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- W3090994094 abstract "Reliability and durability of aeronautical components and systems are directly influenced by fatigue, which is perhaps the most prominent mode of their failure. Quality aspects like surface integrity affect component reliability, and in turn determine system safety. Quality–reliability–risk–safety paradigm is thus self-reinforcing, either as a vicious or a virtuous cycle. System safety principles, originally proposed by Joseph H. Saleh, are high-level, domain-independent and technologically agnostic principles built on the notion of level of safety hazard and its escalation to accident sequence. They include (i) fail-safe safety principle, (ii) safety margin principle, (iii) ungraduated-response principle, (iv) defence-in-depth principle, (v) observability-in-depth principle; to which (vi) human factors principle and (vii) integration-in-totality principle can be added. Reliability of the component, and safety of the system, can be effectively examined by applying these cardinal principles. The technical article brings out a few case studies related to fatigue failure of aero-engine and aircraft components, analyzing the progression of failure in light of the system safety principles. Suitable remedial measures are recommended to obviate the destructive manifestation of fatigue damage, like improving stiffness and fatigue strength, enhancing attenuation/damping, monitoring fatigue life consumption, isolating contributory factors, etc. so that crack initiation and propagation can be controlled by early anticipation, regular monitoring and timely actions. Fatigue fracture failure of airborne systems can be effectively analyzed using Functional Resonance Analysis Method (FRAM) propounded by Erik Hollnagel. The paper demonstrates the use of ‘FRAMED-IN-FRAM® Diagram’ developed by the authors, an improved version of the ‘FRAM Diagram’, for understanding the combinational, resonant and temporal aspects related to the emergence of a safety hazard consequent to fatigue deterioration of the component. The authors also introduce a new concept of ‘Reflexive Resonance’ using FRAMED-IN-FRAM® Diagram for analyzing and depicting the vulnerability/durability of fatigue-damage-prone components and systems." @default.
- W3090994094 created "2020-10-08" @default.
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- W3090994094 date "2020-10-02" @default.
- W3090994094 modified "2023-10-06" @default.
- W3090994094 title "Quality-Reliability-Risk-Safety Paradigm—Analyzing Fatigue Failure of Aeronautical Components in Light of System Safety Principles" @default.
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- W3090994094 doi "https://doi.org/10.1007/978-981-15-4779-9_18" @default.
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