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Page 1: DRSA Inreach

DRSA Inreach

Internal Stresses in Aluminum Engines

Data

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Introduction of research project Solidification of casting alloys Stresses and strains Crystal lattices Diffraction Neutrons Experimental design Data Analysis of data

Measuring Residual Stresses

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FCC Aluminum Diffraction Pattern

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Experimental Geometry

Detectors

Engine Head

Beam Aperture

Transmitted Neutron Beam

Scattered Neutrons

Monochromator

Sampling Volume

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Experimental Geometry

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Count scattered neutrons as a function of scattering angle for the Al (311)

For a neutron wavelength of 0.154906 nm the Al (311) peak is at 2θ of about 79 degrees

Plot counts against angle to map out the peak

Diffraction Peaks

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Peaks

77 77.5 78 78.5 79 79.5 80 80.50

500

1000

1500

2000

2500

Aluminum (311)

Scattering Angle (degrees)

Neu

tron

Cou

nts

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Goal is to measure strains and ultimately stresses Strain is measured relative to unstressed sample Therefore, repeat all measurements on

unstressed samples◦Made by cutting up the engine and re-measuring the

samples removed from the engine◦Removing the samples from engine relieves stresses

Reference Peak Positions

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Bragg’s Law has a Direction

IncidentBeam Scattered

Beam

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Look at three directions around the valve ports

Stress Components

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Stress Components

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Stress Components

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In 1-D, law was σ=Eε, where:◦ σ is stress,◦ E is Young’s Modulus and◦ ε is strain

More complicated in 3-D:

Where:◦ σ R,A,H is the Radial, Axial or Hoop stress (pick one) ◦ ε R,A,H is the Radial, Axial or Hoop Strain (pick one)◦ ν is Poisson’s Ratio

Hook’s Law in 3-D

),,,, (

211 HARHARHARE

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Al (311) Scattering Angle

Depth (mm) Radial Axial Hoop

0 78.7291° 78.8203° 78.7864°

6 78.7701° 78.7942° 78.7632°

12 78.6396° 78.7036° 78.6999°

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From the peak angles, calculate the “d” spacings From the “d” spacings, calculate the strains using:◦Strain ε = (d-d0)/d0 , for Al (311) do = 0.122082 nm

From Young’s Modulus (E) and Poisson’s ratio (ν), calculate components of stress using:

Al E=68.9 GPa, ν=0.33 For R,A,H pick one component each time and

recalculate

Data Analysis

),,,, (

211 HARHARHARE

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Next week: Analysis of Data

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Poisson’s Ratio

Isotropic MaterialStrain in x-direction is εx = ΔL/LStrain in transverse (y and z) direction is εT = ΔL’/LPoisson’s Ratio is ν = - εT/εx


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