发明名称 |
AIRCRAFT FUSELAGE MADE OUT WITH COMPOSITE MATERIAL AND MANUFACTURING PROCESSES |
摘要 |
Aircraft fuselage made out with composite material and manufacturing processes. The structure of the fuselage (1 1 ) comprises a skin (13), a plurality of frames (17) positioned transversely to the longitudinal axis (9) of the fuselage (11) and a plurality of longitudinal stiffening elements (14, 15) that can be either stringers (14) or beams (15), being the ratio between the distance (X) between frames (17) and the distance (Y) between longitudinal stiffening elements (14, 15) is less than one. If the stiffening elements are stringers (14) the manufacturing process is based on assembling the fuselage section (11) joining the skin (13) with the stringers (14) to the frames (17). If the stiffening elements are beams (15) the manufacturing process is based on joining the skin to an internal structure made up with frames (17) and beams (15). |
申请公布号 |
WO2012001207(A3) |
申请公布日期 |
2012.07.05 |
申请号 |
WO2011ES70478 |
申请日期 |
2011.06.30 |
申请人 |
AIRBUS OPERATIONS S.L.;AREVALO RODRIGUEZ, ELENA;CRUZ DOMINGUEZ, FRANCISCO JOSE |
发明人 |
AREVALO RODRIGUEZ, ELENA;CRUZ DOMINGUEZ, FRANCISCO JOSE |
分类号 |
B64C1/06 |
主分类号 |
B64C1/06 |
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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