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TMF tests were carried out on EN-GJSA-XNiSiCr35-5-2 at constant minimum temperature (400 °C) and varying maximum temperatures (Tmax = 700 °C, 800 °C, 900 °C) with hold times of 180 s at Tmax and two phase angles (in-phase (IP), 180° out-of-phase (OP)). The results showed a comparable strength under OP- and IP-TMF loading. At Tmax = 700 °C and 900 °C, the lifetime in IP-tests was slightly longer than that of OP-tests, while it is vice versa at Tmax = 800 °C. The IP-tests at Tmax = 900 °C showed a similar lifetime as OP-tests at Tmax = 700 °C and 800 °C, which was unexpected for such a high testing temperature. All IP-tests at Tmax = 900 °C showed a continuous cyclic softening from the beginning on, which was different from all other testing conditions. Complementary metallographic investigations indicated that under this test condition, intergranular creep damage is present in the volume of the test pieces.
The knowledge of the temperature-induced changes of the superconductor volume and of the thermomechanical behavior of the different coil and tooling materials is required for predicting the coil geometry and the stress distribution in the coil after the Nb3Sn reaction heat treatment. In this paper, we have measured the Young’s and shear moduli of the HL-LHC 11 T Nb3Sn dipole magnet coil and reaction tool constituents during in situ heat cycles with the dynamic resonance method. The thermal expansion behaviors of the coil components and of a free standing Nb3Sn wire were compared based on dilation experiments.
Austenitic cast iron was primarily used as material for pumps and mountings due to their excellent corrosion resistance. Certain grades, especially those with spherical graphite morphology, offer also a good high temperature strength and a high scaling resistance, which opened new fields of application e.g. for casing part of gas turbines, exhaust manifolds and turbo chargers. For such applications, a high ductility and creep resistance is beneficial, as exhibited by the studied alloy EN-GJSA-XNiSiCr35-5-2. Its high Ni-content produces the austenitic matrix, while Cr increases strength, hardness and scaling resistance.
The alloy is standardized according to DIN EN 13835 with respect to chemical composition and mechanical properties (strength, elongation at fracture, Young's modulus, hardness and impact energy) at room temperature. However, data on mechanical properties at high temperature were rarely published in the open literature.
In a recently completed research project, we comprehensively characterized the alloy EN-GJSA-XNiSiCr35-5-2 in terms of its temperature dependent mechanical behavior concerning strength and to isothermal as well as non-isothermal fatigue behavior. The results were used to calibrate a material and lifetime model. TMF tests were carried out with a constant minimum temperature (Tmin = 400 °C) and varying maximum temperatures (Tmax = 700 °C, 800 °C, 900 °C) with hold times of 180 s at Tmax and two phase angles (in-phase (IP), 180° out-of-phase (OP)).
The investigated alloy showed a strongly deviating TMF behavior as compared to ferritic SiMo alloys investigated in a previous project: the austenitic material exhibits a comparable strength under OP- and IP-TMF loading, while the ferritic alloys showed a distinct higher strength under IP- than under OP-TMF load. At Tmax = 700 °C and 900 °C, the lifetime of Ni-Resist in IP-tests is slightly longer than that of OP-tests, while it is vice versa at Tmax = 800 °C. The IP-tests at Tmax = 900 °C show a comparable lifetime as OP-tests at Tmax = 700 °C and 800 °C, which was unexpected for such a high testing temperature. When plotting the stress range versus N it becomes clear that the behavior at Tmax = 900 °C is different from the other investigated temperatures: at 700 °C and 800 °C the stress-curve exhibits a range of stabilized stress for both phase angles. This is also true for the OP-tests at Tmax = 900 °C. However, all IP-tests at Tmax = 900 °C show a continuous cyclic softening from the beginning on.
The stiffness of the test pieces decrease continuously with increasing number of cycles and their surfaces show numerous cracks. Complementary metallographic investigations showed that beside classical fatigue damage with cracks initiated at the surface, intergranular creep damage was found in the volume of the test pieces. Pores and cracks are formed at grain boundaries perpendicular to the applied load. This is also a distinct difference to the SiMo alloys.
The thermal shock behavior of three commercial-advanced ceramics (SSiC, MgO–PSZ, Al2O3) is characterized in air and vacuum applying a laser thermal shock. The available testing system permits the reproducible setting of defined temperature profiles in thin disks and allows a heating-up thermal shock in various media. Due to the accurate determination of the time- and space-resolved temperature distribution, the local stress state can be calculated as a function of time. It is shown that the thermal shock strength is highest for SSiC and lowest in Al2O3 with MgO–PSZ in between. The approach presented in this work allows quantifying the stress state at failure in terms of tangential tensile stress. The investigated environment does not affect the thermal shock resistance under the studied experimental conditions.
Thermal barrier coatings (TBCs) are used to increase the operating temperature of land-, sea-, or air-based turbines. As failure of the coating may result in serious damage of the turbine, reliable estimation of the lifetime is essential. Most experiments to assess the lifetime or to determine parameters for simulations of the behavior of TBCs are done by burner-rig-tests, where the operating conditions are simulated by cyclic heating of the surface and cooling of the backside of a coated sample.
In this work a possibility is presented to do comparable experiments by heating the surface with laser irradiation instead of a burner. For this purpose a Nd:YAG-laser with a maximum output power of 1?kW and a wavelength of 1064?nm is used. The laser spot can be moved by integrated optics across the sample surface to achieve homogeneous heating of the coating. Cooling of the backside is done by air. The temperature of the sample surface is determined by an infrared-camera which also enables the possibility to detect failures in the coating via thermography. Additionally, acoustic sensors attached to the sample holder are used to detect failures in the sample. The investigated ceramic material (yttria stabilized zirconia) has a very low absorption coefficient at the used laser wavelength. Therefore, a pre-treatment of the samples was needed to increase the absorption coefficient to be able to heat up the samples.
In this paper, the experimental setup and first experimental results are presented.
The room temperature tensile properties of iron with different purity levels (commercially pure, high-purity, and ultra-high-purity) were characterized at different strain rates in the framework of an international Round-Robin involving four laboratories (BAM, IMR-TU, NIST, and SCKCEN). The test results were collected and analyzed by NIST, and are presented in this Technical Note.
Data from all the participating laboratories were found in good agreement, thus allowing a clear assessment of the influence of strain rate and purity level on tensile properties (mechanical resistance and ductility). A clear increase of yield strength and, to a lesser extent, tensile strength was observed for all materials as strain rate increases and purity level decreases. The highest strain rate sensitivity was associated with the highest purity level (ultra-high-purity Fe). Ductility trends were less unequivocal, but typically an increase of elongation at fracture and reduction of area was detected as strain rate and purity level increase. Significant differences in tensile properties were observed between the two investigated types of high-purity Fe, which can be attributed to an influence of the production process in terms of melting environment (atmosphere and crucible), as well as differences in chemical compositions.
The load-independent Vickers hardness (HV) of the individual phases in a non-reacted Nb3Sn
wire has been measured and the yield strength (YS) of the individual components estimated
from the HV values. The YS and tensile strength (Rm) of the composite wire are calculated
according the rule of mixtures (ROM). Calculated tensile properties are compared with tensile
test results that were obtained for the entire composite wire, for the wire after removal of the
Cu stabiliser and for single Nb-7.5wt.%Ta fibres.
This study investigates the room‐ and high‐temperature (650 °C) tensile and low‐cycle‐fatigue behavior of Inconel 718 produced by laser powder bed fusion (PBF‐LB/M) with a four‐step heat treatment and compares the results to the conventional wrought material. The microstructure after heat treatment is characterized on different length scales. Compared to the wrought variant, the elastic and yield properties are comparable at both test temperatures while tensile strength, ductility, and strain hardening capacity are lower. The fatigue life of the PBF‐LB/M variant at room temperature is slightly lower than that of the wrought material, while at 650 °C, it is vice versa. The cyclic stress response for both material variants is characterized by cyclic softening, which is more pronounced at the higher test temperature. High strain amplitudes (≥0.7%) at room temperature and especially a high testing temperature result in the formation of multiple secondary cracks at the transitions of regions comprising predominantly elongated grain morphology and columns of stacked grains with ripple patterns in the PBF‐LB/M material. This observation and pronounced crack branching and deflection indicate that the cracks are controlled by sharp micromechanical gradients and local crystallite clusters.
The degradation mechanisms of state-of-the-art Nb-Ti/Cu superconductors are described, based on in-situ synchrotron X-ray diffraction measurements during heat treatment. A quantitative description of the Nb-Ti/Cu degradation in terms of critical current density, Cu stabiliser resistivity and mechanical composite strength is presented. In an applied magnetic field a significant critical current degradation is already observed after a 5-minute 400 °C heat treatment, due to variations of –Ti precipitate size and distribution within the Nb-Ti alloy filaments. A strong degradation of the strand mechanical properties is observed after several minutes heating above 550 °C, which is also the temperature at which the formation of Cu-Ti intermetallic phases is detected. Several minutes heating at 250 °C are sufficient to increase the RRR of the strongly cold work strands inside a Rutherford type cable from about 80 to about 240. Heating for several minutes at 400 °C does not cause a significant conductor degradation in self-field and, thus, leaves enough temperature margin for the electrical interconnection of Nb-Ti/Cu conductors with common low temperature solders.