3 rd installation: chicane magnetic field tests
DESCRIPTION
Electron cloud installation studies at SLAC. 3 rd INSTALLATION: chicane magnetic field tests. PEP-II e+ ring. 1 st and 2 nd. Cherrill Spencer. Feb 2008. ILC tests - SLAC. “Ecloud1” SEY test station in PEP-II SLAC. PEP-II LER. 2 samples facing beam pipe are irradiated by SR. e+ . - PowerPoint PPT PresentationTRANSCRIPT
3rd INSTALLATION: chicane magnetic field tests
PEP-II e+ ring
1st and 2nd
Feb 2008
Electron cloud installation studies at SLAC
ILC tests - SLAC
Cherrill Spencer
ILC DR Workshop - KEK
““Ecloud1” SEY test station in PEP-II SLACEcloud1” SEY test station in PEP-II SLAC““Ecloud1” SEY test station in PEP-II SLACEcloud1” SEY test station in PEP-II SLAC
Transfer system at 0o
PEP-II LER e+
Transfer system at 45o
2 samples facing beam pipe are irradiated by SR
Isolation valves
ILC tests, M. Pivi et al. – SLAC
ILC DR Workshop - KEK
Results of TiN conditioning in PEP-II e+ beam line
SEY of Tin-samples measured before and after 2-months conditioning in the beam line. 2 samples inserted respectively in the synchrotron radiation fan plane (0o position) and out of this plane (45o).
ILC tests, M. Pivi et al. – SLAC
Before installation in beam line
After beam conditioning
e- dose >
40mC/mm**2
Similar low SEY recently measured in situ in KEKB beam line S. Kato, Y. Suetsugu et al.
LER#1
XPS Before installation XPS After exposure in PEP-II LER for 2 months (e dose 40mC/mm^2)
Carbon content is strongly reduced after exposition to PEP-II LER synchrotron radiation + electron + ion conditioning. This is a different result if compared to electron (only) conditioning in laboratory set-up where carbon crystals growth has been observed by many laboratories.
Surface analysis: Carbon content decrease
TiN samples: X-ray Photon Spectroscopy.
ILC tests, M. Pivi et al. – SLAC
Results of NEG conditioning in PEP-II e+ beam line
ILC tests – SLAC
NEG as received
After beam conditioning
March 2008
After NEG heating
KEK, Feb 2008
Clearing electrodes in KEKB magnetic free region
Y. Suetsugu, KEK
Y. Suetsugu, KEK
11 March, 2008 SPS meeting. Mauro Pivi SLAC
Gianluigi Arduini, Elena Chapochnikova, Paolo Chiggiato, Miguel Jimenez, Mauro Taborelli (CERN) Mauro Pivi, Lanfa Wang, Frank Cooper, Munro Morrison (SLAC)Marco Venturini, Miguel Furman (LBNL)
SPS Groove Chamber Tests Collaborators
Secondary electron yield (SEY) estimate: SPS Groove
0 100 200 300 400 500 600 7000
0.2
0.4
0.6
0.8
1
1.2
1.4
Energy (eV)
SE
Y
0=1.20,B=2 Tesla,R
tip=0.13mm,H=2mm
Grooved SurfaceFlat Surface
0 200 400 600 8000
0.2
0.4
0.6
0.8
1
1.2
1.4
Energy (eV)
SE
Y
Grooved SurfaceFlat Surface
0=1.20,B=2 Tesla,R
tip=0.13mm,H=1mm
Height=2mm Height=1mm
In this simulation the groove height is taken to be the effective total height from top to valley
Lanfa Wang, SLAC
Marco Venturini, LBNL
electron cloud build-up as a function of time for 1mm deep grooves with angle alpha =80 deg, for various choices of the groove tip radius. Groove on bottom and top sides. In these simulations hg=1mm is the height of the groove triangle.
Simulation of electron cloud build up
•Max. e-cloud linear density vs. groove tip radius (SEY=1.3)•For flat surfaces the max. linear density is ~ 1.5 nC/m). •In the SPS tests, grooves on top and bottom side. •In these simulations hg=1mm is the height of the groove triangle.
Marco Venturini, LBNL
Simulation of electron cloud build up
• Roundness of tips and valley is important• Manufacture Tolerances on roundness are
rather tight for 1mm grooves
• Few more work on simulations:– In the SPS, would it be more realistic to assume
initial SEY=1.5 (?!), since no photon scrubbing. – Define tolerance roundness to obtain SEY<1– For small 1mm groove important to consider the
effective groove height (after roundness)
munro 16
TRIANGULAR GROOVE CHAMBER MFG
January , 2008
Requirements
Triangular Grooves
Groove Width 0.35 mm
Groove Depth 1 mm
Overall Depth 2 mm
Groove Length 0.5 M
Taper Angle 20 degrees
Radius at Top & Bottom 0
Basic Problems
• Very small grooves are difficult to fab
• Sharp radii at base & top of grooves unattainable by normal mfg methods
• Mfg options are to either have grooves as part of vac chamber, or fab grooves as separate item & then attach to vac chamber.
Mfg Options• Extrusion: Very small radii at top & bottom of
grooves are difficult to mfg• Machining: Mill multiple slots in solid material• Metal Folding: Form multiple folds• EDM: Small radii are beyond normal tolerances • Brazed-up Assembly: Use individual razor type
foil blades• Isostatic Pressing or Metal Injection Molding:
Uses powdered metal & binders which would probably would not be suitable for vacuum usage. Also have difficulty in forming small radii
Groove Options Manufactured
Series of aluminum extrusions fabricated
• Grooves all around chamber (2 different groove profiles)
• Grooves at top & bottom of chamber
• Separate linear extrusion for insertion into existing stainless vacuum chamber
Cost Considerations
• Assuming long sections required, the extrusion approach is by far the least expensive.
• Limited to aluminum material
• Copper may be possible, but could not find vender
Aluminum triangular grooves by ALMAG.Original design for the SPS: 2mm depth, limited by the groove sharpness.SLAC 2008
Aluminum triangular groove:
depth 1.9mm, angle 20deg, radius top 0.095mm, radius valley 0.140mm
With final geometryThe real geometry:
radius of tip=0.095mm
radius of valley =0.14mm
0 100 200 300 400 500 600 7000.2
0.4
0.6
0.8
1
1.2
1.4
1.6
1.8
2
Energy (eV)
SE
Y
0=1.50,Height=1.9mm, =200
Flat surfacer=0.14mm,B=2 Teslar=0.14mm,B=0.2Teslar=0.09mm,B=2 Teslar=0.09mm,B=0.2Teslaaverage,B=2 Tesla
Lanfa Wang, SLAC
Manufacturing Options depth 1mm: Metal Folding
Metal Folding: Form multiple folds. [EMEGA Company, USA]
Manufacturing Options depth 1mm: Razor Blades
Brazed-up Assembly: Use individual razor type foil blades
Manufacturing Options depth 1mm: Razor Blades