Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2...

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Fatigue Workshop A12

Transcript of Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2...

Page 1: Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2 Workshop A12 – Goals Goal: –In this workshop our goal.

Fatigue

Workshop A12

Page 2: Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2 Workshop A12 – Goals Goal: –In this workshop our goal.

March 29, 2005Inventory

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Workshop Supplement

Fatigue Module

Workshop A12 – Goals

• Goal: – In this workshop our goal is to perform a Fatigue analysis of the

connecting rod model (ConRod.x_t) shown here. Specifically, we will analyze two load environments: 1) Constant Amplitude Load of 4500 N, Fully Reversed and 2) Random Load of 4500N.

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Workshop Supplement

Fatigue Module

. . . Workshop A12 - Start Page

• From the launcher start Simulation.

• Choose “Geometry > From File . . . “ and browse to the file “ConRod.x_t”.

• When DS starts, close the Template menu by clicking the ‘X’ in the corner of the window.

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Workshop Supplement

Fatigue Module

. . . Workshop A12 – Preprocessing

• Change the working unit system to metric (m, kg, Pa …).

1. “Units > Metric (m, kg, Pa, C, s)”

• Verify the material is set to “Structural Steel”.

2. Highlight the “Part 1” in the geometry branch.

3. If not, click in the “Material” field and “browse”.

1.

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Workshop Supplement

Fatigue Module

. . . Workshop A12 – Preprocessing

4. Select the “Structural_Steel” material and then click [Open].

4.

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Fatigue Module

. . . Workshop A12 – Preprocessing

• Apply the following boundary conditions (see next page):

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Workshop Supplement

Fatigue Module

. . . Workshop A12 – Preprocessing

5. Highlight the Environment branch.

6. Highlight the connecting rod surface shown…

7. Insert a force load.– “RMB > Insert > Force”

8. From the detail window change to “Components” and “Z = - 4500 N”.

6.

5.

7. 8.

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Fatigue Module

. . . Workshop A12 – Preprocessing

9. Highlight the Environment branch.

10. Highlight the connecting rod surfaces shown…

11. Insert a cylindrical support.– “RMB > Insert > Cylindrical Support”

• From the Details of “Cylindrical Support” window:

12. Set Radial=“Fixed”, Axial=“Free”, Tangential=“Free”

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9.

11.12.

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Fatigue Module

. . . Workshop A12 – Preprocessing

13.Highlight the Environment branch.

14.Highlight the connecting rod surface shown…

15. Insert a fixed support.– “RMB > Insert > Fixed Support”

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Fatigue Module

• Add results to Solution:

16.Highlight the solution branch.

17.RMB > Insert > Stress > Equivalent (von Mises).

18.RMB > Insert > Deformation > Total.

. . . Workshop A12 – Solution Setup

17.

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Fatigue Module

• Insert fatigue tool:

19.Highlight the solution branch.

20.RMB > Insert > Fatigue > Fatigue Tool.

. . . Workshop A12 – Solution Setup

20.

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Fatigue Module

• From the Details of “Fatigue Tool” window:

21.Specify a Fatigue Strength Factor (Kf) of .8 (material data represents a polished specimen and the in-service component is cast).

22.Specify fully reversed loading to create alternating stress cycles.

23.Specify a stress-life fatigue analysis (No mean stress theory needs to be specified since no mean stress will exist – fully reversed loading).

24.Specify that Von Mises stress will be used to compare against fatigue material data.

. . . Workshop A12 – Solution Setup

22.

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Fatigue Module

• Add results to the Fatigue Tool:

25. Insert “Safety Factor”:

– RMB > Insert > Fatigue > Safety Factor.

• From the Details of “Safety Factor” window:

26.Set the Design Life to 1e6 cycles.

. . . Workshop A12 – Solution Setup

25.

26.

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Fatigue Module

• Add results to the Fatigue Tool (cont.):

27. Insert “Fatigue Sensitivity”:– RMB > Insert > Fatigue > Fatigue Sensitivity

• From the Details of “Fatigue Sensitivity” window:

28.Specify a minimum base load variation of 50% (an alternating stress of 2250N) and a maximum base load variation of 200% (an alternating stress of 9000N).

. . . Workshop A12 – Solution Setup

27.

28.

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Fatigue Module

• Add results to the Fatigue Tool (cont.):

29. Insert “Biaxiality Indication”:– RMB > Insert > Fatigue > Biaxiality Indication

• Solve

. . . Workshop A12 – Solution Setup

29.

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Workshop Supplement

Fatigue Module

• View Results

• Highlight and plot the “Total Deformation” result.

. . . Workshop A12 – Results

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Fatigue Module

• Highlight and plot the “Equivalent Stress” result.

. . . Workshop A12 – Results

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Fatigue Module

• Highlight and plot the “Safety Factor” result for a design life of 1e6 cycles.

. . . Workshop A12 – Results

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Fatigue Module

• Highlight and plot the “Fatigue Sensitivity” result for a minimum base load variation of 50% and a maximum base load variation of 200%.

. . . Workshop A12 – Results

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Workshop Supplement

Fatigue Module

• Find the sensitivity of available life with respect to loading for a maximum base load variation of 400%. Note, must resolve to obtain the new Fatigue Sensitivity results.

. . . Workshop A12 – Results

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Workshop Supplement

Fatigue Module

• Highlight and plot the “Biaxiality Indication” result. Note, the stress state near the critical location is not far from uniaxial (.1~.2), which gives an added measure of confidence since the material properties are uniaxial. Recall, a biaxiality of zero corresponds to uniaxial stress, a value of –1 corresponds to pure shear, and a value of 1 corresponds to a pure biaxial state.

. . . Workshop A12 – Results

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Workshop Supplement

Fatigue Module

• Insert a second fatigue tool to analyze a random load of 4500N. Assume that we have strain gauge results that were collected experimentally from the component and that we know that a strain gauge reading of 200 corresponds to an applied load of 4500N:

30.Highlight the solution branch.

31.RMB > Insert > Fatigue > Fatigue Tool.

. . . Workshop A12 – Solution Setup

31.

30.

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Fatigue Module

• From the Details of “Fatigue Tool 2” window:

32.Specify a Fatigue Strength Factor (Kf) of .8 (material data represents a polished specimen and the in-service component is cast).

33.Specify fatigue loading as coming from a scale history and select scale history file containing strain gauge results over time (browse and open the “SAEBracketHistory.dat” file).

34.Define the scale factor to be .005 (we must normalize the load history so that the FEM load matches the scale factors in the load history file):

. . . Workshop A12 – Solution Setup

33.

34.

32.

005.gaugestrain 200

load FEM 1

gaugestrain 200

1000

1000

load FEM 1

lbs

lbs

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Fatigue Module

• From the Details of “Fatigue Tool” window (cont.):

35.Specify Goodman theory to account for mean-stress effects.

36.Specify that a signed Von Mises stress will be used to compare against fatigue material data (use signed since Goodman theory treats negative and positive mean stresses differently).

37.Specify a bin size of 32 (Rainflow and Damage matrices will be of dimension 32x32).

. . . Workshop A12 – Solution Setup

35.36.

37.

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Fatigue Module

• Add results to the Fatigue Tool 2:

38. Insert “Life”:

1. RMB > Insert > Fatigue > Life

39. Insert “Safety Factor”:– RMB > Insert > Fatigue > Safety Factor

• From the Details of “Safety Factor” window:

40.Set the Design Life to 1000 cycles.

. . . Workshop A12 – Solution Setup

39.

40.

38.

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Fatigue Module

• Add results to the Fatigue Tool (cont.):

41. Insert “Fatigue Sensitivity”:– RMB > Insert > Fatigue > Fatigue Sensitivity

• From the Details of “Fatigue Sensitivity” window:

42.Specify a minimum base load variation of 50% (an alternating stress of 2250N) and a maximum base load variation of 200% (an alternating stress of 9000N).

. . . Workshop A12 – Solution Setup

41.

42.

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Fatigue Module

• Add results to the Fatigue Tool (cont.):

43. Insert “Biaxiality Indication”:– RMB > Insert > Fatigue > Biaxiality Indication

44. Insert “Rainflow Matrix”:– RMB > Insert > Fatigue > Rainflow Matrix

. . . Workshop A12 – Solution Setup

43.

44.

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Fatigue Module

• Add results to the Fatigue Tool (cont.):

45. Insert “Damage Matrix”:– RMB > Insert > Fatigue > Damage Matrix

• From the Details of “Damage Matrix” window:

46.Set the Design Life to 1000 cycles.

• Solve

. . . Workshop A12 – Solution Setup

45.

46.

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Fatigue Module

• View Results

• Highlight and plot the “Life” result.

. . . Workshop A12 – Results

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Fatigue Module

• Highlight and plot the “Safety Factor” result for a design life of 1000 cycles.

. . . Workshop A12 – Results

If the loading history corresponded to the loading experienced by the part over a months time, the damage and FS will be at a design life of 1000 months. Note that although a life of only 112 loading blocks is calculated, the needed scale factor (since FS @ 1000=.64) is only .64 to reach a life of 1000 blocks.

Note, the “scale factor” is the scale factor for the loading to make it meet the life of 1000 months.

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Workshop Supplement

Fatigue Module

• Highlight and plot the “Fatigue Sensitivity” result for a minimum base load variation of 50% and a maximum base load variation of 200%.

. . . Workshop A12 – Results

Page 32: Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2 Workshop A12 – Goals Goal: –In this workshop our goal.

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Workshop Supplement

Fatigue Module

• Highlight and plot the “Biaxiality Indication” result.

. . . Workshop A12 – Results

Page 33: Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2 Workshop A12 – Goals Goal: –In this workshop our goal.

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Workshop Supplement

Fatigue Module

• Highlight and plot the “Rainflow Matrix” result.

. . . Workshop A12 – Results

Here, one can see from the rainflow matrix that the majority of the cycle counts are for low mean stress and low stress amplitude (range).

Page 34: Fatigue Workshop A12. Workshop Supplement Fatigue Module March 29, 2005 Inventory #002216 WSA12-2 Workshop A12 – Goals Goal: –In this workshop our goal.

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Workshop Supplement

Fatigue Module

• Highlight and plot the “Damage Matrix” result.

. . . Workshop A12 – Results

Although, from the previous slide, one saw that most of the counts were for the low mean and range bins, these do not cause the most damage at the critical location, as shown in this damage matrix.  Instead, the 'medium' stress amplitude cycles cause the most damage at the critical location.