Nonferrous for Heat Exchangers, · PDF filetAlloys for Heat Exchangers, Pumps, and Piping ... Figure 11 - Curve, Flexural Fatigue Curves, Cufenloy 40 (Annealed) Figure 12 - Curve,

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  • Io

    Fatigue Properties o f NonferroustAlloys for Heat Exchangers,

    Pumps, and Piping

    Assignment 86 1o8MEL R&D Report 232/66

    May 19656

    By

    M. R. Gross and R. C. Schwab

    U. S. NAVY1

    MARINE ENGINEER-ING LABORATORYI

    II apolis, Md/O t P ~ ,~

    .601

    DedicatcM To- PROGRESS IN MARINE ENGINEERIN(e

    Bet.st Available, Copy

    Distribution of this document is unlimited.

    ~O6 4'?~b OO

  • Fatigue Properties of NonferrousAlloys for Heat Exchangers,

    Pumps, and Piping

    Assignment 86 108MEL R&D Report 232/66

    May 1966

    By

    M. R. Gross and R. C. Schwab

    M. R. GROSS

    R. C. SCHWAB

    Approved by:A

    )istribution of thi~g"G~~umv,,,t is ur ime- d

    46 t% T%

  • ABSTRACT

    The fatigue behavior of 13 nonferrous

    alloys used for corrosion-resistant heat

    exchangers, pumps, and piping systems was

    investigated over a broad life spectrum of

    100 to 100-million cycles. Both cast and

    wrought copper-base and nickel-base alloys

    were studied. It is concluded that wrought

    Monel* and forged Ni-Al bronze have the

    highest fatigue strengths, whereas gun metal

    and valve bronze have the lowest. The effect

    of salt water on fatigue performance was not

    found to be highly significant. The use of

    Langer's equation to predict stress-cycle

    relationships gave satisfactory results for

    wrought alloys but appeared to be overly con-

    servative for cast alloys.

    II

    *Registered trade name of the International Nickel Company,Incorporated. C

    iii

  • MEL Report 232/66

    TABLE OF CONTENTS

    Page

    !RIBUTION LIST ii'RACT iii:ODUCTION 1:RIALS INVESTIGATED 2[OD OF TEST 2oURE CRITERIA 4rLTS OF TESTS 5'ARISON OF FATIGUE STRENGTHS 6!LUSIONS:RENCES

    8

    OF FIGURESFigure 1 - Drawing, Rotating Cantilever Beam

    Fatigue SpecimenFigure 2 - Drawing, Low-Cycle Fatigue SpecimenFigure 3 - Curve, Flexural Fatigue Curves, Gun Metal

    (Cast)Figure 4 - Curve, Flexural Fatigue Curves, Valve

    Bronze (Cast)Figure 5 - Curve, Flexural Fatigue Curves, Ni-Al

    Bronze (Cast)Figure 6 - Curve, Flexural Fatigue Curves, Ni-Al

    Bronze (Forged)Figure 7 - Curve, Flexural Fatigue Curves, Superston

    40 (cast)Figure 8 - Curve, Flexural Fatigue Curves, 70-30

    Cupronickel (Cast)Figure 9 - Curve, Flexural Fatigue Curves, 70-30

    Cupronickel (wrought)Figure 10 - Curve, Flexural Fatigue Curves, 90-10

    Cupronickel (Hard)Figure 11 - Curve, Flexural Fatigue Curves, Cufenloy

    40 (Annealed)Figure 12 - Curve, Flexural Fatigue Curves, Cufenloy

    40 (DSR)Figure 13 - Curve, Flexural Fatigue Curves, Cupro-

    nickel 707 (Wrought)Figure 14 - Curve, Flexural Fatigue Curves, Monel

    "E'T (Cast)Figure 15 - Curve, Flexural Fatigue Curves, Monel

    (Wrought)

    v

  • Introduction

    Many copper-base and nickel-base alloys are used in the con-

    struction of heat exchangers, pumps, and piping systems designed

    to handle fresh or saline water. In the selection of materials

    for such applications, consideration is given primarily to corro-

    sion resistance, erosion resistance, and heat transfer charac-

    teristics. In most applications the applied stress levels are

    low. Accordingly, the structural strength properties of the

    materials are relatively unimportant.

    In recent years, more and more attention has been given to

    the structural properties of these alloys because of (1) cost and

    weight reduction programs, (2) conservation of strategic materials,

    (3) development of new high-strength alloys, and (4) new applica-

    tions which impose high stress levels. Typical of the latter are

    sea-connected cooling systems for hydrospace vehicles.

    One of the most likely modes of mechanical failure in systems

    undergoing cyclic pressurization or thermal shock loading is

    metal fatigue. The frequency of stress cycling in such systems

    may vary from that of an occasional start-up and shutdown to

    vibrational forces developed by the movement of the heat-exchanger

    fluids. Little or no published information on the alloys used in

    this type of service was found in reviewing the literature several

    years ago. Accordingly, tests were conducted at the U. S. Navy

    Marine Engineering Laboratory to establish the fatigue behavior of

    1

  • ariety of corrosion-resistant nonferrous alloys. The results

    these tests are presented in this paper.

    .erials Investigated

    The 13 alloys investigated are listed in Table 1, together

    -h their chemical compocitions and tensile properties.

    .luded are the strength coefficient, K, and strain-hardening

    )onent, n, contained in the true-stress/true-strain relaticn-

    Lp:

    a = K en

    re are some deficiencies in the tensile properties of the cast

    :erials with respect to the governing specifications. This is

    be expected inasmuch as the specification requirements are

    aally based on separately cast test coupons, whereas the values

    ven in Table 1 were obtained on specimens removed from cast

    ates.

    thod of Test

    Two types of flexural fatigue specimens were used in the

    vestigation. The high-cycle fatigue tests were performed with

    tating cantilever-beam specimens having the dimensions shown in

    gure 1. These were constant deadweight load tests with a cycle

    equency of 1450 cpm. The smooth test lengths were circum-

    rentially and longitudinally polished to a metallographic

    nish.

    2

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  • The low-cycle fatigue tests were performed with equipment

    ibed previously.' Flat flexure-type specimens having the

    sions shown in Figure 2 were used. The short end of the

    men was held stationary, while the long end was flexed

    en mechanical stops by a hydraulic piston. One or more

    n gages (0.25-inch gage length) were attached to the mini-

    est section to record the longitudinal strain. The applied

    ng force was measurpd with a load cell. The total strain

    ACT, was obtained from strain gage readings, and the

    al bending-stress range was calculated from elastic stress

    las using the measured load range. Specimens were cycled

    ^pm.

    All of the fatigue tests were of the completely reversed

    (Fatigue ratio = -1). Whereas most of the specimens were

    d in air, a few were tested with Severn'River water con-

    usly wetting the test surface. Severn River water is a

    ish estuary water containing 1/6 to 1/3 the salt content

    tural seawater, depending on the season and the tide.

    ous fatigue tests in both Severn River water and natural

    ter havF. shown no significant differences in the effects

    e two media.

    re Criteria

    Failure in the high-cycle, rotating cantilever-beam tests

    sted of complete fracture. Failure in the low-cycle fatigue

    4

  • tests was defined as one or more surface cracks 3/16 to I/4 inch

    in length.

    Results of Tests

    The results of the tests are plotted in log-log form in

    Figures 3 through 15. Two methods have been used in analyzirvj

    the data. The top graph in each figure is the SR vs N relation-

    ship for the data, where SR is the nominal reversed bending

    stross and N is Lhe number of cycles to failure. SR was calcu-

    lated from the elastic stress formula

    SR =21~

    where AM = bending moment range, in-lb.

    c = distance from neutral axis to outermost fiber at

    minimum cross section, in.

    I = moment of inertia of minimum cross section, in.4

    The bottom graph in each figure is the SPE vs N relationship

    for the data, where SPE is the reversed pseudoelastic or apparent

    elastic stress calculated as follows:

    SPE = 6ET.E ..... (2)

    2

    where ACT = total strain range as determined from strain gages

    on the test section, in/in.

    E = modulus of elasticity (Table 1), psi.

    5 -

  • urvilinear relationship between Spr and N was obtained by

    fitting the following relationship to the data.

    _PE = c + SE .....

    Nm

    C and m = best-fit constants

    SE = endurance limit or fatigue strength at 10s

    cycles, psi.

    _st-fit equation for the SPE vs N data is given in each

    a.

    Equation (3) is a generalization of the following equation

    sed by Langer 2 for predicting the SPE vs N fatigue curve

    tensile test data.

    _ E in ( 00 +S ..... (4