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7/30/2019 IS 5067.1983 Power point
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STATUS REPORT ON
VACUUM CHAMBERS(Dipole & Straight)
&
DIPOLE MAGNETS
FOR TL-2 OF CTF3
A.K. JAIN, S.S. PRABHU,S. KOTAIAH
RRCAT, INDORE (INDIA)
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Vacuum Chambers
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Initially, two test vacuum chambers fabricated in aluminum
grade AA 6061 for qualifying machining & welding
procedure. Surface finish < 0.30 microns achieved.
Welding torch manuveres needed to access some portions
of chamber.
For third chamber, design was changed to simplify welding.
Leak rate obtained ~3 x 10-10 Torr ltr / sec.
Dipole Vacuum Chambers :
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DIPOLE VACUUM CHAMBERS
Machined & Welded Prototype Chamber
Initial Trial Final Trial
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1
1
2
2
3
3
4
4
5
5
6
6
7
7
8
8
A A
B B
C C
D D
E E
F F
NATIONAL INSTITUTE OF NUCLEAR PHISICS
FRASCATI NATIONAL LABORATORY
DRAFTER D ES IG NE R E NG IN EE R APPROVAL
DRAWING N. REVQUALITY ASSURANCE
VACUUM DIAGNOSTIC ACC.PHY. ELEC. ENG.
DATE MATERIAL WEIGHT SCALE
GENERALTOLERANCESUNI EN22768/1-MEDIUM
FINISH NEXT ASSY DWG QUANT. NOTE
A2
CTF3
CAMERA TL
TERZA CAMERA CHICANE
FLANGIA RETTANGOLARE
G. FONTANA
0 8/ 07 /2 00 3 A NT 60 82 T6 1:1
CTF3-013-000 1
CTF3-013-004 A
B B
B-B ( 1 : 1 )
27
27
59,5
59,5
136
18
36
33
3383
96
Sm1X45
A
0,1 A
R12,5
R21,50,05
37
90
55
0,05
C 0,1 B
1080,05
B
0,1 A
3+0,06-0
43
5,5
5,5
45
R35,5
R27
40+0,2+0,1 R14+0,2
+0,1
66
R15,5
8,4 PASS.
Sm 03x45
0,1 A B C
NOTES:
1) ALL MACHININGS MUST BE DONE AS
SPECIFIED
BY DOCUMENT N CTF3-013-SP-A2) ALL INTERNAL SURFACES TO HAVE ROUGHNESS
BETTER THAN 0.4 MICRON
3) ALL EXTERNAL SUFACES TO HAVE ROUGHNESS
BETTER THAN 3.2 MICRON
4) GENERAL TOLERANCES = 0.3 mm
END FLANGES OF DIPOLE VACUUM CHAMBERS
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Fabrication & Processing :Material:
AA6061T6 is silicon magnesium based aluminium alloy.
(Material is solution heat treated and artificially aged).
Tooling :
High-speed cutters were used. Cutters equipped withperipheral mounting, high positive rake angle (340), coated
carbide inserts with 900 approach angle. One of three
inserts had a wiperinsert to get good surface finish.
Processing :Chemical cleaning-Approved by CERN for aluminium alloy
grade AA6061-T6. After chemical cleaning, jobs were hand
scrapped in the lip area to remove oxide layer just before
welding.
Dipole Vacuum Chambers (Contd)
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TIG WELDING :
Welders were qualified as per section IX of ASME code.
Cleanliness and humidity level of the weld room was maintained using air
conditioners, air curtains and Dehumidifiers.
Base material used:
AA 6061 T6 ( containing Si- 0.6%, Mg 1-1.2%, - Cu - 0.27%)
Filler wire used:
AWS A5.10 ER 4043 (Containing Si5%, Mn 0.05% Fe 0.4% Al rest)
Shielding gas used:
XL grade argon 99.999% as per IS-5760-1983 (Grade - 1) (Impurities -
Oxygen less than 1.5 ppm., Moisture less than 1.0 ppm, total
hydrocarbon NIL)
Dipole Vacuum Chambers (Contd)
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Welding Parameters
Peak current 60-70 Amps.
Back ground current 25 Amps.
Pulse frequency 7 Hz. (at high position)
Pulse Ratio 80%
Type of arc Hard Arc
Shielding gas flow rate 8 Ltrs / min
Relative Humidity Less than 35%
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Dipole Vacuum Chambers (Contd)
Present Status :
Fabrication and welding procedures qualified.
Raw material AA 6061 T6 procured.
Awaiting CERNs approval of TL-2 optics design & also magnet design.
Final drawings for chamber fabrication to be taken up thereafter.
Total nos. of dipole chambers ~5. Assembly of dipole chamber with
bending magnet has been tried using CAD. There is no problem in the
assembly.
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Straight Chambers :
RRCAT, Indore will deliver these chambers built out of extruded
aluminum grade AA 6061 T6. This will avoid welding of chambers at
the edges and their machining on a CNC vertical milling machine.
Extrusion job already ordered.
Extruded material expected at RRCAT ~April, 2007. Once TL-2 optics
is frozen, material will be cut to required lengths, ends machined to
suit the welding joints with end flanges.
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NATIONAL INSTITUTE OF NUCLEAR PHISICS
FRASCATI NATIONAL LABORATORY
DRAFTER ENGINEER APPROVAL
DRAWING N. REVQUALITY ASSURANCE
VACUUM DIAGNOSTIC ACC.PHY. ELEC. ENG.
DATE MATERIAL WEIGHT SCALE
GENERAL TOLERANCES UNI EN 22768/1-MEDIUM
FINISH NEXT ASSY DWG QUANT. NOTE
Foglio N.
DESIGNER
A3
A A
A-A ( 1 : 4 )
365 360 365
1090
B
B ( 1 : 2 )
C
C ( 1 : 2 )
D
D ( 1 : 2 )
NOTES:
1) ALL MACHININGS MUST BE DONE AS
SPECIFIED
BY DOCUMENT N CTF3-018-SP-A
2) ALL INTERNAL SURFACES TO HAVE ROUGHNESS
BETTER THAN 0.4 MICRON
3) ALL EXTERNAL SUFACES TO HAVE ROUGHNESS
BETTER THAN 3.2 MICRON4) GENERAL TOLERANCES = 0.3 mm
TIG WELDING TIG WELDING
1,10,05
48,3 0.05
3 4 2 1 2 4 3
A 0,1
1 1 CTF3-018-002
2 2 CTF3-018-0013 2 CTF3-018-003
4 2 CTF3-018-004
Elenco parti
ELE QT NUMERO PARTE DESCRIZIONE NO
B
0,1 A 0,1 B
40 0.05
Straight Chambers
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DIPOLE MAGNETS FOR TL-2
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Specifications
Sr.
No.Parameters
Values (Type-1)
350
Values (Type-2)
17.50
1 Nominal Field 1.3 Tesla 1.3 Tesla
2 Nominal current 340 A 340 A
3 Pole Gap 45 mm 50 micron 45 mm 50 micron
4 Pole width 240 mm 240 mm
5 Coil Pocket size 176 mm (width) X 176 mm (width) X
157.5 mm (height) 157.5 mm (height)
6 Yoke Length 465 mm (235mm)
7 Magnetic Length 518 mm 288 mm
8 Bending Angle 35 17.5
9 Construction Length 920 mm 690 mm10 Core weight 1273 kg 640 Kg
11 Coil weight 860 kg 445 Kg
12 No of Pan Cakes 4 4
13 No of turns 48/pancake 48/pancake
14 Total no of turns 192 192
15 Resistance 60 milli-Ohm 32.5 milli-ohm
16 Voltage 20.4 Volts 11.3 volts
17 Power dissipated 6.8 Kilo-watt (3.8 KW)
18 Cooling water flow 9.5 LPM 9.5 LPM
19 Pressure drop 2.4 ata 1.24 ata
20 No of cooling circuits 4 4
21 Water temperature rise 11 C 5.8 C
22 Quantity Required 2 Nos. 3 Nos.
DIPOLE MAGNET
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Magnet Core Material:
1.5 mm thick low carbon steel sheets supplied by M/s CockrehillSambre.
B/H data and other information :
H in A/m 120 1200 5000 10000B in Tesla 0.7 1.5 1.71 1.81
Variation in B % 15 % 2 % < 2 % 1 %
Coercivity 70 A/m
Carbon content < 0.01 %
Yield Strength 120 N/mm2
Tensile Strength 260 N/mm2
Thickness spread < 1.5 %
Dipole Magnets (Contd)
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Dipole Magnet Bottom Half Block
Dipole Magnet Coil Pan Cake
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DIPOLE MAGNET ASSEMBLY
Overall Mechanical Details of Assembled 35 Dipole MagnetMagnet height 640 mm
Magnet Width 1000 mm (812 + 30 + 158)
Magnet Length 910 mm
Magnet total weight 2200 kg
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03
01
02
CORE BLOCK FOR DIPOLE MAGNET
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Fabrication Stages :
Laser Cutting of Stampings.
Stacking of stampings & pressing to form a
block.
Welding of stampings to get block.
Machining of pole surface & other reference
surfaces.
Assembly of two blocks along with water
cooled coil pancakes.
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Present Status :
Engineering drawings for 350 bending magnet completed;
Sent to CERN, but approval awaited. Quantity required 2 nos.
Fabrication will start only afterCERNs approval of drawing.
Engg drawings for 17.50 bending magnet completed; will be
shortly sent to CERN for approval. Quantity required 3 nos.
Raw material for core & coil procured.
Dipole Magnets (Contd)
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THANK YOU FOR YOUR ATTENTION