| Experimental Study On The Effects OF TMD | | | | Â |
| On Structure Vibration Reduction | | | | Â |
| Â | | | | 5. Getting Data [26] |
| M H Pashaei(1), H Sheydaie (2) I Â Khatami (3)Â M | | | | Using experiment equipment we come to a |
| jazayeri (4) | | | | time-displacement graph which is being showed in Fig |
| Â | | | | 11 , 12 .the first graph shows the displacement of |
|            School of Engineering, University | | | | structure under the free vibration using TMD and the |
| of Mazandaran, P O Box: 484, Babol, Iran | | | | second one not using TMD. |
| Email: (1)Â , (2)(3) | | | | Â |
| Â , < >(4) | | | | Â |
| Â | | | | Â |
| ___Abstract | | | | Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â |
| Damping is a phenomenon which exists in every | | | | Fig 11.Time –Displacement Graph for system without |
| system. Some systems have little and some have | | | | TMD |
| more. it is related to what elements and how they are | | | | Â |
| assembled with each other in system .such | | | | Â |
| phenomena dissipate energy and reduce the vibrating | | | | Â |
| caused by external applied forces to system like earth | | | | Â Â Â Â Â Fig 12. Time _Displacement Graph for |
| quick, wind ,sea wave and thunder .Different types of | | | | system with TMD |
| dampers have been known regarding to their function: | | | | Â |
| passive, active and semi-active. In the field of passive | | | | Â |
| dampers we have many types: tuned mass damper | | | | It is clear if we confess on both graphs it shows the |
| TMD, tuned liquid damper TLD, friction dampers FD | | | | Maximum Displacement reduce from 1.3 mm to 1.1 mm. |
| and viscose dampers VD. | | | | For all the graph we use the   ‘logarithmic |
| The present research experimentally studies damping | | | | decrement’ method to calculate damping ratio . |
| ratio of a three-storey building using TMD and without | | | | Fig 13 shows a graphical representation of a damped |
| TMD damper to see how damper increase the | | | | free vibration. The motion shown in Fig 13 may be |
| damping ratio . To carry out this study A Â structure | | | | represented by the equation: |
| and the necessary equipment including a loading | | | | Â |
| system and a data acquisition system are used.. | | | | Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â |
| Structure examined under the free vibration in this | | | | Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â (3) |
| way: A small displacement implemented to the | | | | Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â |
| structure as a free vibrations. And by carrying out | | | | Where |
| more than 150 tests, the damping ratios of the | | | | Â |
| structure using TMD and without TMD in different | | | | Â |
| loading conditions are obtained. The results show that | | | | Â |
| the Tuned mass damper has a major effect on the | | | | Is the natural frequency, is the damping ratio of the |
| damping characteristics of the structure The results | | | | system and X and are arbitrary constants determined |
| also show that the increasing the loading applied to | | | | from initial conditions. |
| structure doesn’t change the damping ratio which is | | | | The natural logarithm of the ratio of any two |
| analyses an Ansys software . | | | | successive amplitudes, for example  and  in Fig 1, |
| Key Word: damping ,tuned mass damper ,damping | | | | can be written as: |
| ratio | | | | Â Â Â Â Â Â Â Â Â Â Â |
| ___ | | | | Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â (4) |
| 1 Introduction | | | | Where  and can be obtained from Eqn 3 at t=t1 and |
|  | | | | t=t2=t1+τ, respectively. Inserting these values of  and |
| 1.1 Damping concept | | | | Â in Eqn 4 will result in the following equation: |
| Damping is a phenomenon where the amplitude of | | | | Â Â Â Â Â Â Â Â Â Â Â |
| vibration in a mechanical system steadily diminishes. | | | | Â Â Â Â Â Â Â |
| The effect of damping is to remove energy from the | | | | Â Â Â Â (5) |
| system. Energy in a vibrating system can be | | | | For every step of loading we get the result showed in |
| dissipated, being converted into heat [1,2,3]. | | | | Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â |
| Â | | | | Â |
| Â | | | | Â Â Table 1 |
| Damping is present in all vibrating systems. Every | | | | Â |
| system which possesses mass and elasticity is | | | | 6. Results |
| capable of vibration. Dampers are kind of device in | | | | - Damping ratios change with applying different loads |
| order to dissipate vibration forces... Different types of | | | | for the system not using TMD instead it will not change |
| dampers have been known .in general they are divided | | | | for system using TMD .thus it can be show that using |
| in three categories: passive, active and | | | | Tmd increase the damping ratio but if the amplitude of |
| semi-active.[4,5,6,7].Tuned liquid dampers[8] and Tuned | | | | system increase cause by Appling more forces, it will |
| mass dampers[9] are  very usual one which are using | | | | not change. . A Tuned Mass Damper has constant |
| nowadays in many structural system and the second | | | | behavior. |
| one is our research topic. | | | | - For optimize performance of TMD it is better to |
| Â | | | | design optimum range of 0 to 2% of mass and |
| 2 Examined model | | | | stiffness of real structure |
| Â | | | | . If we suppose the structure like a cantilever beam, |
| In present research A Â structure is being designed | | | | the edge of the beam has more displacement during |
| and built as a model of a real structure in Fig.1 | | | | vibration, so it is rational to locate damper where there |
| Â | | | | is more displacement. |
| Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â | | | | Â |
| Â Â Â Â Â Â Â Â Â Â Â Fig 1: drawing and picture of | | | | Â |
| model | | | | Â |
|  the weight of the structure is 200 kg and the | | | |  |
| stiffness of that is k=6.666 N/mm and  the natural | | | |  |
| frequency is w=0.056 Hz which was analyses in a | | | |  |
| finite element software Ansys | | | | Â |
| Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Fig 2: analysed model | | | | Â |
| in software | | | | Â |
| Â | | | | Â |
| 3 TMD design [11~25] | | | | Â |
| Â in order to design the TMD with study of many | | | | Â |
| books and article and the real TMD used in some real | | | | Â |
| structures in the world like Citicope tower in New York | | | | Â |
| [10] we came to this result : the mass of TMD | | | |  |
| can consider 2 percent of structure’s mass or less, | | | |  |
| but it should be design in a optimum way . Natural | | | | Reference |
| frequency of TMD Should be as the natural frequency | | | | Â |
| of real structure. When the real structure approach to | | | | Â |
| its natural frequency caused by external applied | | | | 1-    Jeary, A. P., and Ellis, B. R., ‘Vibration Tests |
| forces, TMD must approach to its natural frequency | | | | on Structures at Varied Amplitudes’ proc. ASCE |
| too. The vibration of TMD at natural frequency causes | | | | EMD Specially conference on Dynamic Response of |
| turbulence in general movement. In this way the | | | | Structures, ASCE, Atlanta, GA, 1981 |
| frequency of structure go further from its natural | | | | 2-    Barkanov, E., ‘Transient response |
| frequency. | | | | analysis of structures made from viscoelastic |
|     As a result, the stiffness of TMD also should | | | | materials’ International J. for numerical methods in |
| consider 2 percent of structure’s stiffness | | | | engineering, vol. 44, 1999 |
| to     .    be as the same. | | | | 3-    Allen, D. ‘The Mero Space Frame |
|  | | | | System’ Proceeding of Australian Conference on |
|            The Mass   Of    | | | | Space Structures, Melbourne, Australia, 1982. |
| TMD:Â Â Â Â Â Â Â Â Â Â Â Â Â | | | | 4-Â Â Â Â Samali B, Kwok KCS. Vibration control |
|                              (1) | | | | systems for civil engineering structures in Australia — |
| Â | | | | actual installations and state-ofthe- art research. In: |
|             The Stiffness Of | | | | Proc. 2nd Int. Conf. on Motion and Vibration Control, |
| TMD:                  (2) | | | | Yokohama, Japan, 1994:k22–35. |
| Â | | | | 5-Â Â Â Â Tamura Y. Suppression of wind-induced |
| Â | | | | vibrations of buildings.J Wind Engng, (JAWE), |
| After determination of mass and stiffness’ amount | | | | 1990;44:71–84. |
| of TMD, a block and spring design and then | | | | 6-Â Â Â Â Kareem A. Mitigation of wind induced motion |
| manufactured at Fig 4 and 5. | | | | of tall buildings.J Wind Engng and Industr Aerodyn |
|                            | | | | 1983;11:273–84 |
| Fig 4: mass | | | | 7-Â Â Â Â Structural control by induced stress based |
|                           Fig 5: | | | | stiffness modification by   By Katie Patricia Whipp |
| spring dimension | | | | ,Augest 2005 nashaville Tennessee . |
| After manufacturing the block as a mass and spring | | | | 8-Â Â Â Â McNamara RJ. Tuned mass dampers for |
| as a stiffness element, they attached to each other | | | | buildings. J Struct Engng, ASCE |
| Fig 6 and assembled on a bearing Fig.7 in order  to | | | | 1977;103(ST9):1785–98. |
| have soft movement .               | | | | 9-    Fujino Y, Sun L, Pacheco BM, Chaiseri P. |
| Â Â Â Â Â Â Â Â Â Â Â Â Â | | | | Tuned liquid damper (TLD) for suppressing horizontal |
| Â | | | | motion of structures. J Engng Mech, ASCE |
| Fig 6. Mass and spring | | | | 1992;118(10):2017–30. |
| attached                        | | | | 10- USGS Response to an Urban Earthquake |
| Â Â Â Â Â Â Â Â Â Â Â Â Fig 7. Mass assembled on | | | | Northridge 94, Prepared by the U.s. Geological Survey |
| bearing | | | | 1 for the Federal Emergency Management Agency |
| Â | | | | (FEMA) Open-File Report 96-263, 1996. |
| And finally whole commission on our modeled structure | | | | 11- Den Hartog, J.P., 1956. ''Mechanical Vibrations, ath |
| to examine how it effect the damping ratio of | | | | Edition''. McGraw-Hill. New York, 436 PP. |
| structure Fig.8. | | | | 12- Frahm, H., 1909. ''Device for Damping Vibration of |
| Â | | | | Bodies'' , US Patent No. 989958, Oct. 30, 1909. |
| Â | | | | 13- Anderson, B. D. O., and Moore, J. B. (1990). Optimal |
| Fig 8 | | | | Control: Linear Quadratic Methods, Prentice Hall, Upper |
| Â | | | | Saddle River. N.J. |
| Â | | | | 14- Bachman, H., and Ammann, W. (1987). Vibrations in |
| 4. Method of loading and equipment | | | | Structures, IABSE, Zurich. |
| To apply load to structure we use a method showed | | | | 15- Bachmann, H.(1995). Vibration Problems in |
| in Fig 9. a block will hang using a rope to structure and | | | | Structures: Practical Guidelines, Birkauzer Verlag. Basel. |
| suddenly the rope will cut then dropping the block | | | | Boston. |
| cause a loading which apply to structure .this | | | | 16- Brogan, W. L. (1991). Modern Control Theory, 3rd ed., |
| procedure carry both condition the structure using | | | | Prentice Hall, Upper Saddle River, N.J. |
| TMD and without TMD .in this way we have the free | | | | 17- Chopra, A. (1995). Dynamics of Structures, Prentice |
| vibration condition . | | | | Hall, Upper Saddle River, N. J. |
| Fig.9 | | | | 18- Clough, J. W., and Penzien, J (1993). Dynamics of |
| Â | | | | Structures, 2nd ed., McGraw-Hill, New York. |
| The equipment Fig .10 to record the data is: | | | | 19- Soong.T.T., and Dargush, G. F. (1997). Passive |
| Â | | | | Energy Dissipation Systems in Structural Engineering. |
| Â a) A sensor which is called transducer | | | | John Wiley & Sons, New York. |
| Â b) A hardware which is called Data Logger which | | | | 20- Strang. G. (1993). Introduction to Linear Algebra, |
| transfer the sensor output to computer | | | | Wellesley-Cambridge Press, Wellesley, Massachusetts. |
| Â c) A computer and the software of Pulse which | | | | 21- Suh. N. P. (1990). The Principles of Design, Oxford |
| show the output in Graph as a graph of | | | | University Press, London. |
| time-displacement. | | | | 22- First World Conference on Structural Control |
| Â | | | | (1994). Intemational Association for Structural Control, |
| Â | | | | Pasadena, California. |
| Â Â Â Fig 10 | | | | 23- 11th International Conference on Structural |
| Â | | | | Mechanics Reactor Technology (1991). Seismic Isolation |
| Â | | | | and Response Control for Nuclear and Non-Nuclear |
| 4. Methodology of experimentin order to have free | | | | Structures, Tokyo, Japan. |
| vibration we should apply the initial speed or initial | | | | 24- International Workshop on Recent Developmenis In |
| displacement to the structure. Our method is initial | | | | Base Isolation Techniques for Buildings (1992). |
| displacement .for this purpose the structure will be | | | | Architectural Institute of Japan. Tokyo, Japan. |
| loaded bye some block and by make them free from | | | | 25- Mechanical Eng. Design by Shigley, Shigley, Sixth |
| the structure the initial displacement will apply to | | | | Edition |
| structure .the loading carried out using steel block and | | | | 26- Thomson, W.t., "Theory of Vibration With |
| different size fro 15 kg until 75 kg with the step of 10 | | | | Application'' 2nd Edition, London, George Allen & Unwin, |
| kg. The test carried out nearly 150 times to get to a | | | | 1993. |
| correct conclusion. | | | | |