发明名称 |
Aircraft with a rear fuselage protection shield |
摘要 |
The invention relates to an aircraft with a protection shield for the rear composite material, fuselage 25) for conducting tail impact tests, in addition to a tail absorber, the shield (11) being formed by a plurality of pieces (21) joined to supports (23) fixed to the rear fuselage (25) behind the tail absorber (1), said pieces (21) having a laminar structure with an outer steel sheet (13), an inner composite sheet (17) and an intermediate high resistance silicon sheet (15).
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申请公布号 |
US8371530(B2) |
申请公布日期 |
2013.02.12 |
申请号 |
US20050794487 |
申请日期 |
2005.12.29 |
申请人 |
AIRBUS OPERATIONS, S.L.;BAUTISTA DE LA LLAVE CESAR;LOPEZ ROMANO BERNARDO;POSTIGO RODRIGUEZ ANGEL;SANCHEZ GOMEZ JOSE |
发明人 |
BAUTISTA DE LA LLAVE CESAR;LOPEZ ROMANO BERNARDO;POSTIGO RODRIGUEZ ANGEL;SANCHEZ GOMEZ JOSE |
分类号 |
B64D7/00;B64C1/00;B64C25/58;F41H5/04 |
主分类号 |
B64D7/00 |
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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