TY - GEN
T1 - Integrated aircraft risk analysis framework for health monitoring systems – a case study for structural health monitoring
AU - Steinweg, Dominik M.
AU - Hornung, Mirko
N1 - Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - Commercial aviation is characterized by severe competition and rigorous safety requirements. Even though dedicated Structural Health Monitoring (SHM) systems have been proposed over 70 years ago to improve airframe maintenance efficiency and enable lighter structures, a widespread commercial use failed to appear until today. In this line, an integrated analysis framework is proposed, connecting monitoring performance to potential useful life extensions considering structural fatigue. The analyzed monitoring system relies either on SHM or operational loads monitoring (OLM) alone or a combination of both, utilizing either the Dempster–Shafer theory (DST) or a Hidden Markov Model (HMM) for information fusion. Using this approach, the influence of varying SHM performance characteristics is evaluated for a representative part under varying loadings and initial crack distributions. Results indicate that the commercial usage of SHM is only economically viable in combination with OLM, enabling significant gains in useful life, impossible with independent SHM systems. It is argued that emerging unified data platforms providing usage statistics over the entire aircraft lifecycle serve as enabler for the broad introduction of SHM in commercial aviation.
AB - Commercial aviation is characterized by severe competition and rigorous safety requirements. Even though dedicated Structural Health Monitoring (SHM) systems have been proposed over 70 years ago to improve airframe maintenance efficiency and enable lighter structures, a widespread commercial use failed to appear until today. In this line, an integrated analysis framework is proposed, connecting monitoring performance to potential useful life extensions considering structural fatigue. The analyzed monitoring system relies either on SHM or operational loads monitoring (OLM) alone or a combination of both, utilizing either the Dempster–Shafer theory (DST) or a Hidden Markov Model (HMM) for information fusion. Using this approach, the influence of varying SHM performance characteristics is evaluated for a representative part under varying loadings and initial crack distributions. Results indicate that the commercial usage of SHM is only economically viable in combination with OLM, enabling significant gains in useful life, impossible with independent SHM systems. It is argued that emerging unified data platforms providing usage statistics over the entire aircraft lifecycle serve as enabler for the broad introduction of SHM in commercial aviation.
UR - http://www.scopus.com/inward/record.url?scp=85088677799&partnerID=8YFLogxK
U2 - 10.2514/6.2020-1453
DO - 10.2514/6.2020-1453
M3 - Conference contribution
AN - SCOPUS:85088677799
SN - 9781624105951
T3 - AIAA Scitech 2020 Forum
BT - AIAA Scitech 2020 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2020
Y2 - 6 January 2020 through 10 January 2020
ER -