MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

61
MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by Wing Lau --with input from AFC group members

description

MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by Wing Lau -- with input from AFC group members. Status of Progress. Status of Progress. Comp. Status of Progress. Heater/thermometer assemble for MICE absorber. AL. block. CX-1050-SD. - PowerPoint PPT Presentation

Transcript of MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Page 1: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

MICE Collaboration meeting at Berkeley

9 – 12 February 2005

AFC Module progressPresented by

Wing Lau --with input from AFC group members

Page 2: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG/YI/ SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 3: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 4: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Window QC – round robin exercise WL Work is on-going. On-going

Understand QC requirements for absorber windows and assign oversight responsibility

WL Need to discuss with the group on who is the best person to do this

On going

Hydrogen system R&D TB / EB

Progress being made. See the previous summary talk.

On --going

Page 5: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG/ YI/ SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 6: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

TOF0 Chev 2 TOF 1&2 Magnetic Shield

Detector Module

Radiation Shield

AFC modules

1 & 3

Coupling Modules

1 & 2

visible ☑ ☑ ☑ ☑ ☑ ☑ ☑

Comp.

Page 7: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG / YI / SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 8: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Heater/thermometer assemble for MICE absorber

HTR-25-100CX-1050-SD

AL. block

Page 9: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Thermometers in absorber

AC Bridge 370S

CX-1050-SD 3716; 16ch Scanner

Page 10: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

L-H2/LHe Level sensor in absorber

CX-1050-SD

DC ~mA

V4

V3

DC Current for L-H2/LHe should be optimized (KEK R&D).

LHeLH2

Page 11: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Wiring of thermometers, level

sensor & heaters

4 wires measurement for thermometers and heaters

AC Bridge 370S with16ch Scanner

Max. 16 CH

6 for absorber (8 6, 2 at top )

2 for windows

2 for LH2 pipes

2 for C-He pipes

3 for Cryocooler

1 for magnet bore

Page 12: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

PC

MICE absorber   monitor/control (R&D at KEK, plan)

IEEE-488/RS232C

Keithley 2700

READ OUTS

16 CX-1050SD’s 3-HTR5-CX-1050

P&VAC Sensors

Abs. HTR-UPCRYOCOOL HTR

DCPS

Abs. HTR-DWN

LAN

Abs. LEVELCX-1050

0.1mA

CRYOSTAT

Inside Abs.

DCPSDCPS

cc1mA

Page 13: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

PC / WS

MICE absorber  monitor/control (plan)

IEEE-488

Keithley/ADCAC Bridge 370S DCPS

READ OUTS

16 CX-1050SD’s

DMR 1-6

3-HTR5-CX-1050

P&VAC&LEVEL Sensors

Abs. HTR-UP

CRYOCOOL HTR

Programmable Controller or LOGIC

DIO

ALRAM, VALVES, CRYOCOOLER-OFF, HEATER-OFF…

DCPS DCPS

Abs. HTR-DWN

LAN

Abs. LEVELCX-1050

cc1mA

DIRECT CONTROL

CRYOSTAT

Inside Abs.

Contacts

2CH

Page 14: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Digital meter relay for MICE absorber/Cryocooler

DMR; DIGITAL METER RELAY (Digital comparator) Watanabe (Japan) for example

INPUTWSM-452HR-R3NNNX-22VD ; DC 0-199.99 mVWSM-452HR-R3NNNX-32VD ; DC 0-1.9999 VWSM-452HR-R3NNNX-42VD ; DC 0-19.999 VWSM-452HR-R3NNNX-52VD ; DC 0-199.99 V

OUTPUT( 4.5 digit set)HI-relay (NC, HO)LO-relay (NC, NO)

Scaling; A-B (V) C-D (Unit)

DC24V

Page 15: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG/YI/ SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 16: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Case No.Forces (MN)

AFC 1 RFCC 1 AFC 2 RFCC 2 AFC 3

1 -0.088 -0.214 0 0.214 0.088

2 0.037 0.186 0 -0.186 -0.037

3 0 -0.211 0 0.211 0

4 -0.398 0 0 0 0.398

5 0.312 -0.313 0 0.313 -0.312

6 -0.084 0.095 -0.313 0 0.401

7 -0.0878 -0.2213 0.0009 0.3057 -0.3121

Force profile received from Yury in January 2005

Page 17: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

MICE cooling channel FEA model with the loading and boundary conditions

Case 1: Forces (in MN) for Flip mode, Stage 6, p=240 MeV/c, β=42cm

Page 18: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Max reaction force in Y direction at the support base is 44548 N

Case 1: vertical reaction force

-50000

-40000

-30000

-20000

-10000

0

10000

20000

30000

40000

50000

1 2 3 4 5 6 7 8 9 10

reac

tio

n f

orc

es N

case 1: horizontal reaction forces

-40000

-30000

-20000

-10000

0

10000

20000

30000

40000

1 2 3 4 5 6 7 8 9 10

rea

cti

on

fo

rce

s N

Case 1: FEA result

Page 19: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Super-module reaction forcesAFC AFC RF/CC RF/CC AFC AFC RF/CC RF/CC AFC AFC

foot Pos1 2 3 4 5 6 7 8 9 10

Normal OperationCase 1 Flip y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4

240Mev/c ymag -0.8 0.8 -4.4 4.4 0.0 0.0 4.4 -4.4 0.8 -0.8y force/foot -1.2 0.4 -5.6 3.2 -0.4 -0.4 3.2 -5.6 0.4 -1.2z force/foot zmag 0.2 0.2 2.8 2.9 0.0 0.0 -2.9 -2.8 -0.2 -0.2z force/side 0.4 5.7 0.0 -5.7 -0.4

Case 2 Non flip y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4240 ymag 0.5 -0.5 3.2 -3.2 0.0 0.0 -3.2 3.2 -0.5 0.5

y force/foot 0.1 -0.9 2.0 -4.4 -0.4 -0.4 -4.4 2.0 -0.9 0.1z force/foot zmag -0.1 -0.1 -2.0 -2.2 0.0 0.0 2.2 2.0 -0.1 -0.1z force/side -0.2 -4.2 0.0 4.2 -0.2

Symmetric QuenchCase 3 AFC Q y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4

ymag -0.3 0.3 -3.1 3.1 0.0 0.0 3.1 -3.1 0.3 -0.3y force/foot -0.7 -0.2 -4.3 1.9 -0.4 -0.4 1.9 -4.3 -0.2 -0.7z force/foot zmag 0.1 0.1 2.0 2.0 0.0 0.0 -2.0 -2.0 -0.1 -0.1z force/side 0.2 4.0 0.0 -4.0 -0.2

Case 4 CC Q y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4ymag -1.9 1.9 -5.5 5.5 0.0 0.0 5.5 -5.5 1.9 -1.9

y force/foot -2.3 1.5 -6.7 4.3 -0.4 -0.4 4.3 -6.7 1.5 -2.3z force/foot zmag 0.5 0.5 3.1 3.8 0.0 0.0 -3.8 -3.1 -0.5 -0.5z force/side 1.0 6.9 0.0 -6.9 -1.0

Case 5 DET Q y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4ymag 0.9 -0.9 -0.4 0.4 0.0 0.0 0.4 -0.4 -0.9 0.9

y force/foot 0.4 -1.3 -1.6 -0.9 -0.4 -0.4 -0.9 -1.6 -1.3 0.4z force/foot zmag -0.3 -0.3 0.4 0.2 0.0 0.0 -0.2 -0.4 0.3 0.3z force/side -0.5 0.5 0.0 -0.5 0.5

Non Symmetric QuenchCase 6 CCQ y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4non sym ymag -0.2 0.3 -0.5 0.7 -0.1 0.3 4.4 -4.5 1.7 -1.8

y force/foot -0.6 -0.1 -1.7 -0.5 -0.5 -0.1 3.2 -5.7 1.3 -2.2z force/foot zmag 0.1 0.1 0.6 0.6 0.1 0.1 -3.0 -2.5 -0.5 -0.5z force/side 0.2 1.2 0.2 -5.5 -1.0

Case 5 DET Q y grav -0.4 -0.4 -1.2 -1.2 -0.4 -0.4 -1.2 -1.2 -0.4 -0.4non sym ymag -1.3 1.4 -9.3 8.4 -0.4 0.5 -3.8 3.9 -1.4 1.5

y force/foot -1.7 1.0 -10.5 7.2 -0.8 0.1 -5.0 2.7 -1.8 1.1z force/foot zmag 0.3 0.3 5.0 5.0 0.2 0.2 2.0 1.8 0.4 0.3z force/side 0.6 10.0 0.4 3.8 0.7

Page 20: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Rail – mounting concept

Combined Roller Bearing

Page 21: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Force transfer concept - Y

Page 22: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG/YI/ SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 23: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Ulisse Bravar26 January 2005

•This note presents the optic solutions for MICE Step III for a large number of different running conditions.

•Two gap distances between the two spectrometers are considered, 800 mm and 1600 mm.

•For the 800 mm gap, a table with forces and peak fields on coil surfaces for the worst case scenarios is

attached, courtesy of H. Witte

•For the 1600 mm gap, all currents in the MICE coils are equal to or less than the worst case currents of the 800 mm

gap.

•Hence, for the 1600 mm case, forces and peak fields are also lower than the ones in the 800 mm case.

•In conclusion, currents, peak fields and forces both in the 800 mm and in the 1600 mm gaps are within

tolerances.

Page 24: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG/YI/ SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 25: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Implement central repository for drawings -- need detector information to add to official drawing

WL Basically complete. On-going liasing with Mississippi on CKOV1 drawings; with Tortora on Calorimeter etcDiffuser still to be addedHyperlink to drawing gallery is now available

Done.

Instrumentation for absorbers must be specified and incorporated into design (temperature sensors, liquid level sensors, …)

SI Proposal now available (see Shigeru’s summary talk) and will be discussed among the AFC group as an on going action for Absorber R&D

Done

Define absorber heater implementation YI / SI Ditto

Done

Continue working to define worst-case magnet forces and collect magnet design notes into design report

MG/YI/ SY

Yury and the team at RAL has now completed that work. Stephanie completed the FEA on forces and displacements. We are now homing in on the rail and anchoring design details

Done

Check if a 1600mm gap between AFC & Tracker matching coils

WL/ UB

Ullisee has completed the calculations and advised that either gap distance (800mm or 1600mm) is acceptable as far as forces and current density are concerned. However, the group has a preference to the 800mm gap.

Done

Revise absorber vent pipe size to make it adequate for He case

WL Agreed to increase this to 15mm diameter. Drawing being updated

Done

Get RAL seismic design criteria and verify that designs meet them

WL/ PD

This is not considered significant as RAL site has relatively low floor response. A static “G” of 0.3 would be sufficient for all components with a natural frequency of above 33Hz.

Complete.

Status of Progress

Page 26: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 27: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by
Page 28: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 29: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 30: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 31: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

T2

T02nd Stage Cold Head

Condensation Plate

Absorber Vacuum Vessel

Liquid Tube (15 mm ID Cu)

Copper Strap

Liquid Hydrogen

Gas Tube (15 mm ID Cu)

Vent Tube 304 St St 15 mm ID

1st Stage Cold Head

50 K Shield

5 mm ID 304 St St H2 Fill Pipe

H2 Fill and Return Valve

T4

T3

60 K Exhchanger for H2 Cooling

He Cool Down Pipe 304 St St

T5

LH2 Absorber

H2 Gas Vent

Small Cooler

30 mm ID H2 Vent Tube 304 St St

Ball Valve For He Transfer Line

T1

Seal for Transfer Tube

H

H

H

Absorber Heater (one or two)

2nd Stage Heater (two)

1st Stage Heater

P

Liquid Fill Vent Valve

4 liter Buffer Volume

Rupture Disc

Fill Neck 304 St St

Page 32: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Hydrogen System Baseline layout

Pressuregauge

Non-returnvalve

-P P VP Vacuum pumpBursting diskPressure

relief valveValvePressure

CoolantOut In

Metal Hydride storage unit

(20m3 capacity)

Purge valve

0.5 bar

0.9 bar

H2 Detector

P

P

VP1

VP2

Purge valve

Chiller/Heater Unit

1 bar

PP

0.5 bar

0.9 bar Helium supply

Hydrogen supply

High level vent

Buffer vessel

Vent outsideflame arrester

Extract hoodH2Detector

PP

Nitrogen supply

PP

PP

1 m3

Hydrogen zone 2

Vent manifold Vent manifold

P1

PV1

PV7

PV8

PV2

PV3

PV4

HV1

Fill valve

Tbed

HV2

HV3

P3

P

P2

PV6

High level vent

Non returnvalve

0.1 bar

-P P VP Vacuum pumpBursting diskPressure

relief valveValvePressure

regulator

CoolantOut In

Absorber window

Metal Hydride storage unit

(20m3 capacity)

Purge valve

0.5 bar

0.9 bar

H2 DetectorH2 Detector

P

P

VP1

VP2

Purge valve

Chiller/Heater Unit

1 bar

PP

0.5 bar

0.9 bar Helium supply

Hydrogen supply

High level vent

Buffer vessel

Vent outsideflame arrester

Extract hoodH2DetectorH2Detector

PP

Nitrogen supply

PP

PP

1 m3

Hydrogen zone 2

Vent manifold Vent manifold

P1

PV1

PV7

PV8

PV2

PV3

PV4

HV1

Fill valve

Tbed

HV2

HV3

P3

P

P2

PV6

High level vent

Non returnvalve

0.1 bar

Safety window

Page 33: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 34: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 35: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Model

Page 36: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Absorber thermal model

Page 37: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 38: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Case No. Max stress MPa

Max displacement mm

Max horizontal reaction force N

Max vertical reaction force N

1 37 0.114 29148 44548

2 28 0.075 21588 33201

3 26 0.063 20672 31797

4 89 0.291 37005 55633

5 70 0.164 3747 9213

6 88 0.28 66833 46302

7 69 0.22 50698 85550

FEA result summary

Page 39: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

Detail arrangement is still being worked out between KEK & RAL

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 40: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Absorber test cryostat ATC-002 (dimensions)

MICE

(needs larger Cryocooler flange for pips)

D2; Cryocooler flange

W W

H2

H1

D1

Page 41: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

July 05

Oct 05

Jan 06

Apr 06

July 06

Oct 06

Jan 07

Apr 07

Phase 1 deliverable fully installed &

tested

Thermal performance test on 1st absorber (KEK)

Thermal performance test on 2nd absorber

Thermal performance test on 3rd absorber

Absorber R & D

Initial design

Detailed design & procurement

Installation & commissioning

Test programme

Prelim. D & S review

Hydrogen system R&D

KEK test cryostat comes to RAL

Permission to operate

Page 42: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 43: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Lab G Solenoid Power Supplyand Quench Protection

PS

Mandrel

Magnet

Warm Resistor

Warm Diode

Power Supply 10 V, 300 A

Cryostat

Page 44: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

PSPower Supply 10 V, 300 A

Total Inductance from 295 H to 410 H

The MICE Coupling Coil Power Supplywith Quench Protection

Page 45: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

The MICE Coupling Coil Power Supplywith Quench Protection

PS

Power Supply 10 V, 300 A

Coupling Magnet

Mandrel

Cold Diode

Cold Resistor

Inductance = 563 H

Note: The coil is shown split into two parts. The coil may besplit into three or four parts instead of two parts.

Page 46: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Detector Magnet Power Supplies

PSPower Supply 10 V, 300 A

PS PSPS PS

Power Supply 10 V, 50 A

Match 1 Match 2 End 1 Center End 2

Page 47: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Concluding Comments on Quenches

• The focusing and coupling magnets will have passive quench protection. The detector magnet will likely have an active quench protection system.

• The three focusing magnets should be in series.

• Each coupling magnet should have its own power supply to reduce the charge time.

• Like detector magnet coils can be put in series.

• A coupling coil quench will quench the rest of MICE. A focus coil quench will not quench a coupling coil.

Page 48: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate merits of cryocooler heater vs. 3-stage cooler w/o heater

MG Concluded that this is no longer an option for our current design

Done

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Finalize interface between radiation shield and detector module- must forces be transmitted

WL Stephanie has done the calc. Forces and displacement s at modules are acceptable for the 7 cases being considered.

Done

Consider participation in KEK and/or Fermilab absorber tests (some coordination maybe called for)

YI / SI

MICE Absorber R&D will be carried out at KEK for the 1st absorber. We are still in discussion with Shigeru on whether the thermal test of the 2nd & 3rd absorbers should be done at KEK or RAL.

On-going

Evaluate magnet interaction during quench-- does one quench induce others

EB / MG

Work is by and large complete. It shows that the 3 focus coils should be powered in series. The 2 Coupling Coils could be powered up either in series or separately.

Done

Raise Change note on the radiation shield design

SY / WL

Done Done

Page 49: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Window QC – round robin exercise WL Work is on-going. On-going

Understand QC requirements for absorber windows and assign oversight responsibility

WL Need to discuss with the group on who is the best person to do this

On going

Hydrogen system R&D TB / EB

Progress being made. See the previous summary talk.

On --going

Page 50: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Task Description

An AFC Module window that was damaged during machining was used to test a non-contact measurement method. A standard CMM was also used for comparison. All measurements were made on both sides of the window with the thickness being determined indirectly from the two sets of data. Measurements consisted of 12 radial slices at 15º increments. The center 80 mm of the window is damaged.

Measurement Methods•Standard CMM with low contact force•Vision machine with medium magnification lens•Vision machine with high magnification (not yet complete)

Summary of Results•Best data obtained from CMM measurement•Vision machine data shows more scatter•Good portion of window is within 40 m of design thickness

Page 51: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Standard CMM Measurement Vision Machine Measurement

Page 52: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by
Page 53: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Discussion

• The vision machine works best when measuring horizontal, smooth surfaces

• The combination of a sloped surface and machining grooves in the window is likely responsible for the data scatter

• Preliminary results indicate that the higher magnification lens may provide better results than the medium lens

• Overall, the best results are achieved using contact CMM

• The following method would provide the highest accuracy: Contact CMM using a low-force tip and appropriate

approach angle resulting in no window deflection The window mounted vertically to allow a single set-up

Page 54: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Window QC – round robin exercise WL Work is on-going. On-going

Understand QC requirements for absorber windows and assign oversight responsibility

WL Need to discuss with the group on who is the best person to do this

On going

Hydrogen system R&D TB / EB

Progress being made. See the previous summary talk.

On --going

Page 55: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Window QC – round robin exercise WL Work is on-going. On-going

Understand QC requirements for absorber windows and assign oversight responsibility

WL Need to discuss with the group on who is the best person to do this

On going

Hydrogen system R&D TB / EB

Progress being made. See the previous summary talk.

On --going

Page 56: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Window QC – round robin exercise WL Work is on-going. On-going

Understand QC requirements for absorber windows and assign oversight responsibility

WL Need to discuss with the group on who is the best person to do this

On going

Hydrogen system R&D TB / EB

Progress being made. See the previous summary talk.

On --going

Revised Action list

Page 57: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Action Who Progress made status

Evaluate the need for redundant LH2 relief paths

EB / TB

This is part of the on-going R&D activity on the Hydrogen System R&D.

On-going

Evaluate absorber heat load with more realistic assessment of surrounding temperatures (is proposed MLI adequate?)

EB/MG/SY

Thermal model set up. Elwyn and his team are making progress on this

On-going

Evaluate stresses at module interconnect flanges and bolts

SV Steve Verostek had done detail FEA on bolt / flange connection and the work is still on-going

On-going

Define RFCC module tie-in to rail system SV This is now in he hands on the RAL design team

On-going

Work out gusset arrangement to transfer CC forces to RFCC module vacuum shell.

SV Await Mike Green to finalise the Cold Mass support arrangement before deciding on how and where to put these gussets

On-going

Window QC – round robin exercise WL Work is on-going. On-going

Understand QC requirements for absorber windows and assign oversight responsibility

WL Need to discuss with the group on who is the best person to do this

On going

Hydrogen system R&D TB / EB

Progress being made. See the previous summary talk.

On --going

Obtain magnet force on AFC module during Stage IV test when only one AFC module is placed between the two detector solenoids

EB / SY

Initial guess is that the force is in the region of 30 tons. Force calculation will be carried out to verify this number. A new temporary bridging plate will be designed for the Stage IV test

New action

Revised Action list

Page 58: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Stage IV arrangement – 2 tracker solenoids + 1 AFC module in between

Page 59: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Magnet force of approx. 30 Tons due to asymmetric quench of magnets

Magnet force of this magnitude may cause excessive bending here

Page 60: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by
Page 61: MICE Collaboration meeting at Berkeley 9 – 12 February 2005 AFC Module progress Presented by

Temporary bridging pieceReinforcement

gussets