Global Design Effort Magnetic and Mechanical FEA of SiD IRENG07 Bob Wands September 18, 2007.

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Presentation transcript:

Global Design Effort Magnetic and Mechanical FEA of SiD IRENG07 Bob Wands September 18, 2007

2 IRENG07 Detector concept SiD Brief Review of Solenoid Design Design is based on a scaling of the successful CMS solenoid Six layers of CMS conductor are used vs. four layers for CMS Operating current is amps vs amps for CMS Central Field is 5 T vs. 4 T for CMS Stored energy is 1.4 GJ vs. 2.7 GJ for CMS

3 IRENG07 Detector concept SiD Comparison of Coils – SiD and CMS R = 3.095m CMS (L = 12.5m) R = 2.645m R = 3.098m SiD (L = 5.18m)

4 IRENG07 Detector concept SiD SiD Geometry – End View

5 IRENG07 Detector concept SiD SiD Geometry – Side View solenoid

6 IRENG07 Detector concept SiD Iron Configuration – Effect on Fringe Fields The basic configuration is 11 iron plates, 20 cm thick, in both the barrel and end door regions Gaps between plates are 4 cm Variations on this geometry were examined in two dimensions to determine the features that most affected fringe fields outside the barrel Fringe field requirements have yet to be specified. Could be as low as 5 g close to the magnet, or >100 g. The 2-d axisymmetric models did not include the PacMan shielding iron, or the anti-solenoids For all but one configuration (the “practical design”) no consideration was given as to how to actually build the iron

7 IRENG07 Detector concept SiD The Simplest Configuration (1/4 shown) barrel end door

8 IRENG07 Detector concept SiD Fringe Field - Simplest Configuration ~6 m

9 IRENG07 Detector concept SiD Two Tapered Configurations Fully Tapered Partially Tapered

10 IRENG07 Detector concept SiD Fringe Field - Two Tapered Configurations Fully Tapered Partially Tapered ~ 3 m

11 IRENG07 Detector concept SiD Fully-Tapered Configuration, 22 cm Plates (note change of scale) ~3 m

12 IRENG07 Detector concept SiD End doors must resist axial magnetic force of ~14000 tonnes Dead weight of the iron alone is in excess of 8000 tonnes Crane and space considerations require segmenting of barrel and end door Design must allow for adequate detector coverage while maintaining small deflections Fringe fields must be within specifications Requirements for a Practical Iron Design

13 IRENG07 Detector concept SiD A Practical Iron Design (H.J. Krebs) total weight (barrel + both end doors) = 8300 tonnes ribs – 150 mm thk bolts – between first and last plates only ribs (not visible) end door bears against barrel

14 IRENG07 Detector concept SiD A Practical Iron Design – Magnetic Model

15 IRENG07 Detector concept SiD Fringe Fields – Practical Design 20 cm plates 22 cm plates ~ 3 m

16 IRENG07 Detector concept SiD magnetic pressures totaling tonnes Axial Deflections of End Door - mm

17 IRENG07 Detector concept SiD Stresses in End Door - MPa

18 IRENG07 Detector concept SiD Conclusions Only full tapering with 22 cm plates produces 5 gauss fringe fields near the barrel, but support of end door is problematic Practical iron designs will almost certainly be untapered to some extent for ease of assembly and support If very low fringe fields (~5 g) are required, then thicker iron plates may be called for, increasing weight and cost The practical design considered here is extremely robust, and could probably be optimized to increase space available for detectors