US4353255A
Expired / Lapsed
US
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Method for determining shape of crack
Assignee: Hitachi Ltd
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Filing: 1981-01-02
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Granted: 1982-10-12
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Expires: 2001-01-02
Abstract
Abstract AE signals due to a crack developed in a metal test object are detected by a number of AE sensors mounted on the metal test object. Based on time differences between the signals from the respective AE sensors, crack source points are determined. Then, based on the crack source points, a crack source plane is determined. The crack source plane is divided into a number of areas and a point of maximum number of crack source points in each of the areas is determined. Based on the points of maximum number of crack source points in the respective areas, a shape of the crack in the test object is determined.
Inventors
- 👤 Yoshio Fukuda
- 👤 Kunio Enomoto
- 👤 Tsutomu Masumoto
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 16:33
CPC Classifications
G; G01; G01N; G01N29/00; G01N29/14; G01H; G01H1/00; G01S; G01S5/00; G01S5/18; G01S5/22; G01N2291/00; G01N2291/02; G01N2291/028; G01N2291/02854; G01N2291/0289
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
99 words
A method for detecting a shape of a crack comprising the steps of detecting acoustic emissions produced due to the crack developed in a test object by a plurality of acoustic emission detecting means mounted on said test object, determining positions of crack source points in said test object based on differences in time points of signals produced by said acoustic emission detecting means, determining a crack source plane based on the positions of said crack source points, and determining the shape of the crack in said crack source plane based on a distribution of said crack source points.
Claim 2
Independent Claim
99 words
A method for detecting a shape of a crack comprising the steps of detecting acoustic emissions produced due to the crack developed in a test object by a plurality of acoustic emission detecting means mounted on said test object, determining positions of crack source points in said test object based on differences in time points of signals produced by said acoustic emission detecting means, determining a crack source plane based on the positions of said crack source points, and determining the shape of the crack in said crack source plane based on a distribution of said crack source points.
Claim 3
Dependent Claim
80 words
A method according to claim 1, further comprising the steps of defining an x-axis and a y-axis orthogonal to each other in said crack source plane, determining first positions each providing a peak number of crack source points along the y-axis in each of n first divided areas which are derived by dividing said crack source plane into n areas along the x-axis, and determining the shape of the crack in said crack source plane based on said first positions.
Claim 4
Dependent Claim
28 words
A method according to claim 2, further comprising a step of displaying a curve connecting said first positions of said first divided areas of said crack source plane.
Claim 5
Dependent Claim
107 words
A method according to claim 1, further comprising the steps of defining an x-axis and a y-axis orthogonal to each other in said crack source plane, determining two second positions each providing one half of a peak number of the crack source points along the y-axis in each of n first divided areas derived by dividing said crack source plane into n areas along the x-axis, determining third positions in said first divided areas each of which is at equi-distance from said two second positions, and determining the shape of the crack in said crack source plane based on said third positions in said first divided areas.
Claim 6
Dependent Claim
28 words
A method according to claim 4, further comprising a step of displaying a curve connecting said third positions in said first divided areas of said crack source plane.
Claim 7
Dependent Claim
126 words
A method according to claim 2 or 4, further comprising the steps of dividing a curve connecting said first positions or said second positions in said first divided areas into m segments, determining two fourth positions each providing one half of a peak number of the crack source points in a direction orthogonal to said segment in each of second divided areas defined by two lines orthogonal to said segment and passing through the opposite ends of said segment in said crack source plane, determining fifth positions each of which are equi-distance from said two fourth positions in each of said second divided areas, and determining the shape of the crack in said crack source plane based on said fifth positions in said second divided areas.
References Cited (Backward Citations)
US3985024A
Cited
US4033179A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1985-10-11 | 1986-04-12 | 1986-10-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-10-11 | 1990-04-12 | 1990-10-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-10-11 | 1994-04-12 | 1994-10-12 | $7700.00 | Window Closed / Lapsed |