Fatigue and creep crack propagation behaviour of Alloy 617 in the annealed and aged conditions
Creators
- 1. Idaho National Laboratory, PO Box 1625, MS 2213, Idaho Falls, ID 83415 (United States)
Description
The crack propagation behaviour of Alloy 617 was studied under various conditions. Elevated temperature fatigue and creep-fatigue crack growth experiments were conducted at 650 and 800 deg. C under constant stress intensity (ΔK) conditions and triangular or trapezoidal waveforms at various frequencies on as-received, aged, and carburized material. Environmental conditions included both laboratory air and characteristic VHTR impure helium. As-received Alloy 617 displayed an increase in the crack growth rate (da/dN) as the frequency was decreased in air which indicated a time-dependent contribution component in fatigue crack propagation. Material aged at 650 deg. C did not display any influence on the fatigue crack growth rates nor the increasing trend of crack growth rate with decreasing frequency even though significant microstructural evolution, including γ' (Ni3Al) after short times, occurred during ageing. In contrast, carburized Alloy 617 showed an increase in crack growth rates at all frequencies tested compared to the material in the standard annealed condition. Crack growth studies under quasi-constant K (i.e. creep) conditions were also completed at 650 deg. C and a stress intensity of K = 40 MPa√(m). The results indicate that crack growth is primarily intergranular and increased creep crack growth rates exist in the impure helium environment when compared to the results in laboratory air. Furthermore, the propagation rates (da/dt) continually increased for the duration of the creep crack growth either due to material ageing or evolution of a crack tip creep zone. Finally, fatigue crack propagation tests at 800 deg. C on annealed Alloy 617 indicated that crack propagation rates were higher in air than impure helium at the largest frequencies and lowest stress intensities. The rates in helium, however, eventually surpass the rates in air as the frequency is reduced and the stress intensity is decreased which was not observed at 650 deg. C. (authors)
Files
46040912.pdf
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Additional details
Publishing Information
- Imprint Title
- Structural Materials for Innovative Nuclear Systems (SMINS-3) - Workshop Proceedings, Idaho National Laboratory, Idaho Falls, United States, 7-10 October 2013
- Imprint Pagination
- 287 p.
- Journal Page Range
- p. 100-109
- Report number
- NEA-NSC-WPFC-DOC--2015-9
Conference
- Title
- Structural Materials for Innovative Nuclear Systems
- Acronym
- SMINS-3
- Dates
- 7-10 Oct 2013
- Place
- Idaho Falls (United States)
INIS
- Country of Publication
- Nuclear Energy Agency of the OECD (NEA)
- Country of Input or Organization
- Nuclear Energy Agency of the OECD (NEA)
- INIS RN
- 46040912
- Subject category
- S36: MATERIALS SCIENCE;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- AGING; CARBIDES; CARBURIZATION; CRACK PROPAGATION; CREEP; GRAIN BOUNDARIES; HELIUM; INCONEL 617; MECHANICAL TESTS; STRESS INTENSITY FACTORS; THERMAL FATIGUE
- Descriptors DEC
- ALLOY-NI54CR22CO13MO9; ALLOYS; ALUMINIUM ADDITIONS; ALUMINIUM ALLOYS; CARBON COMPOUNDS; CHROMIUM ALLOYS; COBALT ALLOYS; CORROSION RESISTANT ALLOYS; ELEMENTS; FATIGUE; FLUIDS; GASES; HARDENING; HEAT RESISTANT MATERIALS; HEAT RESISTING ALLOYS; INCONEL ALLOYS; MATERIALS; MATERIALS TESTING; MECHANICAL PROPERTIES; MICROSTRUCTURE; MOLYBDENUM ALLOYS; NICKEL ALLOYS; NICKEL BASE ALLOYS; NONMETALS; RARE GASES; SURFACE HARDENING; SURFACE TREATMENTS; TESTING; TRANSITION ELEMENT ALLOYS
Optional Information
- Notes
- 15 refs.