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WP9 ITS Mechanics and Cooling Corrado Gargiulo 12 March 2014

WP9 ITS Mechanics and Cooling

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WP9 ITS Mechanics and Cooling. 12 March 2014. Corrado Gargiulo . ITS objectives for 2014 – WP9. Finalization of IB and OB layout IB QM design : Space Frame +Cold Plate, End-Wheel, Cylindrical Structural Shell IB BARREL QM production based on “pad chips” - PowerPoint PPT Presentation

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Page 1: WP9 ITS  Mechanics  and  Cooling

WP9 ITS Mechanics and CoolingCorrado Gargiulo

12 March 2014

Page 2: WP9 ITS  Mechanics  and  Cooling

1. Finalization of IB and OB layout

2. IB QM design: Space Frame +Cold Plate, End-Wheel, Cylindrical Structural Shell

3. IB BARREL QM production based on “pad chips”

4. OB QM design: Space Frame, Cold Plate

5. OB STAVE QM production based on “pad chips”

ITS objectives for 2014 – WP9

EM Engineering Module, Qualification Module (final quality)

Page 3: WP9 ITS  Mechanics  and  Cooling

1. Finalization of IB and OB layout

2. IB QM design: Space Frame +Cold Plate, End-Wheel, Cylindrical Structural Shell

3. IB BARREL QM production based on “pad chips”

4. OB QM design: Space Frame, Cold Plate

5. OB STAVE QM production based on “pad chips”

ITS objectives for 2014 – WP9

Page 4: WP9 ITS  Mechanics  and  Cooling

BP outer radius 19

Layer 0 mean radius 23.38

Layer 0 inner boundary >21.8

Middle Layer radius TDR6 / TDR7

Stave width 15+1 (FPC)

Stave length (cold plate) IL 320 (4th IB layer)

IL 290=9.6+270.8+9.6

ML 870= 14.85+840.3+14.85 1066

OL 1502=15.7+1470.6+15.7

(TDR, endorsed)1. Finalization of IB and OB layout Detectors boundary radius@ >21.8mm

Page 5: WP9 ITS  Mechanics  and  Cooling

Beam Pipe NEW DESIGN 19mm OR

Submitted to LEB commitee for approval

Page 6: WP9 ITS  Mechanics  and  Cooling

R 19,0

Gap >2.8 mm No change in the ITS layers radius (TDR)

19.0

ITS VS BP

Page 7: WP9 ITS  Mechanics  and  Cooling

TDR 6

TDR 7

Baseline

Simulation results by the end of March

ITS Outer Barrel

Page 8: WP9 ITS  Mechanics  and  Cooling

1. Finalization of IB and OB layout

2. IB QM design: Space Frame +Cold Plate, End-Wheel, Cylindrical Structural Shell

3. IB BARREL QM production based on “pad chips”

4. OB QM design: Space Frame, Cold Plate

5. OB STAVE QM production based on “pad chips”

ITS objectives for 2014 – WP9

Page 9: WP9 ITS  Mechanics  and  Cooling

Flex Printed Circuit

9 PIXEL Chip

Cold Plate

Spaceframe

Inner layer stave 300mm length, 1.6 gram weight

Polyimide tubes ID 1.024mm; wall thickness 25 micron

Inner Barrel

Page 10: WP9 ITS  Mechanics  and  Cooling

IB Carbon spaceframe

o Stiffness test sag <10 µm

o Thermoelastic test on going

IB

DEVELOPMENT TEST on EM (Engineering Module)o Thermal test OK

10

o Vibrational test >100Hz

167 Hz

status

o Dimensional next

sag

o Production of new spaceframe with high dimensional accuracy new moulds under production

PRODUCTION QM (FINAL QUALITY)

o Production of full barrel (48 staves)

next

Page 11: WP9 ITS  Mechanics  and  Cooling

on going

11

20µ

70µ

20µ

30µ

45µm

(30µ)

45µm

45µm

Alternative option under investigation to further improve stiffness and thermo-elastic stabilityChange of Carbon fleece with K13D2U(same weight)

EM IB Carbon spaceframe

Carbon paper

K13D2U

M60J

Page 12: WP9 ITS  Mechanics  and  Cooling

12

QM IB Connectors

DESIGNo 3D, 2D production drawings OK……need validation fro WP6, needs additional considerations on survey strategy

status

nextPRODUCTIONo 100 CONNECTORSo Design and Production of assembly jig, to glue the connector to the spaceframe

Deisgn modified respect to TDR to increase accuracy

provide staves position accuracy

Page 13: WP9 ITS  Mechanics  and  Cooling

QM IB production Spaceframe+Coldpalte n.48 2014 JULY

Tentative schedule

Page 14: WP9 ITS  Mechanics  and  Cooling

14

QM IB End-Wheels

DESIGNo 3d, OK…

nextDESIGNo Design and Production of molds for layer assembly

status

…need further consideration on cable and piping routing

Page 15: WP9 ITS  Mechanics  and  Cooling

15From Antonello & Antoine

QM IB End-Wheels

Page 16: WP9 ITS  Mechanics  and  Cooling

16

QM IB CYlindrical Support Structure

DESIGNo 3d, OK…

nextDESIGNo Design and Production of molds

status

…needs further consideration on survey targets locations and interface with Service Barrel

Page 17: WP9 ITS  Mechanics  and  Cooling

QM IB production End-Wheels and CYSS 2014 SEPTEMBER

Page 18: WP9 ITS  Mechanics  and  Cooling

Production site Bldg 167 new

… ongoing

CERN GS HSEMaterial HazardFire extinguisher

CERN electrical inspection

Ventillation system installation 90m2 clean environment, 18-23°C, 50% humidity

Page 19: WP9 ITS  Mechanics  and  Cooling

Almost there!

YannickSamuelEvgeny &Viktor

Page 20: WP9 ITS  Mechanics  and  Cooling

1. Finalization of IB and OB layout

2. IB QM design: Space Frame +Cold Plate, End-Wheel, Cylindrical Structural Shell

3. IB BARREL QM production based on “pad chips”

4. OB QM design: Space Frame, Cold Plate

5. OB STAVE QM production based on “pad chips”

ITS objectives for 2014 – WP9

Page 21: WP9 ITS  Mechanics  and  Cooling

Outer Barrel

Page 22: WP9 ITS  Mechanics  and  Cooling

22

DEVELOPMENT TESTo Bending test &FEA sag ≈95µm

o Thermal (150 and 300 mW/cm2), hydraulic test Oko Thermal test on full length coldplate next

o Vibrational test 1st freq=51Hz; dynamic response ongoing

o Thermoelastic test αexp ~ 12 x 10-6 K-

1

On spaceframe (Carbon fiber K13 D2U)

On coldpalte

Outer Barrel stave

o Production of 1 SPACEFRAME+ 2COLDPLATESo Production of EMs

PRODUCTION QM (FINAL QUALITY)

next

status

Page 23: WP9 ITS  Mechanics  and  Cooling

on goingo Improve stave stiffness Full k13 spaceframe has shown to be too brittle N.2 Produced and tested, spaceframe M55j baseline N.2 Produced and tested, spaceframe M55j with additional layer N.2 Produced and tested, spaceframe M55j with two layers

K13D2U(embedded)

EM OB Carbon spaceframe

0 40 80 120 160 200 2400

50

100

150

200

250

M55j

M55J +M55J+K13

sag [mm]

load

[gr]

0 25 50 75 100 125 150

Lumped mass (test)

Distributed mass (derived from test)

3 point bending test results

Confirmed previous test

Page 24: WP9 ITS  Mechanics  and  Cooling

2424

20µ

90µ

20µ

30µ

45µm

30µ

70/45µm

45µm

ID=2.67mm, wt=0.065mm

ID=2.00mm;wt=0.032mm

o Option b) Alternative option under investigation to further improve stiffness and thermo-elastic stability

Mould modified (for ID 2mm), Grenoble New 2mm ID pipes arrived K13 from Berkley arrived

o Production of 1 cold plate 1,5m/ID=2mm/option-ao Production of 1 cold plate 1,5m/ID=2mm/option-bo Production of 1 cold plate 300mm for thermal test

for both option a and b

o Option a) Baseline

on goingEM OB Coldplate

Page 25: WP9 ITS  Mechanics  and  Cooling

SpaceframeQM OB Spaceframe CONNECTOR new design

New design

TDR baseline

Removed spring connection between stave and end-wheels

Ruby sphere

Reference Plane on the End-Wheels

SpringSpring

xx

x

Page 26: WP9 ITS  Mechanics  and  Cooling

26

DESIGNo EM 3D, 2D production drawings

OK… … need to be validated by WP7,8 and by test

status

nextPRODUCTIONo 20 CONNECTORSo Design and Production of assembly jig needed to glue the connector to the spaceframe

QM OB Spaceframe CONNECTOR revised design

Page 27: WP9 ITS  Mechanics  and  Cooling

DESIGNo 3d, 2D production drawings OK……needs validation by WP7,8

status

next

QM OB Cold Plate CONNECTOR

PRODUCTIONo 20 CONNECTORSo Design and Production of assembly jig, to glue the connector to the spaceframe

Page 28: WP9 ITS  Mechanics  and  Cooling

28

EM OB End-Wheels

DESIGNo EM 3d model proposal

status

nextDESIGNo EM 3D design

Page 29: WP9 ITS  Mechanics  and  Cooling

EW

300mm

300mm

300mm

150mm

300mm

Definition of cooling modularity and cooling scheme

Definition of electrical and hydraulic connection layout

DC-DC converter mechanics and cooling

EM OB End-Wheels

DC-DC

P. Kuijer 2014-3-11

Page 31: WP9 ITS  Mechanics  and  Cooling

Next

EM Inner stave & Outer stave -optimize carbon plies lay-up

QM Inner stave & QM Outer stave

-freeze connector design and start production-develop jigs for connector to spaceframe gluing