STRUCTURAL COMPONENT OF AN AIRCRAFT OR SPACECRAFT AND A FUSELAGE COMPONENT ARRANGEMENT OF AN AIRCRAFT OR SPACECRAFT |
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| 申请号 | PCT/EP2009065227 | 申请日 | 2009-11-16 | 公开(公告)号 | WO2010060824A4 | 公开(公告)日 | 2010-07-22 |
| 申请人 | AIRBUS OPERATIONS GMBH; GROSS CLAUS-PETER; | 发明人 | GROSS CLAUS-PETER; | ||||
| 摘要 | The invention relates to a structural component (2) of an aircraft or spacecraft comprising a fuselage section connection area (10) for connecting to an associated fuselage section (5) having a thermal expansion coefficient that is approximately aligned with the associated fuselage section (5); an inner connection area (11) for connecting to an associated installation element having a thermal expansion coefficient that is approximately aligned with the associated installation element; and a separating area (12) for connecting the fuselage section connection area (10) and the inner connection area (11), wherein at least one of the areas (10, 11, 12) has a high thermal resistance (R13, R14, R15). | ||||||
| 权利要求 | |||||||
| 说明书全文 | |||||||
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