Dynamic Modeling and Active Vibration Control for the Integrated Composite Laminates with Embedded Mfcs DOI
Yu Zhang, Wei Sun, Hui Zhang

и другие.

Опубликована: Янв. 1, 2024

A novel integrated composite laminate (ICL) with embedded macro-fiber composites (MFCs) is proposed to improve the vibration reduction performance of thin-walled structures. Its dynamic modeling and active suppression are investigated. The structure can not only achieve good but also provide protection for MFCs, while related experimental studies rarely reported in published works. This paper proposes a general method ICL MFCs. Considering piezoelectric effect MFC material, semi-analytical model established by combining first-order shear deformation theory Lagrange equation. On this basis, state-space equation control calculation design Proportional-Integral-Derivative (PID) controller given. Furthermore, preparation specimen MFCs introduced, an system capable testing built. comparative results simulations experiments demonstrate accuracy approach effectiveness capability structure. Finally, effects fiber distribution angle on structural modal characteristics damping investigated, influence laws skin plate thickness PID parameters revealed. findings new technical

Язык: Английский

Integrated design of intelligent structures for composite laminates with embedded MFCs: Theoretical modeling and experimental study DOI
Yu Zhang, Wei Sun, Hui Zhang

и другие.

Composite Structures, Год журнала: 2025, Номер 357, С. 118913 - 118913

Опубликована: Фев. 7, 2025

Язык: Английский

Процитировано

4

Modeling and free vibration analysis of bolted composite flanged cylindrical-cylindrical shells under partial bolt loosening conditions DOI
Honghao Liu, Wei Sun, Xiaofeng Liu

и другие.

Thin-Walled Structures, Год журнала: 2024, Номер 199, С. 111853 - 111853

Опубликована: Апрель 2, 2024

Язык: Английский

Процитировано

8

Vibration of bolted composite cylindrical-cylindrical flanged shells considering contact characteristics DOI
Honghao Liu,

Wei Sun,

Xiaofeng Liu

и другие.

International Journal of Mechanical Sciences, Год журнала: 2024, Номер 280, С. 109545 - 109545

Опубликована: Июль 8, 2024

Язык: Английский

Процитировано

8

Modeling and Dynamic Analysis of a Rotating Shaft-Disk System with Contact Friction at the Bolted Interface DOI
Yulin Jiang,

Yazheng Zhao,

Hongyuan Cao

и другие.

Опубликована: Янв. 1, 2025

Highly loaded rotor systems, such as those in aero-engines, exhibit complex vibration behaviors due to the discontinuities bolted structure, which generate friction at connection interfaces. This leads nonlinear dynamics for system. A dynamic model of system is established using finite element theoretical Methods, incorporating connections around entire circumference. The procedure assessing stick-slip states bolts different positions during motion provided. study examines phenomenon interface under various conditions, including preload values, rotational speeds, bolt numbers, and coefficients. Trends equivalent stiffness energy dissipation these conditions are analyzed. Additionally, critical force each stage speeds discussed. region viscous-slip-shear state also presented. research introduces a modeling approach understanding characteristics systems operating viscous-slip regime their It provides an analytical that serves foundation design calculation interfaces engineering applications.

Язык: Английский

Процитировано

0

Composite-airfoil-plate with embedded macro-fiber-composites: Aero-thermo-electro vibration analysis and active control DOI
Yu Zhang, Hui Zhang, Hongwei Ma

и другие.

International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110143 - 110143

Опубликована: Март 1, 2025

Язык: Английский

Процитировано

0

Dynamic modeling of a shaft-disk system considering bolted interface friction DOI
Yulin Jiang,

Yazheng Zhao,

Hongyuan Cao

и другие.

International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110332 - 110332

Опубликована: Май 1, 2025

Язык: Английский

Процитировано

0

Effective contact stiffness model for bolted flange joint with spigot DOI

Yuan Song Cui,

Yan Qing Wang

International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110213 - 110213

Опубликована: Апрель 1, 2025

Язык: Английский

Процитировано

0

Recent advancement in surface modification of aramid fiber assisted by supercritical carbon dioxide DOI
Jigar Patadiya,

Prajakta Vilas Chougale,

Minoo Naebe

и другие.

Polymers for Advanced Technologies, Год журнала: 2023, Номер 34(12), С. 3748 - 3758

Опубликована: Авг. 27, 2023

Abstract The exceptional mechanical properties of aramid fibers make them a popular choice for high‐performance materials; despite that, their potential is limited due to surface bonding energy and interfacial strength with matrix materials. enhanced resistance poly‐aramid (AFs) severe surroundings improved interlaminar adhesion in sandwich compounds admirable characteristics are becoming great challenge various chemical physical treatment techniques. Supercritical carbon dioxide (scCO 2 ) sustainable approach that can effectively bond homogeneously deposit functional groups or nanoparticles exhibit the excellent performance fibber modification. This article examines fibers' modification advancements using scCO ‐assisted techniques, including monomer grafting, impregnation, functionalization nanoparticles. Additionally, discusses challenges faced fiber what future holds this technology.

Язык: Английский

Процитировано

8

Failure modes of laminated porous panel with different connection methods DOI

Junling Zou,

Qingtian Deng,

Xueli Song

и другие.

Structures, Год журнала: 2024, Номер 68, С. 107245 - 107245

Опубликована: Сен. 12, 2024

Язык: Английский

Процитировано

0

Vibration Analysis and Active Control of Irregular Integrated Composite Sandwich Plates with Incompletely Constrained Boundaries DOI
Yu Zhang, Wei Sun, Hui Zhang

и другие.

Опубликована: Янв. 1, 2024

Studies on active vibration suppression and analysis of integrated composite sandwich plates (ICSPs) embedded macro-fiber composites (MFC) have been rarely studied in previous papers, especially with incompletely constrained boundaries irregular geometric shapes. This paper aims to provide a new structural design for thin-walled structures such as aircraft wings improve the anti-vibration performance study influence modal damping characteristics structures. The dynamic model ICSPs considering piezoelectric effect is established based first-order shear deformation theory (FSDT) Lagrange equation. influences shapes incomplete constraint are introduced into through coordinate mapping artificial spring technology. test pieces ICSP prepared, experimental system which can be used testing control, established. On this basis, accuracy proposed modeling method reduction verified by combining finite element results. Moreover, frequency veering behavior caused change position segment analyzed, some interesting phenomena length revealed. boundary conditions control parameters discussed. Some research results helpful reference similar

Язык: Английский

Процитировано

0