Enhanced electromagnetic-interference shielding effectiveness and mechanical strength of Co-Ni coate

来源 :中国航空学报(英文版) | 被引量 : 0次 | 上传用户:n464j7428bh
下载到本地 , 更方便阅读
声明 : 本文档内容版权归属内容提供方 , 如果您对本文有版权争议 , 可与客服联系进行内容授权或下架
论文部分内容阅读
An efficient method was proposed to prepare high-performance conductive Aramid-Carbon Blend Fabrics (ACBF) with cobalt-nickel (Co-Ni) alloy coatings,which is conducive to industrial production.The grid-like substrate composed of aramid and carbon fibers was innova-tively used in flexible Electromagnetic Interference (EMI) shielding materials.The natural network structure is advantageous to the uniform deposition of metal particles to the establishment of con-ductive pathways subsequently in order to improve conductivity.The induction of a synergistic effect from Electromagnetic (EM) wave-reflection and EM wave-absorption through the whole carbon-Co-Ni-ternary system notably enhanced the EMI Shielding Effectiveness (SE) value to an average of 42.57 dB in the range of 30-6000 MHz.On the other hand,together with the inherent toughness of the alloy coatings,the tensile strength of the aramid fibers used for bulletproof made a significant contribution to the desired mechanical properties.The light weight of the resultant composite made it applicable to aerospace vehicles simultaneously.X-ray Photoelectron Spectroscopy (XPS) was conducted to investigate the variations of elements and groups on the sample surface in pre-treating process.The elemental components and surface morphologies of fabric samples during dif-ferent stages of the process were investigated by Scanning Electron Microscope (SEM) and Energy Dispersive spectrometer (EDX) measurements.X-Ray Diffraction (XRD) results indicated that the obtained Co-Ni alloy coating had a combined Hexagonal Closed-Packed (HCP) and Faced-Centered Cubic (FCC) crystalline phase.The relatively high corrosion resistance demonstrated in different acid and alkaline conditions was instrumental in more complex environments as well.
其他文献
The low-speed wind tunnel experiment is carried out on a simplified aircraft model to explore the influence of wing flexibility on the aircraft aerodynamic performance.The investigation involves the measurements of force,membrane deformation and velocity
SiCp/Al composites are difficult-to-cut materials.In recent years,electrical arc discharge machining has been developed to improve the machinability of these materials.However,there is a big challenge to build a satisfactory heat transfer model of SiCp/Al
Electrically Controlled Rotor (ECR),also called as swashplateless rotor,applies blade pitch inputs via trailing-edge flaps system instead of traditional swashplate mechanism.In addition to primary control,rotor vibration reduction and noise alleviation ar
The present study performed a numerical investigation to explore the performance enhancement of a co-flow jet (CFJ) airfoil with simple high-lift device configuration,with a specific goal to examine the feasibility and capability of the proposed configura
Emissions produced by the aviation industry are currently a severe environmental threat;therefore,aviation agencies and governments have set emission targets and formulated plans to restrict emissions within the next decade.Hybrid aircraft technology is b
In this paper fretting fatigue crack behavior in 1045 steel is studied by in-situ observation and finite element analysis,in-situ fretting fatigue experiments are conducted to capture real-time fretting fatigue crack formation and propagation process.The
Reasonable and effective fatigue load spectrum is key of aircraft structural fatigue test.Two kinds of load spectra simplification approaches based on statistical consistent fatigue damage model are proposed in the paper.One method is to simplify the orig
The multiple jets impingement heat transfer is widely applied in the wing anti-icing sys-tem.It is challenging to apply the similarity criterion to carry out the anti-icing experiments due to the complex flow and heat transfer behavior.In the present stud
Research on the transition phase of tail-sitter Unmanned Aerial Vehicles (UAVs) is cru-cial for trajectory planning and performance analysis.This study focuses on the analysis of the tran-sition characteristics and path of a small dual-rotor tail-sitter U
This paper addresses the robust attitude control problem for quadrotors subject to model mismatch and disturbances.A dynamic inversion based attitude control scheme is proposed,which consists of an outer loop attitude controller and an inner loop angular