Step IV - Engineering Jason Tarrant – Integration Engineering

Slides:



Advertisements
Similar presentations
ANALYSIS OF STATICALLY DETERMINATE STRUCTURES
Advertisements

Mechanical Engineering Design Review BL ARPES Endstation Derek Yegian, Jonathan Denlinger, Keith Franck 4/18/2008.
SPL Intercavity support Conceptual design review 04/11/ A. Vande Craen TE/MSC-CMI.
Work Done by a Constant Force
Summary of Twisted Racetrack / Clamp Analysis K. D. Freudenberg.
Overview of Loads ON and IN Structures / Machines
MICE- AFC Unit Mechanical Design of the Cold Mass Support System Oxford University Rohan Senanayake.
Beams and Frames.
Introduction to Beam Theory
CUFSM Advanced Functions
MICE Collaboration Meeting at Frascati, Jun 26~29, 2005 Iron Shield Mounting Design Stephanie Yang.
Strength of Material Shear Strain Dr. Attaullah Shah.
Suitability of a structure or machine may depend on the deformations in the structure as well as the stresses induced under loading. Statics analyses.
Roller Coaster Dynamics-1: Energy Conservation
What is good for small mechanisms is very good for very big ones. Above is the major reciprocating parts of a rally engine. At top right is the force applied.
Department of Civil and Environmental Engineering, The University of Melbourne Finite Element Modelling – Element Types and Boundary Conditions (Notes.
Analyses of Bolted Joint for Shear Load with Stainless Steel Bushing and Frictionless Shim-Flange Interface Two cases of shim plates were investigated.
 2005 Pearson Education South Asia Pte Ltd 7. Transverse Shear 1 CHAPTER OBJECTIVES Develop a method for finding the shear stress in a beam having a prismatic.
MECHANICS OF MATERIALS Fourth Edition Ferdinand P. Beer E. Russell Johnston, Jr. John T. DeWolf Lecture Notes: J. Walt Oler Texas Tech University CHAPTER.
Energy Transformations and Conservation of Mechanical Energy 8.01 W05D2.
An Analysis of Shell Structure for Dead Load H.M. Fan PPPL September 16, 2005.
Analyses of Bolted Joint for Bolt Preload and Shear Load
Mechanical Properties of Materials
Deformation of Axially Loaded Members - Single Member
Strength of Materials Malayer University Department of Civil Engineering Taught by: Dr. Ali Reza Bagherieh In The Name of God.
Stress and Strain – Axial Loading
Cavity support scheme options Thomas Jones 25/06/15 1.
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.
FEM Analysis of the Stage3 Support Frame H.M. Fan March 14, 2007.
Friction.
16 T dipole in common coil configuration: mechanical design
Stress and Strain – Axial Loading
Status of the PANDA Magnet mechanics (yoke & cryostat)
Stress and cool-down analysis of the cryomodule
Solenoid Yoke Door-Barrel Connection
Sample Problem 4.2 SOLUTION:
Stress and Strain – Axial Loading
Shear in Straight Members Shear Formula Shear Stresses in Beams
Poisson’s Ratio For a slender bar subjected to axial loading:
Longitudinal Strain Flexure Formula
Pure Bending.
C. K. Pithawalla College of Engg. & Tech.
Step IV - Engineering Jason Tarrant – Integration Engineering
Stress and Strain – Axial Loading
Overview of Loads ON and IN Structures / Machines
Work Done by a Constant Force
Thermal Shield Connection Study
By Arsalan Jamialahmadi
Deflections using energy methods
Friction.
Contents Introduction Identification of the knowledge gap
Poisons Ratio Poisons ratio = . w0 w Usually poisons ratio ranges from
Poisson’s Ratio For a slender bar subjected to axial loading:
Stresses, Strains and Deflections of Steel Beams in Pure Bending
Structure I Course Code: ARCH 208 Dr. Aeid A. Abdulrazeg
Physics: Review Forces.
Created analysis model
Sample Problem 4.2 SOLUTION:
Structural Member Properties
CHAPTER OBJECTIVES Determine deformation of axially loaded members
Engineering Mechanics: Statics
Stress and Strain – Axial Loading
Structural Geology Structural geology is the study of rocks deformed by stress and strain This involves trying to understand stress and strain forces to.
Engineering Mechanics: Statics
Engineering Mechanics: Statics
MQXFAP2 SG Readings ---Update (up to quench #22)
Poisson’s Ratio For a slender bar subjected to axial loading:
Simple Stresses & Strain
Mechanics Chapter 3 Vertical Motion.
Dove-Tail Tack Block Design
Presentation transcript:

Step IV - Engineering Jason Tarrant – Integration Engineering Bobbin support & stiffness – for discussion at magnet meeting 05/10/2016 05 Oct

PRY SS Stand-Off Loads Bobbin strap pre-tension / pre-load 6000 lb pre-load / strap warm, not change when cold (S Virostek) Vacuum contraction of OVC Depends on actual ave T & CTE Preload to 6000 lb Bobbin cool down to 4 K Strap cool down to 170 K

SS Bobbin Strap properties Steve Virostek estimated 45 GPa tensile stiffness warm and up to +15 % when cold = ~ 52 Gpa Model set-up ¼ model with fixed & frictionless constraints = radially flexible but ‘on rails’ axial movement, i.e. if the pins & bands disconnect the bobbin does not drop on slack end ¼ model has ¼ load applied to end

SS Bobbin ‘Final’ predicted loads (as of 05/10/16)

(from locked connections) SS Bobbin Bobbin movement – fixed straps & 15 - 40 tonne loads Straps & pins bonded 6000 lb / 27 kN preload Elastic modulus 40 GPa 15 tonne / ~147 kN -ve X, then 40 tonnes / ~392 kN +ve X Note ‘S’ bend (from locked connections)

Note band has been lost from pin SS Bobbin Bobbin movement – flexible straps & 15 tonne load Straps flexible around pins – frictionless connection 6000 lb / 27 kN preload Elastic modulus 52 GPa 15 tonne / ~147 kN -ve X Note band has been lost from pin

Note band has been lost from pin SS Bobbin Bobbin movement – flexible straps & 40 tonne load Straps flexible around pins – frictionless connection 6000 lb / 27 kN preload Elastic modulus 52 GPa 40 tonne / ~392 kN -ve X Note band has been lost from pin See also plot next page

SS Bobbin Loss of pretension With a preload of 6000 lb / 27 kN John Cobb estimated that with the 60 degree strap angle, strap preload would be lost around 11 tonnes. Deflection plot from 40 tonne bobbin analysis (last slide) Tonnes 10 20 30 15° 40 Step 1 shows the deformation in the straps due to the 27 kN preload Step 2 the 40 tonne (392 kN) load is applied linearly, the bobbin starts to move… 0-5 tonnes the deformation is relatively flat as material in the bands is moving too 5-just over 10 tonnes the graph takes a steady linear angle of 15 deg from horizontal Just over 10 - 40 tonnes the graph rises by 15 deg to 30 deg from horizontal 15 deg + 15 deg is indicative of the stiffness halving from just over 10 tonnes, this appears to coincide with John’s predicted loss of preload in one set of bands

(lower view rotated 35 deg for side on view) SS Bobbin Possible off-axis bobbin movement 15° 10 20 30 40 Tonnes Deflection plot from 40 tonne bobbin analysis With this set-up @ 11 tonnes ~ 1 mm of axial bobbin movement occurs before the bands slip their pins*. The bands on the bottom would lose control of the bobbin at this point but those on top would still be in contact, however as the bobbin moves axially further the top bands would rotate between their anchor point on the OVC and their anchor point on the bobbin potentially changing the height of the bobbin on the slack band end *Actual movement where bands slip & total drop in height is dependant on stiffness of bands + gravity effects, however assuming further ~ 4 mm of movement [from 1 mm to 4.81 mm] the drop in height of the end of the bobbin could be as shown in the adjacent table [based purely on geometric rotation from 60 degrees of bands then reduced for 35 degree angle] band geometry (lower view rotated 35 deg for side on view)

SS Bobbin Conclusion - Strap Supports Model with frictionless strap-pin connections appears to behave as expected losing pre-load at just over 10 tonnes with 6000 preload 15 tonnes = 1.5 mm bobbin axial movement (52 GPa / 6000 lb) 40 tonnes = 4.5 mm bobbin axial movement (52 GPa / 6000 lb) Analysis models ‘on rails’ constraints do not allow a vertical displacement / gravitational drop if band slips the pins, however ‘geometric’ estimates show that for 4 mm of movement after the bands lose contact, the bobbin may drop ~1.9 mm