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Strategies to Remove Particulate Contamination from Ablator Capsule Surface Presentation at Target Fabrication Meeting Santa Fe, New Mexico May 24, 2012 Suhas Bhandarkar, J Reynolds, S, Baxamusa, S. Letts, N. Antipa, E. Lindsey, K. Moreno

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  • Strategies to Remove Particulate Contamination from Ablator Capsule Surface

    Presentation at Target Fabrication Meeting

    Santa Fe, New Mexico May 24, 2012

    Suhas Bhandarkar, J Reynolds, S, Baxamusa, S. Letts, N. Antipa,

    E. Lindsey, K. Moreno

  • • CH capsule surfaces – Isolated contamination of the

    outer surface (particles, etc) – Isolated defects on the outer

    surface (bumps)

    • Likewise, hydrogen ice layer – Roughness, isolated defects,

    contaminant crystals, etc

    Debris on the capsule surface can contribute to Mix

    Suhas Bhandarkar 2

    R-T instabilities are exacerbated by surface roughness of the

    ablator layers

    R-T instabilities: Colors indicate density profile after unstable acceleration

    The numerous parameters that affect ignition have been grouped into four categories

    8/21/2012

  • Capsules can be contaminated with particles with a range of sizes, shapes and compositions

    3

    1. Implementation of clean-rooms and clean handling procedures

    1. Both at GA and LLNL

    2. Metrology of the capsule surface with sub-μm resolution

    3. Mitigation strategy: Capsule cleaning

    Three efforts to diagnose and reduce particle contamination

    Suhas Bhandarkar

    Particle Volume (μm3)

    Cube dimension

    (μm)

    Number Allowed

    >30* >3.1 0

    15 – 30 2.5 – 3.1 10

    7.5 – 15 2 – 2.5 50

    < 7.5

  • Cleaning needs to happen just before final assembly to minimize risk of further pick up of debris

    4

    Inspect

    Clean

    Inspect

    Capsule placed in diagnostic band

    Final assembly

    Suhas Bhandarkar 8/21/2012

  • Fill-tube bond is extremely fragile: all cleaning techniques have to avoid any degradation of the bond

    5

    NIC scale capsule fill-tube bond fails in tension at ~0.03N (3 gmf) We have set the spec at 1 gmf for any cleaning operation

    Delicate fill-tube bond (max 5pL) is the main challenge

    Tensile pull tests of ignition-spec CFTAs:

    Suhas Bhandarkar

    0

    1

    2

    3

    4

    0 100 200 300

    forc

    e (g

    )

    distance (um)

    57 CH

    0

    1

    2

    3

    4

    Bon

    d st

    reng

    th (g

    )

    8/21/2012

  • 10 μm

    5 μm

    We need to overcome the particle – capsule interfacial bond strengths that can vary by orders of magnitude

    • van der Waals – London dispersion: 2 induced dipoles (< 45 kJ/mol) – Debye: 1 induced/1 permanent dipole ( < 3) – Keesom : 2 permanent dipoles (< 25)

    • Hydrogen bonding (< 55) • Electrostatic

    – Localized regions on CH capsule surface can easily tribo-charge

    • Liquid bridge – Capillary retained liquid (water)

    • High temperature bonding – Say during mandrel pyrolysis

    • Visco-elastic force – Particle embedded in a high viscosity fluid or the

    capsule surface itself • Solid bridge

    – Deposition/Precipitation at interface with capsule surface

    Gravity: 1e-13 N

    vdW: 5-10e-8 N

    Capillary 3e-6 N

    Viscous drag 1e-5 N

    Glued particle 1e-3 N

    Electrostatic 5e-7 N

    6 Suhas Bhandarkar

    Particles can be held by different mechanism with a wide range of forces

    8/21/2012

  • Suhas Bhandarkar 7

    Electrostatic – Induced charged on

    a 25um metal wire

    Surface energy – Particle would rather be in

    a fluid than on the capsule

    Sacrificial layer – Removable coating that

    sheds just before assembly

    Localized agitation – Thermal shock using

    a liquid cryogen

    Hydrodynamic drag – High velocity helium jet

    from ~75um capillary

    Increasing particle removal efficiency

    Incr

    easi

    ng ri

    sk to

    cap

    sule

    or f

    ill-tu

    be

    Strategies to remove particles from a CH capsule with an attached fill-tube

    8/21/2012

  • 0

    200

    400

    600

    0.E+00

    2.E-02

    4.E-02

    6.E-02

    0.0E+00 5.0E-06 1.0E-05

    rate

    of L

    N e

    vapo

    ratio

    n g/

    mm

    2.s

    heat

    flux

    (J/m

    m2)

    Time (s)

    heat flux

    rate of evaporation of LN

    Cleaning using liquid nitrogen (LN) relies on thermal shock that the very small fill-tube bond can withstand

    Suhas Bhandarkar 8

    Rapid evaporation at the surface concentrated pressure bursts

    75

    125

    175

    225

    275

    0 50 100 150 200

    tem

    pera

    ture

    T (K

    )

    Wall location (um)

    )2( 22

    drdT

    rrT

    dtdT

    +∂∂

    = κ

    α1

    α2

    Bubble initiation:

    Intense bubbling & any CTE (α) mis-match can generate powerful stresses on particle-capsule interfacial bond

    1

    2

    3

    4

    Initial condition

    Free-stream entrainment

    Dislodge particle

    Capsule surface

    Foreign particle

    Liquid nitrogen

    t= 10 μs

    t= 0.2 μs

    Temperature profile in capsule wall vs time

    Heat flux & LN evaporation rate

    Outer surface

    Inner surface

    Increasing time

    8/21/2012

  • Though no detriment to the C-FT bond, results from LN cleaning showed considerable variability

    0 5

    10 15 20 25

    20 10 5

    Num

    ber

    Particle 'dia' (um)

    1st capsule before after

    0

    5

    10

    20 10 5

    Num

    ber

    Particle 'dia' (um)

    4th capsule before after

    0

    5

    10

    15

    20

    20 10 5

    Num

    ber

    Particle 'dia' (um)

    7th capsule before after new

    Process not seen to be robust due to the variability in particle removal efficiency

    0

    20

    40

    60

    80

    100

    20 10 5

    Rem

    oval

    Effi

    cien

    cy (%

    )

    Particle diam (um)

    Liq N2 Cleaning trials 1st

    2nd

    3rd

    4th

    5th

    6th

    7th

    8th

    Ave

    9 Suhas Bhandarkar

    Before

    After LN clean

    Capsule cleaned with LN flow

    30μm

    8/21/2012

  • LN cleaning has lower efficiency for particles with higher surface charge

    20

    40

    60

    80

    100

    20 10 5

    Rem

    oval

    Effi

    cien

    cy (%

    )

    Particle size (um)

    PP

    Al

    Cu1

    Cu2

    SS1

    SS2

    10 Suhas Bhandarkar

    Typical after

    • Non-polar LN can make only vdW bonds with particles • Need polar liquid to entrain the particles

    Typical before

    100um 50um

    Polypropylene particles

    SS Cu, Au Si, PP Teflon

    Triboelectric series +ve

    -ve

    Skin, hair Glass Nylon Al SS

    Expected particle charge vs material composition

    Measured efficiency for different materials

    Typical after

    Increasing charge

    8/21/2012

  • Low boiling point for fast drying; counter to high P and H

    To sustain entrainment of charged particles

    Another technique is to use surface energy principles to separate particles from capsule

    To enable liquid-particle bonding

    11 Suhas Bhandarkar

    Low surface energy to wet the particle and help debond it: counter to high H Oxide~1000 Metals~500-1500 Plastics: 40-60

    Hamaker constant A123 can be negative if the intervening εliq is intermediate, leading to repulsion RICH~1.55 RIPlastic~1.5-1.6

    We want a solvent with: • γ < 40 and high n, ideally 1.55, (for bond breakage), •high P and H (for good entrainment); •B little over 30oC (to minimize impact on CH or adhesive)

    Liquid Polarity

    P Hyd bond

    H Boiling Pt

    B Surf Energy

    γ RI n

    (Hansen parameter) C dyne/cm methyl formate 6.5 12.5 32 25 1.36 methyl iodide 7.7 5.3 42 25.8 1.53 methylene chloride 6.3 6.1 40 27.2 1.42 methanol 12.3 22.3 65 22.6 1.33 diethyl ether 2.9 5.1 35 17 1.35 toluene 0 0 36 18 1.51 trichlorotrifluoro ethane 1.6 0 44 14 1.36 Liquid nitrogen 0 0 0 9 1.21 water 16 42.3 100 72 1.33 formamide 26.2 19 210 58 1.45 glycerol 12.1 29.3 290 63 1.47

    8/21/2012

  • Of the four top solvents methyl formate provides the best combination of the attributes we are looking for

    Liquid Polarity Hyd bond Boil Pt Surf

    Energy RI methyl formate 6.5 12.5 32 25 1.36 methyl iodide 7.7 5.3 42 25.8 1.53 methyelne chloride 6.3 6.1 40 27.2 1.42 methanol 12.3 22.3 65 22.6 1.33

    Suhas Bhandarkar 12

    0

    15

    30

    45

    1 10 100

    Stre

    ngth

    (MPa

    )

    time (min)

    Methyl formate

    methylene chloride

    Strength of adhesive after solvent exposure

    Halogenated solvents (such as methylene chloride & methyl iodide) are too aggressive

    8/21/2012

  • Concept is to combine strong solvation forces with hydrodynamics to get most efficiency of removal

    Suhas Bhandarkar 13

    Technique: Methyl formate impinged on capsule at high velocity through a 100μm nozzle with limited total time duration

    • Tip velocity: 2-5 m/s • Max force on capsule due to

    momentum of jet: 0.02 g • Holding force of a 500μm

    vacuum wand: 1g • Driving pressure for fully

    developed flow of jet through the nozzle: 12 psi

    Experimental station to test the solvent-jet technique Removal of the separated particles is mediated by a

    high- velocity jet

    Drain

    Nozzle

    CFTA

    8/21/2012

  • Initial tests with intentional contamination with a cocktail of particles were very effective

    14 Suhas Bhandarkar

    Bef

    ore

    Afte

    r 1st tr

    ial

    Afte

    r 2nd

    tria

    l

    SEM image of full capsule before & after solvent jet cleaning

    50um

    50um

    High Magnification SEM image

    Bef

    ore

    Afte

    r

    Surface has mixture of metal (Al, Cu), oxide (Al2O3) and polymer (nylon & polypropylene) particles

    8/21/2012

  • This technique was also effective on ‘real’ debris on capsules

    Suhas Bhandarkar 15

    500um 100um

    20um 20um

    200um 200um

    Bef

    ore

    Bef

    ore

    Bef

    ore

    After

    After

    After

    SEM images of sections of real capsules

    8/21/2012

  • Fill-tube joints on 8 capsule assemblies showed no signs of degradation & were leak-tight

    Suhas Bhandarkar 16

    100um

    10um

    10um

    SEM images of the bonds connecting the fill-tubes to the capsule after 30 min of exposure to methyl formate show little change

    8/21/2012

  • We have modeled the fluid velocity field on the capsule using mechanisms described by Watson*

    Suhas Bhandarkar 17 * E.J. Watson, J Fluid Mech. 20, 481, 1964

    r

    u(r, y)

    y

    jet, flowrate Q kinematic viscosity ν

    h(r) ∫=)(

    0

    2rh

    udyrQ π

    )()()(1

    0

    2 rhgrhdrdhg

    yudyru

    drd

    r xyh

    +−∂∂

    −=∫ ν

    Continuity:

    Momentum:

    For a sphere:

    r= Rs(sinθ)

    Radial spread of impinging jet on a sphere

    jet

    θ Rs

    8/21/2012

  • Model indicates that the fluid spreads over the capsule as a film whose thickness is ~40μm, independent of the incoming jet velocity

    Suhas Bhandarkar 18

    Modeled results of film thickness compared to experiments

    Model Capsule periphery Liquid layer

    Video 0

    100

    200

    300

    400

    500

    0 2000 4000 6000 8000 10000

    Max

    siz

    e of

    dro

    p fo

    r 1 p

    g re

    sidu

    e

    contamination level in fluid (ppb)

    Typical drop size

    Max allowed contamination

    Fluid cleanliness needed for a residue of no more than 1pg per drop

    8/21/2012

  • 0

    0.2

    0.4

    0.6

    0.8

    1

    1.2

    1.4

    1.6

    1.8

    2

    0 50 100 150

    Free

    sur

    face

    vel

    ocity

    (m/s

    )

    angle (degrees)

    Velocity, 2m/s

    Velocity, 4m/s

    Highest fluid velocities only occur close to the incoming jet stream, calling for rastering of the jet

    Suhas Bhandarkar 19

    We need to raster the jet stream over the capsule

    Jet velocity 2m/s or 4m/s

    Modeled results for free-surface velocity of the liquid film around the capsule

    8/21/2012

  • Strategies to Remove Particulate Contamination from Ablator Capsule SurfaceDebris on the capsule surface can contribute to MixCapsules can be contaminated with particles with a range of sizes, shapes and compositionsCleaning needs to happen just before final assembly to minimize risk of further pick up of debrisFill-tube bond is extremely fragile: all cleaning techniques have to avoid any degradation of the bondWe need to overcome the particle – capsule interfacial bond strengths that can vary by orders of magnitude Strategies to remove particles from a CH capsule with an attached fill-tubeCleaning using liquid nitrogen (LN) relies on thermal shock that the very small fill-tube bond can withstandThough no detriment to the C-FT bond, results from LN cleaning showed considerable variabilityLN cleaning has lower efficiency for particles with higher surface chargeAnother technique is to use surface energy principles to separate particles from capsuleOf the four top solvents methyl formate provides the best combination of the attributes we are looking forConcept is to combine strong solvation forces with hydrodynamics to get most efficiency of removalInitial tests with intentional contamination with a cocktail of particles were very effectiveThis technique was also effective on ‘real’ debris on capsulesFill-tube joints on 8 capsule assemblies showed no signs of degradation & were leak-tightWe have modeled the fluid velocity field on the capsule using mechanisms described by Watson*Model indicates that the fluid spreads over the capsule as a film whose thickness is ~40μm, independent of the incoming jet velocityHighest fluid velocities only occur close to the incoming jet stream, calling for rastering of the jetSlide Number 20