Manganese bronze, which, in order to obtain merely a high tensile strength, being structurally become all β adding somewhat large amounts of Mn., Al., Sn., &C., shows remarkable brittleness and decrease of elongation, by the precipitation of a brittle compound in the grain boundaries, at about 350 degrees centigrade when very slowly cooled after casting as in the case of large propeller casting. In view of this fact, in case of decreasing the amounts of alloying elements, its structure becomes α+β and accordingly the brittleness is avoided, but the strength is not sufficient.
Moreover, the Author confirms that, by the investigation of many examples of damaged propeller blades, many cracks due to corrosien fatigue have started from grain boundaries at the casting defects near the root's surface of propeller blades.
Therefore, for such material as manganese bronze for propeller, by the precipitation of different phases γ in grain boundaries as above-mentioned, its corrosion fatigue becomes inferior, the influence being greater when the structure is a single phase, say β from this point of view, the Author explains in this paper that without enbrittliug by slow cooling after casting, it consists structurally of two phases and furthermore it becomes necessary to select considerably high strength.
Now, after investigation under such consideration as above, the Author attained new alloy near to this object, but various tests being still continued, its mechanical properties is briefly shown in this paper.
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