Finite element analysis of ground borne vibrations in sensitive buildings using inputs from free field measurements
T.N. Tuan Chik
1, J.M.W. Brownjohn
2, M. Petkovski
3
1,2,3 University of Sheffield, Department of Civil and Structural Engineering
Sir Frederick Mappin Building, Mappin Street, Sheffield, S1 3JD, United Kingdom
Email: [email protected], [email protected], [email protected]
Abstract The development in modern fabs manufacturing of micro-electronics components like chip processors and
laboratories fully equipped with high resolution devices requires very low level of vibration due to small
allowable tolerances of the size of the equipment. As a result, the generated vibration level at the site is
critical for estimating and providing suitable conditions for vibration sensitive facilities. For this purpose,
ground borne vibration levels at specified locations are considered as input for the simulation analysis
which is used in assessing the response of the structure in time domain and also in one third octave band
frequency domain. This paper investigates the transmission of the amplitude of ground borne vibrations
generated by external sources, into low rise structures housing sensitive facilities. Finite element analyses
of the structure are used to predict the dynamic response of the structure, which is then compared with the
free field measurements (input). The results of FE analyses are checked against the generic vibration
criteria guidelines for vibration sensitive equipment. The results show that prediction based on dynamic
response analysis can be used for selecting and designing an effective foundation system. The effect of the
foundation system will provide guidelines for designing new vibration sensitive facilities.
1 Introduction
The modern laboratories producing integrated circuits consisting of smaller, more tightly packaged and
high-tech elements require greater precision and stability in micro-electronics manufacturing and
evaluation equipment. There is a need for a better understanding of the effects of environmental low level
vibrations on this type of equipment, in order to enable microelectronics facility designers to provide a
suitable condition without costly overdesign of the structure. Manufacturers provide vibration
specification for some, but not all sensitive equipment. With a few exceptions, the information provided is
incomplete. In these cases further analyses have to be carried out to ensure that the equipment follows the
existing guidelines.
In this paper, the state of the art of low level ground borne vibration with a focus on vibration criteria for
sensitive facilities and dynamic response of the buildings is assessed. Ground borne vibration induced by
external sources such as moving traffic like trucks, trams, trains etc. can produce unacceptable vibration to
humans and especially to buildings which accommodate very sensitive equipment [1]. The vibrations
propagate through the ground and into buildings often causing vibrations at the resonant frequencies of
various components of the building, such as floors and walls. Predicting the transmission of ground borne
vibration waves to a structure is one of the problems that need to be taken into account when designing the
building. The potential sites for advanced technology buildings are limited by varying degrees of ground
borne vibrations from a variety of potential sources [2].
The vibration sensitive equipment has been investigated by Gordon [3] and his colleagues since 1980s, for
various vibration sources, including ground borne vibration. There are several significant research
contributions with theoretical and experimental studies related to vibration sensitive equipment. Gendreau
et al. [4] investigated a desirable vibration environment at a site may be degraded by ground borne
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propagation of waves from a variety of external sources as well. They proposed that a site vibration
evaluation is needed for all facilities requiring the equivalent of VC-D or more stringent as shown in
Figure 1 and described in Table 1. Because of poor performance of several types of equipment, Gordon
[2] found that some vendors had inadequate vibration control, where their tool specification was either did
not satisfy the standard or was not reliable for facility design. He also introduced the generic vibration
criteria with Ungar [5]. Kim and Amick, Bayat and Davis and Bessasson et al. [6-8] have the same issues
with sensitive equipment. They proposed several methods of active vibration control to reduce excessive
vibration. They also used specific vibration criteria for equipment designing tools as shown in Figure 1.
1.1 Generic vibration criteria
Generic vibration criteria are essential in this study as a guideline when designing facilities for research,
microelectronics manufacturing and other similar activities. They were introduced by Ungar and Gordon
[5][9]. The criteria are specified as a set of one third octave band velocity spectra levels, from VC-A (least
severe) to VC-E (most severe). This criteria were upgraded several years later by Amick et al. [10] to VC-
G with the smallest value 0.78µm/s as shown in Figure 1(b). The application and range of the VC limits
including ISO criteria for humans is described in Table 1. The amplitude of velocity is measured in one
third octave frequency band over the frequency range of 8 to 80 Hz for VC-A and VC-B or 1 to 80 Hz for
VC-C to VC-G. The detail size of the equipment is referred to line width in the case of microelectronics
fabrication, the particle (cell) size in the case of medical and pharmaceutical research, etc. These criteria
curves are used in this study to evaluate the simulated response of the structures. Gordon [3]
recommended these criterion curves as a means of evaluating the performance of the floor that supported
vibration sensitive equipment.
(a)
(b)
Figure 1: Generic vibration criterion (VC) curves for vibration-sensitive equipment, showing also the ISO
guidelines for people in building. (a) Ungar and Gordon version [5] (b) Amick et al version [10]
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Vibration Curve Amplitude,
µm/s
Detail size,
µm
Application and experience
Workshop (ISO) 800 N/A Distinctly perceptible vibration. Appropriate to workshops and
no sensitive areas.
Office (ISO) 400 N/A Perceptible vibration. Appropriate to offices and no sensitive
areas.
Residential day
(ISO)
200 75 Barely perceptible vibration. Appropriate to sleep areas in most
instances. Usually adequate for computer equipment, hospital
recovery rooms, semiconductor probe test equipment, and
microscopes less than 40X.
Operating theatre
(ISO)
100
25 Vibration not perceptible. Suitable in most instances for surgical
suites, microscopes to 100X and other equipment of low
sensitivity.
VC-A 50 8 Adequate in most instances for optical microscope to 400X,
microbalances, optical balances, proximity and projection
aligners, etc.
VC-B 25 3 Appropriate for inspection and lithography equipment
(including steppers) to 3 µm line widths.
VC-C 12.5 1 - 3 Appropriate standard for optical microscopes to 1000X,
lithography and inspection equipment (including moderately
sensitive electron microscopes) to 1 µm line widths. TFT-LCD
stepper/scanner processes.
VC-D 6.25 0.1 – 0.3 Suitable in most instances for demanding equipment, including
electron microscopes (TEMs and SEMs) and E-Beam systems.
VC-E 3.12 < 0.1 A difficult criterion to achieve in most instances. Assumed to be
adequate for the most demanding of sensitive systems including
long path, laser-based, small target systems, E-Beam
lithography systems working at nanometer scales and other
systems requiring extraordinary dynamic stability.
VC-F 1.56 N/A Appropriate for extremely quiet research spaces, generally
difficult to achieve in most instances, especially cleanrooms.
Not recommended for use as a design criterion, only for
evaluation.
VC-G 0.78 N/A Appropriate for extremely quiet research spaces, generally
difficult to achieve in most instances, especially cleanrooms.
Not recommended for use as a design criterion, only for
evaluation.
Table 1: Application and range of the vibration criteria curve of Figure 1[10]
2 Finite element modeling techniques
Finite element modelling is a default norm for determining the dynamic performance of structures by
saving valuable design time and money in construction. In this study, the numerical simulation of
vibration response of typical building housing sensitive equipment was carried out by using ANSYS [11],
general purpose FE package and MATLAB software. ANSYS is finite element analysis software which
enables the researcher to develop models of structures, products, components or systems. It can apply
operating loads or other design performance conditions and also can optimise a design early in the
development process to reduce production costs, whilst MATLAB is a high-level programming language
and interactive environment that enables the researcher to perform computationally intensive tasks faster
than with traditional programming languages. All the relevant outputs from ANSYS were processed by
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means of MATLAB programmes, developed to determine the absolute response of the structure, and to
compare the structural performance with generic vibration criteria. The flow of the whole FE analysis for
this study is shown in Figure 2, showing the useful link of using ANSYS and MATLAB. ANSYS will
analyse the model (structure) to obtain dynamic response (output). MATLAB will continue the process of
analysis by calculating the obtained response (output) with the generic desired criteria values. If there any
errors occurred or the output over the criteria limits, the model need to be analysed again by performing
structural optimisation with several design variables changed. The further section will explain all required
analysis related to this study.
Figure 2: The structural vibration analysis process
2.1 Response to base excitation
The response analysis for a multi storey frame subjected to base acceleration, as in the case of earthquake,
is similar to the analysis of systems subjected to external force. From dynamic equilibrium, the equations
of motion for free (unforced) vibration are:
0)( tftftf kcI (1)
Where If = ( )mx t is inertia force, ( ( ) ( ))c gf c x t x t is damping force and ( ( ) ( ))k gf k x t x t is
elastic spring force (positive when gx x ), gx and gx are ground displacement and velocity respectively.
By substituting for kf etc. and dropping the (t),
0)()( xxkxxcxm gg (2)
Adding gxm (where gx is ground acceleration) to both sides of equation (2) gives:
gggg xmxxkxxcxxm )()()( (3)
It is the relative movement that gives rise to spring and damper forces; hence the relative displacement of
the mass with respect to the foundation can be defined as
gxxv (4)
Replacing (4) in (3) gives:
gmv cv kv mx (5)
Equation (5) can be used for determining the relative response to any base excitation. The absolute
response can be found by adding the base response.
ANSYS
YS
MATLAB
BAB
Excitation
(input)
Desired
criteria
Structure Response
(output)
Compare with
criteria values
Error, if any
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2.2 Modal analysis
The modal analysis was used to determine the dynamic properties (natural frequencies and mode shapes)
of the structure considered in this study. In this analysis, a Block Lanczos Eigen solver is used as a
solution method. This is an efficient algorithm which is suitable for modal analysis of large models. The
dynamic properties provide insight into the possible causes for vibration problems and therefore they can
be used as a basis for quality assurance in the design analysis. As a quick way to determine structural
flexibility, it can be used for prediction of structural performance under given vibration inputs. Also, the
model analysis is used as the first step in the more detailed dynamic analyses, such as a transient dynamic
analysis which is performed by using the mode superposition technique.
2.3 Transient analysis
Further analysis is the transient (time history) analysis which is a linear analysis technique used to
determine the dynamic response of a structure under the action of any general time-dependent loads. It is
used to determine the time-varying displacements, strains, stresses, and forces in a structure as it responds
to any combination of static and time varying loads while simultaneously considering the effects of inertia
or damping [12].
Transient analysis can be carried out using three methods; namely full method, reduced method and mode
superposition method [13]. The full method is the easiest way to use, does not reduce the dimension of the
considered problem since original matrices are used to compute the solution. All kinds of nonlinearities
may be specified, automatic time stepping is available, all kinds of loads may be specified, masses are not
assumed to be concentrated at the nodes and finally all results are computed in a single calculation. The
main disadvantage is the fact that the required solution time will increase with the size of the considered
model.
The reduced method will reduce the system matrices to only consider the Master Degree of Freedom
(MDOFs) to solve the transient problem. The calculations are much quicker than full method. However,
automatic time stepping is not possible. Consequently, this method is not very popular any more since all
its disadvantages do not really compensate the advantage of lower costs in solution time.
The mode superposition method is a very powerful method to reduce the number of unknowns in a
dynamic response analysis. This method requires a preliminary modal analysis, as factored mode shapes
are summed to calculate the structure's response. It is the quickest of the three methods, but it requires a
good deal of understanding of the problem at hand. It reduces the dimension of the original problem as the
transient analysis is finally performed in the modal subspace which has the dimension of the number of
mode shapes used for the superposition, thus reducing the solution time. The accuracy of the solution
depends only on the number of mode used for the modal superposition. The results of this analysis give
the relative response to which the input motion should be added in order to obtain the absolute response of
the structure.
2.4 Dynamic response by mode superposition
It is usually necessary to determine the dynamic response of a structure to applied forcing functions. This
amounts to finding the solution to the equation of motion of the equivalent multi degree of freedom as
given by:
fkxxcxm (6)
The solution for the displacements x can be used to calculate internal forces and stresses at any instant of
time [14]. In this analysis, direct numerical integration is used to solve equation (6) by mode superposition
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method, which is generally more efficient for linear structures. Mode superposition is based upon the fact
that the deflected shape of the structure is expressed as a linear combination of all the modes:
N
n
nnNN YYYYYx1
332211 ... (7)
The coefficients nY are the modal amplitudes, which vary with time, and n are the mode shapes.
Equation (7) may be written in the more compact matrix notation:
Yu (8)
Where the modal matrix is whose columns are the mode shapes, and Y is a vector of the modal
amplitudes:
N ...321 (9)
Nn
T YYYYYY ......321 (10)
The modal amplitudes, nY are often referred to as generalized coordinates which may be contrasted with
the natural coordinates x. Modal analysis is a process of decomposing (6), using generalized coordinates,
so as to obtain a set of differential equations that are uncoupled, each of which may be analyzed as a
single degree of freedom.
Mode superposition is an efficient method of analysis because of the modal summation, given by (7), is
usually dominated by the lower modes of vibration, allowing higher modes to be excluded from the
analysis without significant error.
3 Structure characteristics and materials properties
The FE model was developed based on a particular three story industrial building in South East Asia. The
building has dimensions of 29mx20m in plan and a total height of 17m. The basic structure consists of a
reinforced concrete frame comprising columns and beams with various cross sectional dimensions without
a pile system. This frame structure supports slabs with three different thicknesses: 300mm at first floor,
160mm at second and third floor and 225mm at the roof level. Figure 3 shows the 3D FE model of this
building. The structural material used for columns and beams is concrete with density of =2400 kg/m3,
Young’s Modulus, E=38GPa, and Poisson ratio, =0.2. The modal damping ratio was assumed to be
=2%. The beam and column elements were modeled in ANSYS by using BEAM4 element, while the
slab was modeled using SHELL63 element. The base slab is fixed to the ground.
The response of the building was assessed by means of transient analysis of the response to free field input
signal (acceleration) as shown in Figure 4. One third octave band for the acceleration input with the
vibration criteria curve (VC-D) is shown in Figure 5. The structural velocity response was checked against
the VC-D curve to determine whether it velocity was over the limits or not.
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Figure 3: Finite element mesh of the industrial building
Figure 4: Acceleration input, time history (top) and frequency (bottom)
Figure 5: One third octave velocity spectra with vibration criteria curve (VC-D)
3.1 The structural response with rigid base foundation
The FE Model developed in ANSYS shows that the lowest mode of the superstructure with a rigid body
(sway) mode occurs at 2.58 Hz (mode 1) as shown in Figure 6(a). A few other modes are also shown in
the same figure. For example, the third floor has a vertical deformation at 11.33 Hz (mode 16), the first
mode where floor response significantly. The second floor similarly has a vertical deformation at 19.31
Hz. The FE model predicts about 50 modes of the structure falling under 20 Hz. These low frequency
modes display mostly global horizontal bending modes and global torsional modes of the whole building.
The remaining mode above 20 Hz indicates global horizontal bending of the whole building and the
columns.
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(a) Mode 1, 2.58 Hz
(b) Mode 16, 11.33 Hz
(c) Mode 50, 19.31Hz
Figure 6: Mode shapes and natural frequencies for selected modes
Figure 7 shows the responses from transient analysis both the time histories and frequency contents for
velocity responses for the investigated floors. The first floor was not considered as it is a fixed base onto
the ground. The maximum instantaneous velocity responses of the second and third floor were 2µm/s and
4µm/s, respectively. The peak amplitude is similar for both floors at about 7 Hz. The ground vibrations
above 20 Hz are not transmitted to both floors, which is a consequence structural damping.
Figure 8 shows one third octave velocity spectra for both floors. The structural responses are checked with
the design vibration criteria whether they lie within the acceptable limits or not. It shows both investigated
floors are not exceeding the limit VC-D (input signal). It is VC-B for the second floor, which is most
suitable for vibration sensitive equipment, for example an inspection and lithography equipment
(including steppers) to 3 µm line widths for the size of microns. For the third floor, the analysis shows
VC-A is adequate in most instances for optical microscope up to 400X, microbalances, optical balances,
proximity and projection aligners, etc up to the size of 8 microns.
These analyses demonstrate that the three stories of the structure fall within the limit of the design
vibration criteria. These predictions on dynamic response analysis will be used for selecting and designing
an effective pile foundation system. The effect of the foundation system to the same structure will be
investigated whether it still follows the limitation or not.
(a)
(b)
Figure 7: Time history and frequency content of the vertical structural velocity in the middle of (a) second
floor and (b) third floor
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Figure 8: One third octave band spectra with the vibration criteria curve for second floor (top, VC-B) and
third floor (bottom, VC-A)
3.2 The structural response with pile foundation
Further analysis is done by applied the similar structure with the piles as a foundation system to support
the structure. The foundation system in this analysis are comprises 15 piles with 7.5m length. The material
properties of piles with radius r= 0.3m and the wall thickness is 0.15m [15]. Bending stiffness is
=0.34GPam4, axial stiffness is =11GPam
4, Young’s modulus of piles is E=28GPa and density
=2667kg/m3. The properties of the soil are Young’s modulus, E=0.28GPa, density =2000kg/m
3, Poisson
ratio, =0.4 and damping loss factor=0.02. The piles were simulated in ANSYS by using elastic BEAM
element [16].
The effects of the piles to the structure were evaluated by comparing the results with the results obtained
for building with rigid base foundation. Figure 9 shows selected vibration modes which include
deformation of the piles. The first mode increased from 2.58 Hz (rigid base) to 3.66 Hz (pile foundation).
Mode 1 and Mode 2 show a global torsional and bending mode for the columns as shown in Figure 9(a)
and 9(b). The vertical deformations of the floors (third floor and roof) occur at 11.27 Hz (mode 13).
Figure 9(d) shows vertical bending modes in all floors at a frequency of 12.04 Hz. The other vibration
modes mostly show global horizontal bending of the whole structure. The pile does not affect significantly
the behavior of the superstructure at all obtained frequencies.
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(a) Mode 1, 3.66 Hz
(b) Mode 2, 5.37 Hz
(c) Mode 13, 11.27 Hz
(d) Mode 19, 12.04 Hz
Figure 9: Selected mode shapes and natural frequencies of the structure supported on pile foundation
Time histories analysis and frequencies content for structure is shown in Figure 10. For the second floor,
its maximum velocity response is 0.02µm/s and the peak amplitude occurs at 9 Hz. Significant vibration
amplification can be seen between 5 to 10 Hz for the second floor (Figure 10 (a)). The ground vibrations
are not transmitted to the second floor after 10 Hz, but different response occurred with the third floor
until 20 Hz. Third floors has a similar response with the previous analysis, which is the piles did not
influence too much for the floor behavior.
According to the design vibration criteria analysis, it can be found that for both floors, they have same
criteria curve which are VC-A as shown in Figure 11. Second floor shows the significant changed from
VC-B to VC-A after analyzed with the piles foundation. These analyses also shows the whole structures
are acceptable within the limits of generic vibration criteria for sensitive facilities guidelines.
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(a)
(b)
Figure 10: Time history and frequency content of the vertical structural velocity in the middle of the floor
structure with pile foundation system, (a) second floor and (b) third floor
Figure 11: One third octave velocity spectra for second floor (top, VC-A) and third floor (bottom,
VC-A); structure with pile foundation system
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3.3 Comparisons results with vibration criteria (VC) curve
The comparison of the results of two analyses (rigid base and pile) with design vibration criteria is
presented in Table 2. It shows that the vibration criteria for sensitive equipment for the structure are
achieved; the response vibrations are not over the limit from the input signal. Pile foundation system does
not affect performances of the structure due to transmission of ground vibration into the observed floor.
However, it increases the detail size of the sensitive equipment from 3 microns to 8 microns (VC-B to
VC-A) for second floor. The performance of the third floor is not affected by the foundations system. The
response was the same for a structure fixed at the base or supported on pile foundation.
Observed
floors
Foundation
system
Maximum
velocity
Peak
amplitude
Design
criteria,
VC
Comparison with
input, VC-D
Second floor Rigid base 2 µm/s 7 Hz VC-B OK
Piles 0.02 µm/s 9 Hz VC-A OK
Third floor Rigid base 4 µm/s 7 Hz VC-A OK
piles 4 µm/s 7 Hz VC-A OK
Table 2: Comparing results with design vibration criteria for both floors
4 Conclusions
The main aim of this study was to assess the feasibility and rationality of a method of low level vibration
simulation analysis based on free field measurement, in which the boundary condition of the simulation
model is defined by the acceleration time history of finite points obtained through site measurement. The
work was carried out as a stage-by-stage design procedure using a combination of site vibration
measurement and numerical simulation analysis. The results of the analyses were compared with design
criteria for vibration sensitive facilities and showed that, for the given structure and site vibration
conditions, the stringent micro-vibration criteria were satisfied.
The following conclusions can be drawn from this study:
1. The results of numerical simulations agree with on-site measurements of response.
2. The vibration response of the building with rigid base foundation predicted by the finite element
analysis, which was verified by the free field measurement, provides reference for the next design
(building with pile foundation system).
3. The compared results of finite element analysis shown that the applied methodology is rational
and feasible.
Acknowledgements
This research is fully funded by Ministry of Higher Education Malaysia (KPTM) and Universiti Tun
Hussein Onn Malaysia (UTHM). Their financial support is gratefully acknowledged.
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