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Showing papers on "Inconel published in 1971"


01 Jan 1971
TL;DR: Inconel 718 has very good weldability as discussed by the authors, but the difficulty of obtaining good penetration with the root pass is encountered in most nickel-base alloys and is due to the poor fluidity of the molten metal.
Abstract: Penetration In general, Inconel 718 has very good weldability. Welding tests were made using gas metal-arc (GMA) and gas tungsten arc (GTA) processes and satisfactory results were obtained. Welds were also made in the unaged and aged conditions and no major difficulties arose. The one problem always encountered was the difficulty of obtaining good penetration with the root pass. This is encountered in most nickel-base alloys and is due to the poor fluidity of the molten metal. It was therefore decided to study this aspect more closely and to try to

31 citations


Journal ArticleDOI
TL;DR: A thermodynamic theory has been used to predict the chromium content at equilibrium with chromium carbide particles and a matrix containing Ni-10Fe-16Cr for varying carbon contents and heat treatments as discussed by the authors.
Abstract: A thermodynamic theory has been used to predict the chromium content at equilibrium with chromium carbide particles and a matrix containing Ni-10Fe-16Cr for varying carbon contents and heat treatments Corrosion measurements and electron microscopic studies have been used to confirm the predictions made by the theory An important surface effect produced during the solution heat treatment is reported It is concluded that sensitization of Inconel 600 occurs by a chromium depletion mechanism similar to that which takes place in stainless steel

24 citations


Journal ArticleDOI
TL;DR: In this article, the reaction bands show evidence of grain boundary penetration and internal oxidation; the chromite phase contains little or no iron or nickel while the adjacent metallic phase is highly depleted of chromium.

10 citations


Journal ArticleDOI
TL;DR: In this paper, the authors investigated the creep properties of Inconel 718 under thermal cycling conditions and found that the creep rates were lower than the results of isothermal creep experiments.
Abstract: The creep properties of Inconel 718 under thermal cycling conditions were investigated. It was found that the creep rates under thermal cycling conditions are lower than the creep rates calculated from results of isothermal creep experiments. It was also found that an abrupt temperature decrease during steady-state creep is followed by a certain period of zero creep rate. It was shown that the decrease of strain rate during creep under cycling conditions is due to this stopping effect.

7 citations


Journal ArticleDOI
01 Oct 1971
TL;DR: In this article, the rate of formation of intermetallic compounds between aluminum and three ferritic steels, one austenitic steel, and Inconel, was determined by an electrolytic method.
Abstract: The rate of formation of intermetallic compounds between aluminum and three ferritic steels, one austenitic steel, and Inconel has been determined by an electrolytic method. The steel was held at zero potential with respect to aluminum in a NaCl-AlCl3 melt, and the current measured. Comparison of measured thicknesses of intermetallic layers with those calculated from the integrated current gives an average deposition efficiency of 95 pct. For the Type 304 austenitic steel thickness \((mm) = k\sqrt {time}\) (min), andk is given by logk= −6400/T(0K) +4.469. The ferritic steels show a linear rate of growth of Al5Fe2, with an initial higher rate such that extrapolation of the linear curve back to zero time gives an intercept of 16±7 μm. The rate constants (mm min−1) may be represented by log (rate)=α/T+β, and the values of α and β are respectively −2650 and−0.788 for a plain carbon steel,−6580 and + 3.469 for a 1.3 pct Cr, 0.4 pct Mo steel, and−5950 and +2.466 for a 2.2 pct Cr, 0.9 pct Mo steel. The more highly alloyed steels are thus attacked, more slowly. Results for Inconel could not be fitted to any simple equation. With the ferritic steels growth is by aluminum diffusing inwards; with Inconel it is by nickel diffusing outward.

5 citations


Journal ArticleDOI
01 Jan 1971-JOM
TL;DR: Although INCONEL* nickel-chromium-molybdenum alloy has good resistance to sensitization caused by carbide precipitation, some sampies of the material have less resistance than others as discussed by the authors.
Abstract: Although INCONEL* nickel-chromium-molybdenum alloy 625 has good resistance to sensitization caused by carbide precipitation, some sampies of the material have been found to have less resistance than others. Laboratory studies of the precipitation reactions in the alloy give no indication that any particular phase is responsible for the increased corrosion rate. The studies do show, however, that the degree of sensitization is related to the total chromium content of the precipitates, and that control of processing, particularly annealing procedures, can produce material having maximum resistance to sensitization.

5 citations



Journal ArticleDOI
TL;DR: In this paper, an experimental study made of the effect that the corrosive environment due to high temperature gives on the stress-rupture strength and the fatigue strength of Inconel 700 which is heat resisting Ni-base alloy.
Abstract: Hereunder is reported an experimental study made of the effect that the corrosive environment due to high temperature gives on the stress-rupture strength and the fatigue strength of Inconel 700 which is heat resisting Ni-base alloy.The experiments were carried out in such environments as residual fuel combustion gas, vanadium ash, mixture of vanadium ash and nickel sulfide and their combination at 700° and 750°C. The results are summarized as follows:(1) The strength of the alloy showed a remarkable declining tendency in sulfur-bearing environment.(2) The corrosive effect was found larger on the whole in the fatigue test than in the stress-rupture test. This is presumably due to the fact that the alloy is more sensitive to intergranular corrosion and notches under repeated stress than under static stress.(3) The estimation of the stress-rupture life of this alloy under gradually increasing stress caused by corrosion was investigated by using linear damage rule. The estimated life showed critical value when the corrosive environment is due to sulfur content.

3 citations



Journal ArticleDOI
TL;DR: The terminal characteristics of Inconel 600 alloy (76% Ni, 16% Cr, 7% Fe) were examined and compared following cold reduction by 5, 10, 20, 30, and 40, explosive expansion of thin-walled cylinders by 1,10, 25, and 62%, and explosive shock loading to pressures of 80, 180, 240, and 460 kbar.

2 citations




Book ChapterDOI
01 Jan 1971
TL;DR: In this paper, the authors developed methods for making aircraft quality parts from forged Inconel Alloy 718 metal powder preforms, defined as those having room-temperature tensile and fatigue properties, and 1200 °F.
Abstract: The objective of the program was to develop methods for making aircraft quality parts from forged Inconel Alloy 718 metal powder preforms. Aircraft quality parts were defined as those having room-temperature tensile and fatigue properties, and 1200 °F. tensile and 1300 °F. stress-rupture properties meeting aircraft specifications.