TUNERS FOR SRF CAVITIES A Comparative Study – Mechanical Characteristics Presented by N. Dhanaraj.

Slides:



Advertisements
Similar presentations
FE analysis with beam elements
Advertisements

Principle of the process Design For Manufacturing (DFM)
Mechanical Department
Various Fasteners Non-permanent fasteners (threaded)
Explosive joining of dissimilar metals: experiment and numerical modeling Anan’ev S.Yu., Andreev A.V., Deribas A.A., Yankovskiy B.D. Joint Institute for.
Professor Joe Greene CSU, CHICO
MICE- AFC Unit Mechanical Design of the Cold Mass Support System Oxford University Rohan Senanayake.
N. Dhanaraj, Y. Orlov, R. Wands Thermal-Stress Analysis of CC1 Space Frame.
Chapter 3 – Stress and Deformation Analysis (ref MCHT 213!!)
On the Advanced Efficiency Analysis for Half Toroidal CVT -The Efficiency Analysis Considering Deformation of CVT Components - Masayuki Ochiai Kinji Yukawa.
The various engineering and true stress-strain properties obtainable from a tension test are summarized by the categorized listing of Table 1.1. Note that.
Chapter 17 Design Analysis using Inventor Stress Analysis Module
MACHINE DESIGN II CLUTCHES.
Progress on the MICE 201 MHz Cavity Design Steve Virostek Lawrence Berkeley National Lab RF Working Group Fermilab August 22, 2007  automatic.
Methods of exerting forces and displacements introduction to the design of „basic machine”
CTC / MTC 222 Strength of Materials
Analysis of Basic Load Cases Axial Stress
ENGR 225 Section
Static and Fatigue Bolt Design
ME 307 Machine Design I ME 307 Machine Design I Dr. A. Aziz BazouneChapter 8: Screws, Fasteners and the Design of Nonpermanent Joints CH-8 LEC 35 Slide.
4.5 FORCE METHOD OF ANALYSIS FOR AXIALLY LOADED MEMBERS
1 RF-Structures Mock-Up FEA Assembly Tooling V. Soldatov, F. Rossi, R. Raatikainen
PROBLEM mm x y 800 mm P = 1500 N z y 50 mm 100 mm
Power Screws & Threaded Fasteners
Luca Dassa – 23/02/ / 8 CRAB cavities meeting Preload Bolt size (1) Shear load: 602 N (p=0.26 MPa) -> Min preload: 2006 with Static friction coefficient:
Beam Design for Geometric Nonlinearities
Principal Stresses and Strain and Theories of Failure
Cost comparison of tuners H. Hayano, KEK AWLC14
SSR1 Tuner studies (work in progress) 1 L. Ristori – 29 Nov 2011 With slides from I. Gonin, M. Hassan and D. Passarelli.
RFCC Module Design Update  automatic tuners  cavity suspension  cavity installation Steve Virostek Lawrence Berkeley National Lab MICE Collaboration.
 2005 Pearson Education South Asia Pte Ltd TUTORIAL-1 : UNIAXIAL LOAD 1 PROBLEM-1 1 m P A composite A-36 steel bar shown in the figure has 2 segments,
The ratio of stress and strain, called modulus of elasticity. Mechanical Properties of Solids Modulus of Elasticity.
Poisson’s Ratio For a slender bar subjected to axial loading:
Feedback Control Systems (FCS) Dr. Imtiaz Hussain URL :
Section VIII Belt Drives.
1 20-Oct-15 Last course Lecture plan and policies What is FEM? Brief history of the FEM Example of applications Discretization Example of FEM softwares.
Shuichi Noguchi,SRF2007,10.71 New Tuners for ILC Cavity Application Shuichi Noguchi KEK.
 2005 Pearson Education South Asia Pte Ltd TUTORIAL-1 : STRESS & STRAIN 1 PROBLEM-1 The hanger assembly is used to support a distributed loading of w=16kN/m.
CTC / MTC 222 Strength of Materials Chapter 1 Basic Concepts.
Machine Design I (MCE-C 203) Mechatronics Dept., Faculty of Engineering, Fayoum University Dr. Ahmed Salah Abou Taleb Lecturer, Mechanical Engineering.
Mechanisms Jeopardy Q $100 Q $200 Q $300 Q $400 Q $500 Q $100 Q $200 Q $300 Q $400 Q $500 Final Jeopardy.
Carlo Pagani University of Milano & INFN Milano - LASA WP8 Tuner Status & Perspective ILC-HiGrade Kick-Off Meeting DESY, Hamburg 29 August 2008 Material.
Mechanical Properties of Materials
Forging new generations of engineers
Status report AHCAL Mechanics Karsten Gadow CALICE Collaboration Meeting KEK, Studies of AHCAL absorber structure stability.
4/19/ Helium tank comparison Nicola Panzeri INFN – Mi LASA.
Unit-5. Torsion in Shafts and Buckling of Axially Loaded Columns Lecture Number-3 Mr. M.A.Mohite Mechanical Engineering S.I.T., Lonavala.
BoltJoin ppt P. Rogoff 3/24/2011. NSTX Supported by P. R. 3/9/2011 Update Ring Bolted Joint Design and Recommend the Joint Geometry using bolts.
UNIT-01. SIMPLE STRESSES & STRAINS Lecture Number - 06 Prof. S.C.SADDU MECHANICAL DEPARTMENT SIT LONAVALA Strength of Materials.
Nonlinear Analyses of Modular Coils and Shell structure for Coil Cool-down and EM Loads Part 1 – Results of Shell Structure and Modular Coils H.M. Fan.
Andrew Biehl.  The objective of this project is to develop a method for determining the nut factor of a bolted joint using the finite element method.
LCLS II Tuner Mechanics; Accessibility/Replacement E. Borissov, Yu.Pischalnikov SRF cavity Tuner Workshop, FNAL, Oct. 13.
Adam Carreon July 19, 2012 Technical Division SRF Department Dressed SSR1 Cavities.
Chapter Objectives Understand how to measure the stress and strain through experiments Correlate the behavior of some engineering materials to the stress-strain.
A. Lambert: Thermal and Mechanical Analysis PXIE RFQ Design Review, Berkeley, CA April 12, 2012 Thermal and Mechanical Analysis of the PXIE RFQ Andrew.
NCSX Modular Coil Joint Load/Stress Calculation By Leonard Myatt Myatt Consulting, Inc.
The HiLumi LHC Design Study is included in the High Luminosity LHC project and is partly funded by the European Commission within the Framework Programme.
Calculations for the bolted helium vessel February 2nd 2015 Norbert Kuder, EN/MME.
Principle of the process Design For Manufacturing (DFM)
Pipe Integrity Check using Finite Element Analysis
The various engineering and true stress-strain properties obtainable from a tension test are summarized by the categorized listing of Table 1.1. Note that.
Fredrik Fors Mechanical Engineering, JLab 04/22/2016
CRAB cavities Cryomodule review Tuner
1.6 Allowable Stress Allowable Load < Failure Load
Six Simple Machines Lever Wheel & Axle Pulley Inclined Plane Wedge
Ch. 2: Fundamental of Structure
Tutorial in Mechanical Properties
4.7 STRESS CONCENTRATIONS
Principle of the process Design For Manufacturing (DFM)
PDT 153 Materials Structure And Properties
Presentation transcript:

TUNERS FOR SRF CAVITIES A Comparative Study – Mechanical Characteristics Presented by N. Dhanaraj

1.3 GHz Tuner Comparison – Mechanical Specifications* TypeEnd Lever tunerSlim blade tuner A.K.ATTF tuner or Saclay tunerModified blade tuner LocationCavity endcoaxial CuBe screw specsM12 x 1.5 mmM12 x 1.5 mm (max. specified) CuBe screw coatingBalinit-C (tungsten carbide)Lamcoat (tungsten disulfide) Nut coatingBalinit-C (tungsten carbide) Axial force on driving screw at max. elongation409 N (calculated) 1600 N (loaded) and 2000 N (unloaded) (literature) Max. cavity elongation2 mm1.8 mm (12 screw turns) Tuner stiffness100 KN/mm (measured) KN/mm Coarse/slow tuning range± 400 kHz~ 600 kHz * Various sources

What is the axial force required to yield the thread Bolt tensile force required to yield entire thread cross section is F = A t S y ~ Pi/4 (0.9 d) 2 S y, S y = 28 ksi F = 17.6 KN for thread pitch 1 mm F = 15.7 KN for thread pitch 1.5 mm

End Lever Tuner – Saclay Tuner I P=δ K cavity R1 R2Force on CuBe screw (F) Simplification of Lever Equivalent Mathematical Model

End Lever Tuner – Saclay Tuner I (contd.) Force Calculation: Known parameters: Mechanical advantage range reported – 1:17 to 1:25 Solution: Stiffness of cavity (Kcav) = 3473 N/mm Max. elongation (δ) = 2 mm Load exerted by cavity (P) = δ * Kcav = 6946 N Therefore, Axial force on CuBe screw (F) = P / mechanical adv. Ratio = 6946 / 17 = N (Max.) If mechanical adv. 1:25 considered, then F = 277 N (min)

Blade Tuner – INFN Design and FEA Results FEA Results: Axial Force reported 2000 N (unloaded). Axial Force reported 1600 N (loaded), corresponds to 1.8 mm of maximum elongation and 12 turns of the CuBe screw. Inference: Considering 1.5 mm pitch of the CuBe screw,10 turns of screw required to produce a tuner displacement or elongation of 1.5 mm.

Blade Tuner – FNAL Measurements C. Grimm, N. Dhanaraj, D. Passarelli 10 Turns => 0.87 mm, 1mm pitch

Blade Tuner – FNAL Torque Measurements Torque measured using torque wrench: 2.9 Nm at 0.8 mm displacement or elongation of cavity. Axial force calculation from measured torque Torque = k. axial force. Diameter of screw Where k is the friction factor, 0.35 for Tungsten carbide on copper. Assume 50 % friction reduction using Lamcoat. Therefore, Axial force on screw = Torque / k. Diameter F = 2900/0.175 * 12 = 1381 N

Blade Tuner – FNAL FEA (unloaded) FEA Parameters: FNAL modified Tuner geometry Non-linear Material Properties (as per ASME, Div. 2) Mesh 1.32e6 nodes, 1mm elements on 66 mm long blades Displacement controlled analysis Large Deformation Model

Blade Tuner – FNAL FEA Force Results

Blade Tuner – FNAL Results FEA – 10 Turns 1 mm Measured – 10 Turns 0.95 mm

Acknowledgement Tom Peterson Chuck Grimm Bob Wands Donato Passarrelli Tuner Folks SRF DD