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US4959548A Expired / Lapsed US ⏱️ 0.0 years remaining

Neutron apparatus for measuring strain in composites

Assignee: United States Department of Energy
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Filing: 1989-05-02
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Granted: 1990-09-25
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Expires: 2009-05-02
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Abstract

Abstract A method and apparatus for orienting a pulsed neutron source and a multi-angle diffractometer toward a sample of a ceramic-matrix or metal-matrix composite so that the measurement of internal strain (from which stress is calculated) is reduced to uncomplicated time-of-flight measurements.

Inventors

  • 👤 David S. Kupperman
  • 👤 Saurindranath Majumdar
  • 👤 John F. Faber, Jr.
  • 👤 J. P. Singh

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-02 05:58
CPC Classifications
G; G01; G01N; G01N23/00; G01N23/20; G01N23/207; G01N23/2073; G01L; G01L1/00; G01L1/25

Claims Analysis

Total Claims: 15
Claim 1
Independent Claim 70 words
A method for real-time simultaneous measurement of strain in the constituents of a composite comprising: directing a polychromatic beam of neutrons from a pulsed source toward a sample, orienting a multi-angle diffractometer so that two opposite detectors are on a line perpendicular to said neutron beam, measuring, using Bragg's law, the strain on a vector bisecting the angle between said neutron beam and said line perpendicular to said neutron beam.
Claim 2
Independent Claim 70 words
A method for real-time simultaneous measurement of strain in the constituents of a composite comprising: directing a polychromatic beam of neutrons from a pulsed source toward a sample, orienting a multi-angle diffractometer so that two opposite detectors are on a line perpendicular to said neutron beam, measuring, using Bragg's law, the strain on a vector bisecting the angle between said neutron beam and said line perpendicular to said neutron beam.
Claim 3
Dependent Claim 14 words
The method of claim 1 wherein said sample is a ceramic-matrix or metal-matrix composite.
Claim 4
Dependent Claim 44 words
The method of claim 2 wherein said sample is oriented so that a line parallel to the longitudinal direction of the fiber embedded in said ceramic-matrix or metal-matrix composite bisects the angle between said neutron beam and said line perpendicular to said neutron beam.
Claim 5
Dependent Claim 38 words
The method of claim 3 including, calculating, using Bragg's law, the strain parallel to the longitudinal direction of the fibers and the strain perpendicular to the longitudinal direction of the fibers embedded in said ceramic-matrix or metal-matrix composite.
Claim 6
Dependent Claim 33 words
The method of claim 4 including collimating said neutron beam and orienting said neutron beam toward a small volume within said ceramic-matrix or metal-matrix composite and measuring the strain within said small volume.
Claim 7
Dependent Claim 33 words
The method of claim 5 including orienting said neutron beam toward a multiplicity of small volumes within said ceramic-matrix or metal-matrix composite and averaging the strain measured within said multiplicity of small volumes.
Claim 8
Dependent Claim 37 words
The method of claim 4 including calculating the residual stress in a ceramic-matrix or metal-matrix composite by comparing the time-of-flight of neutrons in an unstressed sample to the time of flight of neutrons in a stressed sample.
Claim 9
Dependent Claim 31 words
The method of claim 7 including validating models for determination of residual stress by comparing residual stress as projected by said models to the results of said calculations of residual stress.
Claim 10
Dependent Claim 18 words
The method of claim 2 wherein said sample is a composite of A1 2 O 3 and SiC.
Claim 11
Dependent Claim 38 words
The method of claim 9 wherein said sample is oriented so that a line parallel to the {111} plane of the SiC whisker bisects the angle between said neutron beam and said line perpendicular to said neutron beam.
Claim 12
Independent Claim 71 words
A method of determining the strain at the fiber-matrix interface in a ceramic-matrix or metal-matrix composite comprising: determining the lattice spacing d over a volume of a strain-free powdered sample of a ceramic-matrix or metal-matrix composite, determining the lattice spacing d 0 associated with a particular lattice plane in a stressed sample of said composite, calculating the strain associated with said lattice plane using the formula e=(d-d 0 )/d 0 .
Claim 13
Independent Claim 71 words
A method of determining the strain at the fiber-matrix interface in a ceramic-matrix or metal-matrix composite comprising: determining the lattice spacing d over a volume of a strain-free powdered sample of a ceramic-matrix or metal-matrix composite, determining the lattice spacing d 0 associated with a particular lattice plane in a stressed sample of said composite, calculating the strain associated with said lattice plane using the formula e=(d-d 0 )/d 0 .
Claim 14
Independent Claim 52 words
An apparatus for the real-time measurement of strain comprising: a pulsed neutron source emitting a neutron beam, a multi-angle diffractometer oriented so that two opposite detectors are on a line perpendicular to said neutron beam, means for determining the time of flight of said diffracted neutrons from a sample to said detectors.
Claim 15
Independent Claim 52 words
An apparatus for the real-time measurement of strain comprising: a pulsed neutron source emitting a neutron beam, a multi-angle diffractometer oriented so that two opposite detectors are on a line perpendicular to said neutron beam, means for determining the time of flight of said diffracted neutrons from a sample to said detectors.

References Cited (Backward Citations)

US3934138A Cited
SU1293594A1 Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1993-09-24 1994-03-26 1994-09-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1997-09-24 1998-03-26 1998-09-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2001-09-24 2002-03-26 2002-09-25 $7700.00 Window Closed / Lapsed

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