发明名称 |
PROCEDIMIENTO PARA FABRICAR UN PERFORADOR PARA UN PROYECTIL CON JAULA PROPULSORA |
摘要 |
<p>Missile made from hard metal, such as W or U comprises a penetrator, a drive cage and an aerodynamic hood whereby the penetrator from front area to stern is made as one part. The penetrator in its middle region has a lower strength and higher toughness than in the front region and the stern region has a higher strength and lower toughness than in the middle region and a lower strength and higher toughness than in the front region.</p> |
申请公布号 |
ES545085(D0) |
申请公布日期 |
1987.05.01 |
申请号 |
ES19850005450 |
申请日期 |
1985.07.11 |
申请人 |
VOEST-ALPINE AKTIENGESELLSCHAFT |
发明人 |
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分类号 |
B22F3/00;(IPC1-7):B22F3/00;F42B13/04 |
主分类号 |
B22F3/00 |
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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