Academic literature on the topic 'Vibration Isolation System'

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Journal articles on the topic "Vibration Isolation System"

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Smirnov, Vladimir, and Vladimir Mondrus. "Probability Analysis of Precision Equipment Vibration Isolation System." Applied Mechanics and Materials 467 (December 2013): 410–15. http://dx.doi.org/10.4028/www.scientific.net/amm.467.410.

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The article deals with probability analysis for a vibration isolation system of sensitive equipment. Vibration isolation system is subjected to external base vibrations due to ambient oscillations (background noise). Considering Gauss distribution for ambient vibrations, we estimate the probability when the relative displacement of isolated mass will still be lower than the vibration criteria. The problem is solved in three-dimensional space, evolved by the system parameters damping and natural frequency. According to this probability distribution, the chance of exceeding vibration criteria for a vibration isolation system is evaluated and different vibration isolation systems are compared.
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Smith, Michael Reaugh, and Frank Bradley Stamps. "Vibration isolation system." Journal of the Acoustical Society of America 105, no. 4 (1999): 2073. http://dx.doi.org/10.1121/1.426803.

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Heertjes, Marcel Francois, and Jan-Gerard Cornelis Van Der Toorn. "Vibration Isolation System." Journal of the Acoustical Society of America 129, no. 4 (2011): 2353. http://dx.doi.org/10.1121/1.3582194.

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Platus, David L. "Vibration isolation system." Journal of the Acoustical Society of America 94, no. 2 (1993): 1177. http://dx.doi.org/10.1121/1.406935.

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Platus, David L. "Vibration isolation system." Journal of the Acoustical Society of America 97, no. 3 (1995): 2013. http://dx.doi.org/10.1121/1.412026.

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Jurevicius, M., V. Vekteris, V. Turla, A. Kilikevicius, and G. Viselga. "Investigation of the dynamic efficiency of complex passive low-frequency vibration isolation systems." Journal of Low Frequency Noise, Vibration and Active Control 38, no. 2 (2019): 608–14. http://dx.doi.org/10.1177/1461348418822230.

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In this study, the theoretical and experimental investigations of the dynamics of complex passive low-frequency vibration systems are described. It is shown that a complex system consisting of a vibrating platform, an optical table and a vibration isolation system of quasi-zero stiffness loaded by a certain mass may isolate low-frequency vibrations in a narrow frequency range only. In another case, the system does not isolate vibrations; it even operates as an amplifier. The frequencies that ensure the top efficiency of the vibration damping system of quasi-zero stiffness were established.
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Li, Shan, Liang Xu, and Yu Qi Wang. "The Research of COMAS Vibrating Conveyor Noise Reduction." Applied Mechanics and Materials 184-185 (June 2012): 583–86. http://dx.doi.org/10.4028/www.scientific.net/amm.184-185.583.

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In a cigarette silk production line of a cigarette factory, the noise of vibrating conveyor not only endangers the health of workers’ listening, but also reduces work efficiency. In this paper, the modal of the frame was analyzed with the ANSYS software. The analysis results show that the frame has torsion vibration and swing. These vibrations will bring adverse effects and noise. Through designing a vibration isolation system on the vibrating conveyor, the reasonableness and effectiveness of the isolation component were proved with static and dynamic analysis of the vibration isolation system with finite element method. At the same time, some rules what select the spring parameters were summed up. Through analyzing the isolation effect of the vibration isolation system in different parameters, these regularity conclusions will provide a basis for the noise reduction [1].
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Tanaka, N., and Y. Kikushima. "On the Hybrid Vibration Isolation Method." Journal of Vibration and Acoustics 111, no. 1 (1989): 61–70. http://dx.doi.org/10.1115/1.3269824.

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For the purpose of isolating the vibration transmission from machines to soil and vice versa, this paper presents a new active vibration isolation method, that is, a hybrid vibration isolation method capable of isolating the vibration in the whole frequency range. The hybrid isolation method contains the following three characteristics: (1) a low-pass filter of a conventional elastic support method; (2) a high-pass filter of an active vibration isolation method; (3) suppression of a resonant peak due to an elastic support by a servo damper method; First, this paper presents the principle of the hybrid vibration isolation method and shows a fundamental structure of the system. Then by making the active isolator work as a damper, the suppression of a resonant peak due to an elastic support is achieved. Next, taking into consideration both the control effect and the stability of the system, the design procedure of the hybrid vibration isolation system is shown. Moreover, a control chart to estimate the control effect for suppressing the force transmissibility is presented. Finally, an experiment is carried out, demonstrating that the hybrid isolation method is capable of suppressing the exciting force in almost all the frequency range.
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Tanaka, N., and Y. Kikushima. "A Study of Active Vibration Isolation." Journal of Vibration and Acoustics 107, no. 4 (1985): 392–97. http://dx.doi.org/10.1115/1.3269278.

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For the purpose of suppressing ground vibration produced by vibrating machines, such as forging hammers, press machines, etc., this paper presents an active vibration isolation method. Unlike conventional isolators, the active isolator proposed in this paper permits rigid support of the machines. First, the principle of the active isolation method is shown, and the system equations are derived. Secondly, the characteristics and the design parameters of the active isolation system are presented. Thirdly, from the point of view of the feedforward control method, the dynamic compensators are designed so as to sufficiently suppress the exciting force. Finally, an experiment is carried out to demonstrate that the active isolator is applicable for suppressing the ground vibration.
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Mofidian, S. M. Mahdi, and Hamzeh Bardaweel. "Displacement transmissibility evaluation of vibration isolation system employing nonlinear-damping and nonlinear-stiffness elements." Journal of Vibration and Control 24, no. 18 (2017): 4247–59. http://dx.doi.org/10.1177/1077546317722702.

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Undesired oscillations commonly encountered in engineering practice can be harmful to structures and machinery. Vibration isolation systems are used to attenuate undesired oscillations. Recently, there has been growing interest in nonlinear approaches towards vibration isolation systems design. This work is focused on investigating the effect of nonlinear cubic viscous damping in a vibration isolation system consisting of a magnetic spring with a positive nonlinear stiffness, and a mechanical oblique spring with geometric nonlinear negative stiffness. Dynamic model of the vibration isolation system is obtained and the harmonic balance method (HBM) is used to solve the governing dynamic equation. Additionally, fourth order Runge–Kutta numerical simulation is used to obtain displacement transmissibility of the system under investigation. Results obtained from numerical simulation are in good agreement with those obtained using HBM. Results show that introducing nonlinear damping improves the performance of the vibration isolation system. Nonlinear damping purposefully introduced into the described vibration isolation system appears to eliminate undesired frequency jump phenomena traditionally encountered in quasi-zero-stiffness vibration isolation systems. Compared to its rival linear vibration isolation system, the described nonlinear system transmits less vibrations around resonant peak. At lower frequencies, both nonlinear and linear isolation systems show comparable transmissibility characteristics.
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Dissertations / Theses on the topic "Vibration Isolation System"

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Krull, Alexander G. (Alexander Gerhard). "Experimental testing of LIGO vibration isolation system." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/40439.

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Thesis (S.B.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.<br>Includes bibliographical references (leaf 29).<br>The LIGO (Laser Interferometer Gravitational-wave Observatory) project is designed to detect gravitational waves using precision interferometry. The detection from astrophysical sources has the potential to test Einstein's Theory of General Relativity, and additionally open a new window into the universe and its origin. The Initial LIGO detectors are currently operating at a strain sensitivity of 10-21 Hz, or equivalently 1018 m/ [square root of] Hz, at 100 Hz. In order to attain improved sensitivity required for guaranteed detection of astrophysical sources, e.g. coalescing neutron star binaries and black holes, pulsars, and supernovae collapses, improvements of the strain sensitivity must be achieved. Next generation detectors such as Advanced LIGO are under development, which aims to improve the sensitivity by more than a factor of 10 at all frequencies, compared to initial LIGO. This improvement in sensitivity will be achieved in part by improved seismic isolation one component of which is an active vibration isolation platform. Currently, research and development is being conducted at MIT on a prototype of this vibration isolation system. The work described in this thesis focuses on the Internal Seismic Isolation (ISI) system under development for Advanced LIGO.<br>(cont.) This system consists of a three-stage in-vacuum seismic isolation system which is supported by an external hydraulic actuation stage known as the Hydraulic External Pre-Isolation (HEPI) stages of the active vibration control system. HEPI uses forces generated by hydraulic pressure to cancel low frequency seismic noise, primarily due to forces from ground vibration. The ISI is an actively controlled platform, in which each stage is supported by three maraging steel blade springs. The vibration is sensed in six degrees of freedom and reduced by applying forces through a control feedback loop. In order for the feedback loop to function properly, it is important to know and be able to predict the position of the ISI stages to within a few thousandths of an inch. Since the load being applied to the spring blades is known, the compliance of each spring along with various shim thicknesses will determine the final position of the stages. Although compliance is a material and geometric property, and should remain constant from spring to spring, due to imperfections of the fabrication process and variation in the material properties, small variations in the long and short spring compliance value were detected using a Spring Tester.<br>(cont.) The blades were designed based on their resonant frequencies and the load which they would be supporting - more specifically, their geometry (length, width, and thickness) were defined such that the load each supported brought them to a 1/3 of their failure stress. For my undergraduate thesis, I determined the compliance of multiple long and short springs was determined using a specially designed apparatus - the "Spring Tester." Ideally, three blade springs of identical compliance should be used to eliminate system imbalance, but to variation during fabrication may be difficult to achieve Using the Spring Tester the mean values for each set of long and short spring linear compliance data were found to be 0.729 +.008 mils/lb and 0.670 ±.027 mils/lb, respectively, while the means for the long and short angular compliance data were 0.078 + .001 mrad/lb and 0.089 ±.003 mrad/lb, respectively.<br>by Alexander G. Krull.<br>S.B.
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Beavers, George D. "System identification of an ultra-quiet vibration isolation platform." Thesis, Monterey, California. Naval Postgraduate School, 1997. http://hdl.handle.net/10945/9052.

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Approved for public release; distribution is unlimited<br>This thesis details the system identification and initial system validation of the an Ultra-Quiet Vibration Isolation Platform (UQP). With the move toward lighter and more flexible spacecraft, the effects of vibration are of immense concern. As natural or passive damping becomes less effective in controlling undesired vibrations, active vibration control becomes essential. The UQP uses a special configuration of the six degree of freedom Stewart Platform with piezoceramic strut actuators and geophone sensors. This combination gives an extremely sensitive and responsive six degree-of-freedom active vibration control system. Each actuator was designed to be controlled independently without coupling with other actuators. In order to develop control laws, the plant must be identified in terms of system zeros and poles and the uncoupled design validated. Dynamic modeling using parametric estimation methods can accurately describe a complex system. Using parameter estimation methods, models of the actuator system dynamics were obtained. A simple lead-lag controller was applied to individual actuators then all six actuators acting simultaneously to verify system coupling. Significant interaction between base adjoining actuators was discovered.
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Miu, Kevin Kar-Leung. "A low cost, DC-coupled active vibration isolation system." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/46061.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2008.<br>Includes bibliographical references (p. 303-306).<br>In this thesis, I designed and implemented an isolation system that interfaces with traditional air mounts for improved force disturbance rejection relative to passive optical tables.Force disturbance rejection and position alignment are two major functional requirements of vibration isolation systems. With conventional passive isolation systems, a tradeoff exists between improving force disturbance rejection maintaining ground vibration isolation. Commercial active isolators address such a tradeoff through the use of inertial sensors, but the AC-coupled nature of the sensors leads to an inconvenient low frequency response. By referencing a payload stiffly to a softly suspended proof mass, both of the aforementioned functional requirements can be resolved while maintaining ground disturbance isolation performance. Philips Applied Technologies originally developed the concept, named Advanced Isolation ModuleS (AIMS).The AIMS system uses a relative displacement measurement between a payload which is to be isolated from vibrations and a proof mass as feedback. The displacement sensor allows the inertial measurement to be DC-coupled. The objective of this research is to find a relatively low-cost approach for the AIMS concept.A 1-DOF active vibration isolation system based on closed loop control utilizing the DC-coupled inertial measurement as feedback was retrofitted onto an optical table. The coil of a commercial geophone was used as the proof mass, as the geophone provides a relatively inexpensive, low frequency suspension. Error budgeting was performed on the system to estimate and improve payload acceleration noise levels. The results yielded a system bandwidth of 30 Hz and a total system acceleration la value of approximately 1 mm/s².<br>by Kevin Kar-Leung Miu.<br>S.M.
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Macháček, Ondřej. "Magnetorheological Strut for Vibration Isolation System of Space Launcher." Doctoral thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2018. http://www.nusl.cz/ntk/nusl-391819.

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Práce se zabývá návrhem magnetoreologické (MR) vzpěry vibroizolačního systému (VIS) pro kosmický nosič. V rešeršní části jsou popsány vybrané VIS a vzpěry těchto systémů, které byly v kosmických nosičích využity v minulosti. Každá z těchto vzpěr obsahující kapalinu byla těsněna pomocí statických těsnění a pružných vlnovců vyrobených z oceli. Důkladněji byla analyzována vzpěra pasivního systému VIS s označením ELVIS, jehož konstrukce se stala inspirací pro tuto práci. Jedná se o tříparametrický systém, v němž je tlumič uložen na pružině, jejíž tuhost přibližně odpovídá objemové tuhosti vlnovců respektive jejímu průmětu do axiálního směru (pressure thrust stiffness). V práci je představena metodika pro stanovení “pressure thrust stiffness” na základě geometrie vlnovce a také uvedeny parametry vlnovce díky kterým je možné měnit poměr mezi axiální a “pressure thrust stiffness” vlnovce. Tento poměr ovlivňuje v dané koncepci vzpěry její dynamické chování a tím i chování celého VIS. Pro predikci dynamického chování vzpěry byl vytvořen multi-body model VIS založeného na Stewartově plošině a detailnější model jediné vzpěry. Simulace provedené v tomto modelu odhalily parametry, které mají vliv na výkonost tlumiče ve VIS: časová odezva a dynamický rozsah. Díky modelu byl určen rozsah těchto parametrů, ve kterých bude zaručena efektivní funkce vzpěry ve VIS, konkrétně: časová odezva: 0-5ms, dynamický rozsah: 5-10. Před finálním návrhem vzpěry byla sestrojena vzpěra experimentální vzpěra, jejíž parametry byly přesně naměřeny a využity pro verifikaci jednotlivých modelů. Poznatky získané během experimentů byly využity při návrhu finální vzpěry. Jeden z nejdůležitějších poznatků byla nutnost náhrady feritového magnetického obvodu s ohledem na jeho křehkost. Proto byl odvozen tvarový přístup k navrhování rychlých magnetických obvodů z oceli s využitím 3D tisku, který byl následně patentován. Navržená vzpěra obsahuje magnetoreologický ventil jehož odezva je predikována na 1.2 ms a dynamický rozsah 10. V závěru práce je představena metodika, díky které byla vzpěra navržena.
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Cinarel, Dilara. "Vibration Isolation Of Inertial Measurement Unit." Master's thesis, METU, 2012. http://etd.lib.metu.edu.tr/upload/12614069/index.pdf.

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Sensitive devices are affected by extreme vibration excitations during operation so require isolation from high levels of vibration excitations. When these excitation characteristics of the devices are well known, the vibration isolation can be achieved accurately. However, it is possible to have expected profile information of the excitations with respect to frequency. Therefore, it is practical and useful to implement this information in the design process for vibration isolation. In this thesis, passive vibration isolation technique is examined and a computer code is developed which would assist the isolator selection process. Several sample cases in six degree of freedom are designed for a sample excitation and for sample assumptions defined for an inertial measurement unit. Different optimization methods for design optimizations are initially compared and then different designs are arranged according to the optimization results using isolators from catalogues for these sample cases. In the next step, the probable designs are compared according to their isolator characteristics. Finally, one of these designs are selected for each case, taking into account both the probable location deviations and property deviations of isolators.
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Berba, Michail. "Research of passive low-frequency vibration isolation systems." Doctoral thesis, Lithuanian Academic Libraries Network (LABT), 2013. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2013~D_20130524_145420-89585.

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In dissertation discuss about new created dynamic characteristics establishment of low-frequency (0,7–50 Hz) vibrations isolation system. Presented theoretical and experimental investigations. Main goal of dissertation – is creation of dynamic parameters establishment methods for low-frequency vibration isolation systems and stiff quasi-zero vibrations isolation system, also investigate their dynamical characteristics and usage possibilities. Investigation object – low-frequency vibrations isolation mechanical systems and their dynamic characteristics establishment. Wish to realize investigation goal, were solved those tasks: 1) In scientifically literature investigates types of passive and active vibration isolation systems, constructions, work principals and analyze; 2) Analyzed and theoretically introduced mechanical conceptions of dynamic characteristics establishment methods of the vibration isolation systems; 3) Created stiff quasi-zero vibration isolation method and system based on zeroing of spring stiffness; 4) Done experimental dynamic characteristics evaluations of optics tables with pneumatic isolation and stiff quasi-zero vibration isolation systems; 5) Done vibration measurement uncertainty and given results reliability evaluation. Dissertation contents introduction, three parts, general conclusion of the results, used literature and list of author’s themes published dissertations, three attachments. In introduction part discuss about investigation problems... [to full text]<br>Disertacijoje nagrinėjamas naujai sukurtų mechaninių pasyviųjų žemojo (0,7–50 Hz) dažnio virpesių izoliavimo sistemų dinaminių charakteristikų nustatymas. Pateikiami teoriniai ir eksperimentiniai tyrimai. Pagrindinis disertacijos tikslas – sukurti mechaninių pasyviųjų žemojo dažnio virpesių izoliavimo sistemų dinaminių parametrų nustatymo metodiką ir kvazinulinio standžio virpesių izoliavimo sistemą, ištirti dinamines jų charakteristikas ir naudojimo galimybes. Tyrimų objektas – žemojo dažnio pasyviosios virpesių izoliavimo mechaninės sistemos ir jų dinaminių charakteristik nustatymas. Siekiant įgyvendinti tyrimų tikslą, išspręsti šie uždaviniai: 1) atlikta mokslinės literatūros apie pasyviųjų ir aktyviųjų virpesių izoliavimo sistemų tipus, konstrukcijas, veikimo principus analizė; 2) išanalizuoti ir pagrįsti mechaninių pasyviųjų virpesių izoliavimo sistemų dinaminių charakteristikų nustatymo metodai; 3) sukurtas kvazinulinio standžio virpesių izoliavimo metodas ir sistema, pagrįsta spyruoklių standžio įnulinimu; 4) atliktas optinių stalų su pneumatiniais izoliatoriais ir kvazinulinio standžio virpesių izoliavimo sistemos eksperimentinis dinaminių charakteristikų įvertinimas; 5) atliktas virpesių matavimo neapibr ėžties ir gautų rezultatų patikimumo įvertinimas. Disertaciją sudaro įvadas, keturi skyriai, rezultatų apibendrinimas, naudotos literatūros ir autoriaus publikacijų disertacijos tema sąrašai, trys priedai. Įvadiniame skyriuje aptariama tiriamoji problema, darbo... [toliau žr. visą tekstą]
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Zuo, Lei 1974. "Element and system design for active and passive vibration isolation." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/30341.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, February 2005.<br>Includes bibliographical references (p. 277-294).<br>This thesis focusses on broadband vibration isolation, with an emphasis on control of absolute payload motion for ultra-precision instruments such as the MIT/Caltech Laser-Interferometric Gravitational Wave Observatory (LIGO), which is designed to measure spatial strains on the order of 10-²¹. We develop novel passive elements and control strategies as well as a framework for concurrent design of the passive and active elements of single-stage and multi-stage isolation systems. In many applications, it is difficult to construct passive isolation systems compliant enough to achieve specifications on low-frequency ground transmission without introducing hysteresis as well as high-frequency transmission resonances. We develop and test a compliant support that employs a post-buckled structure in con- junction with a compliant spring to attain a low-frequency, low-static-sag mount in a compact package with a large range of travel and very clean dynamics. Most passive damping techniques increase ground transmission at high frequency, but tuned-mass dampers are decoupled from the ground. We explore the tuned-mass damper as a passive realization of the skyhook damper, obtain the optimal designs for multiple-SDOF systems of dampers, propose the concept of a multi-DOF damper, and show that MDOF dampers that couple translational and rotational motion have the potential to provide performance many times better than that traditional tuned-mass dampers. Active control can be used to improve low-frequency performance, but high-gain control can amplify sensor and actuator noise or cause instability. We study several control strategies for uncertain plants with high-order dynamics.<br>(cont.) In particular, we develop a novel control strategy, "model-reaching" adaptive control, that drives the system onto a dynamic manifold defined directly in terms of the states of the target. The method can be used to robustly increase the apparent compliance of an isolation mount and maintain a -40 dB/decade roll-off above the resulting corner frequency.<br>by Lei Zuo.<br>Ph.D.
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Le, Toan T. "A Single-Stage Passive Vibration Isolation System for Scanning Tunneling Microscopy." DigitalCommons@CalPoly, 2021. https://digitalcommons.calpoly.edu/theses/2272.

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Scanning Tunneling Microscopy (STM) uses quantum tunneling effect to study the surfaces of materials on an atomic scale. Since the probe of the microscope is on the order of nanometers away from the surface, the device is prone to noises due to vibrations from the surroundings. To minimize the random noises and floor vibrations, passive vibration isolation is a commonly used technique due to its low cost and simpler design compared to active vibration isolation, especially when the entire vibration isolation system (VIS) stays inside an Ultra High Vacuum (UHV) environment. This research aims to analyze and build a single-stage passive VIS for an STM. The VIS consists of a mass-spring system staying inside an aluminum hollow tube. The mass-spring system is comprised of a circular copper stage suspended by a combination of six extension springs, and the STM stays on top of the copper stage. Magnetic damping with neodymium magnets, which induces eddy currents in the copper conductor, is the primary damping method to reduce the vibrations transferred to the mass-spring system. FEMM and MATLAB® are used to model magnetic flux density and damping coefficients from eddy current effect, which will help determine the necessary damping ratios for the VIS. Viton, which demonstrates a high compatibility with vacuum environments, will also serve as a great damping material between joints and contacts for the housing tube. Viton will be modeled as a Mooney-Rivlin hyperelastic material whose material parameters are previous studied, and Abaqus will be used as a Finite Element Analysis software to study the Viton gaskets’ natural frequencies. The natural frequencies of the aluminum hollow tube will also be investigated through Abaqus.
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Knijnenburg, Gerard Franciscus. "Development of a vibration isolation system for a rotary wing unmanned aerial vehicle." Diss., University of Pretoria, 2017. http://hdl.handle.net/2263/62777.

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Antiresonance vibration isolation has long been a well known, studied and applied method for alleviating vibrations in stiff structures where small static deflection and a low transmissibility is needed, making it ideal for use in the rotor-craft industry. Most prior arts focus on passive single frequency antiresonance vibration isolation, while some, most notably liquid inertia vibration isolators, are adapted to actively isolate vibrations at more than one frequency. Very little literature is found on the adaptation of mechanical pendulum antiresonance vibration isolators for in-flight tunable multiple frequency isolation, and although these systems predate the more modern liquid inertia type isolator, there is merit in their further development and use as low cost, robust and low maintenance isolators. A feasibility study on the performance of changing each fundamental design variable to achieve antiresonance tuning concludes, that for the antiresonance frequency shift range of interest in this dissertation, no specific design variable change quantifiably outperforms another with respect to tuning the antiresonance. Concept designs are created and investigated, finding the superior method of tuning the vibration isolator based on other criteria like overall weight, design simplicity, practicality, robustness and reliability. Shifting the tuning mass on the pendulum arm is deemed to be the superior concept, with respect to the helicopter being developed, and a tunable multi-frequency pendulum antiresonance vibration isolation system with a sliding concentrated mass is developed with ADAMS multi-body dynamics software and SolidWorks. The isolation system along with a full scale dummy fuselage and transmission-rotor assembly is manufactured and experimentally tested. Initial experimental results show antiresonance frequencies 10Hz higher than the design targets, this phenomenon is later discovered to be related to friction in the pin joints of the pendulum hinges, increasing the system overall stiffness. Needle roller bearings are inserted to eliminate the friction, and experimental and ADAMS model results are again compared showing good correlation, with experimental results isolating close to the three target frequencies within 3% error. An astonishing level of vibration isolation is observed with the largest transmissibility obtained at the three frequencies being 0:5%. This dissertation proves the concept of a tunable mechanical pendulum vibration isolator, and its design methodology, particularly with respect to shifting the position of the tuning mass. Suggestions for further work are: to implement this system with an actuation mechanism, further research on the effects of friction in isolators and the use of said phenomenon as a tuning method, development of isolators implementing the other concept of changing the design variables and a comparison between the effect of normal damping and friction damping on vibration isolation.<br>Dissertation (MEng)--University of Pretoria, 2017.<br>Mechanical and Aeronautical Engineering<br>MEng<br>Unrestricted
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Giaime, Joseph Anthony. "Studies of laser interferometer design and a vibration isolation system for interferometric gravitational wave detectors." Thesis, Massachusetts Institute of Technology, 1995. http://hdl.handle.net/1721.1/11383.

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Books on the topic "Vibration Isolation System"

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Beavers, George D. System identification of an ultra-quiet vibration isolation platform. Naval Postgraduate School, 1997.

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Kim, Y. K. Equations of motion for the g-LIMIT microgravity vibration isolation system. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 2001.

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Johnson, Terry L. Development of a simulation capability for the space station Active Rack Isolation System. National Aeronautics and Space Administration, Langley Research Center, 1998.

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Sani, R. L. Modeling and new equipment definition for the vibration isolation box equipment system: Progress report. National Aeronautics and Space Administration, 1993.

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Pearson, Lillian. Design of a vibration isolation system for a cycle ergometer to be used on board the space shuttle. Mechanical Engineering Design Projects Program, University of Texas at Austin, 1991.

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Pearson, Lillian. Design of a vibration isolation system for a cycle ergometer to be used on board the space shuttle. Mechanical Engineering Design Projects Program, University of Texas at Austin, 1991.

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Pendergast, Karl J. Use of passive reaction wheel jitter isolation system to meet the advance X-ray Astrophysics Facility Imaging performance. National Aeronautics and Space Administration, 1998.

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A, Furman F., and Rivin Eugene I, eds. Applied theory of vibration isolation systems. Hemisphere Pub. Corp., 1990.

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Florence, Dennis E. Time and frequency domain synthesis in the optimal design of shock and vibration isolation for large structural systems. Naval Postgraduate School, 1997.

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Oran, Nicks Colby, and Langley Research Center, eds. Six degree-of-freedom "live" isolation system tests. National Aeronautics and Space Administration, Langley Research Center, 1986.

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Book chapters on the topic "Vibration Isolation System"

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Chen, Michael Z. Q., and Yinlong Hu. "Inerter-Based Isolation System." In Inerter and Its Application in Vibration Control Systems. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-10-7089-1_3.

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Yue, Xueming, Yin Wang, and Fanbiao Bao. "Vibration Isolation System of Test Equipment." In Proceedings of IncoME-V & CEPE Net-2020. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-75793-9_35.

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Willen, G. S., and E. M. Flint. "Thermally Conductive Vibration Isolation System for Cryocoolers." In Cryocoolers 11. Springer US, 2002. http://dx.doi.org/10.1007/0-306-47112-4_90.

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Verma, Mohit, and Christophe Collette. "Active Vibration Isolation System for Drone Cameras." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-8049-9_67.

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Wei, Zhongliang, Minghui Chen, Sijuan Zheng, et al. "Cab Suspension Vibration Isolation Analysis Based on Vibration Decoupling Theory." In Proceedings of the 13th International Conference on Man-Machine-Environment System Engineering. Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-38968-9_25.

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Pesik, L., A. Skarolek, and O. Kohl. "Vibration Isolation Pneumatic System with a Throttle Valve." In The Latest Methods of Construction Design. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-22762-7_12.

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Karnovsky, Igor A., and Evgeniy Lebed. "Vibration Isolation of a System with One or More Degrees of Freedom." In Theory of Vibration Protection. Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-28020-2_1.

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Platz, Roland. "Approach to Assess Basic Deterministic Data and Model Form Uncertaint in Passive and Active Vibration Isolation." In Lecture Notes in Mechanical Engineering. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-77256-7_17.

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AbstractThis contribution continues ongoing own research on uncertainty quantification in structural vibration isolation in early design stage by various deterministic and non-deterministic approaches. It takes into account one simple structural dynamic system example throughout the investigation: a one mass oscillator subject to passive and active vibration isolation. In this context, passive means that the vibration isolation only depends on preset inertia, damping, and stiffness properties. Active means that additional controlled forces enhance vibration isolation. The simple system allows a holistic, consistent and transparent look into mathematical modeling, numerical simulation, experimental test and uncertainty quantification for verification and validation. The oscillator represents fundamental structural dynamic behavior of machines, trusses, suspension legs etc. under variable mechanical loading. This contribution assesses basic experimental data and mathematical model form uncertainty in predicting the passive and enhanced vibration isolation after model calibration as the basis for further deterministic and non-deterministic uncertainty quantification measures. The prediction covers six different damping cases, three for passive and three for active configuration. A least squares minimization (LSM) enables calibrating multiple model parameters using different outcomes in time and in frequency domain from experimental observations. Its adequacy strongly depends on varied damping properties, especially in passive configuration.
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Chernyshev, V., and O. Fominova. "Control of Damping Process in System of Vibration Isolation." In Proceedings of the 4th International Conference on Industrial Engineering. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-95630-5_37.

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Masano, Ryo, Nanako Miura, and Akira Sone. "Experimental Vibration Analysis of Seismic Isolation System Using Inertial Mass Damper." In Vibration Engineering for a Sustainable Future. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-48153-7_33.

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Conference papers on the topic "Vibration Isolation System"

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Jiang, Rong-Jun, and Shi-Jian Zhu. "Vibration Isolation and Chaotic Vibration." In ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/detc2003/vib-48589.

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Taking single degree of freedom vibration isolation system under simple harmonic excitation as an example, and considering the energy, the vibration isolation performance in different conditions was studied theoretically and numerically. The results shows that when the simple harmonic excitation import energy is definite, the vibration isolation performance at the primary harmonic frequency of the nonlinear vibration isolation system is better than that of the linear system, and the vibration isolation performance of the nonlinear vibration isolation system in chaotic vibration state is much better than that in non-chaotic vibration state. For the same isolated object, if can let the vibration isolation system vibrate chaotically, the system will possess the best isolation performance at the primary frequency.
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Bastin, P. H., and D. L. Edberg. "Microgravity Payload Vibration Isolation System Development." In International Conference On Environmental Systems. SAE International, 1994. http://dx.doi.org/10.4271/941416.

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Stebbins, Robin T., David Newell, Sam N. Richman, Peter L. Bender, James E. Faller, and James Mason. "Low-frequency active vibration isolation system." In SPIE's 1994 International Symposium on Optics, Imaging, and Instrumentation, edited by Colin G. Gordon. SPIE, 1994. http://dx.doi.org/10.1117/12.188876.

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Zhao, Cun-Sheng, Shi-Jian Zhu, and Zhen-Zhong Zhang. "Optimization Design of Vibration and Shock Isolation System." In ASME 2006 International Mechanical Engineering Congress and Exposition. ASMEDC, 2006. http://dx.doi.org/10.1115/imece2006-14035.

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The combination optimization design problem of vibration isolation and shock resistance system is studied in consideration of acoustical concealment performance and lifeforce of ships. The weakness of design method based on continuity is pointed out and combination optimal design method is brought forward. Then the limiting performance of shock isolation system is analyzed and two realization methods are discussed. One method is to adopt linear stiffness component with large damping. The other method is to use multiple linear stiffness components without damping. Amplitude of steady excitation is much smaller than that of shock input during experiment. Experimental results showed that the optimal loss factor is still 0.4 when the stiffness of shock bumper is much larger than that of vibration isolator, just the same with that suffered from only shock loads. Experimental results also showed that limiting performance can be achieved by configuration optimal design using multiple linear components. The two discussed methods can be used to direct engineering application.
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Liu, Yanning, Yanchu Xu, and Bill Flynn. "Isolation and Vibration Transmission Reduction of Systems Mounted on a Flexible Structure." In ASME 2003 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/detc2003/vib-48558.

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Issues addressed in this paper are related to the isolation and vibration transmission of vibration-sensitive systems mounted on a flexible support. The normal operation of certain electronic, optical and mechanical systems requires a vibration-free environment. To obtain such an environment, these systems are usually isolated from their supports with soft springs. When an array of such systems is needed, due to space constraints or other reasons, they are typically mounted on a common support, which in practice is flexible. Although such a design generally is effective in isolating vibration from ground support, vibration from one system, due to excitations other than from its support, can easily transmit to nearby systems. The level of the transmitted vibration (also known as vibration interaction) can be very significant, especially when all the systems are designed identically for simplicity and with less damping for effective ground vibration isolation. Isolator frequency separation (decoupling), viscous and viscoelastic damping are studied for the reduction of vibration transmission among the systems and their effects on system isolation are discussed. It is found that although the isolator frequency separation and viscous damping could be used for vibration transmission reduction among the isolated systems on the flexible support, the addition of viscoelastic damping reduces the vibration transmission without sacrificing their isolation performance. The difference between viscous and viscoelastic damping on ground vibration isolation is explained theoretically in the final part of the paper using a one degree of freedom model.
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Mizutani, Kazuki, Yoshitaka Fujita, and Ryojun Ikeura. "On an Improvement of Hybrid Vibration Isolation System." In ASME 1997 Design Engineering Technical Conferences. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/detc97/vib-3805.

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Abstract This paper proposes a hybrid-type vibration isolation system controlled by a phase compensated LQ control method with a frequency shaped weighting function. The hybrid system is composed of a passive spring-damper system reducing vibrations of high frequency range and an active one reducing those of low frequency range. This system is controlled by the phase compensated digital LQ optimization method with a frequency shaped weighting function. By the proposed method, the phase-lag of the control system is compensated so that the vibration isolation performance is improved. Simulations for the active system are carried out and the effectiveness of the phase compensation is shown. Then, experiments for the hybrid system are carried out for sinusoidal or random excitations. It is confirmed that the purposed hybrid system has the excellent isolation performance for excited vibrations over the wide frequency range.
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Hu, Yinlong, Michael Z. Q. Chen, Zhan Shu, and Lixi Huang. "Vibration analysis for isolation system with inerter." In 2014 33rd Chinese Control Conference (CCC). IEEE, 2014. http://dx.doi.org/10.1109/chicc.2014.6896099.

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Quenon, Dan, Jim Boyd, Paul Buchele, et al. "Miniature vibration isolation system for space applications." In SPIE's 8th Annual International Symposium on Smart Structures and Materials, edited by Anna-Maria R. McGowan. SPIE, 2001. http://dx.doi.org/10.1117/12.429654.

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Edberg, Donald L., Conor D. Johnson, L. Porter Davis, and Eugene R. Fosness. "Development of a launch vibration isolation system." In Smart Structures and Materials '97, edited by L. Porter Davis. SPIE, 1997. http://dx.doi.org/10.1117/12.274216.

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McMickell, M. B., Thom Kreider, Eric Hansen, Torey Davis, and Mario Gonzalez. "Optical payload isolation using the Miniature Vibration Isolation System (MVIS-II)." In The 14th International Symposium on: Smart Structures and Materials & Nondestructive Evaluation and Health Monitoring, edited by L. Porter Davis, B. K. Henderson, and M. Brett McMickell. SPIE, 2007. http://dx.doi.org/10.1117/12.715446.

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Reports on the topic "Vibration Isolation System"

1

Ponslet, E. R., and M. S. Eldred. Discrete optimization of isolator locations for vibration isolation systems: An analytical and experimental investigation. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/244592.

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