VG1 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Recent Study Topics Full length model with wafers, hybrids and cable as dead weight.

Slides:



Advertisements
Similar presentations
N. Dhanaraj, Y. Orlov, R. Wands Thermal-Stress Analysis of CC1 Space Frame.
Advertisements

ATLAS Pixel Detector September 2002 N. Hartman LBNL 1 Pixel Support Tube: Design, Prototyping, and Production PST Progress Update September 2002.
W.O. Miller i T i VG 1 Bridge Analysis Objective Objective –Develop model suited to examining effect of low velocity air flow through the isolating air.
Designing for Stiffness
MICE Collaboration Meeting at Frascati, Jun 26~29, 2005 Iron Shield Mounting Design Stephanie Yang.
Tracker Solenoid Module Design Update Steve VirostekStephanie Yang Mike GreenWing Lau Lawrence Berkeley National LabOxford Physics MICE Collaboration Meeting.
CM 197 Mechanics of Materials Chap 14: Stresses in Beams
Final Project1 3/19/2010 Isogrid Buckling With Varying Boundary Conditions Jeffrey Lavin RPI Masters Project.
Centre of gravity and centroid
Thin ladder development Status of ladder development for the thin ladderfest.
Outer Stave Prototype Update E. Anderssen, M. Cepeda, M. Garcia-Sciveres, M. Gilchriese, N. Hartman, J. Silber LBNL W. Miller, W. Shih Allcomp, Inc ATLAS.
M. Gilchriese Pixel Stave thermal/mechanical studies for Valencia Upgrade Workshop M. Gilchriese, M. Garcia-Sciveres, M. Cepeda LBNL W. Miller and W. Miller,
Pixel Upgrade Local Supports Based on Thermally Conducting Carbon Foam E. Anderssen, M. Cepeda, S. Dardin, M. Garcia-Sciveres, M. Gilchriese, N. Hartman,
MECHANICS OF MATERIALS 7th Edition
Carbon-Epoxy Composite Base Plates for the PHOBOS Spectrometer Arms J.Michalowski, M.Stodulski The H.Niewodniczanski Institute of Nuclear Physics, Krakow.
I T i womiller VG1 Meeting UCSC November 10, 2005 ATLAS Upgrade Workshop Silicon Tracker Stave Mechanical Issues.
Shear Stress and Strain
CTC / MTC 222 Strength of Materials
Engineering Mechanics: Statics
WBS Stave Mechanics, Cooling and Support - LBNL ATLAS Upgrade R&D Meeting UC Santa Cruz May 3, 2007 E. Anderssen, M. Cepeda, S. Dardin, M. Gilchriese,
1 Design of Solenoid and iron yoke for GLD KEK Hiroshi Yamaoka Ken-ichi Tanaka July 13, ‘05.
W.O. Miller i T i VG 1 Example Barrel Structures- Disk Primary FEA of Disk Frame Supports FEA of Disk Frame Supports –Structure 2m long with two end plates.
Thomas Jefferson National Accelerator Facility Page 1 IPR October Independent Project Review of 12 GeV Upgrade Jefferson Lab October 18-20,
M. Gilchriese Integrated Stave Mechanics/Cooling Backup ATLAS Upgrade Workshop Valencia December 2007 M. Cepeda, S. Dardin, M. Gilchriese, C. Haber and.
Equilibrium and Elasticity
Copyright © 2010 Pearson Education South Asia Pte Ltd
26 April 2013 Immanuel Gfall (HEPHY Vienna) Belle II SVD Overview.
M. Gilchriese Integrated Stave Mechanics/Cooling June 5, 2008 CERN.
M. Gilchriese ATLAS Upgrade Mechanics/Cooling and System Design by LBL January 2008.
1 Advanced Endplate - mechanics: Development of a Low-Material TPC Endplate for ILD Dan Peterson Laboratory for Elementary-Particle Physics, Cornell University.
ATLAS LBNL Pixel Support Study 1 W.O. Miller HYTEC ATLAS Pixel Detector Support Structure Status and Future Developments February 19, 1999 W. Miller HYTEC.
M. Gilchriese - November 12, 1998 Status Report on Outer Support Frame W. Miller Hytec, Inc E. Anderssen, D. Bintinger, M. Gilchriese LBNL.
Sag of ZTF components Callahan 9/4/2014. Corrector Trim Plate analysis.
Engineering Division 1 Coupled Layer Prototype Update E Anderssen, M Cepeda, M Gilchriese, N Hartman, T Johnson, J Silber, LBNL W Miller Allcomp Inc ATLAS.
VG1 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Upgrade Stave Study Topics Current Analysis Tasks –Stave Stiffness, ability to resist.
L0 and L1 Structure Deflections During Installation of Silicon Sensors C H Daly 8/24/2003.
Mechanical and Thermal Management for ATLAS Upgrade Silicon Tracking System W. O. Miller (iTi) Carl Haber (LBNL), Gil Gilchriese (LBNL) Carl Haber (LBNL),
Thermal & Mechanical Support for Diamond Pixel Modules Justin Albert Univ. of Victoria Nov. 6, 2008 ATLAS Tracker Upgrade Workshop.
Preliminary Calculation of the Tracking Detector Barrels and the Support Tube Szymon Sroka CLICdp Tracker Technology Meeting Szymon Krzysztof Sroka 30/07/2015.
Static Analysis Static Analysis, Internal Forces, Stresses: Normal and Shear 1.
PHENIX Silicon Vertex Tracker. Mechanical Requirements Stability requirement, short and long25 µm Low radiation length
An Analysis of Shell Structure for Dead Load H.M. Fan PPPL September 16, 2005.
The Mechanical Structure for the SVD Upgrade
Strength of Material-1 Introduction. Dr. Attaullah Shah.
Finite Element Analysis of the18 Turn Beam H. F. Fan November 5, 2004.
W.O. Miller i T i VG 1 Two Pixel Configurations Under Study First: A Monolithic Integrated Structure First: A Monolithic Integrated Structure –Axial array.
Sam Krueger.  Entertainment Center  Preliminary design  Initial  36 plies, glass epoxy  [0 11 /±45 1 /90 5 ] s  No core  Modified design  36 plies,
1 Monophase Measurements on Prototype Pixel Structures D. Bintinger, M. Gilchriese, J. Taylor and J. Wirth and contributions from D. Cragg, E. Perrin and.
D. M. Lee, LANL 1 07/10/07 Forward Vertex Detector Overview Technical Design Overview Design status.
Thermal Model of Pixel Blade Conceptual Design C. M. Lei 11/20/08.
Walter Sondheim 6/9/20081 DOE – Review of VTX upgrade detector for PHENIX Mechanics: Walter Sondheim - LANL.
General Rheology Senior/Graduate HMA Course Asphalt Binder
Clic Vertex Thermal Setup and stave studies 21/10/2013 Francois-Xavier NUIRY Andrea Catinaccio Fernando Duarte Ramos 1 CERN PH/DT/EO.
A hollow stave Ian Wilmut – August LBL stave At the March UG week LBL showed a prototype asymmetric stave. This prompted consideration of the strip.
ATLAS ITk Upgrade: SLIM Update
10 September 2010 Immanuel Gfall (HEPHY Vienna) Belle II SVD Upgrade, Mechanics and Cooling OEPG/FAKT Meeting 2010.
Thermal Shield Update Niklas Templeton 15/02/16 (final update of placement  )
B [OT - Mechanics & Cooling] Stefan Gruenendahl February 2, 2016 S.Grünendahl, 2016 February 2 Director's Review -- OT: Mechanics &
Thermal modeling, interfaces, test results LBNL Composites Workshop February 29-March 3, 2016.
Stave studies 6/15/2013 François-Xavier Nuiry Wolfgang Klempt Fernando Duarte Ramos Miguel Angel Villarejo 1.
EC: 7 DISK concept Preliminary considerations
Are there better ways to build a stave?
Example 6.04 SOLUTION: Determine the shear force per unit length along each edge of the upper plank. For the upper plank, Based on the spacing between.
WP9 ITS Mechanics and Cooling
Week 2 Experimentation TS Term 2.
WG4 – Progress report R. Santoro and A. Tauro.
Theory of Simple Bending
Material Properties and Forces
Example 6.04 SOLUTION: Determine the shear force per unit length along each edge of the upper plank. For the upper plank, Based on the spacing between.
Strain Transformation
Presentation transcript:

VG1 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Recent Study Topics Full length model with wafers, hybrids and cable as dead weight –0.173in dia. support pins –Clamped pin vertical supports, but with pins at one fixed in Z –Core thickness 4.6mm Half length model with wafers, hybrids and cable as dead weight –0.173in support pin –By necessity for symmetry the middle is fixed in Z, thus it looks like all pins clamped vertically at ends, but floating in Z –Model will be modified to add structural coupling of wafers, and hybrids –Core thickness 5.88m Model of pins and end cap alone with stave weight imposed –0.173in diameter –0.25in diameter Significant Changes –Calculated apparent density of two phase fluid. For entering and exit quality the mean density is 60kg/m 3, whereas liquid density is 1660kg/m 3 –Previous solutions used an average of 1000kg/m 3, so the liquid dead weight is reduced noticeably –Round circular tube in half length model Accommodated the change to 5.88mm core –Varied core shear modulus, reflected in density change to material 66 to 210kg/m 3, CVD carbon foam 56 and 110kg/m 3, honeycomb Models

VG2 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Sandwich Core Differences in Model FEA Models –4.6mm core height model has elongated cooling tubes and the foam does not contact the tubes Hydraulic diameter 5mm Less core material than in the half length model, possibly an effect in sag –5.88mm core height has round tubes and the core comes in contact, except at the very top. Internal diameter 5.27mm Intent is to use the core material to improve thermal contact 4.6mm 5.88mm

VG3 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade FEA Sandwich Core Summary Based on reduced coolant density

VG4 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Core Thickness Estimated stave sag for two core thickness based on bending only, no core shear deflection (analytical based on “fixed end supports”) –Foam Shear Modulus (not included) –4.6mm thick foam (facing separation), δ=35μm –5.88mm thick foam, δ=29μm FEA Solution for Shear Modulus=26.9MPa (lowest density foam) with facings 4 to 1 K13D2U fiber orientation (Coolant density 60kg/m 3 ) –4.6mm, δ=59.4μm (both ends free to move axially) –5.88mm, δ=62.1μm (1/2 length model, since only one end modeled by necessity it simulates as if both ends free to move axially) Little difference in solutions

VG5 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Stave Gravity Sag Conditions –Mass of cable, hybrids, wafers, and chips included in facing density –Mass of two-phase fluid included in tube density –Homogeneous two- phase fluid density average is 60kg/m 3 –C 3 F 8 liquid density is 1660kg/m 3 –Fluid vapor fraction varies from ~0.3 to 0.8 –Virgin RVC foam Core foam density is 66kg/m 3 Peak deflection at stave center is 53.7μm Full Length Model- At One end, pins are Fixed in Z K13D2U 4/1

VG6 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Simple BC at Both Ends Full Length Model- Symmetrical Deflection –Sag increased from 53.7 to 59.4μm (originally one end fixed in Z, now Z fixed in middle) –For same conditions the ½ length model with 5.88mm core thickness was 62.1 μm Sandwich core thickness 4.6mm K13D2U 4/1

VG7 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Sandwich Core CVD Carbon Core foam density is 210kg/m 3 Other Conditions –Mass of cable, hybrids, wafers, and chips included in facing density –Mass of two-phase fluid included in tube density –Homogeneous two-phase fluid density average is 60kg/m 3 –C 3 F 8 liquid density is 1660kg/m 3 –Fluid vapor fraction varies from ~0.3 to 0.8 Peak deflection at stave center is 54.8μm Full length model- One End, pins fixed Fixed in Z K13D2U 4/1

VG8 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Carbon Foam-No CVD Core foam density is 66kg/m 3 Other Conditions –Mass of cable, hybrids, wafers, and chips included in facing density –Mass of two-phase fluid included in tube density –Homogeneous two-phase fluid density average is 60kg/m 3 –C 3 F 8 liquid density is 1660kg/m 3 –Fluid vapor fraction varies from ~0.3 to 0.8 Sandwich height –5.88mm versus 4.6mm Half Length Model-Pins fixed against vertical motion δ=62.1microns K13D2U 4/1

VG9 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Sandwich Core CVD Carbon Core foam density is 210kg/m 3 Other Conditions –Mass of cable, hybrids, wafers, and chips included in facing density –Mass of two-phase fluid included in tube density –Homogeneous two-phase fluid density average is 60kg/m 3 –C 3 F 8 liquid density is 1660kg/m 3 –Fluid vapor fraction varies from ~0.3 to 0.8 Sandwich height –5.88mm versus 4.6mm Peak deflection at stave center is 65μm Half Length Model-Pins free to move axially K13D2U 4/1

VG10 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Carbon Foam-No CVD Core foam density is 66kg/m 3 Other Conditions –Mass of cable included in facing density –Mass of two-phase fluid included in tube density –Homogeneous two-phase fluid density average is 60kg/m 3 –C 3 F 8 liquid density is 1660kg/m 3 –Fluid vapor fraction varies from ~0.3 to 0.8 Sandwich height –5.88mm Half Length Model-Includes Silicon Wafers and Hybrids in stiffness simulation δ=52microns K13D2U 4/1

VG11 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Detectors and Hybrids Stiffness Contribution 1/2 Length Model- K13D2U 4/1 fiber orientation, coolant density 60kg/m 3 –Silicon modules and hybrids as dead weight-62microns –Silicon modules and hybrids part of stiffness-52microns –Mass of 1 st solution kg without module stiffness –Mass of second solution kg with module and hybrid stiffness –Difference in gravity loading 4.1%; had hoped for same mass –Difference in central deflection 19.2%

VG12 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Fiber Orientation Comparing 4 to 1 K13d2U versus Quasi-isotropic K13D2U facings –Modulus in direction of stave axis is different by factor of 1.96 –Thermal distortion solutions with the unbalanced lay up was OK Comparison made for pins free to move in axial direction –Difference between pins fixed on one end and both free is 5.7μm Sag is reduced by a factor of 1.59 K13D2U Quasi-isotropic δmax=94μm K13D2U 4 to 1 lay up δmax=59.4μm

VG13 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Beryllium End Parts Conditions –K13D2U quasi-isotropic fiber orientation –0.173in dia Be pins –Be end cap –Coolant 60kg/m 3 –Pins at end free to move in Z, fixed in Y –Z fixed at mid span, X constrained at two ends Sag decreased from 94.6μm to 80.6 μm through use of Be

VG14 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Solve for Effective Core Shear Modulus 96cm Model of Stave –Use simple edge supports, K13D2U 4/1 –Apply forces at quarter points, ¼ from each end –Extract deflection at Δ 4 and Δ 2, quarter point and mid-span Use relationship Result for 4.6mm core with Al tubes –~128 MPa versus 26.9 MPa for virgin foam –Tubes contribute most of the shear stiffness, except at very high foam densities P/2 hc Δ bending est=36.7μm Δ core shear est=8.2 μm Division between bending and shear, based 0n estimate of core shear of 128MPa Combined Δ=45microns (FEA 53.7 μm for one end of the pins fixed) Using sandwich relationships for fixed ends

VG15 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade Estimate for 2m Stave Use analogy of a uniformly loaded beam –G-core shear properties –L- length of beam –c- height of sandwich core –b- width of sandwich –t- facing thickness –h-overall distance across facings –B- expression –w- uniform load Shear Deflection for 2m stave with 20mm core height quasi K13 facings –G=26.9MPa, δ=56μm –G=212MPa, δ=7μm Based on ~uniform load of 7.9N/m (does include an estimate for mass of 3 internal ribs Bending Deflection estimate for 2m stave –81μm for fixed end condition (fixed) (uniform loading)

VG16 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade

VG17 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade 2m Stave Core Design

VG18 i T i March 9, 2006 W. O. Miller ATLAS Silicon Tracker Upgrade End Cap Model Only Deflection of end cap for ½ stave mass Pin diameter 0.173in δ=.26μm Pin diameter 0.25in δ=.20μm