US4881030A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method and apparatus for measuring and precisely locating internal tensile stresses in hardened regions of components by measuring coercive field strength and barkhausen noise amplitude
Assignee: Siemens AG
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Filing: 1988-04-18
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Granted: 1989-11-14
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Expires: 2008-04-18
Abstract
Abstract A method and apparatus for ascertaining internal stresses in a hardened region to be tested for a component made of a predetermined material includes measuring coercive field strength and amplitude of magnetic Barkhausen noise as a function of mechanical stress and hardness in calibration samples of a predetermined material of known hardness and known internal stress. Calibration functions are ascertained from the measured values indicating the dependency of the hardness and the amplitude of the magnetic Barkhausen noise as functions of the hardness and mechanical stress. The coercive field strength and the amplitude of the magnetic Barkhausen noise is measured in a location-dependent manner over the region of the component to be tested. The measured values of the coercive field strength and the amplitude of the magnetic Barkhausen noise are converted in the region to be tested into location-dependent hardness and into location-dependent mechanical stress using the ascertained calibration functions. The location-dependent mechanical stress and the location-dependent hardness in the region to be tested are present independently of one another and are available for further processing.
Inventors
- 👤 Erwin Stuecker
- 👤 Gerhard Hofer
- 👤 Dietmar Koch
- 👤 Uenal Guenes
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 16:14
CPC Classifications
G; G01; G01N; G01N27/00; G01N27/72; G01N27/725
Claims Analysis
Total Claims: 18
Claim 1
Independent Claim
177 words
Method for ascertaining internal stresses in a hardened region to be tested of a component made of a predetermined material, which comprises: (a) measuring coercive field strength and amplitude of magnetic Barkhausen noise as a function of mechanical stress and hardness in calibration samples of a predetermined material of known hardness and known internal stress; (b) ascertaining calibration functions from the measured values indicating the dependency of the hardness and the amplitude of the magnetic Barkhausen noise as functions of the hardness and mechanical stress; (c) measuring the coercive field strength and the amplitude of the magnetic Barkhausen noise in a location-dependent manner over the region of the component to be tested; (d) converting the measured values of the coercive field strength and the amplitude of the magnetic Barkhausen noise in the region to be tested into location-dependent hardness and into location-dependent mechanical stress using the ascertained calibration functions, and providing the location-dependent mechanical stress and the location-dependent hardness in the region to be tested independently of one another and in a form available for further processing.
Claim 2
Dependent Claim
177 words
Method for ascertaining internal stresses in a hardened region to be tested of a component made of a predetermined material, which comprises: (a) measuring coercive field strength and amplitude of magnetic Barkhausen noise as a function of mechanical stress and hardness in calibration samples of a predetermined material of known hardness and known internal stress; (b) ascertaining calibration functions from the measured values indicating the dependency of the hardness and the amplitude of the magnetic Barkhausen noise as functions of the hardness and mechanical stress; (c) measuring the coercive field strength and the amplitude of the magnetic Barkhausen noise in a location-dependent manner over the region of the component to be tested; (d) converting the measured values of the coercive field strength and the amplitude of the magnetic Barkhausen noise in the region to be tested into location-dependent hardness and into location-dependent mechanical stress using the ascertained calibration functions, and providing the location-dependent mechanical stress and the location-dependent hardness in the region to be tested independently of one another and in a form available for further processing.
Claim 3
Dependent Claim
14 words
Method according to claim 1, which comprises selecting a turbine blade as the component.
Claim 4
Dependent Claim
25 words
Method according to claim 1, which comprises selecting the predetermined material for the calibration samples from the group consisting of X20Cr13 and X10CrNiMo V12 22.
Claim 5
Dependent Claim
27 words
Method according to claim 1, which comprises converting the measured values of the coercive field strength and the amplitude of the magnetic Barkhausen noise into Vickers hardness.
Claim 6
Dependent Claim
23 words
Method according to claim 1, which comprises carrying out the further processing in the form of a visual display of the stress distribution.
Claim 7
Dependent Claim
15 words
Method according to claim 1, which comprises carrying out the further processing in a computer.
Claim 8
Dependent Claim
22 words
Method according to claim 1, which comprises selecting the region to be tested as the hardened leading edge of a turbine blade.
Claim 9
Dependent Claim
23 words
Method according to claim 1, which comprises selecting the region to be tested as the hardened leading edge of a low-pressure turbine blade.
Claim 10
Dependent Claim
51 words
Method according to claim claim 1, which comprises moving an exciter and a measurement pickup system at a defined speed on a defined measurement track in the region to be tested, and obtaining a local association of the measured values from the chronological succession thereof as a result of the movement.
Claim 11
Dependent Claim
148 words
Apparatus for ascertaining internal stresses in a hardened region to be tested of a component made of a predetermined material, comprising: (a) an exciter system and a measurement pickup system measuring at least one of amplitude of magnetic Barkhausen noise and coercive field strength and producing measured values; (b) electronic evaluation means connected to said measurement pickup system for processing the measured values of the coercive field strength and the amplitude of the magnetic Barkhausen noise in parallel; (c) said electronic evaluation means including at least one memory having calibration data or calibration functions for at least one material relating to dependencies between the Barkhausen noise amplitude, the coercive field strength, the hardness and the mechanical stress; and (d) said electronic evaluation means including a conversion stage converting the measured values into material properties of hardness and stress using the calibration data stored said at least one memory.
Claim 12
Dependent Claim
148 words
Apparatus for ascertaining internal stresses in a hardened region to be tested of a component made of a predetermined material, comprising: (a) an exciter system and a measurement pickup system measuring at least one of amplitude of magnetic Barkhausen noise and coercive field strength and producing measured values; (b) electronic evaluation means connected to said measurement pickup system for processing the measured values of the coercive field strength and the amplitude of the magnetic Barkhausen noise in parallel; (c) said electronic evaluation means including at least one memory having calibration data or calibration functions for at least one material relating to dependencies between the Barkhausen noise amplitude, the coercive field strength, the hardness and the mechanical stress; and (d) said electronic evaluation means including a conversion stage converting the measured values into material properties of hardness and stress using the calibration data stored said at least one memory.
Claim 13
Dependent Claim
34 words
Apparatus according to claim 10, wherein said exciter system and said measurement pickup system are movable along a defined measurement path at a defined speed in a region of a component to be tested.
Claim 14
Dependent Claim
34 words
Apparatus according to claim 10, wherein said exciter system and said measurement pickup system are movable along defined measurement path at a defined speed in a region of a turbine blade to be tested.
Claim 15
Dependent Claim
30 words
Apparatus according to claim 11, wherein said exciter system is a magnetic exciter system also forming a magnetic holder for said measurement pickup system on the component to be tested.
Claim 16
Dependent Claim
30 words
Apparatus according to claim 12, wherein said exciter system is a magnetic exciter system also forming a magnetic holder for said measurement pickup system on the component to be tested.
Claim 17
Dependent Claim
26 words
Apparatus according to claim 13, wherein said magnetic exciter system includes a magnet yoke having two magnetic poles between which said measurement pickup system is movable.
Claim 18
Dependent Claim
26 words
Apparatus according to claim 14, wherein said magnetic exciter system includes a magnet yoke having two magnetic poles between which said measurement pickup system is movable.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1992-11-13 | 1993-05-15 | 1993-11-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1996-11-13 | 1997-05-15 | 1997-11-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2000-11-13 | 2001-05-15 | 2001-11-14 | $7700.00 | Window Closed / Lapsed |