This is the low power SPL (LP-SPL) optimized for PS2 and LHC. Length: ~430 ...
1.2. 0.8 (2.5 GeV) + 0.4 (5 GeV). HP-SPL beam characteristics. ~500 m. 5 GeV ...
Status of the SPL cryo-module development V.Parma, TE-MSC (with contributions from WG3 members)
SPL seminar, CERN 18th February 2010
Content • SPL architecture and parameters • Work organisation • Layout studies and machine sectorisation (vacuum+cryogenics) • Cryogenic scheme (for the prototype) • Supporting schemes • Next steps • Summary
Layout injector complex SPS
PS2 ISOLDE
PS
SPL
Linac4
The SPL study Goals of the study (2008-2012): • Prepare a Conceptual Design Report with costing to present to CERN’s management for approval • This is the low power SPL (LP-SPL) optimized for PS2 and LHC
10 x 6 β=0.65 cavities
High β cryomodules
5x8 β=1 cavities
High β cryomodules
13 x 8 β=1 cavities
Kinetic energy (GeV)
LP-SPL beam characteristics
Debunchers
To PS2
Medium β cryomodule
427 m 4 GeV
Ejection
186 m 1.4 GeV
110 m 0.73 GeV
TT6 to ISOLDE
From Linac4
0m 0.16 GeV
Length: ~430 m 4
Beam power at 4 GeV (MW)
0.16
Rep. period (s)
0.6
Protons/pulse (x 1014)
1.5
Average pulse current (mA)
20
Pulse duration (ms)
1.2
The SPL study (cont.d) • Study a 5 GeV and multi MW high power beam, the HP-SPL • Major interest for non-LHC physics: ISOLDEII/EURISOL/Fixed Target/Neutrino Factory
6x8 β=1 cavities
Option 1
Option 2
2.5 or 5
2.5 and 5
3 MW (2.5 GeV) or 6 MW (5 GeV)
4 MW (2.5 GeV) and 4 MW (5 GeV)
Rep. frequency (Hz)
50
50
Protons/pulse (x 1014)
1.5
2 (2.5 GeV) + 1 (5 GeV)
Av. Pulse current (mA)
20
40
Pulse duration (ms)
1.2
0.8 (2.5 GeV) + 0.4 (5 GeV)
Energy (GeV) Beam power (MW)
~500 m 5 GeV High β cryomodules
Debunchers
To PS2
High β cryomodules
Ejection
5x8 β=1 cavities
~300 m 2.5 GeV
to Eurisol
10 x 6 β=0.65 cavities
High β cryomodules
186 m 1.4 GeV Ejection
Medium β cryomodule
110 m 0.73 GeV
TT6 to ISOLDE
From Linac4
0m 0.16 GeV
12 x 8 β=1 cavities
Length: ~500 m
HP-SPL beam characteristics
Cryo--module: Goal & Motivation Cryo Goal: • Design and construct a full-scale cryo-module prototype (part of the SPL Design Study) Motivation: • Develop technologies and demonstrate construction capability on a cryo-module with 8 β=1 cavities • Learning of the critical assembly phases (e.g. clean-room) • Enable RF testing on a multi-cavity assembly in real operating conditions (horizontal cryostat) • Investigate and acquire experience on cryogenic operation issues (e.g. process control)
Working group (WG3) members System/Activity
Responsible/member
Lab
Machine architecture
F.Gerigk
CERN, BE/RF
WG3 coordination
V.Parma
CERN, TE-MSC
Cryo-module conceptual design & Integration
V.Parma, N.Bourcey, A.Vande Craen, D.Caparros, P.Coelho, Th.Renaglia
CERN, TE/MSC, EN-MME
Cryostat detailed design
P.Duthil
CNRS/IN2P3-Orsay
Cryostat assembly tooling
S.Chel
CEA-Saclay
WG 2 activity (RF cavities/He vessel/tuner, RF coupler)
W.Weingarten/S.Chel/O.Capatina/ CERN BE/RF, CEA-Saclay E.Montesinos
Vacuum systems
S.Calatroni
CERN, TE/VSC
Cryogenics
U.Wagner
CERN, TE/CRG
Survey
D.Missiaen
CERN, BE/ABP
Quad.doublet
D.Tommasini
CERN, TE/MSC
Activity of WG 3 • Regular WG meetings since May 2009 – Web page: https://twiki.cern.ch/twiki/bin/view/SPL/CryoModules
• Topics covered (or in progress): – – – – – –
Cryomodule longitudinal study SPL mechanical layouts Sectorisation issues Cryogenic cooling schemes Integration of RF Coupler Cryo-module design: supporting systems, thermal shielding,...
• Close collaboration with WG2 (cavities and ancillaries) • Relevant workshops 2009: – Workshop on Mechanical issues of SPL cavities/cryomodules: http://indico.cern.ch/conferenceDisplay.py?confId=68968 – Workshop on Cryogenic and vacuum sectorisation of the SPL: http://indico.cern.ch/conferenceDisplay.py?confId=68499
• Coming up soon (16-17 March): Review of the RF Couplers
Planned supplies for prototype cryocryo-module Institute
Responsible person
Description of contribution
CEA – Saclay (F)
S. Chel
1. Design & construction of 2 β=1 cavities (EuCARD task 10.2.2) 2. Design & construction of 2 helium vessels for β=1 cavities (French in-kind contribution) 3. Design & construction of cryostat assembly tools (French inkind contribution) 4. Supply of 8 tuners (French in-kind contribution)
CNRS - IPN – Orsay (F)
P. Duthil
1. Design and construction of prototype cryomodule cryostat (French in-kind contribution)
Stony Brook/BNL/AES team
I.Ben-zvi
(Under DOE grant) 1. Designing, building and testing of 1 β=1 SPL cavity.
CERN
O.Capatina
1. 8 β=1 cavities 2. 7 He tanks in titanium 3. 1 He tank in st.steel
CERN
E.Montesinos
1. 10 RF couplers (testing in CEA, French in-kind contribution)
Cryo-module Cryolongitudinal integration study (β (β=1) =1)
+
Longitudinal mechanical layouts «Continuous» vs. «fully segmented» cryostat SPL layouts Continuous cryostat "Compact" version (gain on interconnections):
è 5 Gev version (HP): SPL length = 485 m (550 m max available space)
"Warm quadrupole" version (with separate cryoline):
è 5 Gev version (HP): SPL length = 535 m
(550 m max available space)
CRYOGENICS AND VACUUM SECTORISATION Outcome of workshop on cryogenic and vacuum sectorisations of the SPL (November 9-10, 2009)
Possible cryogenic feeding: “continuous” cryostat Cryo-plant
Isolde extraction
CIB
Cryogenic Interconnect Box Cryo Unit Cryogenic bridge
Eurisol extraction
“continuous” cryostat • • • •
“Long” and “continuous” string of cavities in common cryostat Cold beam tube “straight” cryogenic lines in main cryostat common insulation vacuum (between vacuum barriers, if any present)
String of cryo-modules between TSM Technical Service Module (TSM) Cold-Warm Transition (CWT) Insulation vacuum barrier Warm beam vacuum gate valve
Possible cryogenic feeding: Cryogenic Distribution Line Cryo-plant
Isolde extraction
CIB
Cryogenic Interconnect Box Cryo-module Units Cryogenic Distribution Line
Eurisol extraction
“segmented” cryostat • • • •
Cryostat is “segmented”: strings of (or single) cryo-modules, 2 CWT each Warm beam zones Cryogenic Distributio Line (CDL) needed Individual insulation vacuum on every string of cryo-module (Vacuum Barriers, w.r.t. CDL) Cryogenic Distribution Line (CDL) String of (or single) cryo-modules Technical Service Module (TSM) Cold-Warm Transition (CWT) Insulation vacuum barrier Warm beam vacuum gate valve
Main issues •
Machine availability: –
•
“work-horse” in the injection chain
Reliability of built-in components and operational risks – Typical faults expected on: cavities, couplers, tuners... – Operation with degraded performance (cavities, optics, leaks...)
•
Maintainability: – Warm-up/cool-down . Time and reliability. Need for partial or complete warm-up of strings to replace built-in components or even one cryo-module – Accessability of components for regular maintenance or repair
•
Design complexity of compared solutions
•
Operational complexity (e.g.cryogenics with 1.7% slope)
•
Installation and commissioning
•
Safety. Coping with incidents (MCI): Loss of beam and/or insulation vacuum (helium and air leaks):
•
Cost differences between options
VACUUM
SPL Sectorisation Variants
Continuous
Segmented Option A
Segmented Option B
Vacuum sectorisation
22
09/11/09
Summary: comparison of vacuum aspects Drawbacks
Advantages
Drawbacks
-Compact long.layout -fewer components -Reduced vac systems (integrated He lines)
- Long beam vacuum sectors , cold sector valves don’t exist! - Some sensitive equipment needs vacuum compatibility and validation
-Modular design - Easier access, repairs, upgrades - Modules are complete & tested before installation
-More vacuum components (eg CWT) -More vacuum instrumentation
-Insulation vacuum systems are exposed to tunnel environment - Beam/cavity vacuum more exposed?
-Minimize tunnel work/problems modules are complete and tested before installation - Staged acceptance tests - Decoupling of problems
- Equipment will see more thermal cycles –> create leaks?
- Reduced search/repair zones - Reduced coactivity - Local warm-up and opening of vacuum system – cost & downtime
- Difficult access at CWT – not std interconnect design
- Cavities re-commissioning after venting -RF processing with helium required for field above < 6 MV/m - Movable blocks or valves to absorb field emission electrons?
-Pre-commissioning before installation - Staged tests – smoothing of resources, - Earlier identification of problems - Decoupling of problems - Re-commissioning of ‘weak’ module possible
- More volumes to commission
MCI would affect more equipment
- Limit MCI affected zone by interlocked beam vacuum valves - Limit zone of degraded ins vacuum (helium leak) - Easier diagnosis of problems
- More equipment (fixed pumping systems & valves) - More interlocks - More risk of equipment failure - More maintenance
Repair
- Less tasks for systematic repairs on modules – venting, re-pumping..
Commisioning Operation
Segmented with CDL
Advantages
Installation
Design
“continuous” cryostat
Simpler controls Redundancy in fixed pumping systems
CRYOGENICS
Cryogenics • Cavities cooled with helium II at ~ 2.0 K (3.1 kPa), similar to XFEL – Cavities inside saturated bath (slightly sub-cooled due to hydrostatic head) – Profit from low Δp and good p-stability
Vapor flow large JT Vapour Liquid
Beam tube
Gas return tube Two phase tube
support
2.2 K forward 2 K return
5 K forward
80 K return
40 K forward 300 mm
8 K return 2 K 2-phase
cool down/ warmup
Effect of slope cavity coupler
XFEL
Module Schemes Scheme no 3: “ILC-like”
1.7 %
Diameter “x” [mm]
SPL Workshop NOv. 2009
26
LP SPL
HP SPL
40
80
6/11/2009
Module Schemes Scheme no 7 : “ILC like SPL version “A” with separate cryogenic line equipped for independent cool-down, warm-up and purge”
1.7 %
SPL Workshop NOv. 2009
27
6/11/2009
Separate cryogenic line Advantages / Disadvantages
• Advantages • Less complexity for the main cryostat • Potential to completely isolate “faulty” modules
• Disadvantages • Requires more tunnel space • Higher static heat load
• Cost aspect • Not easy to identify separate line most probably more expensive • More complex cryostat and installation vs. cryostat plus line, two installations and more tunnel space SPL Workshop NOv. 2009
28
6/11/2009
modified cryogenic scheme (proposal)
Warm valves Warm recovery line
Cryogenic issues (ongoing) • High dynamic heat load: ~200 W/cryo-module (~25 W/m)! – Thermal break-down to be checked (q