Long life fatigue strength design method for metallic material

• US 6,912,913 B2
• Filed: 03/11/2002
• Issued: 07/05/2005
• Est. Priority Date: 03/23/2001
• Status: Active Grant

• Current Assignee: Kyushu TLO Company Limited, NSK Limited
• Original Assignee: Kyushu TLO Company Limited, NSK Limited
• Inventors: Murakami, Yukitaka
• Primary Examiner(s): Lefkowitz, Edward
• Assistant Examiner(s): DAVIS, OCTAVIA L
• Application Number:
  US10/472,383
• Publication Number:
  US 20040112141A1
• Time in Patent Office: 1,212 Days
• Field of Search: 738/08, 738/06, 738/10, 738/13, 737/99, 737/89, 737/87, 735/77, 735/78, 420/111, 378/72, 72/53, 702/34, 428/544
• US Class Current: 73/808
• CPC Class Codes: G01N 2203/0073 Fatigue
• CPC Class Codes: G01N 2203/0218 Calculations based on experimental data
• CPC Class Codes: G01N 2203/0246 Special simulation of "in situ" conditions, scale models or dummies
• CPC Class Codes: G01N 3/32 by applying repeated or pulsating forces
• CPC Class Codes: G01N 33/2045 Defects

Abstract

A long life fatigue strength design method for a metallic material is capable of allowing design of an optimum mechanical part according to a set service life by considering an increase in ODA (area affected by hydrogen observed blackish by a metallurgical microscope) size according to the assumed service life of the mechanical part. The method includes obtaining, from the results of a fatigue test, a functional relation between the number of stress cycles to failure and the size of a hydrogen affected area around an inclusion affected by trapped hydrogen. From the functional relation, equivalent defect sizes as the sizes of the inclusions after growth corresponding to the assumed number of cycles of working stress on the mechanical part using the metallic material are obtained, and the mechanical part is designed using the equivalent defect sizes in the calculation of a long life fatigue strength such as allowable stress, whereby a failure life design can be performed with the ODA size growth taken into account according to the assumed service life of the mechanical part.

Claims

1. A long-life fatigue strength design method for a mechanical part to be made of a metallic material, comprising:

determining a functional relationship between a number of stress cycles to failure and a size of a trapped-hydrogen-affected area around a non-metallic inclusion in the metallic material, said determining of the functional relationship being based on a fatigue test performed on a portion of the metallic material;

determining an equivalent defect size, the equivalent defect size being a size of the non-metallic inclusion after growth corresponding to an assumed number of working stress cycles on a mechanical part to be made of the metallic material, said determining of the equivalent defect size being based on the determined functional relationship; and

designing the mechanical part by using the equivalent defect size in a calculation of an ultra-long life fatigue strength.

2. The method of claim 1, wherein:

said determining of the functional relationship comprises preparing a graph illustrating the functional relationship, the graph having;

a first axis indicating the number of stress cycles to failure, N_f; and

a second axis indicating a ratio √

(area′

)/√

(area), wherein √

(area′

) is the equivalent defect size expressed by the square root of the sum of areas A₀ and A₁, in which A₀ is an area of the non-metallic inclusion in the metallic material at fatigue failure origin, in which A₁ is an area of the trapped-hydrogen-affected area, and in which √

(area) is an initial size of the non-metallic inclusion expressed by the square root of area A₀; and

said determining of the equivalent defect size comprises determining the equivalent defect size, √

(area′

), corresponding to the inclusion initial size, √

(area), by finding on the graph a value on the second axis corresponding to the assumed number of working stress cycles on the first axis.

3. The method of claim 2, further comprising:

preparing a second graph of statistics of extreme value distribution of sizes of the non-metallic inclusions at fatigue failure origins in the metallic material; and

wherein said determining of the equivalent defect size includes moving the line of the second graph of statistics of extreme value distribution in parallel thereto based on a relationship between the equivalent defect size √

(area′

) and the inclusion initial size √

(area), so as to calculate a return period corresponding to a size of the mechanical part on the moved parallel line; and

said designing of the mechanical part comprises using a maximum equivalent defect size √

(area′

)_max* of a largest non-metallic inclusion in the metallic material to be used in the mechanical part in an estimate of allowable stress.

4. The method of claim 3, wherein the metallic material is high tensile steel.

5. The method of claim 3, wherein said designing of the mechanical part comprises using a formula having the maximum equivalent defect size √

(area′

)_max* as a parameter, the equation being as follows;

σ

=1.56(HV/9.8+120)/(√

(area′

)_max*)^1/6((1−

R)/2)^α

wherein;

σ

is the allowable stress (MPa) corresponding to the assumed number of cycles of working stress;

HV is the Vickers hardness (MPa);

R is the stress ratio (=minimum stress/maximum stress); and

α

=0.226+HV/9.8×

10<sup>−

4</sup>.

6. The method of claim 5, wherein the metallic material is high tensile steel.

7. The method of claim 2, wherein said designing of the mechanical part comprises using a formula having the maximum equivalent defect size √

(area′

)_max* as a parameter, the equation being as follows;

σ

=1.56(HV/9.8+120)/(√

(area′

)_max*)^1/6((1−

R)/2)^α

wherein;

σ

is the allowable stress (MPa) corresponding to the assumed number of cycles of working stress;

HV is the Vickers hardness (MPa);

R is the stress ratio (=minimum stress/maximum stress); and

α

=0.226+HV/9.8×

10<sup>−

4</sup>.

8. The method of claim 7, wherein the metallic material is high tensile steel.

9. The method of claim 2, wherein the metallic material is high tensile steel.

10. The method of claim 1, wherein the metallic material is high tensile steel.