A hollow stave Ian Wilmut – August 2011. LBL stave At the March UG week LBL showed a prototype asymmetric stave. This prompted consideration of the strip.

Slides:



Advertisements
Similar presentations
2x2 module & stave layouts. 2 options “Small chip” “Big chip” Boundary between “small” and “big” is determined by the 6” sensor wafer layout that must.
Advertisements

How to Build a Tree Stump Cache Original Idea by Cedar Bend Gang.
US Bracket Support for Stave D. Lynn (BNL), LBNL Mechanical Meeting, Sep
QA during Stave Core Assembly Stephanie Qing Yang (Oxford) 25 th Sept 2014 WP4 f2f meeting at RAL.
Tube to Foam Interface (Tim). Outline Discuss what’s known about the tube to foam interface – Describe problem – Issues – Theoretical Calculations – Anecdotal.
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.
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.
Vertex Detector Mechanics Bill Cooper Fermilab VXD.
1 Outer Tracker Mechanics, indico: May 2014, A.Onnela 21 May 2014 Thermally conductive carbon-fibre composite material for module and mechanics.
Module mounting Ian Wilmut (RAL). Martin Gibson Martin has been developing the module mounting system at RAL for the last two years – everything we have.
Pixel Upgrade Local Supports Based on Thermally Conducting Carbon Foam E. Anderssen, M. Cepeda, S. Dardin, M. Garcia-Sciveres, M. Gilchriese, N. Hartman,
Mechanical Work Plan Discussion Bill Cooper Fermilab.
M. Gilchriese Update on Pixel Prototype Mechanics/Cooling Structures at LBNL February 1, 2008 M. Cepeda, S. Dardin, M. Garcia-Sciveres, M. Gilchriese and.
Mechanics: Status and Plans Bill Cooper (Fermilab) (Layer 1) VXD.
13 Dec. 2007Switched Capacitor DCDC Update --- M. Garcia-Sciveres1 Pixel integrated stave concepts Valencia 2007 SLHC workshop.
Pixel Support Tube Requirements and Interfaces M.Olcese PST CDR: CERN Oct. 17th 2001.
Update on alignment kit and stave 250 frame M.Gibson (RAL) 1.
SLHC Pixel Layout Studies S. Dardin, M. Garcia-Sciveres, M. Gilchriese, N. Hartman LBNL November 4, 2008.
18 November 2010 Immanuel Gfall (HEPHY Vienna) SVD Mechanics IDM.
26 April 2013 Immanuel Gfall (HEPHY Vienna) Belle II SVD Overview.
Stave Core QC Peter Sutcliffe RAL 24 th Sept 2014.
Raw Material & Sub-Assembly QA (Tim) 25/09/14 25/09/2014Material & Sub-assembly QA1.
ATLAS Upgrade ID Barrel: Services around ‘outer cylinder’ TJF updated According to the drawing ‘Preparation outer cylinder volume reservation’
Calorimeter Analysis Tasks, July 2014 Revision B January 22, 2015.
1 VI Single-wall Beam Pipe tests M.OlceseJ.Thadome (with the help of beam pipe group and Michel Bosteels’ cooling group) TMB July 18th 2002.
Progress on staves – mechanical & thermal. Core and materials.
US Stave Core Production D. Lynn (BNL), LBNL Mechanical Meeting, Sep
Back up stave test program status Eric VIGEOLAS Pixel week December 2000 Pre production status Assembling phase comments Geometrical control Stave Qualification.
VXD Mechanical R&D at the University of Washington H. Lubatti, C. Daly, W. Kuykendall LCRD in conjunction with Fermilab, SLAC.
M. Gilchriese - November 12, 1998 Status Report on Outer Support Frame W. Miller Hytec, Inc E. Anderssen, D. Bintinger, M. Gilchriese LBNL.
Spacecraft Interface/Handling Ring Robert Besuner 12 August 2004.
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.
ACFA-7; Taipei, Nov 2004 H.Weerts status Si licon D etector Status H.Weerts Fermilab/Michigan State Univ. (Progress on Si-tracker layout)
Ideas for LC mechanics (we will work on sensors as well – particular CMOS)
L0 and L1 Structure Deflections During Installation of Silicon Sensors C H Daly 8/24/2003.
Module mounting. Status Stave 250 received… damaged – Repair now complete (see extras) Friday at 8:30 it will be collected by RAL driver and transported.
Berlin talk outline Draft 2 – 7 th March Introduction UK has recently started to systematically try and understand structural requirements and how.
Baby MIND coil modules assembly the aluminium folded strip solution 1 Alexey, Philippe, Gabriella, Helder, Herman Baby Mind Magnet CERN June.
Strip Stave cores Stephanie Yang ATLAS upgrade Oxford activities, January 2015.
Thermo-mechanical petal status Sergio Díez Cornell 23Jan 2015.
Tilt angles reloaded, and status of some other things.
Plank #7 and beyond. 2 What was new for plank#7? Carbon-fibre jig Oversize (by 10mm) facesheets during stave core build –Facesheets now at the very limit.
M. Gilchriese Stave Prototype Status Summary July 5, 2006.
Pixel Upgrade Carbon Foam and Outer Stave Update E. Anderssen, M. Cepeda, M. Garcia-Sciveres, M. Gilchriese, T. Johnson, J. Silber Lawrence Berkelely National.
Local Supports to IDR Discussion ATLAS Upgrade Week November 2014.
Jan. 28, 2014W. Bertl, PSI BPIX Cooling Status W. Bertl, PSI.
Stave programme. 2 Staves recently build Stave#7 –I think is at QML –Intend was to aggressively thermally cycle and look for structural issues Stave#8.
Mechanics R&D Ian Wilmut. Talk Scope This talk is to provoke conversation – not to direct activities. The slides should do no more than start the conversation.
Some Comments on the Use of CGL for the Foam-Pipe Interface 1 D. Lynn (BNL), LBNL Mechanical Meeting, Sep 2012 We have been using CGL exclusively in the.
1.2 m Stave with Co-cured Facings Using Low Areal Density Fiber G. Viehhauser (Oxford) C. Haber (LBNL) T. Hurteau, W. Emmet (Yale) R. Rurns, D. Lynn (BNL)
Stave #12 This stave core was built together with William Emmet, Tom Hurteau, and Jeffery Ashenfelter from Yale University in the week of November.
Comments on Engineering talk by A. Catinaccio at Inner Tracker Engineering Meeting CERN ) Fixed length barrel layout drawing by C. Bault (Strawman.
(Tim Jones).  Who am I? ATLAS-UK Tracker Upgrade work-package leader for WP4 (Mechanics)  Materials, Cooling, Stave Core Assembly, Module Mounting,
HE NgCCM integration issues Ianos Schmidt, August 26, 2015.
B [OT - Mechanics & Cooling] Stefan Gruenendahl February 2, 2016 S.Grünendahl, 2016 February 2 Director's Review -- OT: Mechanics &
1 IST development status  Seattle  Composite Design.
24 September 2012 Immanuel Gfall (HEPHY Vienna) SVD Status of Mechanics PXD-SVD Meeting Göttingen.
24 September 2012 Immanuel Gfall (HEPHY Vienna) Annekathrin Frankenberger (HEPHY Vienna) SVD Status of Mechanics PXD-SVD Meeting Göttingen.
SPS High Energy LSS5 Thermal contact & cooling aspects
EC: 7 DISK concept Preliminary considerations
Micro Vertex Detector of PANDA Status of Strip BARREL and DISC
Are there better ways to build a stave?
Local Supports for Inclined Layout: CERN Update
A comparison of Some Properties of Sandwich Test Tokens with Various Core Materials (Tim)
Sensor Layout Options Aim is to understand the implication and constrains of possible sensor design/layout on the general ID Layout. Keep both ATLAS “drum”
Mechanics: (Tim).
Materials qualification meeting
Equipment for Assembly – UK Experiences
WG4 – Progress report R. Santoro and A. Tauro.
Presentation transcript:

A hollow stave Ian Wilmut – August 2011

LBL stave At the March UG week LBL showed a prototype asymmetric stave. This prompted consideration of the strip stave to see if some of the same ideas could be applied. This is being looked at in the context of the 45gsm UD K13D2U If the fibre needs to bend around a 5mm radius the stiff fibre must approach the bend at 15° to the axis of the radius (assumes a 25mm minimum bend radius)

The basic idea Build a stave from skins, but leave out the core and instead install simple tubes that form both the skin to skin coupling and the close outs in one. The tubes should also contribute to the thermal path from the periphery of the stave to the Pocofoam. Because the contact areas between elements are large, flat and thin they are good candidates for co-curing. Thus it might be possible to eliminate most of the cold cure adhesives. This would serve to save the material overhead of the glue.

Proposed Structure Four tubes are made around mandrels as per the US Pixel structure, there are two layups that will result in CW and CCW twist on one member of each type Two skins are also made as asymmetric layups. Again one will twist CW and one CCW – this is not central to the idea, but a ±15° skin will curl less than a 0-90° one. The stave could then be assembled using a 0° layer (in red) as a glue layer. It would need the mandrels back in the tubes and outer platterns The gluing of the Poco Foam needs a lot more consideration It would be desirable to glue poco to tubes at the sides with a “heat proof” adhesive to constrain thermal load of the pipe. K13D2U +15° K13D2U -15° K13D2U 0° K13D2U -15° K13D2U +15° K13D2U –15° K13D2U +15° K13D2U -15° K13D2U +15° K13D2U -15° K13D2U –15° K13D2U +15°

Benefits Loss of cold cure glue, saving on “non-productive” material. The close outs become an integrated part of the design. The fibres in the tubes should serve to conduct heat from the hybrids into the poco-foam. – Note, it could be expected that the ends of the stave might be warmer as not as many fibres conduct to the foam (~75mm). There might be a saving of material from this design – depending on how thin the skins can be made. The skins should be able to be made very flat and smooth to minimise the amount of glue needed below the modules. As the fibres in the skins are no longer at 0° and 90° the widthways and length ways performance can be tuned to have appropriate length and widthways performance. ±15° fibres provide 75:25% lengthways: widthways split in performance. So 4 layers at ±15° perform as 0,0,0,90 but can be made symmetric to alleviate curling during cure

Drawbacks When the modules are mounted a “filler” will probably be needed to support the tube. This design has may cases of asymmetric fibre layups so many parts will be twisted or bowed before they are integrated, and it might be that if the final assembly stage is a co-cure then the final object contains distortions. There are less width wise fibres so the thermal performance might be lower – it is expected there will be the equivalent of one widthways thin layer of fibres.

Additional Locking points would clearly not seem to be immediately compatible – however if a cut out was added to the outer edge the present design could be installed in much the present way The end close outs would have to be carefully considered. It is obvious that they can only be present at one end (probably z=0). The forms to build the tubes have been shown by LBL to be successfully made from Aluminium. Here the high CTE of aluminium allows there removal once the structure has cooled The module mounting forms need to be able to expand to fill the appropriate tube as the fit will need to be excellent to prevent excess glue use during module mounting.

Conclusion Simple FEA and study of material follows in additional presentation This looks like it might be feasible, but unless offers concrete improvements to the present design is probably not worth worrying about. To understand if it is worth pursuing it will be necessary to: – Understand thermal performance – including ends – Understand mechanical performance – Prototype small section