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1. 发明申请

WO2012098331A3 FISH JOINT DEVICE HAVING AN IMPROVED MECHANICAL HOLD 审中-公开
标题翻译：鱼联合装置具有改进的机械控制
公开(公告)号：WO2012098331A3
公开(公告)日：2012-09-13
申请号：PCT/FR2012050102
申请日：2012-01-17
申请人： AIRBUS OPERATIONS SAS , GUILLEMAUT JULIEN , GALLANT GUILLAUME
发明人： GUILLEMAUT JULIEN , GALLANT GUILLAUME
IPC分类号： B64C1/26
CPC分类号： B64C1/26 , F16B5/02 , Y10T403/74
摘要： The invention relates to a fish joint device for securing first and second structural elements (1, 2) of an aircraft to each other, said device comprising two fish plates (20, 30) arranged either side of the structural elements (1, 2) and fixed thereto by means of a set of cross-members (11) for fixing fish plates. According to the invention, the fish joint device comprises at least one intermediate fish joint plate (40, 50) that is arranged between one of said fish plates (20, 30) and said structural elements (1, 2) partially covered by said intermediate plate, and is fixed thereto by a set of cross-members (11) for fixing intermediate plates, including the set of cross-members (11) for fixing fish plates.
摘要翻译：本发明涉及一种用于将航空器的第一和第二结构元件（1,2）相互固定的鱼尾接头装置，所述装置包括布置在结构元件（1,2）两侧的两个鱼尾板（20,30）并通过用于固定鱼尾板的一组横向构件（11）固定于其上。根据本发明，鱼尾接头装置包括至少一个布置在一个所述鱼尾板（20,30）和所述结构元件（1,2）之间的至少一个中间鱼尾板（40,50），所述结构元件（1,2）部分地被所述中间体并通过一组用于固定中间板的横向构件（11）固定于其上，该中间板包括用于固定鱼尾板的一组横向构件（11）。

2. 发明申请

WO2013057355A3 IMPROVED IMPACT-RESISTANT AND DAMAGE-TOLERANT AIRCRAFT FUSELAGE 审中-公开
标题翻译：改进的抗冲击和耐损伤飞机的融合
公开(公告)号：WO2013057355A3
公开(公告)日：2013-08-08
申请号：PCT/ES2012070731
申请日：2012-10-19
申请人： AIRBUS OPERATIONS SL , AIRBUS OPERATIONS SAS
发明人： MARTINO GONZALEZ ESTEBAN , VINUE SANTOLALLA EDUARDO , FOLCH CORTES DIEGO , GOYA ABAURREA PABLO , GUINALDO FERNANDEZ ENRIQUE , GUILLEMAUT JULIEN
IPC分类号： B64C1/06 , B64D27/00
CPC分类号： B64C1/068 , B64C1/06 , B64C1/061 , B64C1/062 , B64D27/14 , B64D2027/005 , Y02T50/66
摘要： Improved impact-resistant and damage-tolerant aircraft fuselage. The invention relates to a section (32) of the fuselage of an aircraft suffering impacts from external bodies, the fuselage of the aircraft having a curved form with at least one vertical plane of symmetry (A-A) and a central longitudinal axis, and comprising a skin (35) and a plurality of ring frames (37) arranged perpendicularly to said longitudinal axis, said section (32) of the fuselage also comprising at least one reticular internal structure (51, 53) mounted on a support structure (41, 43), which includes longitudinal beams (39) connected to the skin (35) and interconnected with said ring frames (37), said reticular internal structure (51, 53) being arranged in order to create at least one closed cell (75) with the skin (45) in order to improve the strength thereof and the tolerance thereof to damage from said impacts.
摘要翻译：改进的抗冲击和耐损伤飞机机身。本发明涉及遭受外部冲击的飞机机身的部分（32），飞机机身具有至少一个垂直的对称平面（AA）和中心纵向轴线的弯曲形式，并且包括（35）以及垂直于所述纵向轴线布置的多个环形框架（37），所述机身的所述部分（32）还包括安装在支撑结构（41,43）上的至少一个网状内部结构），其包括连接到表皮（35）并与所述环形框架（37）相互连接的纵梁（39），所述网状内部结构（51,53）被布置成用以形成至少一个闭合单元（45），以改善其强度及其对所述冲击造成的损害的耐受性。

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