Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Markus Winklberger"'
Publikováno v:
Aerospace, Vol 8, Iss 11, p 320 (2021)
An idealized 1:2 scale demonstrator and a numerical parameter optimization algorithm are proposed to closely reproduce the deformation shape and, thus, spatial strain directions of a real aerodynamically loaded civil aircraft spoiler using only four
Externí odkaz:
https://doaj.org/article/a0738a4bc977408aae3466871b8b70e6
Autor:
Markus Winklberger
Publikováno v:
Markus Winklberger
Lightweight structures are optimized designs with minimal weight and with additional consideration of many boundary conditions. In different fields of engineering there are many reasons to reduce the weight of structures, e.g., to increase the payloa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::aa3e0a920a7574714c021c0085c3641c
Publikováno v:
Procedia Structural Integrity. 42:72-79
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::628fc0c68216af8890c7af4504826ae6
https://doi.org/10.1016/j.prostr.2022.12.008
https://doi.org/10.1016/j.prostr.2022.12.008
Crack Identification in Necked Double Shear Lugs by Means of the Electro-Mechanical Impedance Method
Publikováno v:
Sensors, Vol 21, Iss 1, p 44 (2020)
This contribution investigates fatigue crack detection, localization and quantification in idealized necked double shear lugs using piezoelectric transducers attached to the lug shaft and analyzed by the electro-mechanical impedance (EMI) method. The
Externí odkaz:
https://doaj.org/article/fba2e58618b5487abe63f427f25a5538
Autor:
Markus Winklberger, Martin Schagerl
Publikováno v:
Materialwissenschaft und Werkstofftechnik. 51:284-296
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f476685571c06320dc57a79624c3ff22
https://doi.org/10.1002/mawe.201900220
https://doi.org/10.1002/mawe.201900220
Publikováno v:
Procedia Structural Integrity. 28:1473-1480
This paper investigates a strain-based structural health monitoring (SHM) method for damage detection and propagation assessment in composite sandwich structures. As case example, an idealized Airbus A-340 spoiler is considered. Critical failure mode
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bedecb819a7e11bf18fcc23babcc7934
https://doi.org/10.1016/j.prostr.2020.10.121
https://doi.org/10.1016/j.prostr.2020.10.121
Publikováno v:
Health Monitoring of Structural and Biological Systems XV.
Artificially introduced cracks in necked double shear lugs are monitored using piezoelectric transducers attached to the lug shaft and analyzed by the electro-mechanical impedance (EMI) method with a model-based approach. Numerical simulations with c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2f7d39d672c323e38a792ad15a5725c0
https://doi.org/10.1117/12.2583208
https://doi.org/10.1117/12.2583208
Crack Identification in Necked Double Shear Lugs by Means of the Electro-Mechanical Impedance Method
Publikováno v:
Sensors (Basel, Switzerland)
Sensors, Vol 21, Iss 44, p 44 (2021)
Sensors
Volume 21
Issue 1
Sensors, Vol 21, Iss 44, p 44 (2021)
Sensors
Volume 21
Issue 1
This contribution investigates fatigue crack detection, localization and quantification in idealized necked double shear lugs using piezoelectric transducers attached to the lug shaft and analyzed by the electro-mechanical impedance (EMI) method. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::86d6bc6da519362890a96446a3c82de5
https://pubmed.ncbi.nlm.nih.gov/33374853
https://pubmed.ncbi.nlm.nih.gov/33374853
Fatigue strength and weight optimization of threaded connections in tie-rods for aircraft structures
Publikováno v:
Procedia Engineering. 213:374-382
Tie-rods are connecting elements used in an aircraft and they basically consist of a straight tube and two screwed in adapter ends. In order to optimize the tie-rod in terms of weight reduction a detailed knowledge of its fatigue strength is importan
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f7179ea449bf0453db664d1de3ab8a93
https://doi.org/10.1016/j.proeng.2018.02.037
https://doi.org/10.1016/j.proeng.2018.02.037
Publikováno v:
Engineering Failure Analysis. 126:105454
This paper investigates a strain-based structural health monitoring (SHM) method for damage detection and localization in composite sandwich structures. As case example, an idealized aircraft spoiler of a large civil aircraft is considered. Critical
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbccf897ffbb668b72d4f496b0d2827a
https://doi.org/10.1016/j.engfailanal.2021.105454
https://doi.org/10.1016/j.engfailanal.2021.105454