348 research outputs found

    DISTRIBUTED ELECTRO-MECHANICAL ACTUATION AND SENSING SYSTEM DESIGN FOR MORPHING STRUCTURES

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    Smart structures, able to sense changes of their own state or variations of the environment theyโ€™re in, and capable of intervening in order to improve their performance, find themselves in an ever-increasing use among numerous technology fields, opening new frontiers within advanced structural engineering and materials science. Smart structures represent of course a current challenge for the application on the aircrafts. A morphing structure can be considered as the result of the synergic integration of three main systems: the structural system, based on reliable kinematic mechanisms or on compliant elements enabling the shape modification, the actuation and control systems, characterized by embedded actuators and robust control strategies, and the sensing system, usually involving a network of sensors distributed along the structure to monitor its state parameters. Technologies with ever increasing maturity level are adopted to assure the consolidation of products in line with the aeronautical industry standards and fully compliant with the applicable airworthiness requirements. Until few years ago, morphing wing technology appeared an utopic solution. In the aeronautical field, airworthiness authorities demand a huge process of qualification, standardization, and verification. Essential components of an intelligent structure are sensors and actuators. The actual technological challenge, envisaged in the industrial scenario of โ€œmore electric aircraftโ€, will be to replace the heavy conventional hydraulic actuators with a distributed strategy comprising smaller electro-mechanical actuators. This will bring several benefit at the aircraft level: firstly, fuel savings. Additionally, a full electrical system reduces classical drawbacks of hydraulic systems and overall complexity, yielding also weight and maintenance benefits. At the same time, a morphing structure needs a real-time strain monitoring system: a nano-engineered polymer capable of densely distributed strain sensing can be a suitable solution for this kind of flying systems. Piezoresistive carbon nanotubes can be integrated as thin films coated and integrated with composite to form deformable self-sensing materials. The materials actually become sensors themselves without using external devices, embedded or attached. This doctoral thesis proposes a multi-disciplinary investigation of the most modern actuation and sensing technologies for variable-shaped devices mainly intended for large commercial aircraft. The personal involvement in several research projects with numerous international partners - during the last three years - allowed for exploiting engineering outcomes in view of potential certification and industrialization of the studied solutions. Moving from a conceptual survey of the smart systems that introduces the idea of adaptive aerodynamic surfaces and main research challenges, the thesis presents (Chapter 1) the current worldwide status of morphing technologies as well as industrial development expectations. The Ph.D. programme falls within the design of some of the most promising and potentially flyable solutions for performance improvement of green regional aircrafts. A camber-morphing aileron and a multi-modal flap are herein analysed and assessed as subcomponents involved for the realization of a morphing wing. An innovative camber-morphing aileron was proposed in CRIAQ MD0-505, a joint Canadian and Italian research project. Relying upon the experimental evidence within the present research, the issue appeared concerns the critical importance of considering the dynamic modelling of the actuators in the design phase of a smart device. The higher number of actuators involved makes de facto the morphing structure much more complex. In this context (Chapter 2), the action of the actuators has been modelled within the numerical model of the aileron: the comparison between the modal characteristics of numerical predictions and testing activities has shown a high level of correlation. Morphing structures are characterized by many more degrees of freedom and increased modal density, introducing new paradigms about modelling strategies and aeroelastic approaches. These aspects affect and modify many aspects of the traditional aeronautical engineering process, like simulation activity, design criteria assessment, and interpretation of the dynamic response (Chapter 3). With respect the aforementioned aileron, sensitivity studies were carried out in compliance with EASA airworthiness requirements to evaluate the aero-servo-elastic stability of global system with respect to single and combined failures of the actuators enabling morphing. Moreover, the jamming event, which is one of the main drawbacks associated with the use of electro-mechanical actuators, has been duly analyzed to observe any dynamic criticalities. Fault & Hazard Analysis (FHA) have been therefore performed as the basis for application of these devices to real aircraft. Nevertheless, the implementation of an electro-mechanical system implies several challenges related to the integration at aircraft system level: the practical need for real-time monitoring of morphing devices, power absorption levels and dynamic performance under aircraft operating conditions, suggest the use of a ground-based engineering tool, i.e. โ€œiron birdโ€, for the physical integration of systems. Looking in this perspective, the Chapter 4 deals with the description of an innovative multi-modal flap idealized in the Clean Sky - Joint Technology Initiative research scenario. A distributed gear-drive electro-mechanical actuation has been fully studied and validated by an experimental campaign. Relying upon the experience gained, the encouraging outcomes led to the second stage of the project, Clean Sky 2 - Airgreen 2, encompassing the development of a more robotized flap for next regional aircraft. Numerical and experimental activities have been carried out to support the health management process in order to check the EMAs compatibility with other electrical systems too. A smart structure as a morphing wing needs an embedded sensing system in order to measure the actual deformation state as well as to โ€œmonitorโ€ the structural conditions. A new possible approach in order to have a distributed light-weight system consists in the development of polymer-based materials filled with conductive smart fillers such as carbon nanotubes (CNTs). The thesis ends with a feasibility study about the incorporation of carbon nanomaterials into flexible coatings for composite structures (Chapter 5). Coupons made of MWCNTs embedded in typical aeronautic epoxy formulation were prepared and tested under different conditions in order to better characterize their sensing performance. Strain sensing properties were compared to commercially available strain gages and fiber optics. The results were obtained in the last training year following the involvement of the author in research activities at the University of Salerno and Materials and Structures Centre - University of Bath. One of the issues for the next developments is to consolidate these novel technologies in the current and future European projects where the smart structures topic is considered as one of the priorities for the new generation aircrafts. It is remarkable that scientists and aeronautical engineers community does not stop trying to create an intelligent machine that is increasingly inspired by nature. The spirit of research, the desire to overcome limits and a little bit of imagination are surely the elements that can guide in achieving such an ambitious goal

    Conceptual designs of multi-degree of freedom compliant parallel manipulators composed of wire-beam based compliant mechanisms

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    This paper proposes conceptual designs of multi-degree(s) of freedom (DOF) compliant parallel manipulators (CPMs) including 3-DOF translational CPMs and 6-DOF CPMs using a building block based pseudo-rigid-body-model (PRBM) approach. The proposed multi-DOF CPMs are composed of wire-beam based compliant mechanisms (WBBCMs) as distributed-compliance compliant building blocks (CBBs). Firstly, a comprehensive literature review for the design approaches of compliant mechanisms is conducted, and a building block based PRBM is then presented, which replaces the traditional kinematic sub-chain with an appropriate multi-DOF CBB. In order to obtain the decoupled 3-DOF translational CPMs (XYZ CPMs), two classes of kinematically decoupled 3-PPPR (P: prismatic joint, R: revolute joint) translational parallel mechanisms (TPMs) and 3-PPPRR TPMs are identified based on the type synthesis of rigid-body parallel mechanisms, and WBBCMs as the associated CBBs are further designed. Via replacing the traditional actuated P joint and the traditional passive PPR/PPRR sub-chain in each leg of the 3-DOF TPM with the counterpart CBBs (i.e. WBBCMs), a number of decoupled XYZ CPMs are obtained by appropriate arrangements. In order to obtain the decoupled 6-DOF CPMs, an orthogonally-arranged decoupled 6-PSS (S: spherical joint) parallel mechanism is first identified, and then two example 6-DOF CPMs are proposed by the building block based PRBM method. It is shown that, among these designs, two types of monolithic XYZ CPM designs with extended life have been presented

    Conjoined piezoelectric harvesters and carbon supercapacitors for powering intelligent wireless sensors

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    To achieve total freedom of location for intelligent wireless sensors (IWS), these need to be autonomous. To achivethis today there is a need of broadband piezoelectric energy harvesting and a long-lasting energy. The Harvester needto be able to provide sufficient amount of energy for the intelligent wireless sensor to perform its task. The energystorage needs to fulfill the requirement of a large number of charge discharge cycles and contain sufficient power forthe intelligent wireless sensor.The biggest issue with piezoelectric energy harvesting today is the bandwidth limitation. Solutions today to achievelarger bandwidth make a tradeoff where the output is decreased. The biggest issue for energy storage today is thelimitation of energy density for supercapacitors and the lack of sufficient life cycles for batteries.This thesis aims to realize piezoelectric energy harvesters with broad bandwidth and maintained power output.Moreover, for energy storage in the form of supercapacitors realize an electrode material that has a high effectivesurface area, good conductivity not dependent on a conductive agent and can be used without a binder. This thesiscover background and history of the two fields, discussion of technologies used and presents solutions for piezoelectricenergy harvesting and carbon based supercapacitor storage.A Backfolded piezoelectric harvester was made of two conjoined piezoelectric cantilevers, one placed on top of abottom cantilever. By the backfolded design this thesis show that by utilizing the extended stress distribution of thebottom cantilever a maintained power output is achieved for both output peaks. By introducing asymmetry where thetop cantilever have 80% length compared with the bottom cantilever the bandwidth was increased. An effectivebandwidth of 70 Hz with voltage output above 2,75 V for 1 g is achieved.To achieve further enhanced bandwidth a piezoelectric energy harvester with selftuning was designed. Theselftuning was achieved by a sliding mass on a beam, which is conjoined, to two piezoelectric cantilevers in abackfolded structure. By introducing length asymmetry, the effective bandwidth was enhanced to 38 Hz with a poweroutput above 15 mW, for 1 g, which is sufficient for an intelligent wireless sensor to start up and transmit data.To utilize the positive output effect from conjoined cantielvers a micro harvester was fabricated. The design wasbased on the same principle as for the backfolded, but for fabrication reasons the design was made in one plane. Theharvester contain two outer cantilevers conjoined to a backfolded middle cantilever. Due to fabrication difficulties,only a mechanical characterization of the harvester was possible. The result from the characterization looks promisingfrom a harvesting point of view, by showing a clear peak that seems to be somewhat broadband.Energy storage for an autonomous wireless intelligent sensor (IWS) needs to be able to charge and discharge duringthe lifetime of the IWS. Therefor the choice fell on supercapacitors instead of batteries. Over time the supercapacitordue to its superior amount of charge and discharge cycles, outperform a battery when energy density is compared.Increasing the energy density for supercapacitors gives the advantage to prolong the providing of power to theIWS. One such electrode material is conjoined carbon nanofibers and carbon nanotubes. The material is not dependenton conductive agents or binders. The effective surface area can be expanded through a denser structure of CNF, wheremore CNT can grow. In combination with activation, which will yield more micropores, hence an increasedcapacitance for the presented synthesized material yielded 91 F/g with an effective surface area of 131 m2.There is many challenges to power an IWS on a gasturbine. This thesis cover challenges like vibrations on cables,placement issues and the charge of a supercapacitor by harvested energy that comes in small chunks. Solutions forthese challenges are offered.The presented work in this thesis shows how the bandwidth for piezoelectric energy harvesters can be broader byasymmetric implementation of conjoined resonators. In addition, the advantages of conjoined carbon electrodematerials to be implemented as electrode material in supercapacitors. Both harvester and storage are intended to beused as energy sources for intelligent wireless sensors

    Materials Science and Technology

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    Materials are important to mankind because of the benefits that can be derived from the manipulation of their properties, for example electrical conductivity, dielectric constant, magnetization, optical transmittance, strength and toughness. Materials science is a broad field and can be considered to be an interdisciplinary area. Included within it are the studies of the structure and properties of any material, the creation of new types of materials, and the manipulation of a material's properties to suit the needs of a specific application. The contributors of the chapters in this book have various areas of expertise. therefore this book is interdisciplinary and is written for readers with backgrounds in physical science. The book consists of fourteen chapters that have been divided into four sections. Section one includes five chapters on advanced materials and processing. Section two includes two chapters on bio-materials which deal with the preparation and modification of new types of bio-materials. Section three consists of three chapters on nanomaterials, specifically the study of carbon nanotubes, nano-machining, and nanoparticles. Section four includes four chapters on optical materials

    ์„ฑ๋Šฅ-์นจ๊ฐ•์•ˆ์ •์„ฑ ์ƒ์ถฉ ๋ฌธ์ œ ํ•ด๊ฒฐ์„ ์œ„ํ•œ ๋ณตํ•ฉ์ฒด ๊ธฐ๋ฐ˜ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์— ๋Œ€ํ•œ ์—ฐ๊ตฌ

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    ํ•™์œ„๋…ผ๋ฌธ (๋ฐ•์‚ฌ) -- ์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› : ๊ณต๊ณผ๋Œ€ํ•™ ์žฌ๋ฃŒ๊ณตํ•™๋ถ€, 2021. 2. ์„œ์šฉ์„.Magnetorheological (MR) fluids are smart materials composed of magnetic particles dispersed in magnetically-insulating carrier medium. With magnetic field, chain-like structures are formed due to dipole-induced magnetostatic interaction between magnetic particles, and the structures inhibit the flow and increase the viscosity of MR fluids in very short time. This characteristic enables the rheological properties of MR fluids to be easily tailored with magnetic field strength. Due to this unique response, MR fluids can be used for actuator systems like power steering pumps haptic devices, and active suspensions, and damper systems in automobile, bridges, buildings and so on. A huge obstacle for application of MR fluids is their poor long-term stability against the sedimentation of magnetic particles. The large difference in the density between heavy magnetic particles and light medium make magnetic particles quickly go down to bottom, reducing the MR fluids length of life. One of the strategies for improvement of the long-term stability was to reduce the density of magnetic particles by synthesizing magnetic composite materials. Fabrication of magnetic composites using light materials such as polymer, silica, carbon materials efficiently have reduced the density mismatch between magnetic materials and carrier medium, enhancing the long-term stability of MR fluids. However, there was trade-off between long-term stability and performance of MR fluids because use of light materials is equivalent to the deterioration in magnetic properties. In this study, various magnetic composites with different composition and structures were fabricated for the objective of producing MR fluids having excellent performance and long-term stability simultaneously. As a first step, hollow structured polymer-Fe3O4 composite particles were synthesized using SiO2 as sacrificial template. With cavity inside, the hollow magnetic composite particles showed the density only 40 % of bare Fe3O4 and the large improvement in long-term stability of MR suspensions could be observed. To avoid huge decline in MR performance with non-magnetic polymers, hierarchically-structured Fe3O4 nanoparticles were prepared with simple electrospraying process. By excluding polymers, hierarchically-structured Fe3O4 had magnetization value very closed to its primary nanoparticles, leading to MR performance higher more than 3 times of hollow structured polymer-Fe3O4 suspensions. At the same time, the pores inside reduced the density of the structured particles by 23 %, resulting in better long-term stability of hierarchically-structured Fe3O4 suspension than bare Fe3O4 suspension. To minimize the trade-off between MR performance and long-term stability (density of magnetic particles), non-spherical, CoFeNi-based magnetic composites were fabricated and applied for MR fluids. CNT-Co0.4Fe0.4Ni0.2 composite was produced by synthesizing Co0.4Fe0.4Ni0.2 on the surface of functionalized CNTs. Much higher magnetization of Co0.4Fe0.4Ni0.2 compared to Fe3O4 enabled CNT-Co0.4Fe0.4Ni0.2 suspension to have much superior MR performance than Fe3O4 composite-based MR fluids. Also, due to high aspect ratio of CNTs, outstanding long-term stability of 22 % light transmission was observed with formation of 3-dimensional network structures. Finally, magnetically non-active CNTs were replaced by magnetizable, flake-shaped sendust. The high drag coefficient of flake sendust, combined with roughened surface due to attached Co0.4Fe0.4Ni0.2 nanoparticles, resulted in excellent stability with 23 % of light transmission despite of the high density of sendust-Co0.4Fe0.4Ni0.2 composite particles. Also, because both constituents of sendust-Co0.4Fe0.4Ni0.2 are both magnetic materials with high magnetization value, the MR fluids retained very high yield stress value์ž๊ธฐ์œ ๋ณ€์œ ์ฒด๋Š” ์ž์„ฑ์ž…์ž๊ฐ€ ๋น„์ž์„ฑ ๋งค๊ฐœ์•ก์— ๋ถ„์‚ฐ๋œ ํ˜„ํƒ์•ก ํ˜•ํƒœ์˜ ์Šค๋งˆํŠธ๋ฌผ์งˆ์ด๋‹ค. ์™ธ๋ถ€ ์ž๊ธฐ์žฅ ํ•˜์—์„œ ์ž์„ฑ์ž…์ž๋“ค ์‚ฌ์ด์˜ ์Œ๊ทน์ž๋กœ ์ธํ•œ ์ •์ž๊ธฐ์„ฑ ์ƒํ˜ธ์ž‘์šฉ์œผ๋กœ ์ฒด์ธ ํ˜•ํƒœ์˜ ๊ตฌ์กฐ๊ฐ€ ํ˜•์„ฑ๋˜๊ณ , ์ด ๊ตฌ์กฐ๊ฐ€ ์œ ์ฒด์˜ ํ๋ฆ„์„ ๋ง‰์•„ ๋งค์šฐ ์งง์€ ์‹œ๊ฐ„ ๋‚ด์— ์ ๋„๊ฐ€ ํฌ๊ฒŒ ํ–ฅ์ƒ๋˜๊ฒŒ ๋œ๋‹ค. ์ด๋Ÿฌํ•œ ์„ฑ์งˆ๋กœ ์ธํ•ด ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์œ ๋ณ€ํŠน์„ฑ์„ ์™ธ๋ถ€ ์ž๊ธฐ์žฅ์„ ํ†ตํ•ด ์‰ฝ๊ฒŒ ์กฐ์ ˆํ•˜๋Š” ๊ฒƒ์ด ๊ฐ€๋Šฅํ•˜๋‹ค. ์ด๋Ÿฌํ•œ ์™ธ๋ถ€์ž์žฅ์— ๋Œ€ํ•œ ํ†กํŠนํ•œ ๋ฐ˜์‘์„ฑ์œผ๋กœ ์ธํ•ด, ํ–…ํ‹ฑ ๋””๋ฐ”์ด์Šค ํŒŒ์›Œ์Šคํ‹ฐ์–ด๋ง ํŽŒํ”„, ๊ทธ๋ฆฌ๊ณ  ์ž๋™์ฐจ, ๋‹ค๋ฆฌ, ๊ฑด๋ฌผ ๋“ฑ์˜ ์ถฉ๊ฒฉ ๋ฐฉ์ง€ ์‹œ์Šคํ…œ์— ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด๋ฅผ ์ด์šฉํ•  ์ˆ˜ ์žˆ๋‹ค. ํ•˜์ง€๋งŒ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ํ™œ์šฉ์€ ์ž์„ฑ์ž…์ž์˜ ์นจ์ „์— ๋Œ€ํ•œ ์•ˆ์ •์„ฑ์˜ ๋ถ€์กฑํ•จ์œผ๋กœ ์ธํ•ด ํฌ๊ฒŒ ์ œํ•œ ๋  ์ˆ˜ ์žˆ๋‹ค. ๋ฐ€๋„๊ฐ€ ๋†’์€ ์ž์„ฑ์ž…์ž์™€ ๋ฐ€๋„๊ฐ€ ๋‚ฎ์€ ๋งค๊ฐœ์•ก ์‚ฌ์ด์˜ ํฐ ๋ฐ€๋„์ฐจ์ด๋กœ ์ธํ•ด ์ž์„ฑ์ž…์ž๊ฐ€ ๋น ๋ฅด๊ฒŒ ๊ฐ€๋ผ์•‰๊ฒŒ ๋˜๋ฉด, ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์ˆ˜๋ช…์ด ํฌ๊ฒŒ ๊ฐ์†Œํ•˜๊ฒŒ ๋œ๋‹ค. ์ด๋Ÿฌํ•œ ๋ฌธ์ œ๋ฅผ ํ•ด๊ฒฐํ•˜๊ธฐ ์œ„ํ•œ ํ•œ๊ฐ€์ง€ ๋ฐฉ๋ฒ•์œผ๋กœ ์ž์„ฑ๋ฌผ์งˆ๊ณผ ๋ฐ€๋„๊ฐ€ ๋‚ฎ์€ ๋ฌผ์งˆ(๊ณ ๋ถ„์ž, ์‹ค๋ฆฌ์นด ํƒ„์†Œ๋ฌผ์งˆ ๋“ฑ)์„ ๊ฒฐํ•ฉํ•˜์—ฌ ์ž์„ฑ๋ณตํ•ฉ์ž…์ž๋ฅผ ํ•ฉ์„ฑํ•จ์œผ๋กœ์จ, ์ž์„ฑ์ž…์ž์˜ ๋ฐ€๋„๋ฅผ ๋‚ฎ์ถ”๊ณ  ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์นจ๊ฐ•์•ˆ์ •์„ฑ์„ ๋†’์ด๋Š” ์—ฐ๊ตฌ๋“ค์ด ์ง„ํ–‰๋˜์–ด ์™”๋‹ค. ํ•˜์ง€๋งŒ ์ด๋Ÿฌํ•œ ๊ฒฝ์šฐ ๋ณตํ•ฉ์ž์„ฑ์ž…์ž์˜ ์ž๊ธฐ์  ์„ฑ์งˆ์ด ์ €ํ•˜๋˜๊ธฐ ๋•Œ๋ฌธ์— ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์นจ๊ฐ•์•ˆ์ •์„ฑ๊ณผ ์„ฑ๋Šฅ์ด ์„œ๋กœ ์ƒ์ถฉ๊ด€๊ณ„์— ์žˆ๋‹ค๋Š” ๋ฌธ์ œ์ ์„ ๊ฐ€์ง€๊ณ  ์žˆ๋‹ค. ๋ณธ ๋…ผ๋ฌธ์—์„œ๋Š” ๋›ฐ์–ด๋‚œ ์„ฑ๋Šฅ๊ณผ ์นจ๊ฐ•์•ˆ์ •์„ฑ์„ ๊ฐ€์ง€๋Š” ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด๋ฅผ ์ œ์กฐํ•˜๊ธฐ ์œ„ํ•ด ๋‹ค์–‘ํ•œ ๋ฌผ์งˆ๊ตฌ์„ฑ๊ณผ ๊ตฌ์กฐ๋ฅผ ๊ฐ€์ง€๋Š” ํ•ฉ์„ฑํ•˜์˜€๋‹ค. ์ฒซ ๋‹จ๊ณ„๋กœ ์‹ค๋ฆฌ์นด๋ฅผ ํ…œํ”Œ๋ ˆ์ดํŠธ๋กœ ์‚ฌ์šฉํ•˜์—ฌ ํ• ๋กœ์šฐ ๊ตฌ์กฐ๋ฅผ ๊ฐ€์ง€๋Š” ๊ณ ๋ถ„์ž-Fe3O4 ๋ณตํ•ฉ์ž์„ฑ์ž…์ž๋ฅผ ํ•ฉ์„ฑํ•˜์˜€๋‹ค. ํ• ๋กœ์šฐ ๊ตฌ์กฐ ๋‚ด๋ถ€์˜ ๊ณต๋™์œผ๋กœ ์ธํ•ด, ์ž…์ž์˜ ๋ฐ€๋„๊ฐ€ ์ˆœ์ˆ˜ Fe3O4 ๋Œ€๋น„ 40 % ์ˆ˜์ค€๊นŒ์ง€ ๊ฐ์†Œํ•˜์˜€๊ณ , ์ด๋กœ ์ธํ•ด ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์นจ๊ฐ•์•ˆ์ •์„ฑ์ด ํฌ๊ฒŒ ์ƒ์Šนํ•˜์˜€๋‹ค. ๋‹ค์Œ ์—ฐ๊ตฌ๋กœ, ๋น„์ž์„ฑ ๊ณ ๋ถ„์ž๋กœ ์ธํ•œ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด ์„ฑ๋Šฅ์˜ ๊ฐ์†Œ๋ฅผ ์ตœ์†Œํ™”ํ•˜๊ธฐ ์œ„ํ•ด, ๊ฐ„๋‹จํ•œ ์ „๊ธฐ๋ฐฉ์‚ฌ ๋ฐฉ๋ฒ•์„ ํ†ตํ•ด ๊ณ„์ธต๊ตฌ์กฐ๋ฅผ ๊ฐ€์ง€๋Š” Fe3O4 ๋‚˜๋…ธ์ž…์ž๋“ค์„ ์ œ์กฐํ•˜์˜€๋‹ค. ์•ž์˜ ์—ฐ๊ตฌ์™€ ๋Œ€๋น„ํ•˜์—ฌ, ๊ณ ๋ถ„์ž์˜ ๋ฐฐ์ œ๋ฅผ ํ†ตํ•ด ๋†’์€ ์žํ™”๊ฐ’์„ ๊ฐ€์ง€๋Š” Fe3O4 ๋‚˜๋…ธ๊ตฌ์กฐ์ž…์ž๋“ค์„ ์–ป์„ ์ˆ˜ ์žˆ์—ˆ๊ณ , ์ด๋ฅผ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์— ์ ์šฉํ•˜์—ฌ ํ• ๋กœ์šฐ ๊ณ ๋ถ„์ž-Fe3O4 ์ž…์ž ๊ธฐ๋ฐ˜ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด ๋Œ€๋น„ 3๋ฐฐ ์ด์ƒ์˜ ์„ฑ๋Šฅ์„ ๊ฐ€์ง€๋Š” ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด๋ฅผ ์–ป์„ ์ˆ˜ ์žˆ์—ˆ๋‹ค. ์ด์™€ ๋™์‹œ์— Fe3O4 ๋‚˜๋…ธ๊ตฌ์กฐ์ž…์ž ๋‚ด๋ถ€์— ์ƒ์„ฑ๋œ ๊ธฐ๊ณต๋“ค๋กœ ์ธํ•ด ์ˆœ์ˆ˜ Fe3O4 ๋Œ€๋น„ ๋ฐ€๋„๊ฐ€ ์•ฝ 23 % ์ •๋„ ๊ฐ์†Œํ•˜์˜€๊ณ , ์ด๋กœ ์ธํ•ด ์นจ Fe3O4 ๋‚˜๋…ธ๊ตฌ์กฐ์ž…์ž๊ธฐ๋ฐ˜ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์นจ๊ฐ•์•ˆ์ •์„ฑ์ด ํ–ฅ์ƒ๋จ์„ ํ™•์ธํ•  ์ˆ˜ ์žˆ์—ˆ๋‹ค. ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์„ฑ๋Šฅ๊ณผ ์นจ๊ฐ•์•ˆ์ •์„ฑ์‚ฌ์ด์˜ ์ƒ์ถฉ์„ฑ์„ ์ตœ์†Œํ™” ํ•˜๊ธฐ ์œ„ํ•ด์„œ ๋น„๊ตฌํ˜•์˜, CoFeNi ํ•ฉ๊ธˆ๊ธฐ๋ฐ˜ ์ž์„ฑ ๋ณตํ•ฉ์ž…์ž๋ฅผ ํ•ฉ์„ฑํ•˜๊ณ  ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์— ์ ์šฉํ•˜์˜€๋‹ค. ๋จผ์ € ๊ฐœ์งˆ๋œ ์นด๋ณธ๋‚˜๋…ธํŠœ๋ธŒ ํ‘œ๋ฉด์— CoFeNi๋ฅผ ํ•ฉ์„ฑํ•˜๋Š” ๋ฐฉ๋ฒ•์„ ํ†ตํ•ด ์นด๋ณธ๋‚˜๋…ธํŠœ๋ธŒ-CoFeNi ๋ณตํ•ฉ์ฒด๋ฅผ ํ•ฉ์„ฑํ•˜์˜€๋‹ค. Fe3O4 ๋Œ€๋น„ ๋†’์€ CoFeNi์˜ ์žํ™”๊ฐ’์œผ๋กœ ์ธํ•ด ์นด๋ณธ๋‚˜๋…ธํŠœ๋ธŒ-CoFeNi ๋ณตํ•ฉ์ฒด ๊ธฐ๋ฐ˜ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด๋Š” Fe3O4 ๋ณตํ•ฉ์ฒด๊ธฐ๋ฐ˜ ์œ ์ฒด ๋Œ€๋น„ 3๋ฐฐ์—์„œ 10๋ฐฐ ์ด์ƒ์˜ ๋›ฐ์–ด๋‚œ ์œ ๋ณ€์„ฑ๋Šฅ์„ ๋ณด์˜€๋‹ค. ๋˜ํ•œ ์ข…ํšก๋น„๊ฐ€ ๋†’์€ ์นด๋ณธ๋‚˜๋…ธํŠœ๋ธŒ๋กœ ์ธํ•ด ๋ณตํ•ฉ์ฒด๊ฐ€ ์œ ์ฒด ๋‚ด์—์„œ 3์ฐจ์› ๋„คํŠธ์›Œํฌ ๊ตฌ์กฐ๋ฅผ ํ˜•์„ฑํ•˜์—ฌ, ๋น› ํˆฌ๊ณผ๋„ 22 %์˜ ๋งค์šฐ ๋›ฐ์–ด๋‚œ ์นจ๊ฐ•์•ˆ์ •์„ฑ์„ ๋ณด์˜€๋‹ค. ๋งˆ์ง€๋ง‰์œผ๋กœ ๋น„์ž์„ฑ ๋ฌผ์งˆ์ธ ์นด๋ณธ๋‚˜๋…ธํŠœ๋ธŒ๋ฅผ, ์ž์„ฑ๋ฌผ์งˆ์ธ ํ”Œ๋ ˆ์ดํฌํ˜• ์„ผ๋”์ŠคํŠธ๋กœ ๋Œ€์ฒดํ•œ ์„ผ๋”์ŠคํŠธ-CoFeNi ๋ณตํ•ฉ์ž…์ž๋ฅผ ํ•ฉ์„ฑํ•˜์—ฌ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์— ์ ์šฉํ•˜์˜€๋‹ค. ํ”Œ๋ ˆ์ดํฌํ˜• ์„ผ๋”์ŠคํŠธ์˜ ๋†’์€ ์ข…ํšก๋น„๋กœ ์ธํ•ด ๋‚˜ํƒ€๋‚˜๋Š” ๋†’์€ ํ•ญ๋ ฅ๊ณ„์ˆ˜๋กœ ์ธํ•ด, ํ•ด๋‹น ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด๋Š” ๋น› ํˆฌ๊ณผ๋„ 23 %์˜, ๋†’์€ ์ž…์ž๋ฐ€๋„ ๋Œ€๋น„ ๋งค์šฐ ๋›ฐ์–ด๋‚œ ์นจ๊ฐ•์•ˆ์ •์„ฑ์„ ๋ณด์˜€๋‹ค. ๋™์‹œ์—, ์„ผ๋”์ŠคํŠธ CoFeNi ๋ชจ๋‘ ๋†’์€ ์žํ™”๊ฐ’์„ ๊ฐ€์ง€๋Š” ์ž์„ฑ๋ฌผ์งˆ์ด๊ธฐ ๋•Œ๋ฌธ์—, ์„ผ๋”์ŠคํŠธ-CoFeNi ๊ธฐ๋ฐ˜ ์ž๊ธฐ์œ ๋ณ€์œ ์ฒด์˜ ์„ฑ๋Šฅ์ด ์นด๋ณธ๋‚˜๋…ธํŠœ๋ธŒ-CoFeNi ์œ ์ฒด ๋Œ€๋น„ ํฌ๊ฒŒ ํ–ฅ์ƒ๋˜๋Š” ๊ฒƒ์„ ํ™•์ธํ•  ์ˆ˜ ์žˆ์—ˆ๋‹ค.Contents Abstract โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ..........i Contents โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.........v List of Tables โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.........x List of Figures โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ..........xi Chapter 1. Introduction โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ............1 1. 1. Magnetorheological (MR) Fluids and Applicationsโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.........1 1. 2. Long-Term Stability Problem and Proposed Solutions โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ...........4 1. 3. Research Objectives โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.โ€ฆ...7 References โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ...........................................................9 Chapter 2. Backgrounds โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.......16 2. 1. Definition of Terms โ€ฆโ€ฆโ€ฆโ€ฆ..................................................................16 2. 1. 1. Shear Stress โ€ฆโ€ฆโ€ฆโ€ฆ........................................................................16 2. 1 .2. Shear Rate โ€ฆโ€ฆโ€ฆโ€ฆ..........................................................................16 2. 1. 3. Shear Viscosityโ€ฆโ€ฆ............................................................................17 2. 1 .4. Viscoelastic Behavior .........................................................................17 2. 1. 4. 1. Storage Modulus and Loss Modulus ..........................................17 2. 2. Yield Stress of MR Fluids โ€ฆโ€ฆโ€ฆโ€ฆ........................................................18 2. 2. 1. Rheological Models for Prediction of Dynamic and Static Yield Stress โ€ฆโ€ฆโ€ฆโ€ฆ.............................................................................................................19 2. 2 .2. Yield Stress Dependency on the Magnetic Field Strength .................22 2. 3. Mechanism of Structures Evolution .........................................................25 References โ€ฆโ€ฆโ€ฆ............................................................................................27 Chapter 3. Suspensions of Hollow Polydivinylbenzene Nanoparticles Decorated with Fe3O4 Nanoparticles as Magnetorheological Fluids for Microfluidics Applications ........31 3. 1. Introduction โ€ฆโ€ฆโ€ฆ....................................................................................31 3. 2. Experimental Section ...............................................................................34 3. 2. 1. Synthesis of Hollow Polydivinylbezene (h-PDVB) Particles ............34 3. 2. 2. Deposition of Fe3O4 onto Hollow PDVB Particles ............................36 3. 2. 3. Characterization ..................................................................................37 3. 3. Results and Discussion .............................................................................41 3. 3. 1 Morphology and Structures ..................................................................41 3. 3. 2. Magnetorheological Behaviors ............................................................48 3. 3. 3. Long-Term Stability of Suspensions ...................................................62 3. 4. Conclusion โ€ฆโ€ฆโ€ฆ.....................................................................................65 References โ€ฆโ€ฆโ€ฆ.............................................................................................67 Chapter 4. Hierarchically Structured Fe3O4 Nanoparticles for High-Performance Magnetorheological Fluids with Long-Term Stability โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ...................................74 4. 1. Introduction โ€ฆโ€ฆโ€ฆ...................................................................................74 4. 2. Experimental Section ................................................................................77 4. 2. 1. Synthesis of Citric Acid-Capped Fe3O4 ..............................................77 4. 2. 2. Fabrication of HS-Fe3O4 with Electrospraying Process .....................78 4. 2. 3. Characterization ..................................................................................79 4. 3. Results and Discussion .............................................................................82 4. 3. 1. Morphology and Structures ................................................................82 4. 3. 2. Magnetorheological Behaviors ...........................................................89 4. 3. 3. Long-Term Stability of Suspensions .................................................103 4. 4. Conclusion โ€ฆโ€ฆโ€ฆ..................................................................................106 References โ€ฆโ€ฆโ€ฆ..........................................................................................108 Chapter 5. High-Performance Magnetorheological Fluids of Carbon Nanotube-CoFeNi Composites with Enhanced Long-Term Stabilityโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.................................116 5. 1. Introduction โ€ฆโ€ฆโ€ฆ...............................................................................116 5. 2. Experimental Section ............................................................................119 5. 2. 1. Functionalization of Carbon Nanotubes ..........................................119 5. 2. 2. Synthesis of Co0.4ยฌFe0.4Ni0.2 and CNT-Co0.4ยฌFe0.4Ni0.2 .......................119 5. 2. 3. Characterization ...............................................................................120 5. 3. Results and Discussion ...........................................................................123 5. 3. 1. Morphology and Structures ..............................................................123 5. 3. 2. Magnetorheological Behaviors .........................................................130 5. 3. 3. Long-Term Stability of Suspensions .................................................142 5. 4. Conclusion โ€ฆโ€ฆโ€ฆ..................................................................................145 References โ€ฆโ€ฆโ€ฆ..........................................................................................146 Chapter 6. Sendust-CoFeNi Magnetic-Magnetic Composites-Based Magnetorheological Fluids for Simultaneous Improvement of Performance and Long-Term Stability โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ..154 6. 1. Introduction โ€ฆโ€ฆโ€ฆ................................................................................154 6. 2. Experimental Section .............................................................................157 6. 2. 1. Synthesis of Citric Acid-Capped Fe3O4 ...........................................157 6. 2. 2. Characterization ...............................................................................157 6. 3. Results and Discussion ...........................................................................159 6. 3. 1. Morphology and Structures ..............................................................159 6. 3. 2. Magnetorheological Behaviors ........................................................163 6. 3. 3. Long-Term Stability of Suspensions ................................................176 6. 4. Conclusion โ€ฆโ€ฆโ€ฆ..................................................................................179 References โ€ฆโ€ฆโ€ฆ..........................................................................................181 Chapter 7. Conclusions โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ....188 7. 1. Overall conclusion โ€ฆโ€ฆโ€ฆ......................................................................188 7. 2. Further works โ€ฆโ€ฆโ€ฆ..............................................................................194 References โ€ฆโ€ฆโ€ฆ...........................................................................................195 ๊ตญ๋ฌธ์ดˆ๋ก โ€ฆโ€ฆโ€ฆ...............................................................................................196 List of Publication โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ.......199 Appendix โ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆโ€ฆ..........โ€ฆ........201 Appendix A. Nonisothermal Crystallization Behaviors of Structure-Modified Polyamides (Nylon 6s) ...............................................................................201Docto

    Directly Printed Nanomaterial Sensor for Strain and Vibration Measurement

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    ํ•™์œ„๋…ผ๋ฌธ (๋ฐ•์‚ฌ) -- ์„œ์šธ๋Œ€ํ•™๊ต ๋Œ€ํ•™์› : ๊ณต๊ณผ๋Œ€ํ•™ ๊ธฐ๊ณ„๊ณตํ•™๋ถ€, 2020. 8. ์•ˆ์„ฑํ›ˆ.Most discussions about Industrie 4.0 tacitly assume that any such system would involve the processing and evaluation of large data volumes. Specifically, the operation of complex production processes requires stable and reliable data measurement and communication systems. However, while modern sensor technology may already be capable of collecting a wide range of machine and production data, it has been proving difficult to measure and analyse the data which is not easy to measurable and feed the results quickly back into an optimised production cycle. This is why the cost and installation of sensor, data acquisition, and transmission systems for flexible and adaptive manufacturing process have not been match the requirement of industrial demands. In this dissertation, directly printed nanomaterial sensor capable of strain and vibration measurement with high sensitivity and wide measurable range was fabricated using aerodynamically focused nanomaterial (AFN) printing system which is a direct printing technique for conductive and stretchable pattern printing onto flexible substrate. Specifically, microscale porous conductive pattern composed of silver nanoparticles (AgNPs) and multi-walled carbon nanotubes (MWCNTs) composite was printed onto polydimethylsiloxane (PDMS). Printing mechanism of AFN printing system for nanocomposite onto flexible substrate in order of mechanical crack generation, seed layer deposition, partial aggregation, and fully deposition was demonstrated and experimentally validated. The printed nanocomposite sensor exhibited gauge factor (GF) of 58.7, measurable range of 0.74, and variance in peak resistance under 0.05 during 1,000 times life cycle evaluation test. Furthermore, vibration measurement performance was evaluated according to vibration amplitude and frequency with Q-factor evaluation and statistical verification. Sensing mechanism for nanocomposite sensor was also analysed and discussed by both analytical and statistical methods. First, electron tunnelling effect among nanomaterials was analysed statistically using bivariate probit model. Since electrical property varies by the geometrical properties of nanomaterial, Monte Carlo simulation method based on Lennard-Jones (LJ) potential model and the voter model was developed for deeper understanding of the dynamics of nanomaterial by strain. By simply counting the average attachment among nanomaterials by strain, electrical conductivity was easily estimated with low simulation cost. The main objective of all processes to manufacture high-tech products is compliance with the specified ranges of permissible variation. In this perspective, all data must be recorded that might provide some evidence of status changes anywhere along the process chain. This dissertation covers the monitoring of forming and milling process. By measurement of mechanical deformation of stamp during forming process, it was possible to estimate the forming force according to various process parameters including maximum force, force gradient, and the thickness of sheet metal. Furthermore, accurate and reliable vibration monitoring was also conducted during milling process by simple and direct attachment of printed sensor to workpiece. Using frequency and power spectrum analysis of obtained data, the vibration of workpiece was measured during milling process according to process parameters including RPM, feed rate, cutting depth and width of spindle. Finally, developed sensor was applied to the digital twin of turbine blade manufacturing that vibration greatly affects the quality of product to predict the process defects in real time. To overcome the wire required data acquisition and transmission system, directly printed wireless communication sensor was also developed using chipless radio frequency identification (RFID) technology. It is one of the widely used technique for internet-of-things (IoT) devices due to low-cost, printability, and simplicity. The developed stretchable and chipless RFID sensor exhibited GF more than 0.6 and maximum measurable range more than 0.2 with high degree-of-freedom of motion. Since it showed its original characteristics of sensing in only one direction independently, sensor patch composed of various sensor with different resonance frequency was capable of measuring not only normal strains but also shear strains in all directions. Sensors in machinery and equipment can provide valuable clues as to whether or not the actual values will fall into the tolerance range. In this aspect, a real-time, accurate, and reliable process monitoring is a basic and crucial enabler of intelligent manufacturing operations and digital twin applications. In this dissertation, developed sensor was used for various manufacturing process include forming process, milling process, and wireless communication using highly sensitive and wide measuring properties with low fabrication cost. It is expected that developed sensor could be applied for the digital twin and process defects prediction in real-time.4์ฐจ ์‚ฐ์—…ํ˜๋ช…์— ๋Œ€ํ•œ ๋Œ€๋ถ€๋ถ„์˜ ๋…ผ์˜๋Š” ๋งŽ์€ ์–‘์˜ ๋ฐ์ดํ„ฐ๋ฅผ ์ฒ˜๋ฆฌํ•˜๊ณ  ํ‰๊ฐ€ํ•˜๋Š” ์‹œ์Šคํ…œ์„ ์•”๋ฌต์ ์œผ๋กœ ๊ฐ€์ •ํ•œ๋‹ค. ํŠนํžˆ, ๋ณต์žกํ•œ ์ƒ์‚ฐ ๊ณต์ •์„ ์šด์˜ํ•˜๊ธฐ ์œ„ํ•ด์„œ๋Š” ์•ˆ์ •์ ์ด๊ณ  ์‹ ๋ขฐํ•  ์ˆ˜ ์žˆ๋Š” ๋ฐ์ดํ„ฐ ์ธก์ • ๋ฐ ํ†ต์‹  ์‹œ์Šคํ…œ์ด ํ•„์š”ํ•˜๋‹ค. ํ•˜์ง€๋งŒ, ์ตœ์‹  ์„ผ์„œ ๊ธฐ์ˆ ์€ ๊ด‘๋ฒ”์œ„ํ•œ ๊ธฐ๊ณ„ ๋ฐ ์ƒ์‚ฐ ๊ณต์ • ์ค‘ ๋ฐ์ดํ„ฐ๋ฅผ ์ˆ˜์ง‘ํ•˜๋Š” ๊ฒƒ์ด ๊ฐ€๋Šฅํ•˜์ง€๋งŒ ์ธก์ •ํ•˜๊ธฐ ์‰ฝ์ง€ ์•Š์€ ๋ฐ์ดํ„ฐ๋ฅผ ์ธก์ •ํ•˜๊ณ  ๋ถ„์„ํ•˜์—ฌ ๊ทธ ๊ฒฐ๊ณผ๋ฅผ ์ตœ์ ํ™”๋œ ์ƒ์‚ฐ ๊ณต์ •์— ์‹ ์†ํ•˜๊ฒŒ ์ œ๊ณตํ•˜๋Š”๋ฐ ํ•œ๊ณ„๋ฅผ ๊ฐ€์ง€๊ณ  ์žˆ๋‹ค. ๋•Œ๋ฌธ์—, ์œ ์—ฐํ•˜๊ณ  ์ ์‘ ๊ฐ€๋Šฅํ•œ ์ œ์กฐ ๊ณต์ •์„ ์œ„ํ•œ ์„ผ์„œ์˜ ๊ฐ€๊ฒฉ๊ณผ ์„ค์น˜ ๋ฐฉ๋ฒ•, ๋ฐ์ดํ„ฐ ์ˆ˜์ง‘ ๋ฐ ์ „์†ก ์‹œ์Šคํ…œ์ด ์‹ค์ œ ์‚ฐ์—…์˜ ์š”๊ตฌ ์‚ฌํ•ญ์— ๋„๋‹ฌํ•˜์ง€ ๋ชปํ•˜๊ณ  ์žˆ๋‹ค. ์ด ํ•™์œ„ ๋…ผ๋ฌธ์—์„œ๋Š” ์œ ์—ฐ ๊ธฐํŒ์— ์ „๋„์„ฑ ๋ฐ ์‹ ์ถ•์„ฑ ํŒจํ„ด์„ ์ง์ ‘ ์ธ์‡„ํ•  ์ˆ˜ ์žˆ๋Š” ๊ณต๊ธฐ์—ญํ•™์  ๋‚˜๋…ธ๋ฌผ์งˆ ์ง‘์† ์ธ์‡„ ์‹œ์Šคํ…œ์„ ์‚ฌ์šฉํ•˜์—ฌ ๋†’์€ ๋ฏผ๊ฐ๋„์™€ ๋„“์€ ์ธก์ • ๊ฐ€๋Šฅ ๋ฒ”์œ„๋ฅผ ๊ฐ€์ง„ ๋ณ€์œ„ ๋ฐ ์ง„๋™ ์„ผ์„œ๋ฅผ ๊ฐœ๋ฐœํ•˜์˜€๋‹ค. ๊ตฌ์ฒด์ ์œผ๋กœ, ์€ ๋‚˜๋…ธ์ž…์ž์™€ ๋‹ค์ค‘ ๋ฒฝ ํƒ„์†Œ ๋‚˜๋…ธํŠœ๋ธŒ๋กœ ๊ตฌ์„ฑ๋œ ๋‚˜๋…ธ ๋ณตํ•ฉ์žฌ๋ฅผ ํด๋ฆฌ๋””๋ฉ”ํ‹ธ์‹ค๋ก์‚ฐ ์œ„์— ์ง์ ‘ ์ธ์‡„ํ•˜์˜€๋‹ค. ์œ ์—ฐ ๊ธฐํŒ ์œ„์— ๊ณต๊ธฐ์—ญํ•™์  ๋‚˜๋…ธ๋ฌผ์งˆ ์ง‘์† ์ธ์‡„ ์‹œ์Šคํ…œ์„ ์‚ฌ์šฉํ•œ ๋‚˜๋…ธ ๋ณตํ•ฉ์žฌ ์ธ์‡„ ๋ฐฉ๋ฒ•์˜ ๊ธฐ์ž‘์ด ๊ธฐ๊ณ„์  ๊ท ์—ด ๋ฐœ์ƒ, ์‹œ๋“œ์ธต ์ ์ธต, ๋ถ€๋ถ„ ์‘์ง‘ ๋ฐ ์™„์ „ ์ฆ์ฐฉ ์ˆœ์œผ๋กœ ๋…ผ์˜ ๋ฐ ์‹คํ—˜์ ์œผ๋กœ ๊ฒ€์ฆ๋˜์—ˆ๋‹ค. ์ธ์‡„๋œ ๋‚˜๋…ธ ๋ณตํ•ฉ์žฌ ์„ผ์„œ๋Š” 58.7์˜ ๊ฒŒ์ด์ง€ ํŒฉํ„ฐ, 0.74์˜ ์ธก์ • ๊ฐ€๋Šฅ ๋ฒ”์œ„๋ฅผ ๋‚˜ํƒ€๋‚ด์—ˆ์œผ๋ฉฐ 1,000๋ฒˆ ๋ฐ˜๋ณต๋œ ์ˆ˜๋ช… ์ฃผ๊ธฐ ํ‰๊ฐ€์—์„œ 5% ๋ฏธ๋งŒ์˜ ์ •์  ์ €ํ•ญ ๋ณ€ํ™”๋ฅผ ํ™•์ธํ•  ์ˆ˜ ์žˆ์—ˆ๋‹ค. ๋˜ํ•œ Q ์ธ์ž ํ‰๊ฐ€ ๋ฐ ํ†ต๊ณ„ ๊ฒ€์ฆ์„ ์‚ฌ์šฉํ•˜์—ฌ ์ง„๋™์˜ ์ง„ํญ ๋ฐ ์ฃผํŒŒ์ˆ˜์— ๋”ฐ๋ฅธ ์ง„๋™ ์ธก์ • ์„ฑ๋Šฅ์„ ํ‰๊ฐ€ํ•˜์˜€๋‹ค. ๋‚˜๋…ธ ๋ณตํ•ฉ์žฌ ์„ผ์„œ์— ๋Œ€ํ•œ ์ธก์ • ๊ธฐ์ž‘ ๋˜ํ•œ ํ•ด์„์  ๋ฐ ํ†ต๊ณ„์  ๋ฐฉ๋ฒ•์œผ๋กœ ๋ถ„์„๋˜์—ˆ๋‹ค. ๋จผ์ €, ๋‚˜๋…ธ๋ฌผ์งˆ ๊ฐ„ ํ„ฐ๋„ ํšจ๊ณผ๊ฐ€ ์ด๋ณ€๋Ÿ‰ ํ”„๋กœ๋น— ๋ชจ๋ธ์„ ํ†ตํ•ด ํ†ต๊ณ„์ ์œผ๋กœ ๋ถ„์„๋˜์—ˆ๋‹ค. ์„ผ์„œ์˜ ์ „๊ธฐ์  ๋ฌผ์„ฑ์ด ๋‚˜๋…ธ๋ฌผ์งˆ์˜ ๊ธฐํ•˜ํ•™์  ๋ฌผ์„ฑ์— ๋”ฐ๋ผ ์ƒ์ดํ•˜๊ธฐ ๋•Œ๋ฌธ์— ๋ณ€์œ„์— ๋”ฐ๋ฅธ ๋‚˜๋…ธ๋ฌผ์งˆ์˜ ๋™์ ์ธ ์ดํ•ด๋ฅผ ์œ„ํ•ด ๋ ˆ๋„ˆ๋“œ์กด์Šค ์ „์œ„ ๋ฐ ์œ ๊ถŒ์ž ๋ชจ๋ธ์„ ๊ธฐ๋ฐ˜์œผ๋กœ ํ•œ ๋ชฌํ…Œ์นด๋ฅผ๋กœ ์‹œ๋ฎฌ๋ ˆ์ด์…˜ ๋ฐฉ๋ฒ•์ด ๊ฐœ๋ฐœ๋˜์—ˆ๋‹ค. ์ด๋ฅผ ํ™œ์šฉํ•˜์—ฌ ๋‚˜๋…ธ๋ฌผ์งˆ ๊ฐ„ ํ‰๊ท  ๋ถ€์ฐฉ ์ˆ˜๋ฅผ ๊ณ„์‚ฐํ•˜์—ฌ ๋‚ฎ์€ ๋น„์šฉ์œผ๋กœ ์ „๊ธฐ์ „๋„๋„๋ฅผ ์ถ”์ •ํ•  ์ˆ˜ ์žˆ์—ˆ๋‹ค. ์ฒจ๋‹จ ์ œํ’ˆ์„ ์ œ์กฐํ•˜๊ธฐ ์œ„ํ•œ ๋ชจ๋“  ๊ณต์ •์˜ ์ฃผ์š” ๋ชฉํ‘œ๋Š” ์ง€์ •๋œ ๋ฒ”์œ„์˜ ํ—ˆ์šฉ ๊ฐ€๋Šฅํ•œ ๋ณ€๋™์„ ์ค€์ˆ˜ํ•˜๋Š” ๊ฒƒ์ด๋‹ค. ์ด๋ฅผ ์œ„ํ•ด ๊ณต์ • ์ค‘ ์–ด๋””์—์„œ๋‚˜ ์ƒํƒœ ๋ณ€๊ฒฝ์˜ ์ฆ๊ฑฐ๋ฅผ ์ œ๊ณตํ•  ์ˆ˜ ์žˆ๋Š” ๋ชจ๋“  ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ๋กํ•˜๋Š” ๊ฒƒ์ด ํ•„์ˆ˜์ ์ด๋‹ค. ์ด ํ•™์œ„ ๋…ผ๋ฌธ์—์„œ๋Š” ์ œ์ž‘๋œ ์„ผ์„œ๋ฅผ ํ†ตํ•ด ์„ฑํ˜• ๋ฐ ์ ˆ์‚ญ ๊ณต์ •์˜ ๋ฐ์ดํ„ฐ๋ฅผ ๊ธฐ๋กํ•จ์œผ๋กœ์จ ๊ณต์ •์„ ๋ชจ๋‹ˆํ„ฐ๋งํ•˜์˜€๋‹ค. ์„ฑํ˜• ๊ณต์ • ๋™์•ˆ ์Šคํƒฌํ”„์˜ ๊ธฐ๊ณ„์  ๋ณ€ํ˜•์„ ์ธก์ •ํ•จ์œผ๋กœ์จ ์ตœ๋Œ€ ํž˜, ํž˜์˜ ๊ตฌ๋ฐฐ ๋ฐ ํŒ๊ธˆ์˜ ๋‘๊ป˜๋ฅผ ํฌํ•จํ•˜๋Š” ๋‹ค์–‘ํ•œ ๊ณต์ • ๋ณ€์ˆ˜์— ๋”ฐ๋ผ ์„ฑํ˜• ํž˜์„ ์ถ”์ •ํ•  ์ˆ˜ ์žˆ์—ˆ๋‹ค. ๋˜ํ•œ, ์ ˆ์‚ญ ๊ณต์ • ์ค‘ ๊ณต์ž‘๋ฌผ์— ์ œ์ž‘๋œ ์„ผ์„œ๋ฅผ ์ง์ ‘ ๋ถ€์ฐฉํ•˜์—ฌ ์ •ํ™•ํ•˜๊ณ  ์•ˆ์ •์ ์ธ ์ง„๋™ ๋ชจ๋‹ˆํ„ฐ๋ง์„ ์ˆ˜ํ–‰ํ•˜์˜€๋‹ค. ์–ป์–ด์ง„ ๋ฐ์ดํ„ฐ์˜ ์ฃผํŒŒ์ˆ˜ ๋ฐ ์ „๋ ฅ ์ŠคํŽ™ํŠธ๋Ÿผ ๋ถ„์„์„ ์ด์šฉํ•˜์—ฌ, ๋ถ„๋‹น ํšŒ์ „ ์ˆ˜, ์ด์†ก ์†๋„, ์Šคํ•€๋“ค์˜ ์ ˆ์‚ญ ๊นŠ์ด ๋ฐ ๋„ˆ๋น„์— ๋”ฐ๋ฅธ ๊ณต์ž‘๋ฌผ์˜ ์ง„๋™์„ ์ธก์ •ํ•˜์˜€๋‹ค. ๋งˆ์ง€๋ง‰์œผ๋กœ ์ œ์กฐ๋œ ์„ผ์„œ๋ฅผ ์ง„๋™์ด ์ œํ’ˆ ํ’ˆ์งˆ์— ํฐ ์˜ํ–ฅ์„ ๋ฏธ์น˜๋Š” ํ„ฐ๋นˆ ๋™์ต ์ œ์กฐ ๊ณต์ •์˜ ๋””์ง€ํ„ธ ํŠธ์œˆ์œผ๋กœ ์ ์šฉํ•˜์—ฌ ์‹ค์‹œ๊ฐ„์œผ๋กœ ๊ณต์ • ๊ฒฐํ•จ์„ ์˜ˆ์ธกํ•˜์˜€๋‹ค. ์œ ์„  ๋ฐ์ดํ„ฐ ์ˆ˜์ง‘ ๋ฐ ์ „์†ก ์‹œ์Šคํ…œ์„ ๊ทน๋ณตํ•˜๊ธฐ ์œ„ํ•ด ์นฉ๋ฆฌ์Šค ๋ฌด์„  ์ฃผํŒŒ์ˆ˜ ์‹๋ณ„ ๊ธฐ์ˆ ์„ ์‚ฌ์šฉํ•˜์—ฌ ์ง์ ‘ ์ธ์‡„๋œ ๋ฌด์„  ํ†ต์‹  ์„ผ์„œ๋ฅผ ๊ฐœ๋ฐœํ•˜์˜€๋‹ค. ์นฉ๋ฆฌ์Šค ๋ฌด์„  ์ฃผํŒŒ์ˆ˜ ์‹๋ณ„ ๊ธฐ์ˆ ์€ ์ €๋น„์šฉ, ์ธ์‡„์„ฑ ๋ฐ ๊ณต์ •์˜ ํ‰์ด์„ฑ์œผ๋กœ ์ธํ•ด ์‚ฌ๋ฌผ ์ธํ„ฐ๋„ท ์žฅ์น˜์— ๋„๋ฆฌ ์‚ฌ์šฉ๋˜๋Š” ๊ธฐ์ˆ  ์ค‘ ํ•˜๋‚˜์ด๋‹ค. ๊ฐœ๋ฐœ๋œ ์œ ์—ฐํ•œ ์นฉ๋ฆฌ์Šค ์„ผ์„œ๋Š” 0.6 ์ด์ƒ์˜ ๊ฒŒ์ด์ง€ ํŒฉํ„ฐ์™€ 0.2 ์ด์ƒ์˜ ์ธก์ • ๊ฐ€๋Šฅ ๋ฒ”์œ„๋ฅผ ๋‚˜ํƒ€๋ƒˆ๋‹ค. ๋˜ํ•œ ์ œ์ž‘๋œ ์„ผ์„œ๋Š” ํ•œ ๋ฐฉํ–ฅ์˜ ๋ณ€์œ„๋งŒ ๋…๋ฆฝ์ ์œผ๋กœ ์ธก์ •ํ•  ์ˆ˜ ์žˆ๋Š” ํŠน์„ฑ์„ ๊ฐ€์ง€๊ณ  ์žˆ๊ธฐ ๋•Œ๋ฌธ์—, ๋ชจ๋“  ๋ฐฉํ–ฅ์˜ ์ˆ˜์ง ๋ฐ ์ „๋‹จ ๋ณ€ํ˜•์„ ์ธก์ •ํ•  ์ˆ˜ ์žˆ๋Š” ๋‹ค์–‘ํ•œ ๊ณต์ง„ ์ฃผํŒŒ์ˆ˜๋กœ ๊ตฌ์„ฑ๋œ ์„ผ์„œ ํŒจ์น˜๊ฐ€ ๊ฐœ๋ฐœ๋˜์—ˆ๋‹ค. ๊ธฐ๊ณ„ ๋ฐ ์žฅ๋น„์˜ ์„ผ์„œ๋Š” ์‹ค์ œ ๊ฐ’์ด ๊ณต์ฐจ ๋ฒ”์œ„์— ์†ํ•˜๋Š”์ง€ ์—ฌ๋ถ€์— ๋Œ€ํ•œ ์ค‘์š”ํ•œ ๋‹จ์„œ๋ฅผ ์ œ๊ณตํ•  ์ˆ˜ ์žˆ๋‹ค. ์ด๋Ÿฌํ•œ ์ธก๋ฉด์—์„œ, ์ •ํ™•ํ•˜๊ณ  ์‹ ๋ขฐํ•  ์ˆ˜ ์žˆ๋Š” ์‹ค์‹œ๊ฐ„ ๊ณต์ • ๋ชจ๋‹ˆํ„ฐ๋ง์€ ์ง€๋Šฅํ˜• ์ œ์กฐ ๊ณต์ • ๋ฐ ๋””์ง€ํ„ธ ํŠธ์œˆ์œผ๋กœ์˜ ์‘์šฉ์„ ์œ„ํ•œ ๊ธฐ๋ณธ์ ์ด๊ณ  ๊ฒฐ์ •์ ์ธ ์š”์†Œ์ด๋‹ค. ์ด ํ•™์œ„ ๋…ผ๋ฌธ์—์„œ ๊ฐœ๋ฐœ๋œ ์„ผ์„œ๋Š” ๋‚ฎ์€ ์ œ์กฐ ๋น„์šฉ๊ณผ ๋†’์€ ๋ฏผ๊ฐ๋„ ๋ฐ ์‹ ์ถ•์„ฑ์„ ๊ฐ€์ง€๊ณ  ์žˆ๊ธฐ ๋•Œ๋ฌธ์— ์„ฑํ˜• ๊ณต์ •, ์ ˆ์‚ญ ๊ณต์ •, ๋ฌด์„  ํ†ต์‹ ์„ ํฌํ•จํ•œ ๋‹ค์–‘ํ•œ ์ œ์กฐ ๊ณต์ •์—์„œ ์‘์šฉ๋˜์—ˆ๋‹ค. ๋ฟ๋งŒ ์•„๋‹ˆ๋ผ ์ œ์ž‘๋œ ์„ผ์„œ๋Š” ๋””์ง€ํ„ธ ํŠธ์œˆ ๋ฐ ๊ณต์ • ๊ฒฐํ•จ์˜ ์‹ค์‹œ๊ฐ„ ์˜ˆ์ธก์„ ์œ„ํ•ด ๋‹ค์–‘ํ•˜๊ฒŒ ์‚ฌ์šฉ๋  ์ˆ˜ ์žˆ์„ ๊ฒƒ์œผ๋กœ ์˜ˆ์ƒ๋œ๋‹ค.Chapter 1. Introduction 1 1.1. Toward smart manufacturing 1 1.2. Sensor in manufacturing 4 1.3. Research objective 11 Chapter 2. Background 16 2.1. Aerodynamically focused nanomaterial printing 16 2.2. Printing system envelope 26 2.3. Highly sensitive sensor printing 34 Chapter 3. Sensor fabrication and evaluation 42 3.1. Highly sensitive and wide measuring sensor printing 42 3.2. Sensing performance evaluation 59 3.3. Environmental and industrial evaluation 87 Chapter 4. Sensing mechanism analysis 97 4.1. Theoretical background 97 4.2. Statistical regression anaylsis 101 4.3. Monte Carlo simulation 104 Chapter 5. Application to process monitoring 126 5.1. Forming process monitoring 126 5.2. Milling process monitoring 133 5.3. Wireless communication monitoring 149 Chapter 6. Conclusion 185 Bibliography 192 Abstract in Korean 211Docto

    Proceedings of the 4th International Conference on Innovations in Automation and Mechatronics Engineering (ICIAME2018)

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    The Mechatronics Department (Accredited by National Board of Accreditation, New Delhi, India) of the G H Patel College of Engineering and Technology, Gujarat, India arranged the 4th International Conference on Innovations in Automation and Mechatronics Engineering 2018, (ICIAME 2018) on 2-3 February 2018. The papers presented during the conference were based on Automation, Optimization, Computer Aided Design and Manufacturing, Nanotechnology, Solar Energy etc and are featured in this book

    Carbon nanotube bearings in theory and practice

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    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2011.Cataloged from PDF version of thesis.Includes bibliographical references (p. 157-170).Carbon Nanotubes (CNTs) are attractive elements for bearings in Micro-Electro-Mechanical Systems (MEMS), because their structure comprises nested shells with no bonding and sub-nanometer spacing between them, enabling relative motion with low friction and wear. A few demonstrations of CNT bearings have been reported in the literature, and atomistic simulations have been used to probe the properties of these bearings. This thesis extends the state of knowledge about these bearing systems, by building on these prior works in both the experimental and simulation domains. The prototype CNT rotor device presented in this thesis, and accompanying fabrication process, improve on existing CNT bearing demonstrators by establishing a vertical bearing orientation (enabling superior rotor balance and speed, and flexibility of placement for drive mechanisms) and a more manufacturable process (employing CNTs grown in place by chemical vapor deposition, and evaluating trade-offs in growth parameters). The device consists of a silicon rotor, supported on a cantilevered CNT shaft, and actuated by impingement of air jets on blades around its perimeter. For the fabrication development, extensive and consistent studies on the compatibility of CNTs with a suite of standard MEMS process were conducted, yielding valuable information for future CNT-based device designers on the effects of these processes on CNTs. Additionally, manual manipulation and placement of loose CNTs into the required vertical alignment was demonstrated, providing an alternate fabrication route, as well as a useful research technique for development of CNT devices. Simulation of friction in a CNT bearing system has been a popular topic, yet many questions remain open. For example, the quantitative estimates of this friction reported to date range by as much as eight orders of magnitude, and simulation techniques employ a variety of disparate simulation paradigms and parameters. This thesis presents a new suite of consistently implemented but complementary and independent simulations, which span the approaches reported to date, yet agree quantitatively within the error margin. Furthermore, the quantitative relationships between friction and sliding speed, temperature, geometry, and simulation implementation parameters are determined, and a description of the causes of friction based on phonon analyses is offered.by Eugene Hightower Cook.Ph.D

    The Development of an Antagonistic SMA Actuation Technology for the Active Cancellation of Human Tremor.

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    Human Tremor is an unintentional bodily motion that affects muscle control among both healthy individuals and those with movement disorders, occasionally to severe detriment. While assistive devices avoid the risk of side effects from pharmacological or surgical treatments, most devices are impractical for daily use due to limitations inherent in conventional actuators. The goal of this research is to address these limitations by developing an antagonistic Shape Memory Alloy (SMA) actuation technology, enabling a new class of active tremor cancellation devices. This is accomplished through the construction of a model and body of empirical support that provides the necessary design insight and predictive power for an antagonistic actuator that ensures stable amplitude and high frequency motion with low power draw. Actuation frequency and power draw were improved while balancing their competing effects through the development of: 1) a method that accurately measures the convective coefficient of SMA to enhance actuator design, 2) a growth process for carbon nanotube cooling fins to enhance cooling in a fixed medium, and 3) an understanding of the antagonistic architecture to produce increased frequency in a controllable manner. To enable applications requiring predictability for positioning and complex control, a thermodynamic model for antagonistic SMA was derived to account for inertial, slack, boiling, friction, and convective effects. Using the model, a series of simulation studies provided design insight on the effect of operating environment, driving signal, and environmental conditions so that the generic actuation system can be utilized in a wide variety of applications beyond tremor cancellation. If high forces are required in such applications, stability issues can arise, which were addressed in experimental shakedown research that broadens the high-stress SMA design space. The technology enabled by this dissertation was demonstrated in a working Active Cancellation of Tremor (ACT) prototype that produced 71% RMS cancellation of human tremor. The cancellation results show significant improvement over the current state of the art by providing intuitive, lightweight, compact hand-held tremor cancellation that is a promising solution to numerous assistive applications in medical, military, and manufacturing sectors.Ph.D.Mechanical EngineeringUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttp://deepblue.lib.umich.edu/bitstream/2027.42/76010/1/apathak_1.pd
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