Failure analysis of an aircraft propeller
Source abstract
Abstract
Abstract Safe operation of an aircraft depends strongly on periodic inspection of high risk parts, particularly rotating parts that are subjected to complex dynamic loads. For the highest level of flight safety, maintenance rules, such as limits and intervals should be applied carefully. This paper describes the root cause of a fracture mechanism in an Cessna-185 aircraft propeller blade due to FOD induced fatigue crack propagation.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Advanced Sensor Technologies Research · Mechanical Failure Analysis and Simulation · Rocket and propulsion systems research
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References (5)
Show source-provided references
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2. Failure of aircraft propeller assembly10.1016/j.engfailanal.2003.08.002 ↗
3. Hellenic Armed Forces,; 2006.
4. Kushan MC, Zafer N. Structure materials of aeroplanes (in Turkish), I. Ulusal Metalurji ve Malzeme Günleri (Prod. Conf.), Eskişehir, Turkey; May 27–28, 2004. p. 368.
5. Kushan MC, Erdem M, Saracyakupoglu T. EB Varestraint test method and an application. In: 23rd ICAS Congress, Toronto, Canada; 8–13 September 2002.