发明名称 |
AIRCRAFT WITH FUSELAGE-MOUNTED ENGINES AND AN INTERNAL SHIELD |
摘要 |
Internal shield in the rear fuselage of an aircraft having a propulsion system formed by two engines mounted on each side of it; the rear fuselage having at least a vertical symmetry plane; the rear fuselage being made of a composite material; the internal shield being located in said vertical symmetry plane and extended in an area that covers the possible trajectories of a set of pre-defined fragments detached from one of said engines in a failure event that would impact on critical elements of the opposite engine; the internal shield having a flat shape and an energy absorption capability that allows stopping said fragments. The invention also refers to a method for determining the area of an internal shield and to an aircraft having said internal shield.
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申请公布号 |
US2013214090(A1) |
申请公布日期 |
2013.08.22 |
申请号 |
US201213724360 |
申请日期 |
2012.12.21 |
申请人 |
AIRBUS OPERATIONS S.L.;AIRBUS OPERATIONS S.L. |
发明人 |
FOLCH CORTES DIEGO;VINUE SANTOLALLA EDUARDO;MARTINO GONZALEZ ESTEBAN;GUILLEMAUT JULIEN;GOYA ABAURREA PABLO |
分类号 |
B64D45/00;B64D27/02 |
主分类号 |
B64D45/00 |
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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