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