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    400 Commonwealth Drive, Warrendale, PA 15096-0001 U.S.A. Tel: (724) 776-4841 Fax: (724) 776-5760

    SAE TECHNICALPAPER SERIES 2002-01-0797

    Component Testing and Materials Properties

    of Ductile Iron Brake Anchors

    Alan P. Druschitz, Nathan J. Sochor and Brandon ReneauIntermet Corporation

    SAE 2002 World CongressDetroit, Michigan

    March 4-7, 2002

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    The appearance of this ISSN code at the bottom of this page indicates SAEs consent that copies of thepaper may be made for personal or internal use of specific clients. This consent is given on the condition,

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    ISSN 0148-7191Copyright 2002 Society of Automotive Engineers, Inc.

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    2002-01-0797

    Component Testing and Materials Properties of Ductile

    Iron Brake Anchors

    Alan P. Druschitz, Nathan J. Sochor and Brandon Reneau

    Intermet Corporation

    Copyright 2002 Society of Automotive Engineers, Inc.

    ABSTRACT

    During product development and production, product

    testing is often desirable to improve design robustness

    and verify consistent product performance. However,

    product testing is very complicated, requires highly

    specialized and trained personnel and utilizes expensive,dedicated equipment and facilities.

    This paper describes two brake anchor component tests

    (pull and impact) and the use of strain gaged components

    to determine the characteristics of the component during

    loading. Data for two brake anchor designs are presented

    and the component properties are then correlated with

    material properties and design. The combined effect of

    material properties and component design on performance

    is demonstrated. The data also demonstrates that

    apparently identical tests on different component designs

    can lead to misleading conclusions.

    BACKGROUND

    Product testing has been and will continue to be a crucial

    part of the product development cycle since current math

    models cannot fully take into account variable material

    properties and cannot fully account for all loading

    conditions that might be encountered in service. For

    example, castings cool at different rates in different

    locations and therefore always have varying mechanical

    properties. Also, the loading conditions in the foundry or

    machining line often exceed those encountered in service.

    Since a math model can only calculate the effect of the

    loads input into the model and the material properties

    assigned to the component, unforeseen loading conditions

    and unforeseen material property variations may produce

    early failures.

    For this study, a relatively simple component (brake

    anchor) was selected to demonstrate how design and

    material properties interact. For this demonstration, a

    variety of tests were performed: 1) one brake anchor

    design was tested in two different loading conditions (pull

    and impact) and 2) two brake anchor designs were tested

    in numerous material conditions (as-cast and various heat

    treatments). This type of data is needed by the design

    engineer when specifying material requirements

    developing new components and developing component

    test specifications.

    COMPONENT DESCRIPTION, TEST

    METHODS AND MATERIAL PROPERTIES

    Two similar brake anchors designed by differen

    companies and produced at the INTERMET Havana

    Foundry were selected for this study. The differences

    between these brake anchors were both obvious and not

    so obvious. The obvious difference was the shape of the

    thin tie bar. In Figure 1a, the tie bar of brake anchor A

    looks much thinner than the tie bar of brake anchor B.

    However, when the brake anchors are inclined, Figure 1b

    the tie bars appear nearly identical. Actually, the tie bar

    of brake anchor A was thicker and had a well roundedcross section whereas the tie bar of brake anchor B had

    two flat surfaces incorporated into the tie bar for fast brake

    pad changes, which significantly reduced the cross

    section thickness, and formed relatively sharp corners.

    The cross sections of the two brake anchor designs are

    shown in Figure 2. The not so obvious difference was the

    microstructure and chemistry of the material. Basically,

    both brake anchor castings had similar microstructures

    with brake anchor A having slightly more pearlite, Figures

    3a and b. However, brake anchor design B was prone to

    carbide formation at the edges of the tie bar due to sharp

    corners that cooled rapidly, Figure 4. Because of this

    design problem, higher silicon content was used to

    produce brake anchor B, which resulted in lower pearlite

    content at approximately the same hardness.

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    Figure 1a. Straight-on view of brake anchor designs A and B.

    Figure 1b. Inclined view of brake anchor designs A and B.

    Two tests were selected for this study: pull and impact.

    The pull test simulated the component loading on the

    vehicle and the impact test simulated the worst case

    handling condition that might be encountered in the

    foundry or machine shop.

    The pull test loads the brake anchor under conditions

    similar to those seen in service. Here, a rigid fixture,

    which would be the steering knuckle on a vehicle, was

    attached to the lower, moveable ram on a hydraulic load

    frame, the brake anchor was bolted to the fixture, the load

    arm swung into position (this arm was connected to the

    upper, fixed ram) and the brake anchor pulled to failure,

    Figures 5a and b. In this test, the load was applied off-

    center and the brake anchor rotated under the attachment

    bolts. This produced a bending stress. Since the brake

    anchor rotated under the bolt, the measured load was a

    function of bolt torque. Production bolts, a specified

    torque value and a specified thread locking adhesive set

    up time were used. During the pull test, the thin tie bar

    broke followed by failure of the thicker section and

    sometimes the upper bolt. Looking more closely at the

    sample orientation, a clear difference in the location of a

    reduced section or pocket on the thicker section of the

    driver side and passenger side castings is evident. The

    importance of this difference will be discussed later.

    Figure 2. Cross sections through the tie bar of brake anchor designsA (left) and B (right). A mm scale is on the bottom of the photograph

    Figure 3a. Typical microstructure in the tie bar region of brake anchordesign A showing well formed graphite nodules in a matrix of ~20%ferrite and 80% pearlite.

    1 mm

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    Figure 3b. Typical microstructure in the tie bar region of brake anchordesign B showing well formed graphite nodules in a matrix of ~30%ferrite and 70% pearlite.

    Figure 4. Carbides in tie bar of brake anchor design B.

    The impact test was developed to simulate the worst case

    loading condition that might occur in the production

    foundry or machine shop. In this test, the brake anchor

    was attached to a rigid fixture and a hydraulic ram

    punched the thin tie bar at a velocity of 254 mm per

    second, Figure 6. The load as a function of ram

    displacement was measured and recorded. From this

    data, the energy required to initiate a crack (area under

    the curve up to the point of maximum load) and the tota

    energy absorbed (area under the entire curve) was

    calculated by numerical integration. These values can be

    compared to various loading events in the foundry and

    machine shop to determine if damage might occur. A

    typical load versus displacement curve is shown in Figure

    7. The orientation of the tie bar cross section was critica

    in this test and thus, an additional angled support was

    necessary to allow the two different components to betested under identical loading conditions.

    Figure 5a. Typical pull test set-up.

    Figure 5b. Close-up of pull test set-up showing dial gages used fordisplacement measurement.

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    Figure 6. Typical impact test set-up.

    Figure 7. Typical load versus displacement curve for the impact test.

    The casting microstructure and chemistry, which

    determined material properties, had a significant effect on

    component performance. To vary the properties in a

    controlled manner, samples of both casting designs were

    sub-critically annealed (softened), normalized (hardened)

    or normalized and tempered. The microstructures were

    characterized using a fully automated Clemex image

    analyzer. All castings had better than 90% nodularity

    The tensile properties where determined from 6.3 mm

    diameter, 25.4 mm gage length tensile bars cut fromcastings. Five tensile bars of each condition were tested

    in accordance with ASTM E8 and the results averaged.

    The material properties of the as-cast and heat treated

    castings are listed in Table I.

    RESULTS AND DISCUSSION

    PULL TEST. The orientation of the specimen in the pul

    test fixture resulted in a difference in the measured load a

    failure of as much as 36%. The reason for this difference

    was the location of the fracture. Lower load at failure

    values were measured when fracture occurred through the

    thin pocket on the thicker section. Figures 8a and b and9a and b show the pull test specimens before and after

    testing. This was not an unexpected result since the

    amount of bending caused by rotation of the component

    during loading was greater near the load application point

    (upper half of the casting). An unforeseen consequence o

    this loading variation was rapid deterioration of the fixture

    for the orientation shown in Figures 9a and b. Due to the

    significantly higher load, the bolt hole tended to elongate

    with a subsequent loss of clamping ability, Figure 10. As

    the amount of bolt hole deformation increased, the

    measured load decreased. After 30 tests (five months)

    the measured average load at failure decreased by 11%.

    Since the purpose of this test was to verify that the

    production process was not changing, this apparent loss

    in load carrying capacity could be erroneously interpreted

    as a manufacturing problem instead of fixture wear. For

    the other fixture and orientation, the lower maximum load

    produced no significant fixture wear and stable month-to

    month average load at failure readings, which verified that

    the production process was not changing significantly

    from month to month. Typical average maximum load

    results are shown in Table II.

    Table I. Average Material Properties of Ductile Iron Brake Anchors

    Design Condition Microstructure UTS, MPa YS, MPa El, % E, GPaHardness,

    BHN

    A As-cast 20% F, 80% P 572 366 6.0 179 183

    A Normalized >99% pearlite 824 517 3.6 170 270

    A Normalized and 675oC tempered spheroidized pearlite 706 453 3.4 172 240

    B As-cast 30% F, 70% P 603 373 9.9 177 190

    B 730oC sub-critically annealed >99% ferrite 459 311 17.7 175 157

    B Normalized >99% pearlite 855 522 4.3 172 258

    B Normalized and 675oC tempered spheroidized pearlite 790 459 7.2 170 242

    0

    1,000

    2,000

    3,000

    4,000

    5,000

    6,000

    7,000

    8,000

    9,000

    10,000

    1.7 1.9 2.1 2.3 2.5 2.7

    Relative Displacement, mm

    Load,

    N

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    Figure 8a. Brake anchor design B driver side in the pull-test fixturebefore testing.

    Figure 8b. Brake anchor design B driver side in the pull-test fixtureafter testing. Note: brake anchor fractures through the reducedsection or pocket.

    Figure 9a. Brake anchor design B passenger side in the pull-testfixture before testing.

    Figure 9b. Brake anchor design B passenger side in the pull-testfixture after testing. Note: brake anchor fractures through the fullsection and not through the reduced section.

    pocket

    pocket

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    Table III. Effect of Loading Orientation on the Impact Properties of Brake Anchor Design B.

    Average

    Maximum

    Load

    (N)

    Average Crack

    Initiation

    Energy (joules)

    Average Deflection

    at Crack Initiation

    (mm)

    Average Total

    Absorbed Energy

    (joules)

    Average Total

    Deflection

    (mm)

    Load Perpendicular to

    Component12,827 46.15 5.08 77.23 10.74

    Load Perpendicular to

    Tie Bar9,196 39.53 6.97 62.73 14.00

    Table IV. Impact Properties of Ductile Iron Brake Anchors Tested with the Load Applied Perpendicular to the Tie Bar.

    Design Condition

    Average

    Maximum

    Load (N)

    Average Crack

    Initiation Energy

    (joules)

    Average

    Deflection at

    Crack Initiation

    (mm)

    Average Total

    Absorbed

    Energy (joules)

    Average

    Total

    Deflection

    (mm)A As-cast 11,597 48.47 6.79 150.33 26.68A Normalized 14,697 69.24 7.68 173.10 26.18

    A Normalized and tempered 12,878 121.87 12.73 215.85 27.40

    B As-cast 9,196 39.53 6.97 62.73 14.00B Sub-critically annealed 7,744 85.59 14.30 132.03 26.13B Normalized 11,134 52.15 7.70 89.47 14.83B Normalized and tempered 10,542 95.42 12.84 146.68 24.48

    Casting microstructure and chemistry, which determined

    material properties, and casting design had a significant

    effect on component performance. Ferrite is soft, weakand very ductile, pearlite is harder, stronger but less

    ductile, and carbides are very hard, very strong and

    brittle. Silicon decreases the amount of pearlite,

    increases the strength of ferrite and suppresses carbides.

    Therefore, the combination of material (microstructure and

    chemistry) and casting design determined the ultimate

    load bearing capacity and the ability to absorb impact.

    When the two designs were compared using similar

    loading conditions and similar microstructure, brake

    anchor design A absorbed more energy initiating a crack

    (22.6% for as-cast, 32.8% for normalized and 27.6% for

    normalized and tempered) and more total energy (139.6%

    for as-cast, 93.5% for normalized and 47.2% fornormalized and tempered) than brake anchor design B.

    The impact properties as a function of heat treatment and

    design are listed in Table IV.

    The sub-critical annealing (softening) heat treatment

    produced a slightly weaker but significantly tougher

    component that was not as stiff as the as-cast

    component, i.e., the load required to initiate a crack

    decreased slightly, the energy absorbed during fracture

    increased significantly, and the amount of deflection

    during fracture increased significantly.

    The normalizing (hardening) heat treatment produced a

    significantly stronger and slightly tougher component tha

    was approximately the same stiffness as the as-cas

    component, i.e., the load required to initiate a crack

    increased significantly, the energy absorbed during

    fracture increased slightly, and the amount of deflection

    during fracture was about the same.

    The normalizing and tempering heat treatment produced a

    slightly stronger and significantly tougher component tha

    was not as stiff as the as-cast component, i.e., the load

    required to initiate a crack increased slightly, the energyabsorbed during fracture increased significantly, and the

    amount of deflection during fracture increased

    significantly.

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    CONCLUSIONS

    1. In this study, a test that accurately simulated the

    orientation and loading conditions on a vehicle was a

    valuable proof test but was not the most appropriate

    test for verifying that consistent product was being

    produced month-to-month. For verifying product

    consistency, a test that produced consistent resultswas critical. In this study, the loading conditions on

    brake anchor design B - passenger side were such

    that deformation of the test fixture could occur and

    this deformation significantly affected the test data.

    2. To properly compare similar components, the

    orientation of the applied load must be consistent

    (preferably in the worst case orientation).

    3. In this study, brake anchor design A exhibited

    consistently better impact properties due to a slightly

    larger cross section and a more uniform cross

    sectional shape that minimized stress risers and the

    formation of carbides.

    4. Heat treatment had a significant effect on the energyrequired to initiate a crack and the total energy

    absorbed during fracture.

    ACKNOWLEDGMENTS

    The authors would like to acknowledge the assistance of

    Dale tenPas (INTERMET Technical Center, Lynchburg,

    VA), Ed Druschitz (summer intern) and Evan Shockley

    (Governors School intern) for performing the pull and

    impact tests, strain gage tests, metallography and tensile

    tests. Melanie Folks is also acknowledged for performing

    the various heat treatments on the castings evaluated in

    this study.

    CONTACT

    Dr. Alan P. Druschitz received his PhD in Metallurgical

    Engineering in 1982 from the Illinois Institute of

    Technology, Chicago, IL. He is currently the Director of

    Materials Research and Development for INTERMET

    Corporation. He is located at the INTERMET Technical

    Center, Lynchburg, VA 24502. He can be reached at

    [email protected] or (434) 237-8749.

    Before joining INTERMET Corporation, he was a staffresearch engineer for General Motors Corporation for

    fourteen years. He has been a member of the American

    Foundry Society for thirteen years, the Society of

    Automotive Engineers for twenty years and ASM

    International for twenty-five years. He is currently the Vice

    President of the Ductile Iron Society, a member of the

    Industrial Advisory Board for the Central Virginia

    Governors School and a Member of the Governors Board

    of Transportation Safety for the Commonwealth of Virginia.