Scatter in Dwell Time Cracking for a Ni-Based Superalloy in Combination With Overloads

Author:

Storgärds Erik1,Saarimäki Jonas2,Simonsson Kjell3,Sjöström Sören3,Gustafsson David4,Månsson Tomas5,Moverare Johan2

Affiliation:

1. Division of Solid Mechanics, Linköping University, Linköping SE-58183, Sweden e-mail:

2. Division of Engineering Materials, Linköping University, Linköping SE-58183, Sweden

3. Division of Solid Mechanics, Linköping University, Linköping SE-58183, Sweden

4. Siemens Industrial Turbomachinery AB, Finspång SE-61283, Sweden

5. GKN Aerospace Engine Systems, Trollhättan SE-46181, Sweden

Abstract

In this paper, scatter in crack growth for dwell time loadings in combination with overloads has been investigated. Multiple tests were performed for surface cracks at 550 °C in the commonly used high temperature material Inconel 718. The test specimens originate from two different batches which also provide for a discussion of how material properties affect the dwell time damage and overload impact. In combination with these tests, an investigation of the microstructure was also carried out, which shows how it influences the growth rate. The results from this study show that, in order to take overloads into consideration when analyzing spectrum loadings containing dwell times, one needs a substantial amount of material data available as the scatter seen from one batch to the other are of significant proportions.

Publisher

ASME International

Subject

Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering

Reference22 articles.

1. Larsen, J., and Nicholas, T., 1983, “Load Sequence Crack Growth Transients in a Superalloy at Elevated Temperature,” 14th National Symposium on Fracture Mechanics, Los Angeles, CA, June 30–July 2, Vol. II: Testing and Applications, ASTM STP 791, pp. II-536–II-552.

2. Hold-Time Effects in Elevated Temperature Fatigue Crack Propagation,1986

3. Effect of Frequency on Fatigue Crack Growth Rate of Inconel 718 at High Temperature,1987

4. Intergranular Crack Tip Oxidation Mechanism in a Nickel-Based Superalloy;Mater. Sci. Eng., A,1992

5. Elevated Temperature Fatigue Crack Growth in Alloy 718—Part I: Effects of Mechanical Variables;Fatigue Fract. Eng. Mater. Struct.,1993

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