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Fatigue Characterization of Alloy 10: A 1300f Disk Alloy for Small Gas Turbine Engines

AUTHOR Nasa, National Aeronautics and Space Adm
PUBLISHER Independently Published (09/19/2018)
PRODUCT TYPE Paperback (Paperback)

Description
A detailed fatigue characterization of Alloy 10, a high strength nickel-based disk alloy, was conducted on test coupons machined from a 'pancake' forging. Smooth bar, strain controlled fatigue testing at various R-ratios was run at representative bore, 750 F, and rim, 1300 F, temperatures. This was followed by notch fatigue testing (Kt=2) run under load control. Analysis of the fatigue data using a Smith-Watson-Topper approach and finite element analysis of the notch root was employed to understand material behavior in these tests. Smooth bar fatigue data showed a significant R-ratio dependence at either test temperature which could be accounted for using a Smith-Watson-Topper parameter (SWT). In general, fatigue life was longer at 750 F than 1300 F for a given SWT. For notch fatigue tests, life was longer at 750 F than 1300 F but only at higher stresses. This was attributed to differences in alloy strength. At lower stresses, finite element analysis suggested that convergence of fatigue life at both temperatures resulted from relaxation of stresses at the notch root in the 1300 F tests.Gayda, JohnGlenn Research CenterFATIGUE (MATERIALS); FATIGUE LIFE; FATIGUE TESTS; HIGH STRENGTH ALLOYS; NICKEL ALLOYS; ENGINE DESIGN; FINITE ELEMENT METHOD; NOTCH TESTS...
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Product Details
ISBN-13: 9781723840609
ISBN-10: 1723840602
Binding: Paperback or Softback (Trade Paperback (Us))
Content Language: English
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Page Count: 44
Carton Quantity: 93
Product Dimensions: 8.50 x 0.09 x 11.02 inches
Weight: 0.28 pound(s)
Country of Origin: US
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Science | Space Science - General
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A detailed fatigue characterization of Alloy 10, a high strength nickel-based disk alloy, was conducted on test coupons machined from a 'pancake' forging. Smooth bar, strain controlled fatigue testing at various R-ratios was run at representative bore, 750 F, and rim, 1300 F, temperatures. This was followed by notch fatigue testing (Kt=2) run under load control. Analysis of the fatigue data using a Smith-Watson-Topper approach and finite element analysis of the notch root was employed to understand material behavior in these tests. Smooth bar fatigue data showed a significant R-ratio dependence at either test temperature which could be accounted for using a Smith-Watson-Topper parameter (SWT). In general, fatigue life was longer at 750 F than 1300 F for a given SWT. For notch fatigue tests, life was longer at 750 F than 1300 F but only at higher stresses. This was attributed to differences in alloy strength. At lower stresses, finite element analysis suggested that convergence of fatigue life at both temperatures resulted from relaxation of stresses at the notch root in the 1300 F tests.Gayda, JohnGlenn Research CenterFATIGUE (MATERIALS); FATIGUE LIFE; FATIGUE TESTS; HIGH STRENGTH ALLOYS; NICKEL ALLOYS; ENGINE DESIGN; FINITE ELEMENT METHOD; NOTCH TESTS...
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Paperback