Determination of the Translational Risk Angle of Uncontained Rotor Fragments
2014; American Institute of Aeronautics and Astronautics; Volume: 51; Issue: 6 Linguagem: Inglês
10.2514/1.c032938
ISSN1533-3868
Autores Tópico(s)Chemical Safety and Risk Management
ResumoNo AccessEngineering NoteDetermination of the Translational Risk Angle of Uncontained Rotor FragmentsDawei Jia and Fanwei SongDawei JiaStress Department, AVIC SAC Commercial Aircraft Company Ltd., 110850 Shenyang, People's Republic of China and Fanwei SongStress Department, AVIC SAC Commercial Aircraft Company Ltd., 110850 Shenyang, People's Republic of ChinaPublished Online:2 Dec 2014https://doi.org/10.2514/1.C032938SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] "Federal Aviation Regulation Part 23—Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes, Subpart E—Powerplant," Federal Aviation Administration, Washington, D.C., 2007, pp. 165–166. Google Scholar[2] "Federal Aviation Regulation Part 25—Airworthiness Standards: Transport Category Airplanes, Subpart E—Powerplant," Federal Aviation Administration, Washington, D.C., 2007, pp. 162–163. Google Scholar[3] "AC 20-128A Design Considerations for Minimizing Hazards Caused by Uncontained Turbine Engine and Auxiliary Power Unit Rotor Failure," Federal Aviation Administration, Washington, D.C., 1997. Google Scholar[4] Federal Register, Federal Aviation Administration, Washington, D.C., Vol. 57, No. 239, 1992, p. 58,844. Google Scholar[5] Federal Register, Federal Aviation Administration, Washington, D.C., Vol. 66, No. 218, 2001, pp. 56,729–56,730. Google Scholar[6] Gong C. and Sun Y.-C., "Research on Harmfulness Assess Model of Aircraft in the Case of Uncontained Turbine Engine Rotor Failure Based on Delmia (in Chinese)," M.S. Thesis, Nanjing Univ. of Aeronautics and Astronautics, Nanjing, PRC, 2010, pp. 32–36. Google Scholar Previous article Next article
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