Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Zhenbo Xie"'
Publikováno v:
Sensors, Vol 24, Iss 22, p 7340 (2024)
The detection of bolt loosening in key components of aircraft engines faces problems such as complex and difficult-to-establish bolt loosening mechanism models, difficulty in identifying early loosening, and difficulty in extracting signal features w
Externí odkaz:
https://doaj.org/article/05b8cae2b34c4076b804b82836a8e186
Publikováno v:
Metals, Vol 13, Iss 10, p 1705 (2023)
In order to deeply explore the high-temperature cyclic characteristics of the FGH96 superalloy under different strain amplitudes, the high-temperature low-cycle fatigue behavior of the FGH96 superalloy was analyzed from the perspective of internal st
Externí odkaz:
https://doaj.org/article/7f8895d617f94bccb62310f83be89d3c
Publikováno v:
IEEE Transactions on Instrumentation and Measurement. 71:1-10
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87757b0045c3b79bb5e38e7222052e98
https://doi.org/10.1109/tim.2022.3149094
https://doi.org/10.1109/tim.2022.3149094
Publikováno v:
Sustainability; Volume 15; Issue 1; Pages: 29
The non-convergence and low efficiency of the thermodynamic model make them difficult to be used in the aero-engines degradation evaluation, while the negligence of the thermodynamics process of data-driven degradation evaluation methods makes them i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::264f1cf34e0f5d52c1a6465ed1bcd058
Publikováno v:
Sustainability; Volume 14; Issue 10; Pages: 6373
Traditional thermodynamic models for military turbofans suffer from non-convergence and inaccuracy due to inaccuracy of the component maps and the instability of the iterative process. To address these problems, a thermodynamically oriented and neura
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f29e006a4fe9c40757902a0f541a75d0
Publikováno v:
Journal of Physics: Conference Series. 1678:012020
To study the anti-foreign object damage (FOD) ability of aero-engine compressor blades, finite element model of compressor blades was established. Blades damage was evaluated with different steel ball diameters and shock angles. Results show that the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18948089aa4dbc32c12f5aeed50512ef
https://doi.org/10.1088/1742-6596/1678/1/012020
https://doi.org/10.1088/1742-6596/1678/1/012020