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 |
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发明人 |
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分类号 |
B63H1/14;B63H1/18;B63H1/28 |
主分类号 |
B63H1/14 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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