Blades and Hubs,” January 24 2006
- Jane’s All the World’s Aircraft 2004–2005 Franklin Watts New York 2004
- 36 41 20 November 2007
- Harlament, W. B. Edinger, R. “Development of an Aircraft Composite Propeller,” SAE Paper 790579 , Society of Automotive Engineers, Business Aircraft Meeting and Exposition 3–6 Apr 1979