发明名称 Mass ejection hole installation method by reinforcing the thickness of propeller blade tips
摘要 PURPOSE: A method for installing a mass ejection hole by reinforcing the thickness of the tip of a propeller blade is provided to prevent the weakening of strength when a pipe line connected from a hollow shaft of a propeller shaft to a mass ejection hole is installed in a blade. CONSTITUTION: A method for installing a mass ejection hole by reinforcing the thickness of the tip of a propeller blade is as follows. A blade of a propeller is cut over 0.92R. A newly manufactured blade is welded at a cut portion. The tip thickness of the propeller blade at the 0.92R is reinforced between 0.92R-1.0R. A mass ejection hole is installed between the 0.92R-1.0R at the tip of the propeller blade. The thickness of the propeller blade over the 0.92R is reinforced by welding.
申请公布号 KR101332956(B1) 申请公布日期 2013.11.25
申请号 KR20110067523 申请日期 2011.07.07
申请人 发明人
分类号 B63H1/14;B63H1/18;B63H1/28 主分类号 B63H1/14
代理机构 代理人
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