Advances in prognostics and health management for aircraft landing gear—progress, challenges, and future possibilities
Prognostics and health management (PHM) has developed into a crucial discipline because
of its never-ending pursuit of safety, effectiveness, and dependability. The aircraft Landing …
of its never-ending pursuit of safety, effectiveness, and dependability. The aircraft Landing …
Effect of WC particle size on the microstructural evolution and tribological properties of laser cladding Ti-bearing Co-based WC reinforced coating
F Ji, C Luo, M Pang, Z Qian - Surface and Coatings Technology, 2024 - Elsevier
To improve the wear resistance of 300 M steel under reciprocating wear in landing gear
shock strut, Ti-bearing Co-based WC reinforced coatings with three different WC particle …
shock strut, Ti-bearing Co-based WC reinforced coatings with three different WC particle …
Effect of surface nano-crystallization induced by supersonic fine particles bombarding on microstructure and mechanical properties of 300M steel
T Zhou, Y Xiong, Z Chen, X Zha, Y Lu, T He… - Surface and Coatings …, 2021 - Elsevier
Supersonic fine particles bombarding (SFPB) technology opens a new territory for
engineering materials towards improved performances. Owing to its merits and emerging …
engineering materials towards improved performances. Owing to its merits and emerging …
Investigation of temperature assisted corrosion failure of an aircraft turbine blade
S Khushbash, A Hameed, A Mumtaz, HA Khan… - Engineering Failure …, 2025 - Elsevier
In this study, the root cause of a recurring corrosion problem at the tip of an internally cooled
high-pressure turbine blade (HPT) of a turbofan engine was investigated. A two-pronged …
high-pressure turbine blade (HPT) of a turbofan engine was investigated. A two-pronged …
Microstructure Evolution and Properties of Gradient Nanostructures Subjected to Laser Shock Processing in 300M Ultrahigh‐Strength Steel
Y Ma, Y Xiong, Z Chen, X Zha, T He, Y Li… - steel research …, 2022 - Wiley Online Library
Herein, gradient nanostructures (GNs) are created in 300M ultrahigh‐strength (UHS) steel
by laser shock processing (LSP). Microstructure evolution and properties of GNs subjected …
by laser shock processing (LSP). Microstructure evolution and properties of GNs subjected …
Strain rate effects of dynamic-driven high dislocation densities in the ultra-high strength Ferrium S53 steel
S Zheng, X Liu, L Fang, L Xiao, L Guo, H Feng… - Materials Today …, 2024 - Elsevier
Ultra-high strength steels achieve exceptional strength and toughness through precipitation
strengthening, of which the properties and structure have absorbed lots of attentions …
strengthening, of which the properties and structure have absorbed lots of attentions …
Investigation of failure and development of mitigation techniques of a cracked aircraft wing spar cap
The research is aimed to identify the failure mechanism which leads to cracks development
in the wing spar cap of a transport aircraft and subsequently devise a mitigation strategy to …
in the wing spar cap of a transport aircraft and subsequently devise a mitigation strategy to …
Failure analysis on abnormal cracking of the main landing gear door of a civil aircraft
TH Jiang, ZG Yang - Engineering Failure Analysis, 2024 - Elsevier
Among the myriad structural and moving components integral to civil aircraft, only a select
few confront the dual challenges of meeting aerodynamic and mechanical performance …
few confront the dual challenges of meeting aerodynamic and mechanical performance …
Failure analysis of a cracked cylinder block assembly of an aircraft brake system
This study contains the analysis of a cylinder block assembly of an aircraft brake system that
failed due to the formation of cracks. The failure analysis was performed using a two-prong …
failed due to the formation of cracks. The failure analysis was performed using a two-prong …
Crack growth life calculation approach of surface cracked landing gear strut under eccentric compression load by bulging effect
L Zhang, X Wei - International Journal of Fatigue, 2023 - Elsevier
The landing gear strut is mainly subjected to eccentric compression load during service, and
the calculation of its stress intensity factor is often considered as a challenge to calculate the …
the calculation of its stress intensity factor is often considered as a challenge to calculate the …