sandia brazing research and modeling capabilities* · sandia brazing research and modeling...

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SECA SOFC Seal Meeting July 8-9, 2003 Sandia Brazing Research and Modeling Capabilities* F. Michael Hosking Materials and Process Sciences Center Sandia National Laboratories Albuquerque, NM 87185-0889 * Sandia is a multiprogram laboratory operated by Sandia Corporation, a Lockheed Martin Company, for the United States Department of Energy’s National Nuclear Security Administration under Contract DE-AC04-94AL85000. Principal SNL/NM Technical Brazing Contacts Metals: Mike Hosking & John Stephens, Org. 1833 & Chuck Walker, Org. 14171 Ceramic: Ron Loehman, Jill Glass & Sandy Monroe, Org. 1843 Microanalysis: Joe Michael, Tom Headley, Paul Kotula & Paul Hlava, Org. 1822 Modeling: Steve Burchett, Frank Dempsey, Rick Givler & Jerry Wellman, Org. 9100

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  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Sandia Brazing Research and Modeling Capabilities*

    F. Michael HoskingMaterials and Process Sciences Center

    Sandia National LaboratoriesAlbuquerque, NM 87185-0889

    * Sandia is a multiprogram laboratory operated by Sandia Corporation,a Lockheed Martin Company, for the United States Department of Energy’s

    National Nuclear Security Administration under Contract DE-AC04-94AL85000.

    Principal SNL/NM Technical Brazing ContactsMetals: Mike Hosking & John Stephens, Org. 1833 & Chuck Walker, Org. 14171

    Ceramic: Ron Loehman, Jill Glass & Sandy Monroe, Org. 1843Microanalysis: Joe Michael, Tom Headley, Paul Kotula & Paul Hlava, Org. 1822

    Modeling: Steve Burchett, Frank Dempsey, Rick Givler & Jerry Wellman, Org. 9100

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Brazing is widely used to join metals and ceramics to each other for a variety of high reliability components

    New active brazing alloys simplify hermetic joining issues

    Basis: Oxide-forming additives to filler metal (e.g., V, Ti, Zr, Hf) promote direct wetting and adhesion to the ceramic materials (Al2O3, Si3N4, cermet, …)

    Payoff: Eliminate complex Mo-Mn metallize / Ni-plate & related processing for conventional alloys

    Issue: Complex reactions between active braze elements and ceramic/metal base materials need to be understood to control and optimize process

    • headers• connectors• feedthroughs• thermal batteries• high voltage tubes• electromechanical devices• storage containers

    TEM ImageTEM Image

    TiO, Ti2O & Cu3Ti3O reaction products

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Braze flow visualization and dissolution reactions are important components in understanding the braze process

    x distancetoLabVIEW + IMAQ Vision Analysis

    ∆x = 0.19 mm

    ≈ 10 D (1.3 mm)

    Laminar Flow

    approx. 5 Hz

    x distancetoLabVIEW + IMAQ Vision Analysis

    x distancetoLabVIEW + IMAQ Vision Analysis

    ∆x = 0.19 mm

    ≈ 10 D (1.3 mm)

    Laminar Flow

    approx. 5 Hz

    Recent Accomplishments• Conference paper / presentations (IBSC’03;

    CSM Materials Science Seminar; C6 ASCI Solidification Working Group)

    • S&T of Welding & Joining journal paper• In-Situ Visualization of Braze Flow patent

    1095ºC

    1145ºC1120ºC

    (at% Ni)

    1095ºC

    1145ºC1120ºC

    (at% Ni)

    66019010181140 (H2Frn)

    321020181145

    1.519514121120

    0.5175631095

    ResidentTime Above

    1085ºC

    JointThickness

    (µm)

    EMPA Ni Content(wt. %)

    Terminal Solidus

    (wt. % Ni)

    Specimen Temperature

    (ºC)

    66019010181140 (H2Frn)

    321020181145

    1.519514121120

    0.5175631095

    ResidentTime Above

    1085ºC

    JointThickness

    (µm)

    EMPA Ni Content(wt. %)

    Terminal Solidus

    (wt. % Ni)

    Specimen Temperature

    (ºC)

    Note: At 1145ºC, Cliquidus ~ 10 wt. % Ni

    0

    20

    40

    60

    80

    100

    0 1000 2000 3000 4000 5000

    Ni

    Cu

    Con

    cent

    ratio

    n (w

    t. %

    )

    distance (µm)

    Cu-Ni Traces Through Center of Cu Braze1120C Peak Work Temperature

    1120ºC

    EMPA Traces

    1120ºC

    EMPA Traces

    Cu-Ni binary braze flow & dissolution experiments

    Braze Capillary Flow Visualization

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Active brazing technology is bridging a wide range of needs because of the fundamental knowledge being developed

    0

    20

    40

    60

    80

    100

    120

    Frac

    ture

    Stre

    ngth

    (M

    Pa)

    94% 94% 94%99.8% 99.8% 99.8%

    Au - 16.0Ni -1.75V - 0.75Mo

    Au - 18.0Ni - 0.8Ti

    Au -17.5Ni - 2.5Ti

    Alumina ceramic / braze interface reactions vary significantly with active element

    Alumina

    Au-Ni-Mo-2V

    reaction layer

    10 nm

    XX--ray diffractionray diffraction

    (Fe, Ni,Co)3Ti

    … no TiAlumina

    Kovar (Fe-29Ni-17Co)

    Ag-Cu-Ti

    Competing reactions between dissimilar base materials can introduce unwanted results

    V activation

    Ti activation… compatibility

    issuesZr activation

    Alumina

    Au-Ni-Mo-2V

    reaction layer

    10 nm

    XX--ray diffractionray diffraction

    (Fe, Ni,Co)3Ti

    … no TiAlumina

    Kovar (Fe-29Ni-17Co)

    Ag-Cu-Ti

    Competing reactions between dissimilar base materials can introduce unwanted results

    V activation

    Ti activation… compatibility

    issuesZr activation

    Fracture strengths for 94 & 99.8% alumina brazed with Ti & V-bearing Au-Ni filler metals exhibit dependency on glassy phase and more stable TiOx reaction product

    Ag-2Zr (wt. %) ABA

    reaction layer

    Alumina

    ZrO2

    15 µm

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    A multidisciplinary approach to characterizing the different brazing reactions and properties is necessary for success

    0

    20

    40

    60

    80

    100

    120

    140Average Tensile Strength (MPa)

    BrazingTemperature

    & Time

    Determining effects of reaction products & microstructures on properties (hermeticity & strength) as a function of active element (thermodynamics / kinetics), base material (adhesion / dissolution), brazing conditions (temperature, time, atmosphere, heating cycle& gradients, orientation), surface preparation (ceramic air-firing).

    Contact Angle vs. [SiO2]

    0

    10

    20

    30

    40

    50

    60

    70

    80

    0 20 40 60 80 100

    [SiO2]

    Wet

    ting

    Ang

    le

    2.5%Hf3.4%Hf6.8%Hf

    1100°C for 30 min in Ar

    Contact Angle vs. [SiO2]

    0

    10

    20

    30

    40

    50

    60

    70

    80

    0 20 40 60 80 100

    [SiO2]

    Wet

    ting

    Ang

    le

    2.5%Hf3.4%Hf6.8%Hf

    Contact Angle vs. [SiO2]

    1100°C for 30 min in Ar

    0

    10

    20

    30

    40

    50

    60

    70

    80

    0 20 40 60 80 100

    [SiO2]

    Wet

    ting

    Ang

    le

    2.5%Hf3.4%Hf6.8%Hf

    1100°C for 30 min in Ar

    200 µm

    96% Al2O3

    Ag-2.5 wt.% Hf

    200 µm96% Al2O3

    200 µm

    96% Al2O3

    200 µm

    96% Al2O3

    Ag-2.5 wt.% Hf

    200 µm96% Al2O3

    Ag-2.5 wt.% Hf

    200 µm96% Al2O3

    200 µm

    96% Al2O3

    Ag-2.5 wt.% Hf

    200 µm96% Al2O3

    200 µm

    96% Al2O3

    200 µm

    96% Al2O3200 µm96% Al2O3

    Ag-2.5 wt.% Hf

    200 µm96% Al2O3

    Ag-6.8 wt. % Hf

    ASTM F19Test Specimen

    ASTM F19Test Specimen

    Al-500 alumina brazed with Ag-3.4Hf & 0.25 mm Kovar™

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Ability to correlate braze interface reactions with desired properties will yield more producible & reliable joints

    0

    21

    42

    63

    84

    105

    0 20 40 60 80 100

    AlSiFeCoNiAgHf

    Co

    nce

    ntr

    atio

    n (

    wt.

    %)

    Distance (µm)

    Job #PBR02014Disk 2file 95

    P. F. Hlava020207

    Trace From Kovar Through Ag - 3.4Hf Braze Alloy into Alumina (Trace 3)Sample Brazed 990°C/10 min., dry H

    2

    BSE image shows continuous HfO2reaction layer at ceramic interface Kovar AL-500

    0

    21

    42

    63

    84

    105

    0 20 40 60 80 100

    AlSiFeCoNiAgHf

    Co

    nce

    ntr

    atio

    n (

    wt.

    %)

    Distance (µm)

    Job #PBR02014Disk 2file 95

    P. F. Hlava020207

    Trace From Kovar Through Ag - 3.4Hf Braze Alloy into Alumina (Trace 3)Sample Brazed 990°C/10 min., dry H

    2

    BSE image shows continuous HfO2reaction layer at ceramic interface Kovar AL-500Kovar AL-500

    Single crystal sapphire & polycrystalline alumina brazed with Ag-2Zr

    94% alumina brazed with Ag-2Zr is hermetic, fails in the bulk ceramic and has 130 MPa tensile strength

    Ag-3.4Hf ceramic braze joints also demonstrate similar excellent properties (hermetic & 125 MPa)

    Recent Accomplishments• Implementation of active brazing in production• Conference paper / presentations (ASM Materials

    Solutions 2002; AWS IBSC’03; ACerS 2003)• Metallurgical Transactions A paper (in publication)• Coating System for Direct Ceramic Brazing patents

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Diffusion bonding offers an alternative joining processCeramic-metal and metal-metal joints are possible

    a) Hard ceramic and comparatively soft metal surfaces come in contact (T, t, P)

    b) Metal surface yields under high local stressesc) Deformation continues mainly in the metal,

    leading to interface diffusion & void shrinkaged) Metallurgical bond is formed

    TWI, Ltd, 2000.

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    FEA Brazing Model Development & Validation

    ThermalResponses Stress & Failure

    Predictions

    Fluid Flow Responses

    Design &Production

    FixturedAssembly

    +

    Engineering Sciences Center Simulations

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    FEA Thermal Modeling of Furnace Brazing

    Work Rack & Parts

    • Nonlinear, 3-D transient thermal finite element code

    • Ability to mesh very fine details (large node and surface radiation enclosure)

    Typical Model Inputs• materials density• thermal conductivity• specific heat• emissivity• thermal boundary

    conditions• convective heating by hydrogen

    gas is assumed negligible• heating driven by radiation from

    furnace elements & conductionfrom Mo shelves to work piece Simulations processed on massively

    parallel teraflop compute server

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Example: Two-Step, Cu + 50Au-50CuBraze Assembly Process Characterization

    Oven - 1/2 section

    FEA Thermal Model

    Shelves/fixtures

    backup ringweight

    housingweight

    fixture alignment

    backupring

    Au-Cu2nd Braze

    Cu1st Braze

    base

    large flange

    small flange

    pins

    housing frame

    backupring

    Braze Fixture

    ceramic ring

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Process Space Simulations

    braze

    Oven control TemperaturesTop ---Sides ---Btm ---

    equalize

    Data acquired:• Peak brazing temperature• Time braze is melted• Temperature uniformity• Determine optimization

    parameters in process spaceversus experimental “point solutions”

    Trends at Peak Temperature:• Top and bottom shelves are

    hottest (trim heater settings)• Middle shelf most uniform• Center unit of five on each shelf

    is coolest (~ 5°C lower)• 10 min. hold at set temp. gives

    uniform heating, but increases time above melting

    • Brazing temperature is uniform within individual units

    4x24x5 7x2

    7x5

    Process Space:• Thermal boundary conditions:

    – 1st ramp rate (10, 40°C/min)– 1st hold time (5, 25 min)– 1st hold temp (930, 960°C)– 2nd ramp rate (10, 40°C/min)– peak temp (1000, 1030°C)– time @ peak temp (0, 10 min)– cooling rate (10, 40°C/min)

    • Number of shelves (4, 7)• Number of fixtures/shelf (2, 5)• Shelf type (solid, perforated)• Fixture material (Mo, Kovar®)• Emissivity (low, high)

    Two-level fractional factorial design for 12 factors in 16 unique trials

  • SECA SOFC Seal MeetingJuly 8-9, 2003

    Example: DoEx Screening Sensitivities forThermal Characterization of Brazing Process

    h l it O h ld H th ld P th ld 1 2 h l T k t6

    8

    1 0

    1 2

    1 4

    Factor sensitivities to the brazing conditions on the central shelf

    47

    2

    525

    5

    960

    930

    0

    40

    10

    1040

    No

    1030

    Yes

    1000

    40

    10

    main effect factor significance

    # of

    She

    lves

    1stho

    ld te

    mp.

    1stho

    ld ti

    me

    Tim

    e @

    pea

    k

    1stra

    mp

    rate

    2nd

    ram

    p ra

    te

    Hol

    e in

    shel

    ves

    Peak

    tem

    p.

    Coo

    ling

    rate

    # of

    Uni

    ts

    time

    abov

    e m

    eltin

    g, m

    in.

    10