SlideShare una empresa de Scribd logo
1 de 20
Local and Global Response of EUV Reticles due to Entrapped Particles during Exposure Chucking  Computational Mechanics Center  (UW-CMC) University of Wisconsin, Madison, WI Preetish Sinha, Vasu Ramaswamy, Andrew R. Mikkelson  and Roxann L. Engelstad
Introduction and Problem Description  ,[object Object],[object Object],[object Object],Front  and Backside Flatness: ~ 30 - 100 nm  p-v  flatness Low Order Thickness Variation (LOTV): ~ 30 - 100 nm  p-v  flatness Freestanding Substrate Requirements (within Quality Area) Quality Area:  142 mm x 142 mm
[object Object],[object Object],Motivation for Research ,[object Object],Micron-sized entrapped particle OPD and IPD of patterned surface   Clamping pressure Millimeter-sized void
Predicting the Effects of Particle Entrapment  ,[object Object],[object Object],[object Object],Effective Particle Height
Particle Entrapment ,[object Object],[object Object],[object Object],Macro-Scale Response ,[object Object],[object Object],[object Object],[object Object],[object Object],Micro-Scale Response ,[object Object],[object Object],[object Object],[object Object],[object Object]
[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Micro-Scale Response of the System Spherical Particle - Description
Spherical Particle – Details of the Model * Measured via nanoindentation testing Axisymmetric FE Model F Model Parameters 12.0 12.0 9.0 8.5 Yield Strength  Y  (GPa) 100 Chuck 100 Particle 250 chrome* Backside Layer 66.3 ULE ®  * Substrate Elastic Modulus  E  (GPa) Material Component 1.0 µm to 10.0 µm Diameter, d p Particle Range Parameter Component Substrate Chuck Particle Chrome Backside  Layer d p Axis of symmetry
Elastic Response Elastic Plastic Response  Chuck / Particle Properties   E  = 100 GPa   Y  = 12 GPa Chuck / Particle Properties   E  = 100 GPa   Y  = 12 GPa ULE ® E  = 66.3 GPa Y  = 8.5 GPa Chrome E  = 250 GPa Y  = 9.0 GPa Spherical Particle - Response Effect of Nonlinear Behavior – 1.0 μm Spherical Particle ULE ®   E  = 66.3 GPa   Y  = 8.5 GPa ULE ® E  = 66.3 GPa Y  = 8.5 GPa
Analytical and Numerical Analyses Substrate Chuck Particle Metal Backside  Layer H Axis of symmetry ,[object Object],[object Object],[object Object],[object Object],R Local Axisymmetric Model Cylindrical  Particle – Details of the Models
Cylindrical Particle -  Analytical Model The total amount a particle is deformed and embedded ( w total ) into the reticle and chuck is given by: w total   = w c  +  w s  +  w p Since  H   was the original height of the particle, the effective height of the particle ( h ) is then given by: h   = H –  ( w c  +  w s  +  w p ) w c  = max embedded into the chuck w s  = max embedded into the reticle substrate w p  = max deformation of the particle Substrate Chuck h
R H 362.5  μ m 362.5  μ m 362.5  μ m 362.5  μ m Axis of symmetry Substrate Chuck ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],Cylindrical Particle – Details of FE Model
Elastic Response Elastic Plastic Response  Chuck / Particle Properties   E  = 100 GPa   Y  = 12 GPa Chuck / Particle Properties   E  = 100 GPa   Y  = 12 GPa chrome E  = 250 GPa Y  = 9.0 GPa ULE ® E  = 66.3 GPa Y  = 8.5 GPa ULE ®   E  = 66.3 GPa   Y  = 8.5 GPa Cylindrical Particle - Response Effect of Nonlinear Behavior – 1.0 μm Cylindrical Particle
Comparison of FE Simulation Results 1.0 μm Cylindrical and Spherical Particles
Comparison of FE Simulation Results 5.0 μm Cylindrical and Spherical Particles
Comparison of FE Simulation Results 10.0 μm Cylindrical and Spherical Particles
Macro-Scale Response of the System Analytical Model for Global Distortions ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],The relationship for gap radius ( a ), particle crush force ( F ) and OPD as a function of  h  were derived by Engelstad and Lovell.*  The equations are based upon classical flexural theory, thus shear effects are not considered.  ,[object Object],r p h t a a Substrate Chuck
Analytical Global Coupling Model for an Elastic Particle Micro Model Equations: p   =  uniform clamping pressure E   =  reticle elastic modulus    =  reticle Poisson’s ratio t   =  reticle thickness   H  =  initial particle height h  =  final particle height    =  amount of particle / spring deformation F  =  particle / spring deformation force k   =  particle / spring stiffness a  = gap radius R  = cylindrical particle radius E p  = particle elastic modulus Macro Model Equations: Rigid Chuck p Cylindrical, Elastic Particle (stiffness k)
Finite Element Model Reticle Bending due to Particle Effects p   =  uniform clamping pressure (4.0 kPa) E   =  reticle elastic modulus (72.6 GPa)    =  reticle Poisson’s ratio (0.164) t   =  reticle thickness (6.35 mm) H  =  initial particle height (1.0 µm) E p  = particle elastic modulus (100 GPa) Assumed Parameters: A spring element (particle of height  H ) is located between the reticle and chuck ,[object Object],[object Object]
Coupling Results and OPD Profile  Analytical Model : FE Model: ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Summary and Conclusions ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]

Más contenido relacionado

La actualidad más candente

FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES
FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES  FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES
FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES
Jordan Suls
 
Dynamic Behavior of Fiber Reinforced Composite Beam With Crack
Dynamic Behavior of Fiber Reinforced Composite Beam With CrackDynamic Behavior of Fiber Reinforced Composite Beam With Crack
Dynamic Behavior of Fiber Reinforced Composite Beam With Crack
IJMERJOURNAL
 
Nano comp lam method
Nano comp lam methodNano comp lam method
Nano comp lam method
skrokkam
 
comp mtl final paper
comp mtl final papercomp mtl final paper
comp mtl final paper
Tushar Dange
 

La actualidad más candente (20)

FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES
FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES  FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES
FRACTURE MECHANICS OF NANO-SILICA PARTICLES IN REINFORCED EPOXIES
 
Dynamic Behavior of Fiber Reinforced Composite Beam With Crack
Dynamic Behavior of Fiber Reinforced Composite Beam With CrackDynamic Behavior of Fiber Reinforced Composite Beam With Crack
Dynamic Behavior of Fiber Reinforced Composite Beam With Crack
 
Preprints202105.0252.v2
Preprints202105.0252.v2Preprints202105.0252.v2
Preprints202105.0252.v2
 
B31008012
B31008012B31008012
B31008012
 
Ch5 epfm
Ch5 epfmCh5 epfm
Ch5 epfm
 
Thesis Defense Presentation-Sabarisha
Thesis Defense Presentation-SabarishaThesis Defense Presentation-Sabarisha
Thesis Defense Presentation-Sabarisha
 
Nano comp lam method
Nano comp lam methodNano comp lam method
Nano comp lam method
 
PhD Dissertation Defense
PhD Dissertation DefensePhD Dissertation Defense
PhD Dissertation Defense
 
Simulation of a fatigue crack problem in electronic devices
Simulation of a fatigue crack problem in electronic devicesSimulation of a fatigue crack problem in electronic devices
Simulation of a fatigue crack problem in electronic devices
 
comp mtl final paper
comp mtl final papercomp mtl final paper
comp mtl final paper
 
Numerical Simulations of the Bond Stress-Slip Effect of Reinforced Concrete o...
Numerical Simulations of the Bond Stress-Slip Effect of Reinforced Concrete o...Numerical Simulations of the Bond Stress-Slip Effect of Reinforced Concrete o...
Numerical Simulations of the Bond Stress-Slip Effect of Reinforced Concrete o...
 
TRANSIENT ANALYSIS OF PIEZOLAMINATED COMPOSITE PLATES USING HSDT
TRANSIENT ANALYSIS OF PIEZOLAMINATED COMPOSITE PLATES USING HSDTTRANSIENT ANALYSIS OF PIEZOLAMINATED COMPOSITE PLATES USING HSDT
TRANSIENT ANALYSIS OF PIEZOLAMINATED COMPOSITE PLATES USING HSDT
 
Impulse excitation technique , experimental stress analysis
Impulse excitation technique , experimental stress analysisImpulse excitation technique , experimental stress analysis
Impulse excitation technique , experimental stress analysis
 
Elastic plastic fracture mechanics
Elastic plastic fracture mechanicsElastic plastic fracture mechanics
Elastic plastic fracture mechanics
 
A fracture mechanics based method for prediction of
A fracture mechanics based method for prediction ofA fracture mechanics based method for prediction of
A fracture mechanics based method for prediction of
 
Numerical simulation of nonlinear elastic wave propagation
Numerical simulation of nonlinear elastic wave propagationNumerical simulation of nonlinear elastic wave propagation
Numerical simulation of nonlinear elastic wave propagation
 
Computational fracture mechanics
Computational fracture mechanicsComputational fracture mechanics
Computational fracture mechanics
 
Determination Of Geometric Stress Intensity Factor For A Photoelastic Compac...
Determination Of  Geometric Stress Intensity Factor For A Photoelastic Compac...Determination Of  Geometric Stress Intensity Factor For A Photoelastic Compac...
Determination Of Geometric Stress Intensity Factor For A Photoelastic Compac...
 
Presentation For Fracture Mechanics
Presentation For Fracture MechanicsPresentation For Fracture Mechanics
Presentation For Fracture Mechanics
 
Anisotropy of Coercive Force of Single Crystals and Sheets of Silicon Iron wi...
Anisotropy of Coercive Force of Single Crystals and Sheets of Silicon Iron wi...Anisotropy of Coercive Force of Single Crystals and Sheets of Silicon Iron wi...
Anisotropy of Coercive Force of Single Crystals and Sheets of Silicon Iron wi...
 

Similar a EIPBN_Particle Entrapment

DYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPING
DYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPINGDYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPING
DYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPING
Varakala Netha
 
Buckling of laminated beam higher order discrete model-main
Buckling of laminated beam  higher order discrete model-mainBuckling of laminated beam  higher order discrete model-main
Buckling of laminated beam higher order discrete model-main
Abdul Khader Shahadaf
 
2015 Fall Contact Polyhedral Mechanics
2015 Fall Contact Polyhedral Mechanics2015 Fall Contact Polyhedral Mechanics
2015 Fall Contact Polyhedral Mechanics
Nianshen Zhang
 
Young_Stress_Analyst_Competetion_Entry
Young_Stress_Analyst_Competetion_EntryYoung_Stress_Analyst_Competetion_Entry
Young_Stress_Analyst_Competetion_Entry
Luqmaan Fazal Ph.D.
 

Similar a EIPBN_Particle Entrapment (20)

EIPBN 2010 Abstract_Preetish
EIPBN 2010 Abstract_PreetishEIPBN 2010 Abstract_Preetish
EIPBN 2010 Abstract_Preetish
 
DYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPING
DYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPINGDYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPING
DYNAMIC RESPONSE RESEARCH OF U SHAPED PIPE WITH VISCOELASTIC DAMPING
 
Finite element analysis in orthodontics/ /certified fixed orthodontic courses...
Finite element analysis in orthodontics/ /certified fixed orthodontic courses...Finite element analysis in orthodontics/ /certified fixed orthodontic courses...
Finite element analysis in orthodontics/ /certified fixed orthodontic courses...
 
Buckling of laminated beam higher order discrete model-main
Buckling of laminated beam  higher order discrete model-mainBuckling of laminated beam  higher order discrete model-main
Buckling of laminated beam higher order discrete model-main
 
Ping Du's Research Highlight
Ping Du's Research HighlightPing Du's Research Highlight
Ping Du's Research Highlight
 
Monitoring of strain and seismic vibrations in structures
Monitoring of strain and seismic vibrations in structuresMonitoring of strain and seismic vibrations in structures
Monitoring of strain and seismic vibrations in structures
 
Analysis of Cross-ply Laminate composite under UD load based on CLPT by Ansys...
Analysis of Cross-ply Laminate composite under UD load based on CLPT by Ansys...Analysis of Cross-ply Laminate composite under UD load based on CLPT by Ansys...
Analysis of Cross-ply Laminate composite under UD load based on CLPT by Ansys...
 
2015 Fall Contact Polyhedral Mechanics
2015 Fall Contact Polyhedral Mechanics2015 Fall Contact Polyhedral Mechanics
2015 Fall Contact Polyhedral Mechanics
 
Effect of lamination angle on maximum deflection of simply supported composit...
Effect of lamination angle on maximum deflection of simply supported composit...Effect of lamination angle on maximum deflection of simply supported composit...
Effect of lamination angle on maximum deflection of simply supported composit...
 
Modal Analysis of Single Rectangular Cantilever Plate by Mathematically, FEA ...
Modal Analysis of Single Rectangular Cantilever Plate by Mathematically, FEA ...Modal Analysis of Single Rectangular Cantilever Plate by Mathematically, FEA ...
Modal Analysis of Single Rectangular Cantilever Plate by Mathematically, FEA ...
 
Finite element modelling and analysis in ansys workbench
Finite element modelling and analysis in ansys workbenchFinite element modelling and analysis in ansys workbench
Finite element modelling and analysis in ansys workbench
 
Aspects Regarding the Elastic Properties of Silicon and Its Influence on the ...
Aspects Regarding the Elastic Properties of Silicon and Its Influence on the ...Aspects Regarding the Elastic Properties of Silicon and Its Influence on the ...
Aspects Regarding the Elastic Properties of Silicon and Its Influence on the ...
 
Generalised_formulation_of_laminate_theory_using_beam_fe_for_delaminated_comp...
Generalised_formulation_of_laminate_theory_using_beam_fe_for_delaminated_comp...Generalised_formulation_of_laminate_theory_using_beam_fe_for_delaminated_comp...
Generalised_formulation_of_laminate_theory_using_beam_fe_for_delaminated_comp...
 
Numerical Simulation of 퐒퐢ퟏ−퐱퐆퐞퐱 Thin Film Solar Cell Using AMPS - 1D
Numerical Simulation of 퐒퐢ퟏ−퐱퐆퐞퐱 Thin Film Solar Cell Using AMPS - 1DNumerical Simulation of 퐒퐢ퟏ−퐱퐆퐞퐱 Thin Film Solar Cell Using AMPS - 1D
Numerical Simulation of 퐒퐢ퟏ−퐱퐆퐞퐱 Thin Film Solar Cell Using AMPS - 1D
 
Photoelastic Stress Analysis of Bell Crank Lever: A Review
Photoelastic Stress Analysis of Bell Crank Lever: A ReviewPhotoelastic Stress Analysis of Bell Crank Lever: A Review
Photoelastic Stress Analysis of Bell Crank Lever: A Review
 
Aeolian vibrations of overhead transmission line bundled conductors during in...
Aeolian vibrations of overhead transmission line bundled conductors during in...Aeolian vibrations of overhead transmission line bundled conductors during in...
Aeolian vibrations of overhead transmission line bundled conductors during in...
 
Young_Stress_Analyst_Competetion_Entry
Young_Stress_Analyst_Competetion_EntryYoung_Stress_Analyst_Competetion_Entry
Young_Stress_Analyst_Competetion_Entry
 
3
33
3
 
E012623035
E012623035E012623035
E012623035
 
Improvement of the Shell Element Implemented in FEASTSMT
Improvement of the Shell Element Implemented in FEASTSMTImprovement of the Shell Element Implemented in FEASTSMT
Improvement of the Shell Element Implemented in FEASTSMT
 

EIPBN_Particle Entrapment

  • 1. Local and Global Response of EUV Reticles due to Entrapped Particles during Exposure Chucking Computational Mechanics Center (UW-CMC) University of Wisconsin, Madison, WI Preetish Sinha, Vasu Ramaswamy, Andrew R. Mikkelson and Roxann L. Engelstad
  • 2.
  • 3.
  • 4.
  • 5.
  • 6.
  • 7. Spherical Particle – Details of the Model * Measured via nanoindentation testing Axisymmetric FE Model F Model Parameters 12.0 12.0 9.0 8.5 Yield Strength Y (GPa) 100 Chuck 100 Particle 250 chrome* Backside Layer 66.3 ULE ® * Substrate Elastic Modulus E (GPa) Material Component 1.0 µm to 10.0 µm Diameter, d p Particle Range Parameter Component Substrate Chuck Particle Chrome Backside Layer d p Axis of symmetry
  • 8. Elastic Response Elastic Plastic Response Chuck / Particle Properties E = 100 GPa Y = 12 GPa Chuck / Particle Properties E = 100 GPa Y = 12 GPa ULE ® E = 66.3 GPa Y = 8.5 GPa Chrome E = 250 GPa Y = 9.0 GPa Spherical Particle - Response Effect of Nonlinear Behavior – 1.0 μm Spherical Particle ULE ® E = 66.3 GPa Y = 8.5 GPa ULE ® E = 66.3 GPa Y = 8.5 GPa
  • 9.
  • 10. Cylindrical Particle - Analytical Model The total amount a particle is deformed and embedded ( w total ) into the reticle and chuck is given by: w total = w c + w s + w p Since H was the original height of the particle, the effective height of the particle ( h ) is then given by: h = H – ( w c + w s + w p ) w c = max embedded into the chuck w s = max embedded into the reticle substrate w p = max deformation of the particle Substrate Chuck h
  • 11.
  • 12. Elastic Response Elastic Plastic Response Chuck / Particle Properties E = 100 GPa Y = 12 GPa Chuck / Particle Properties E = 100 GPa Y = 12 GPa chrome E = 250 GPa Y = 9.0 GPa ULE ® E = 66.3 GPa Y = 8.5 GPa ULE ® E = 66.3 GPa Y = 8.5 GPa Cylindrical Particle - Response Effect of Nonlinear Behavior – 1.0 μm Cylindrical Particle
  • 13. Comparison of FE Simulation Results 1.0 μm Cylindrical and Spherical Particles
  • 14. Comparison of FE Simulation Results 5.0 μm Cylindrical and Spherical Particles
  • 15. Comparison of FE Simulation Results 10.0 μm Cylindrical and Spherical Particles
  • 16.
  • 17. Analytical Global Coupling Model for an Elastic Particle Micro Model Equations: p = uniform clamping pressure E = reticle elastic modulus  = reticle Poisson’s ratio t = reticle thickness H = initial particle height h = final particle height  = amount of particle / spring deformation F = particle / spring deformation force k = particle / spring stiffness a = gap radius R = cylindrical particle radius E p = particle elastic modulus Macro Model Equations: Rigid Chuck p Cylindrical, Elastic Particle (stiffness k)
  • 18.
  • 19.
  • 20.

Notas del editor

  1. Thank you ---- for that kind introduction. And I would like to thank Hans and the organizing committee for the opportunity to speak here today. It is indeed an honor. I would like to recognize my co-authors from the UW-CMC --- And acknowledge support from ----
  2. Thank you ---- for that kind introduction. And I would like to thank Hans and the organizing committee for the opportunity to speak here today. It is indeed an honor. I would like to recognize my co-authors from the UW-CMC --- And acknowledge support from ----
  3. Thank you ---- for that kind introduction. And I would like to thank Hans and the organizing committee for the opportunity to speak here today. It is indeed an honor. I would like to recognize my co-authors from the UW-CMC --- And acknowledge support from ----
  4. elastic model – deformation inelastic (plastic) - crushing
  5. Comment: w c + ws + wp are calculated in the following slides
  6. Skip 1 Read #2 Skip 3 First systemic analysis looking at and compare the chucking response of comparable coulomb and jr chucks And finally, we are using the fe models to identify the range of flatness variations that can be accommodated with e chucking.