ABSTRACT
In the mechanical development of a cellular base station, Bellcore
earthquake resistance certification is one of the most stringent requirements
for the structural design of the cabinet. Historically, earthquake
qualification testing has yielded high cabinet failure rates, resulting in
additional design iterations and increased development cycle time. To prevent
earthquake test failure and reduce cycle time, mechanical development
engineering conducted seismic simulations in parallel with the design of a new
outdoor cellular base station and accompanying battery cabinet. Finite element
models of the Motorola SCTM4812ET RF (Radio Frequency) and Power
Cabinets, weighing 1400 pounds and 3500 pounds respectively, were built and
subjected to Bellcore Zone 4 earthquake loading using ANSYS® finite
element analysis software. The use of the Pro/Engineer® module
Pro/MESH® to create the finite element mesh for both cabinets
greatly reduced the model building time and user expertise requirements. This
enabled a valid seismic simulation to be completed within three weeks,
allowing sufficient time to verify the structural integrity of each cabinet
and make necessary design modifications. As a result, both cabinets passed
earthquake testing on the first pass. This paper presents the modeling process
and experimental correlation results for both cabinets, demonstrating the
strengths and shortcomings of the simulation techniques employed.
INTRODUCTION
Product Description
The Motorola SCTM4812ET is the latest generation outdoor cellular base station developed by Motorola NSS (Network Solutions Sector) in Fort Worth, Texas for shipment in mid 1999. A Motorola SCTM4812ET BTS (Base Transceiver Subsystem) consists of two separate cabinets: an RF (Radio Frequency) cabinet and a power cabinet.
The RF cabinet contains all of the radio electronics and passive RF filtering, combining, and duplexing. The RF cabinet is 1680 mm (66") high x 1425 mm (56") wide x 865 mm (34") deep with a fully loaded mass of 635 kg (1400 pounds). Figure 1 shows the RF cabinet.
The power cabinet contains rectifiers to convert AC (alternating current) to DC (direct current) to power the RF cabinet (which operates on DC only) and batteries to provide battery backup during power outages. The power cabinet is 1680 mm (66") high x 1425 mm (56") wide x 940 mm (37") deep with a fully loaded mass of 1588 kg (3500 pounds).
The Motorola SCTM4812ET program presented some unique structural challenges, which increased the need for seismic analysis. Size is an important consideration for cellular service providers in urban areas where the providers often lease sites based on floor space and/or place the base stations in confined areas. Weight is also an important consideration in transportation and installation, especially on rooftop locations where floor loading is an issue. The need for low weight, corrosion resistance for an outdoor environment, and low fabrication cost drove the design team to make the cabinet skin and structural members out of punched and formed sheet aluminum (instead of plated steel or stainless steel) with a combination of welded, bolted, and riveted joints.

Figure 1. MOTOROLA SCTM4812ET RF CABINET
The unique modular construction of both cabinets allow the non-environmentally sealed section of each cabinet (power amplifiers on RF cabinet and batteries on power cabinet) to be easily removed which reduces the width to approximately 1070 mm (42") for transportation through confined spaces (such as elevators). Due to access restrictions, only two M12 bolts at the top and two at the bottom could be used to attach the smaller power amplifier cabinet to the main portion of the RF cabinet as opposed to traditional cabinet construction, which would have used 8-10 bolts or welds for better distribution of the loads between the two cabinet sections.
Usage of a common heat exchanger in both cabinets required the power
cabinet to orient the batteries vertically along one side of the cabinet. This
presented a significant challenge for seismic since it drastically raised the
center of gravity compared to the more traditional orientation of batteries
horizontally along the bottom of a cabinet. A common mounting pattern between
the cabinets with only 4 mounting points to support up to 1588 kg (3500
pounds) required thorough analysis of the mounting brackets and attachment of
the brackets to the cabinet.
Seismic integrity is extremely important to cellular service providers in regions which often experience seismic activity such as the Asia Pacific and the western United States, both of which contain large numbers of cellular phone users and thus are large and important markets for Motorola cellular base stations. Wireless telephone service often continues to function normally, or can be repaired quickly, following natural disasters that typically down traditional wireline phone lines, which take months to repair.
Bellcore seismic testing which simulates an earthquake is generally the most challenging structural requirement in the design of cellular base stations. For example, the previous generation of Motorola outdoor cellular base station (cabinet originally designed by outside supplier) failed 3 times in seismic testing before finite element analysis (FEA) was used to identify areas of the cabinet that required strengthening. After using FEA to optimize the design, the cabinet passed the next seismic test.
Aggressive schedules for cellular base station development are driven by customer demand and cost reduction. The cellular base station customer base consists of relatively few large customers, so often one or two customers can drive an entire program. Project slippage can cause losses of millions of dollars due to penalty clauses in contracts or missed opportunities for large orders.
In the Motorola SCTM4812ET program, the cost of slippage was
millions of dollars per week. The usage of FEA allowed this program to ship 2
months ahead of the original schedule. Seismic FEA analysis allowed both
Motorola SCTM4812ET cabinets to pass Bellcore seismic certification
testing on the first prototype pass and allowed the Motorola SCTM4812ET
power cabinet to go directly from the first prototype to pilot. A failure
during seismic testing would have resulted in an estimated 8 week slippage
which would have resulted in sales losses of millions of dollars.
Simulation Philosophy
Motorola NSS does not have any dedicated structural FEA analysts in our
Fort Worth facility, thus FEA analysis has generally been limited to simple
static analysis until recently. Motorola NSS physical design is currently
encouraging up-front FEA analysis to simulate mechanical certification testing
to reduce cycle time by eliminating testing failures. Aggressive schedules
require that FEA be done quickly to allow timely inputs to the design team.
The primary purpose of analysis for cellular base station products is to
ensure that the design will pass the certification tests. Cellular base
station products are generally designed with sufficient margin such that the
accuracy of the analysis is not critical. Also, mechanical raw material cost
is a small percentage of a total base station cost, so detailed analysis to
optimize raw material usage is not of prime importance.
The ability of a cabinet to withstand an earthquake is determined by conducting the Bellcore Earthquake Resistance Test. This Bellcore test has four levels of severity. These severity levels correspond to five geographic areas in the United States, designated Zones 0-4. Zone designations refer to earthquake risk. For Zone 0 geographic areas, no earthquake requirements are specified due to the lack of substantial earthquake risk. Zones 1-4 are based on varying levels of risk, with Zone 4 corresponding to the highest risk areas such as the California coast [1]. Since the Zone 4 test severity level is the highest, cellular infrastructure cabinets are most often certified to this level. Historically, Japanese customers have accepted Zone 4 level earthquake testing as an acceptable certification.
For Zone 4 testing, the cabinet must undergo a prescribed acceleration-time
history waveform in each of its three orthogonal axes . This is accomplished
by using a shaker table. The shaker table’s acceleration levels are analyzed
and must meet or exceed the Zone 4 Required Response Spectrum [1]. For
earthquake testing, a response spectrum is a curve that represents the maximum
acceleration versus natural frequency for a single degree-of-freedom system.
This curve captures the frequency and intensity content of a Bellcore Zone 4
acceleration time-history load [2]. Prior to the axis test, sine sweep surveys
are conducted to determine frame-level natural frequencies. All testing is
conducted per Section 5.4.1 of Bellcore GR-63-CORE [1].
To comply with Bellcore, the cabinet must meet the following requirements:
The frame-level natural frequency (first natural frequency) must be greater than 2 Hz.
The top of the cabinet must not deflect more than 3 inches relative to the base.
The cabinet must sustain the waveform without permanent mechanical or structural damage.
The cabinet must be electrically functional before, during, and after each earthquake event.
Additionally, Bellcore states as an objective that the cabinet should have
a frame-level natural frequency of 6 Hz. A complete description of the
physical and functional performance criteria is found in Section 4.4.1 of
Bellcore GR-63-CORE [1].
The primary objective of the Motorola SCTM4812ET seismic
analysis was to allow both cabinets to pass seismic certification testing on
the first pass, thus preventing costly program slippage. To achieve this
objective, the goal was to have first natural frequencies of 10 Hz or higher
in all directions and all stresses to be below material yield strength for
both fully loaded cabinets. Due to the aggressive schedule, there was a window
of opportunity of only 3 weeks to complete initial seismic FEA on each of the
cabinets and make recommendations to the design teams. The initial analysis
indicated that the basic structure of the cabinets was sufficiently stiff, but
it identified several areas which would have experienced localized yielding
during seismic testing. Design changes were made to high stress areas, and the
analysis was rerun quickly to evaluate the effectiveness of the changes.
Three software tools were used to conduct seismic simulation: Pro/ENGINEER®, Pro/MESH®, and ANSYS®. Pro/ENGINEER® provides parametric, feature based solid modeling with full associativity to drawing, analysis, and manufacturing modules. Pro/MESH®, an optional module of Pro/ENGINEER®, provides FEA preprocessing capabilities within the Pro/ENGINEER® environment. Pro/ MESH® allows boundary conditions and bar and mass elements to be associated to the solid model. Pro/MESH® also provides automatic meshing of the solid model for export to an external FEA software package or solution within Pro/ENGINEER® with optional modules and an external solver. ANSYS® is an extensive FEA software package with capability for many types of engineering analysis. ANSYS® is able to directly read in the mesh and boundary conditions generated by Pro/MESH®.
Due to the lack of dedicated structural analysts at Motorola NSS Fort Worth, all mechanical design engineers are being trained to do FEA quickly with the use of Pro/ENGINEER® and Pro/MESH®. By using the Pro/ENGINEER® model as the starting point for analysis and Pro/MESH® to automatically generate the FEA mesh, model building time is significantly reduced compared to traditional FEA model building techniques. User training and expertise is also significantly reduced since Pro/MESH® is a familiar interface to Pro/ENGINEER® users. Model simplification can be done quickly on the Pro/ENGINEER® solid model prior to automeshing. Since the FEA model is generated automatically from the Pro/ENGINEER® model, the FEA model generated by Pro/MESH® is typically more geometrically accurate than one constructed by more traditional element building methods. Pro/MESH® is also a reliable and quick automesher [2]. Material properties and boundary conditions are also assigned within Pro/ENGINEER® such that they are parametrically related to the solid model. Once the initial Pro/ENGINEER® and Pro/MESH® model are completed, design changes can be analyzed very quickly due to the parametric nature of Pro/ENGINEER® and full associativity to the FEA model via Pro/MESH®. Once the design change is made to the Pro/ENGINEER® solid model, the change is reflected in the FEA model simply by remeshing the solid model with Pro/MESH®.
Once the FEA mesh with boundary conditions has been generated from Pro/MESH®, the actual seismic analysis is performed within ANSYS®.
SIMULATION PROCEDURE
For each cabinet, the simulation procedure consisted of the following:
Accounting for all weights and centers-of-gravity for all components, and building the cabinet simulation model.
Meshing and preprocessing the model.
Conducting modal and response spectrum analyses.
Each of the above steps took one engineer approximately one week to complete;
therefore three weeks were necessary to obtain valid simulation results.
The first step in the simulation procedure was to create a spreadsheet containing the mass and centers-of-gravity for all cabinet components. If component masses were unknown, preliminary Pro/ENGINEER® models were used to determine the mass properties. From the spreadsheet, a total mass and frame-level center-of-gravity was computed. This spreadsheet provided for a consistency check with ANSYS®’ total mass and center-of-gravity calculations.
The second step was to build simulation models for each cabinet. Simplified
solid models of the actual part models were built in Pro/ENGINEER®.
The actual cabinet database was not used for two reasons. First, the cabinet
database wasn’t complete; the analysis phase was conducted in parallel with
the design phase. Second, actual cabinet part databases contain design
features which complicate part meshes and are not structurally significant.
Both cabinets were fabricated out of sheet metal of various thicknesses, with
1/8" being the thickness of the outer skin. Therefore, simple thin-walled
structures were used to simulate cabinet components.
All meshing and preprocessing was conducted in the Pro/ENGINEER® environment using Pro/MESH®. Shell elements were used to model all sheet metal parts, including structural members such as vertical stiffeners, mounting rails, etc. No solid elements were used. Using the ANSYS® Shell63 element, an elastic shell element with four nodes [3], Pro/MESH® automatically generated the element mesh from the Pro/ENGINEER® model. Bolts and fasteners in the cabinets were simulated using beam elements. The majority of welds were also modeled using beam elements. Some welded and riveted pieces were simulated using variable thickness shells, a technique which saves time but sometimes results in a liberally stiff structure. Variable thickness shells were used only where appropriate (i.e. where so many welds or rivets were used that the two pieces could be structurally considered as one).
Card cages and other electronic equipment were simulated using mass elements, which are point elements having six degrees of freedom (translation and rotation), mass, and mass moment of inertia properties [3]. The mass elements were applied at datum points located at the component centers-of-gravity, and were tied into the cabinet frame using massless, rigid beams. The rigid beams were installed in such a manner as to prevent artificial stiffening of the cabinet.
The only loads applied to the model were displacement boundary conditions at the cabinet mounting locations. The cabinets are mounted with 12 mm anchor bolts using 51 mm (2") washers. Therefore, a 25 mm (1") diameter circle concentric with the anchor bolt centerline was fixed in all translation and rotation directions at all four mounting points. Fixing the entire mounting bracket and/or the cabinet base is unrealistic due to irregularities of outdoor concrete mounting pads and rooftop installation sites. No forces were applied to the model since the response spectrum analysis determines the accelerations experienced by the cabinet model based on the modal analysis results.
The automatic meshing feature of Pro/MESH® greatly reduced the mesh generation time and user expertise requirements. The simplified RF cabinet model with mass nodes and beam elements is shown in Figure 2. The RF cabinet mesh is shown in Figure 3. Both cabinet models had approximately 26,000 elements: 30-40 Mass21 elements, 200-400 Beam44 elements, and 25,560-25,770 Shell63 elements. All mesh and preprocessing information was outputted from the Pro/ENGINEER® environment for solution in ANSYS®.

Figure 2. RF CABINET SIMULATION MODEL WITH BEAM ELEMENTS
AND MASS NODES SHOWN

Figure 3. RF CABINET MESH
Modal Analysis
Using the mesh and preprocessing information from Pro/MESH®, a
modal analysis was conducted using ANSYS®. Modal analysis
consisted of solving for the cabinet-level front-to-back and side-to-side mode
shapes and natural frequencies. If the first mode extracted was not
cabinet-level and limited to a section of the model, the finite element model
was modified in the Pro/ENGINEER® environment to stiffen the
components and members. If applicable, the stiffening modifications were
discussed with the designers to determine equivalent design changes to the
actual cabinet database. Modal analysis was then repeated until the first mode
extracted had a cabinet-level mode shape (front-to-back for both cabinets) and
the second cabinet-level mode shape was also extracted (side-to-side).
Response Spectrum Analysis
After extracting the cabinet-level modes, a Bellcore Zone 4 response spectrum analysis was conducted in ANSYS®. During the response spectrum analysis, the maximum response of each distinct mode is combined to produce an estimate of the maximum displacement response [4]. Typically, the first cabinet-level mode accounts for the greatest percentage of the total response.
Response spectrum analyses were conducted on both cabinet models in both the front-to-back and side-to-side directions. The response spectrum input corresponded to the Bellcore Zone 4 Response Spectrum as shown in Table 1. Displacement and stress results were viewed in the ANSYS® postprocessor. As expected, the majority of the stress concentrations were located at the mounting brackets. Due to its larger weight, several mounting bracket designs were evaluated with the power cabinet model. The reaction forces at the fixed locations were added to predict the total tensile and shear loading on the mounting bolts.
Table 1. BELLCORE ZONE 4 RESPONSE SPECTRUM [1]
| Frequency, Hz | Acceleration, (g) |
|---|---|
| 0.3 | 0.2 |
| 0.6 | 2 |
| 2 | 5 |
| 5 | 5 |
| 15 | 1.6 |
| 50 | 1.6 |
As a result of the response spectrum analysis, the following was completed: the mounting brackets were quantified and sized, restraining screws were added to heavy components, additional structural members were added, and the anchor bolts were sized.
Both cabinets’ response spectrum results indicated that the cabinet would
pass the Bellcore Zone 4 Earthquake Resistance Test.
EXPERIMENTAL TESTING SUMMARY
Experimental correlation of the simulation results was conducted during the scheduled mechanical certification testing of both the RF and Power cabinet products. During the testing, the primary goal was the completion of the tests on schedule, and not the correlation of the simulations. No tests were repeated for the sole purpose of correlation.
Each cabinet, installed onto concrete pads with anchor bolts per field installation, was mounted onto a shaker table for testing. The experimental testing consisted of sine sweeps to establish the cabinet vibration characteristics (determine natural frequencies) and earthquake qualification tests in all three axes (front-to-back, side-to-side, and up-and-down). The following measurements were taken for comparison with the simulation results for both the front-to-back and side-to-side axis earthquake events:
Natural frequencies
Cabinet top displacement
Mounting bracket strain
Cabinet wall strain
For both cabinets, two strain gages were located at the back left corner of the frame. For both cabinets, the front-to-back natural frequency and earthquake test was conducted before the side-to-side tests.
The RF cabinet testing was uneventful for all three axes. Upon completion of the testing, no structural damage was observed and the cabinet complied with all Bellcore requirements and objectives.
For the Power cabinet earthquake testing, during the front-to-back drive axis, the rocking momentum of the battery-loaded cabinet overcame the friction forces at the two back mounting bracket/cabinet interfaces. This interface consisted of two M12 bolts torqued to 55 ft-lb. Once the friction forces were overcome and the cabinet became loose, the cabinet moved relative to the bracket, with the M12 bolts being pulled up until striking the tops of the slots into which they had been inserted. This occurred repeatedly, with the cabinet gaining more momentum as the test progressed. This physical response greatly contributed to the maximum displacement measured and reduced the cabinet stiffness considerably. However, upon conclusion of the earthquake test in each axis, no permanent structural damage was observed and the cabinet complied with Bellcore requirements and objectives.
Although the Power cabinet passed the Bellcore test, further testing of the
M12 bolts was conducted to experimentally determine the maximum allowable
torque to be specified in the bolts’ installation. As a result, the
specified torque was increased to prevent movement of the cabinet during a
seismic event.
CORRELATON RESULTS AND DISCUSSION
Pre- and Post-Test Simulations
Simulations were conducted before and after the experimental testing. There were two reasons for repeating simulations:
For the Power cabinet, the experimental cabinet was 480 lb. heavier than the pre-test simulation model because heavier batteries were used in the testing.
For the RF cabinet, the experimental displacement results were higher than the pre-test simulation model results.
In regard to reason 1, the original weight of the 24 batteries used in the pre-test simulations was 85 lb. each. However, for the experimental testing, different batteries were used with a weight of 105 lb. each. Therefore, the mass of each battery mass node was increased by 20 lb., adding 480 lb. total to the post-test simulation model.
In regard to reason 2, DRD Technology Corporation, the ANSYS® software distributor, suggested the following modifications:
Remove mass moment of inertia properties from the mass elements.
Rotate all nodal coordinate systems to the active coordinate system.
By specifying mass moments of inertia and using rigid beams to tie the mass
elements to the cabinet frame, rotational resistance was unrealistically
increased. In regard to coordinate rotation, the output file created by
Pro/MESH® specified rotations on specific nodes, affecting
displacement results.
Pre- and Post Test Simulation Comparison Results
For the natural frequency and displacement results, both pre- and post-test results are given. For the RF cabinet, removing mass moment of inertia properties from the mass nodes resulted in a 12-17% increase in natural frequencies and a 30% increase in maximum displacement. Rotating all nodal coordinate systems to the active coordinate system resulted in an additional displacement increase of 60%.
For the Power cabinet, the addition of 480 lb. to the total weight of the system contributed to lowering the simulated front-to-back natural frequency by 30% and increasing the displacement by 300%. The effects of the 480 lb. weight addition, removal of mass moments of inertia, and nodal rotation were not isolated on the Power cabinet model. However, the RF cabinet effects results indicate that the weight increase was the primary contributor to the Power cabinet natural frequency decrease and displacement increase.
For the remainder of the results discussion, only the post-test simulation
results will be compared to the experimental measurements.
RF Cabinet Natural Frequencies
The RF cabinet modal analysis results are shown in Table 2 and plotted in Figure 4. Only the first natural frequencies were measured because the Bellcore test specification [1] requires only a first natural frequency measurement for each test axis. This is because earthquake acceleration levels are largest at lower natural frequencies (see Table 1). The simulated natural frequencies correlate extremely well with errors of 0% and 6% for the front-to-back and side-to-side mode shapes, respectively. The front-to-back and side-to-side mode shapes are shown in Figures 5 and 6.
Table 2. RF Cabinet Natural Frequencies (Hz)
| Mode Shape | Pre-test SImulation | Experimental Testing | Post-test Simulation |
| Front-to-Back | 12.4 | 13.9 | 13.9 |
| Side-to-Side | 14.3 | 15.8 | 16.8 |

Figure 4. RF CABINET NATURAL FREQUENCIES

Figure 5. RF CABINET FRONT-TO-BACK MODE SHAPE

Figure 6. RF CABINET SIDE-TO-SIDE MODE SHAPE
RF Cabinet Displacement
The maximum displacement results at the top of the RF cabinet are shown in Table 3 and plotted in Figure 7. For both drive axis directions, the simulated top displacements correlate poorly with the experimental results. These displacement results are perplexing since the natural frequency results correlated well with actual measurements. Since a response spectrum analysis represents the response of a single degree-of-freedom system, it is expected that the natural frequency and displacement results would have roughly equivalent correlation errors. This is clearly not the case for this model.
As mentioned previously, both removing mass moments of inertia properties and rotating all nodal coordinate systems to the active coordinate system did improve displacement results. Other efforts to improve displacement calculations consisted of increasing the mesh size and changing the shell elements.
The mesh size was increased up to 35,000 elements, resulting in a minimal impact on calculated displacements. Further increases to mesh size required too much computer solution time and memory resources. Also, the ANSYS® Shell63 elements were replaced with Shell93 elements. The Shell93 element has mid-side nodes and has a higher order shape function than the Shell63 element [3], characteristics which would promote more realistic displacement results. Unfortunately, the addition of mid-side nodes greatly increased the model’s number of degrees-of-freedom, straining computer resources and solution time. Therefore, other development engineering priorities prevented obtainment of successful solutions with higher-order elements.
In response to the poor displacement correlation results, DRD Technology Corporation, the ANSYS® software distributor, evaluated the RF cabinet simulation model. Using higher order elements, calculated maximum displacement in the front-to-back direction increased somewhat but was still predicting only 50% of the measured displacement.
TABLE 3 RF CABINET DISPLACEMENT RESULTS
| Drive Axis | Pre-test Simulation | Experimental Testing | Post-test Simulation |
| Front-to-Back | 0.05 | 0.24 | 0.1 |
| Side-to-Side | N/A | 0.18 | 0.07 |

Figure 7. RF CABINET TOP DISPLACEMENT
RF Cabinet Strain Measurements
The RF cabinet strain results are shown in Tables 4 and 5 and plotted in Figures 8 and 9. Microstrains refer to measurement units of 10-6/10-6. For both strain gage locations, the simulated horizontal and vertical strains are on the same order of magnitude as the measurements. However, for the vertical measurements, the strain values are approximately two times greater than the simulation values. There are two possible causes for this divergence:
Displacement errors.
Coarse mesh (discretization error).
As previously mentioned, maximum calculated displacements are off by a factor of two. Strain calculation is dependent upon displacements so it follows that the simulation strain values would underpredict reality due to the low displacement calculations. Also, the mesh could be improved to provide more accurate strain contours and prevent interelement discontinuities. As previously mentioned, efforts were made to increase the model’s mesh size but were abandoned due to other development priorities.
Submodeling could be employed to better predict the strains and stresses in the mounting bracket region. Submodeling refers to an analysis technique in which a secondary finite element model is created containing only the regions of interest. The boundary conditions of this model are determined by the response of the cabinet-level model. Finer meshes can be used in the secondary model to more accurately predict stress and strain levels [5].
TABLE 5 RF CABINET FRONT-TO-BACK MICROSTRAIN
| Location and Direction | Simulation | Experimental Measurement |
| Mounting Bracket Horizontal | 67 | 42 |
| Mounting Bracket Vertical | 210 | 398 |
| Cabinet Wall Horizontal | 79 | 49 |
| Cabinet Wall Vertical | 390 | 578 |
TABLE 6 RF CABINET SIDE-TO-SIDE MICROSTRAIN
| Location and Direction | Simulation | Experimental Measurement |
| Mounting Bracket Horizontal | 60 | 56 |
| Mounting Bracket Vertical | 177 | 325 |
| Cabinet Wall Horizontal | 115 | 41 |
| Cabinet Wall Vertical | 343 | 583 |

Figure 8. RF CABINET STRAIN FRONT-TO-BACK AXIS

Figure 9. RF CABINET STRAIN SIDE-TO-SIDE AXIS
Power Cabinet Natural Frequencies
The Power cabinet modal analysis results are shown in Table 6 and plotted in Figure 10. The front-to-back natural frequency correlates well with a 1% error. The side-to-side natural frequency does not correlate well due to the test order employed when taking sine sweep surveys (determining natural frequencies). Based on the simulation results, the most critical mode shape was front-to-back, so testing was performed in this direction first. Subsequently, side-to-side natural frequency measurement was conducted after front-to-back earthquake testing. As mentioned previously, the Power cabinet moved relative to the rear mounting brackets during the front-to-back earthquake event. This additional movement weakened the cabinet, thereby producing a side-to-side natural frequency lower than the simulation (8.0 versus 15.7 Hz). This weakening conclusion can be made due to the simulations’ success in predicting the RF cabinet natural frequencies and the Power cabinet front-to-back natural frequency. This effect was not observed in the RF cabinet because of its less severe front-to-back earthquake test due to a higher natural frequency and maintenance of a tight mounting bracket/cabinet interface throughout the duration of the test. The simulation model always assumed a rigid connection between the cabinet mounting brackets and the cabinet and was not able to predict this loosening response.
TABLE 6 POWER CABINET NATURAL FREQUENCIES
| Mode Shape | Pre-test Simulation | Experimental Testing | Post-test Simulation |
| Front-to-Back | 14.0 | 9.7 | 9.8 |
| Side-to-Side | 15.9 | 8.0 | 15.7 |

Figure 10. POWER CABINET NATURAL FREQUENCIES
Power Cabinet Displacement
For the power cabinet, correlation between the simulated and measured
results is invalid. The divergence between the simulation and experimentation
displacement values was exacerbated by the cabinet’s response to the
earthquake event in the front-to-back direction. Therefore, the front-to-back
displacement correlation error would be much higher than the equivalent RF
cabinet displacement error and misleading in regard to the validity of the
modeling techniques. Displacement results between the simulation and test are
also incomparable in the side-to-side direction due to the previously
mentioned weakening effect.
Power Cabinet Strain Measurements
The Power cabinet strain results are shown in Table 7 and Figure 11. For the font-to-back direction, the differences between the vertical and horizontal mounting bracket strains and the measurements are 20 and 30%, respectively. For the cabinet wall, the simulated and measured strain values are incomparable due to the cabinet becoming loose relative to the mounting brackets during the test, inducing extremely high strain in comparison to the simulation results. For the side-to-side direction, a comparison between the simulated and measured strain values is also not valid due to the previously mentioned weakening effect.
TABLE 7 POWER CABINET FRONT-TO-BACK MICROSTRAIN
| Location and Direction | Simulation | Experimental Measurement |
| Mounting Bracket Horizontal | 700 | 535 |
| Mounting Bracket Vertical | 1500 | 1895 |

Figure 11. POWER CABINET STRAIN FRONT-TO-BACK AXIS
CONCLUSIONS
Simulation Technique Shortcomings
The certification test results and experimental correlation indicate the following shortcomings in regard to the seismic simulation techniques employed:
Displacement calculations are off by a factor of two, affecting strain and stress calculations.
Use of beams to rigidly attach components prevents the detection of
relative motion between components and doesn’t adequately model
fastener interfacing, guide pins, and latching mechanisms.
Simulation Technique Strengths
The certification test results and experimental correlation indicate the following strengths in regard to the seismic simulation techniques employed:
Natural frequencies and mode shapes can be accurately predicted within 6%. Since the first natural frequency is a good indication of compliance, an accurate prediction of the actual test result is possible.
High stress areas can be detected, and qualitative design enhancements can be evaluated quickly and implemented early in the design stage of the product.
The automatic meshing and response spectrum capabilities of the
software packages used in the simulation greatly reduce user expertise
and analysis time requirements.
Recommendations
The present technique is a recommended method to ensure cabinet compliance with the Bellcore Zone 4 Earthquake Resistance Test.
For subsequent simulations, mass moments of inertia should not be included in the definition of mass elements, and all nodal coordinate systems should be rotated to the active coordinate system to improve displacement results.
Based on the RF cabinet strain and displacement correlation results, a minimum safety factor of two should be used to ensure acceptable stress levels when using these analysis tools and modeling methods.
Submodeling and/or finer meshes in critical high stress areas are recommended to provide better strain and stress results.
By using the Pro/ENGINEER® solid model as the basis for the FEA model and Pro/MESH® for automeshing, seismic analysis in ANSYS® and design inputs for this complicated assembly were completed within 3 weeks, allowing the design work to proceed as scheduled without waiting for analysis results.
Seismic FEA in ANSYS® of the Motorola SCTM4812ET
cabinets allowed both cabinets to pass Bellcore seismic certification
testing on the first prototype pass. Due largely to this success, initial
product shipment was pulled in two months, allowing for millions of dollars
in additional sales.
ACKNOWLEDGEMENTS
The authors would like to thank Ken Huang, Roger Gandee, and John Dascanio
of Motorola and Chris Andersen and Andy Bax of DRD Technology Corporation for
their support and encouragement in this endeavor.
REFERENCES
Bellcore, GR-63-CORE "Network Equipment-Building System (NEBS) Requirements: Physical Protection," Issue 1, 1995.
Bax, A. and Andersen, C., "Bellcore Seismic Analysis Calls on ANSYS®," Analysis Solutions, Spring 1998.
ANSYS® Inc., ANSYS® Help System, Revision 5.4, 1997.
Cook, R.D., Finite Element Modeling for Stress Analysis, John Wiley and Sons, New York, 1995.
DRD Technology Corporation, Advanced ANSYS®/ProFEA: Finite Element Analysis for Pro/ENGINEER®, Revision 2, 1997.