Improving Yield for High Pin Count Wafer Probing Applications

Similar documents
Nomenclature, Advantages, Applications. Logic States, Read Ops, Write Ops

HBM fine pitch micro pillar grid array probing evaluation

Introduction to Structural Member Properties

Supplemental Material for Monolithic Multilayer Microfluidics via Sacrificial Molding of 3D- Printed Isomalt. M. K. Gelber and R.

October Suzhou - Shenzhen, China. Archive TestConX - Image: Breath10/iStock

Identification, analysis and control of high temperatures on wafer test probing gprocesses

Method of Virtual Work Frame Deflection Example Steven Vukazich San Jose State University

AERO 214. Lab II. Measurement of elastic moduli using bending of beams and torsion of bars

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each.

VACUUM SUPPORT FOR A LARGE INTERFEROMETRIC REFERENCE SURFACE

STRUCTURAL SURFACES & FLOOR GRILLAGES

Module 4 : Deflection of Structures Lecture 4 : Strain Energy Method

Bending Load & Calibration Module

DEPARTMENT OF MECHANICAL ENIGINEERING, UNIVERSITY OF ENGINEERING & TECHNOLOGY LAHORE (KSK CAMPUS).

Support Idealizations

ROBUST DESIGN OF A MECHANICAL LATCH

On Nonlinear Buckling and Collapse Analysis using Riks Method

SOLUTION (17.3) Known: A simply supported steel shaft is connected to an electric motor with a flexible coupling.

Chapter 1 General Introduction Instructor: Dr. Mürüde Çelikağ Office : CE Building Room CE230 and GE241

Lecture 2: Introduction to Uncertainty

Laboratory 4 Topic: Buckling

Mechatronics II Laboratory EXPERIMENT #1 MOTOR CHARACTERISTICS FORCE/TORQUE SENSORS AND DYNAMOMETER PART 1

Mechatronics II Laboratory EXPERIMENT #1: FORCE AND TORQUE SENSORS DC Motor Characteristics Dynamometer, Part I

1 Force Sensing. Lecture Notes. 1.1 Load Cell. 1.2 Stress and Strain

INTRODUCTION (Cont..)

Moment Area Method. 1) Read

Part IB EXPERIMENTAL ENGINEERING MODEL STRUCTURES. 1. To compare the behaviour of various different linear-elastic structures with simple theory.

Mechanics of wafer bonding: Effect of clamping

, follows from these assumptions.

RF APERTURE ARCHITECTURES 11 Nov. 08

Q. 1 Q. 5 carry one mark each.

Experimental Lab. Principles of Superposition

Software Verification

Nonlinear static (pushover) analysis will be performed on a railroad bridge bent using wframe to determine its ultimate lateral deflection capability.

Torsion of shafts with circular symmetry

Lecture Slides. Chapter 14. Spur and Helical Gears

D : SOLID MECHANICS. Q. 1 Q. 9 carry one mark each. Q.1 Find the force (in kn) in the member BH of the truss shown.

Chemical Mechanical Planarization

UNIT IV FLEXIBILTY AND STIFFNESS METHOD

M.S Comprehensive Examination Analysis

MEMS Metrology. Prof. Tianhong Cui ME 8254

March 24, Chapter 4. Deflection and Stiffness. Dr. Mohammad Suliman Abuhaiba, PE

Springs Lecture 3. Extension Springs

December 1999 FINAL TECHNICAL REPORT 1 Mar Mar 98

the engineer s notebook 2013

Chapter 4 Deflection and Stiffness

A New Methodology for Assessing the Current Carrying Capability of Probes used at Sort

STRESS STRAIN AND DEFORMATION OF SOLIDS, STATES OF STRESS

TECHNICAL INFORMATION Bulletin

Controlling BP Damage at 129C Probing

Mechanical Design in Optical Engineering

Methods of Analysis. Force or Flexibility Method

Deflections and Strains in Cracked Shafts due to Rotating Loads: A Numerical and Experimental Analysis

557. Radial correction controllers of gyroscopic stabilizer

Advanced Strength of Materials Prof S. K. Maiti Mechanical Engineering Indian Institute of Technology, Bombay. Lecture 27

Available online at ScienceDirect. Procedia IUTAM 13 (2015 ) 82 89

Dynamic Model of a Badminton Stroke

High Tech High Top Hat Technicians. An Introduction to Solid Mechanics. Is that supposed to bend there?

MECH 466. Micro Electromechanical Systems. Laboratory Manual Laboratory #3: Stiction of MEMS and Strength of MEMS Materials

APPENDIX 4.4.A STRAWMAN STRUCTURAL DESIGN OF A 30-M GSMT

Laith Batarseh. internal forces

Advanced Mechanical Principles

The basic dynamic load rating C is a statistical number and it is based on 90% of the bearings surviving 50 km of travel carrying the full load.

ENG1001 Engineering Design 1

Features of static and dynamic friction profiles in one and two dimensions on polymer and atomically flat surfaces using atomic force microscopy

MECH 401 Mechanical Design Applications

1 INTRODUCTION 2 SAMPLE PREPARATIONS

QUESTION BANK ENGINEERS ACADEMY. Hinge E F A D. Theory of Structures Determinacy Indeterminacy 1

DETERMINATION OF EI FOR PULTRUDED GFRP SHEET PILE PANELS. Abstract

THE NEW 1.1 MN m TORQUE STANDARD MACHINE OF THE PTB BRAUNSCHWEIG/GERMANY

Deflections and Strains in Cracked Shafts Due to Rotating Loads: A Numerical and Experimental Analysis

NIST ELECTROSTATIC FORCE BALANCE EXPERIMENT

Quintic beam closed form matrices (revised 2/21, 2/23/12) General elastic beam with an elastic foundation

The drive to make devices smaller and faster

Thermal Interface Materials (TIMs) for IC Cooling. Percy Chinoy

SOLUTION 8 7. To hold lever: a+ M O = 0; F B (0.15) - 5 = 0; F B = N. Require = N N B = N 0.3. Lever,

Critical Load columns buckling critical load

Seismic Pushover Analysis Using AASHTO Guide Specifications for LRFD Seismic Bridge Design

Glossary Innovative Measurement Solutions

New probe design and development for high current capacity using bi-furcated structure

Unified Quiz M4 May 7, 2008 M - PORTION

Chapter 11. Displacement Method of Analysis Slope Deflection Method

Mechanics of Materials II. Chapter III. A review of the fundamental formulation of stress, strain, and deflection

CHAPTER 6 FRICTION AND WEAR ANALYSIS FOR BUSHING

TWISTING (TORSIONAL) STIFFNESS. Barry T. Cease Cease Industrial Consulting

Materials Selection and Design Materials Selection - Practice

Modal Analysis: What it is and is not Gerrit Visser

Shafts: Torsion of Circular Shafts Reading: Crandall, Dahl and Lardner 6.2, 6.3

KINGS COLLEGE OF ENGINEERING DEPARTMENT OF MECHANICAL ENGINEERING QUESTION BANK. Subject code/name: ME2254/STRENGTH OF MATERIALS Year/Sem:II / IV

Blunt Impact Damage Formation on Composite Aircraft Structures

two structural analysis (statics & mechanics) APPLIED ACHITECTURAL STRUCTURES: DR. ANNE NICHOLS SPRING 2017 lecture STRUCTURAL ANALYSIS AND SYSTEMS

Lecture Slides. Chapter 4. Deflection and Stiffness. The McGraw-Hill Companies 2012

Aeroelasticity in Dynamically Pitching Wind Turbine Airfoils

AN INTEGRATED KIRCHHOFF PLATE ELEMENT BY GALERKIN METHOD FOR THE ANALYSIS OF PLATES ON ELASTIC FOUNDATION

New Way Porous Gas Bearings as Seals. Bearings Seals

Engineering Design for Ocean and Ice Environments Engineering Sea Ice Engineering

Lecture-08 Gravity Load Analysis of RC Structures

New Representation of Bearings in LS-DYNA

EDEXCEL NATIONAL CERTIFICATE/DIPLOMA SCIENCE FOR TECHNICIANS OUTCOME 1 - STATIC AND DYNAMIC FORCES TUTORIAL 3 STRESS AND STRAIN

Moment Distribution Method

Transcription:

John R. Goulding Martin Elzingre Larry Hendler Technical Marketing Manager 200mm Product Manager Consultant Electroglas, Inc. Electroglas, Inc. Electroglas, Inc. South West Test Workshop June 11-14 th 2000 San Diego, CA USA Page 1 of 20

Abstract Probe-to-pad contact resistance (C RES ) is seen to increase for die near the edge of the wafer as probe applications move to higher force x64 to x128 probe cards. As a result, far more "good" die will escape the process and end up in the trash heap due to a lack of process control capability or the general lack of process improvement in the test area. This effect is primarily attributed to the combination of low-force high pin count technology and the mechanical deflection of the prober chucktop that results. This paper addresses the relationship between probe overtravel, planarity, C RES, scrub marks, and yield for a variety of probing technologies, and suggests design improvements to ensure that all probe tips make good electrical contact with the bond pads. Page 2 of 20

Presentation Outline Introduction Traditional Probe Mechanism (Stage) Generalized Stage Deflection Relationship to Production System Modeling Elastic Strain, Deflection, and Stability Objective Design Innovation Probe-Centered Z-Drive Mechanism EG4 200 Cross-Section Metrology Characterization Experimental Set-Up Design Validation Conclusion Future Work Page 3 of 20

Introduction By inspecting probe marks to ensure that probe-to-pad connectivity was achieved, we discovered a relationship between C RES and probe location. For low pin count, small array probes (low total probe force), a change in C RES is not measurable over the wafer surface. For high pin count, large array probes (high probe force ~120kg), C RES increases and scrub marks shorten as a function of distance from wafer center due to mechanical deflection and loss of planarity. The mechanical model of chuck top deflection is presented, and the relationships between overtravel and compliance and planarity and yield is established with supportive test results. Prober error is differentiated from probe card error by analysis of variance methods. Page 4 of 20

Traditional Probe Mechanism (Stage) Z-Axis drive (red) is a live post directly attached to chuck. Centered probe load results in uniform deflection. Probe Load Chuck Chuck Support Base or Forcer Stem Air Bearing Platen or X, Y motion system Page 5 of 20

Traditional Probe Mechanism Large bending moments about z-axis live post result when probe load is moved to chuck edge. Edge load bends and tilts chuck and live post system -- deflection is maximum. Probe Load Deflection Torque = F*d Platen or X, Y motion system Page 6 of 20

Generalized Stage Deflection The deflection of the chucktop becomes nonlinear as force is applied further from probe center. 150kg Load max Linear Response Nonlinear Response Deflection of Chucktop d = kf d = Fx 3 /3EI 60kg Load Negligible Load 0 Distance from Center of Chucktop 200 mm Page 7 of 20

Relationship to Production Yield C RES Scrub Marks Overtravel System Deflection In a perfect probe system, a flat array of stiff probe pins contact and penetrate vertically into the wafer with near-zero C RES. In reality, each probe pin deflects to compensate for variation in z-axis tolerance. The probe pin with the least deflection may determine the outcome of the test. Yield is a function of C RES High C RES = false failures and poor yield C RES is a function of Scrub Marks Good penetration is required to achieve good electrical contact Scrub Mark is a function of Overtravel Overtravel is required to compensate for non-planar probe surfaces Yield is a function of System Deflection Page 8 of 20

System Modeling The deflection at any point on the chucktop is the sum of the individual deflections of the system Chucktop Live Post (z-axis) Frame Ring Carrier PCB Idealized Prober Without Load Idealized Prober Under Load d RC = FL 3 /48EI d frame = kf Linear-Elastic Deflection Force d Chuck = FL 3 /3EI d Post = M F L 2 /2EI d System = d Chuck + d Post + d Frame + d RC + d PCB Page 9 of 20

Objective Develop a model to predict the deflection of the chuck for a given probe load and array size for a radial distance from chuck center. Why Predict Deflection? Increase in probe pin counts increases probe forces Probe mechanism exhibits non-linear deflection under high probe loads Many new probe technologies require less overtravel It is critical to model the system to accurately predict overtravel programmed (input) into the prober Understanding leads to design innovation & improvement Page 10 of 20

Design Innovation Low-force high pin count probes were developed, in part, due to a perception that robotic systems (probers) are incapable of holding micron-accuracy tolerances while applying probe forces up to 150kg. While ring carrier and probe card stiffness are important factors they are, often, easier to address since they are static and not usually constrained by weight and, to an extent, by size. The chuck and related motion systems are limited in height and weight by the physical dimensions of the prober. Recent metrology-based advancements to minimize chuck deflection are presented with supportive test results. This development effort supports process improvements related to improving yield for high pin count, high probe force, wafer probing applications in back-end semiconductor manufacturing processes. Page 11 of 20

Probe-Centered Z-Drive Mechanism Chuck Support Probe Load Platen Chuck Forcer Air Bearing Z-Drive Page 12 of 20

Probe-Centered Z-Drive Mechanism Edge load does not tilt chuck or system. Probe Load Uniform Deflection Platen Page 13 of 20

EG4 200 Cross-Section Chuck Support Theta Platen Chuck Forcer Z-drive Page 14 of 20

Metrology Characterization Elimination of Live Post via probe-centered z-axis drive innovation uses metrology of Forcer and Platen to simplify chucktop construction while improving system deflection. System Modeling Linear-Elastic Deflection Beam Deflection Models Probe Mechanics Planarity Measurements Overtravel Calculation Scrub Mark Images (Feedback) Contact Resistance (Feedback) Yield Correlation Page 15 of 20

Experimental Set-Up Test Setup to Measure Deflection Page 16 of 20

Experimental Data Deflection Under Load Data presented at workshop Contact Resistance, C RES Data presented at workshop Probe Mark Images Data presented at workshop Page 17 of 20

Design Validation For high pin count, large array probes (high probe force ~120kg), the change in C RES is negligible over the wafer surface using the probe-centered z-axis mechanism. With nominal overtravel, all probe tips make good electrical contact with the bond pads because the chucktop remains planar to the probe card. Slope Deflection Across a Known Array Size Summary of deflection results measured on EG4 200 prober Data presented at workshop Z-Stage Comparison Comparative analysis (deflection vs force) between conventional and new stage mechanisms Data presented at workshop Page 18 of 20

Conclusion Understanding the system deflection model led to innovation and improvement in probe mechanism design. Probe-Centered z-axis drive Off-Axis overtravel model simplified to d System = ΣkF Uniform deflection across wafer Improved probe-to-pad C RES across wafer Page 19 of 20

Future Work While the benefit of probing low-yield wafers with greater than x32 arrays remains speculative, probing high-yield wafers with x64 or even x128 arrays is advantageous. In addition, decreasing bond pad size and pitch is driving improvements in probe technology to smaller probe pins and highly integrated probe arrays. These smaller probe pins produce less spring force per mil of overtravel. Consequently, understanding the bondpad-to-probe-pin system is key to successful probing. More can be done to improve the prober system. Page 20 of 20