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Thesis Defense of JAI PRAKASH PAUL Graduate Student Mechanical Engineering

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... for Trunnion-Hub Assemblies of Bascule Bridges using Finite Element Methods ... Bascule Bridge Design Tools -Michael Denninger (2000) ... – PowerPoint PPT presentation

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Title: Thesis Defense of JAI PRAKASH PAUL Graduate Student Mechanical Engineering


1
Thesis Defense of JAI PRAKASH PAULGraduate
StudentMechanical Engineering
Sensitivity Analysis of Design Parameters for
Trunnion-Hub Assemblies of Bascule Bridges using
Finite Element Methods
2
Outline
  • Introduction
  • Previous work done (at USF)
  • Objective of Thesis
  • Response Variables Properties of materials used
  • Tests for Different Analyses
  • Results of 5 Variation Analysis
  • Results of AASHTO Analysis
  • Conclusions
  • Questions

3



4
AP1
AP2
  • Assembly Procedure 1 (AP1)
  • Trunnion is cooled in liquid nitrogen
  • Trunnion is fitted into Hub
  • Trunnion-Hub is cooled in liquid nitrogen
  • Trunnion-Hub is fitted into Girder
  • Assembly Procedure 2 (AP2)
  • Hub is cooled in liquid nitrogen
  • Hub is fitted into Girder
  • Trunnion is cooled in liquid nitrogen
  • Trunnion is fitted into Hub-Girder

5
Bascule Bridge Design Tools -Michael
Denninger (2000)
  • Calculate steady state interference stresses
    radial displacements
  • Steady state stresses are well under maximum
    stresses
  • Transient stresses are to be calculated

6
Parametric Finite Element Analysis
-Badri Ratnam (2000)
  • Transient Stresses using ANSYS
  • Hoop Stress Critical Crack Length
  • AP1 and AP2 for 3 different bridges
  • CCL AP2 is better than AP1
  • Hoop Stress below maximum yield strength

7
Experimental Analysis -Sanjeev
Nichani (2001)
  • To measure the stresses during each step of the
    actual assembly procedures
  • To compare the stresses during the 2 assembly
    procedures
  • To validate the previous 2 studies

8
Experimental Analysis
  • Steady state stresses equal for AP1 AP2
  • AP2 is a better alternative than AP1
  • Higher critical crack length (CCL)
  • Lower transient (thermal) stresses
  • Quicker, but possibly costlier
  • FEA versus Experiment
  • Excellent agreement at steady state
  • Good agreement during transient

9
Observations Recommendations
  • Thermal shock was a common problem in both
    processes
  • Consider staged cooling
  • Consider warming one component while cooling the
    other
  • Consider heating the outer component
  • Study the effect of THG geometry

10
AASHTO Standards
  • American Association of State Highway and
    Transportation Officials (AASHTO) call for hub
    radial thickness of 0.4 times the trunnion outer
    diameter
  • Presently a hub radial thickness of 0.1 to 0.2
    times the trunnion outer diameter is used

11
Objective
  • Analyze the effect of geometric parameters such
    as hub radial thickness, trunnion bore to outer
    diameter ratio and variances in interference fits
    on critical crack lengths and critical stresses

12
Response Variables
  • Critical Crack Length
  • Stress Ratio,

13
Finite Element Model
14
Test for Interference Stress
15
Test for Interference Stress
16
Test for Interference Stress
17
Test for Interference Stress
18
Test for Interference Stress
19
Test for Cooling
20
Test for Cooling
21
Test for Cooling
22
Test for Thermal Stress
23
Test for Entire Process
24
Data Analysis
25
2k Factorial Method
26
Geometric Parameters
27
Geometric Parameters
28
5 Variation Analysis
  • 33 27 Experiments
  • To study the effect of parameters on critical
    values
  • To verify the analyses

29
5 Variation Analysis
30
5 Variation Analysis
31
5 Variation Analysis
  • 8 values from the 5 variation analysis to
    find percentage contributions for CCL

32
5 Variation Analysis
  • Percentage contributions for CCL

33
5 Variation Analysis
  • 8 values from the 5 variation analysis to
    find percentage contributions for SR

34
5 Variation Analysis
  • Percentage contributions for SR

35
5 Variation Analysis
  • For Critical Crack Length
  • Interference has most effect (84)
  • Hub thickness follows with 8
  • For Stress Ratio
  • Interference has most effect (94)
  • Interaction of interference hub thickness (5.4)

36
AASHTO Analysis
  • 23 8 Experiments
  • To study the effect of parameters on critical
    values
  • To check if AASHTO standards are better

37
AASHTO Analysis
  • 8 values from the AASHTO analysis to find
    percentage contributions for CCL

38
AASHTO Analysis
  • Percentage contributions for CCL

39
AASHTO Analysis
  • 8 values from the AASHTO analysis to find
    percentage contributions for SR

40
AASHTO Analysis
  • Percentage contributions for SR

41
AASHTO Analysis
  • For Critical Crack Length
  • Hub thickness has most effect (90)
  • Interference follows with 8.67
  • For Stress Ratio
  • Hub Thickness has most effect (74)
  • Interference follows with 25

42
AASHTO Analysis
  • AASHTO standards yielded crack lengths more than
    2 times the presently used standards

43
AASHTO Analysis
  • AASHTO standards yielded stress ratios up to 30
    for min interference and up to 40 for max
    interference more than the present standards

44
Conclusions
  • AASHTO standards are safer
  • Higher Critical Crack Length
  • Higher Stress Ratio
  • Could be more economical as failures can be
    avoided
  • 5 analysis and AASHTO analysis gave different
    results
  • Percentage variations do not determine final
    results
  • Physics of the problem plays major role

45
ACKNOWLEDGEMENTS
  • QUESTIONS ???
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