发明名称 |
PROCEDIMIENTO PARA LA FABRICACION DE PIEZAS GRANDES DE MATERIAL COMPUESTO CONTROLANDO EL ESPESOR DE SUS BORDES |
摘要 |
Procedure for the manufacture of large parts of composite material, controlling the thickness of the edges thereof. It relates to the manufacture of a part (11) possessing edge zone (11) in an aeronautical structure through a join with joining plate (23) and backing plate (25) by means of the following stages: a) Definition of interface surface (15) of edge zone (13) to be in contact with joining plate (23); b) Manufacture of first panel (31) possessing the configuration planned for part (11); c) Obtainment of a map of differences between the thickness of first panel (31) and that which it should possess to be coincident with said interface surface (15); d) Manufacture of supplementary panel (33) having a thickness to be coincident with that of said map of differences; e) joining of supplementary panel (33) to first panel (31). |
申请公布号 |
ES2396327(B1) |
申请公布日期 |
2014.02.06 |
申请号 |
ES20100030897 |
申请日期 |
2010.06.10 |
申请人 |
AIRBUS OPERATIONS, S.L. |
发明人 |
LATORRE PLAZA, TERESA;INIESTA MENENDEZ, JOSE GREGORIO;MORANCHO RODRIGUEZ, JOSEP;MENENDEZ MARTIN, JOSE MANUEL |
分类号 |
B64C3/26;B64C1/12;B64F5/00 |
主分类号 |
B64C3/26 |
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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