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1. 发明授权

US10150553B2 Device and method for assembling two sections of aircraft fuselage 有权
公开(公告)号：US10150553B2
公开(公告)日：2018-12-11
申请号：US13533266
申请日：2012-06-26
申请人： Bruno Cacciaguerra , Alain Depeige , Jean-Claude Lacombe , Hélène Cazeneuve , Marc-Antoine Castanet
发明人： Bruno Cacciaguerra , Alain Depeige , Jean-Claude Lacombe , Hélène Cazeneuve , Marc-Antoine Castanet
IPC分类号： B64C1/06 , B64F5/10 , B64C1/00
摘要： A device and method for assembling two aircraft fuselage sections each comprising a skin and longitudinal stiffeners, the device comprising fishplates fishing couples of mutually aligned longitudinal stiffeners belonging respectively to said sections, each fishplate comprising two fishplate pieces each comprising at least one longitudinal sole plate intended to be fixed to a longitudinal stiffener, and a transverse support head, and at least one demountable connecting member able to mutually clamp the respective support heads of said fishplate pieces to allow a transmission of longitudinal forces between these fishplate pieces.

2. 发明申请

US20130181092A1 DEVICE AND METHOD FOR ASSEMBLING TWO SECTIONS OF AIRCRAFT FUSELAGE 审中-公开
标题翻译：用于组装飞机熔接两段的装置和方法
公开(公告)号：US20130181092A1
公开(公告)日：2013-07-18
申请号：US13533266
申请日：2012-06-26
申请人： Bruno Cacciaguerra , Alain Depeige , Jean-Claude Lacombe , Helene Cazeneuve , Marc-Antoine Castanet
发明人： Bruno Cacciaguerra , Alain Depeige , Jean-Claude Lacombe , Helene Cazeneuve , Marc-Antoine Castanet
IPC分类号： B64C1/06 , B64F5/00
CPC分类号： B64C1/069 , B64C1/068 , B64C2001/0081 , B64F5/10 , Y10T29/49622
摘要： Device for assembling two aircraft fuselage sections each comprising a skin and longitudinal stiffeners, the device comprising fishplates fishing couples of mutually aligned longitudinal stiffeners belonging respectively to said sections, each fishplate comprising two fishplate pieces each comprising at least one longitudinal sole plate intended to be fixed to a longitudinal stiffener, and a transverse support head, and at least one demountable connecting member able to mutually clamp the respective support heads of said fishplate pieces to allow a transmission of longitudinal forces between these fishplate pieces.Set of fuselage sections assembled by means of a device of the type described above.Method of assembling two fuselage sections by means of a device of the type described above.
摘要翻译：用于组装两个飞行器机身部分的装置，每个飞行器机身部分各自包括皮肤和纵向加强件，该装置包括分别属于所述部分的相互对齐的纵向加强件的鱼板钓鱼钩，每个鱼板包括两个鱼板块，每个鱼板包括至少一个用于固定的纵向底板纵向加强件和横向支撑头以及能够相互夹紧所述鱼板片的相应支撑头的至少一个可拆卸连接件，以允许在这些鱼片之间传递纵向力。通过上述类型的装置组装的机身部分组。通过上述类型的装置组装两个机身部分的方法。

3. 发明申请

US20130056582A1 LANDING GEAR MOUNTED UNDER AN AIRCRAFT WING 审中-公开
标题翻译：飞机上安装着陆齿轮
公开(公告)号：US20130056582A1
公开(公告)日：2013-03-07
申请号：US13698204
申请日：2011-05-16
申请人： Sébastien De Conto , Marc-Antoine Castanet
发明人： Sébastien De Conto , Marc-Antoine Castanet
IPC分类号： B64C25/10
CPC分类号： B64C25/12
摘要： A landing gear mounted under an aircraft wing is provided. The aircraft can comprise a fuselage and wings each comprising at least one longitudinal spar connected to a wing box being part of the structure of the fuselage. The landing gear can comprise one leg that pivots, on its upper end, around a rotation axis to occupy at least one extended position and one retracted position and which is provided, on its lower end, with rolling means, the leg being connected, on its upper end, to the longitudinal spar of said wing. The landing gear can also comprise at least one inclined front strut connected, on its lower end, to said leg and connected, on its upper end, to the structure of the fuselage thru connecting means. The connecting means can comprise a sliding bearing crossed by at least one part of the upper end of said strut.
摘要翻译：提供安装在飞机机翼下方的起落架。飞行器可以包括机身和机翼，每个机翼包括连接到作为机身结构的一部分的机翼箱的至少一个纵向翼梁。起落架可以包括一个腿，其在其上端围绕旋转轴线枢转，以占据至少一个延伸位置和一个缩回位置，并且在其下端上设置有滚动装置，该腿连接在其上端，到所述翼的纵向翼梁。起落架还可以包括至少一个倾斜的前支柱，其在其下端连接到所述腿部，并且在其上端部通过连接装置连接到机身的结构。连接装置可以包括由所述支柱的上端的至少一部分交叉的滑动轴承。

4. 发明申请

US20120104170A1 FUSELAGE ELEMENT COMPRISING A FUSELAGE SEGMENT AND JOINING MEANS 有权
标题翻译：包含熔接部分和接合装置的熔接元件
公开(公告)号：US20120104170A1
公开(公告)日：2012-05-03
申请号：US13381673
申请日：2010-07-02
申请人： Guillaume Gallant , Romain Delahaye , Marc Dugerie , Marc-Antoine Castanet
发明人： Guillaume Gallant , Romain Delahaye , Marc Dugerie , Marc-Antoine Castanet
IPC分类号： B64C1/12 , B64C1/06
CPC分类号： B64C1/061 , B64C1/064 , B64C1/068 , B64C1/12
摘要： The invention relates to a fuselage element comprising a fuselage segment (1a) comprising a skin (3a), and junction means (6) for connecting the skin of said segment (1a) to an adjacent segment (1b). The segment (1a) extends along the longitudinal axis (X) of the fuselage, and the skin (3) includes at least one first section (10) at least one end of said segment (1a). The fuselage segment (1a) comprises at least one longitudinal stiffening element (5a) for the fuselage. The junction means (60) are arranged so as to contact an outer surface (30) of said first section (10) of the skin (3a), and the stiffening element (5a) partially extends at the junction means (6) along the longitudinal axis (X).
摘要翻译：本发明涉及一种机身元件，它包括一个包括皮肤（3a）的机身段（1a）和用于将所述段（1a）的皮肤连接到相邻区段（1b）的接合装置（6）。所述片段（1a）沿着所述机身的纵向轴线（X）延伸，并且所述皮肤（3）包括所述片段（1a）的至少一个端部中的至少一个第一部分（10）。机体段（1a）包括用于机身的至少一个纵向加强元件（5a）。接合装置（60）布置成接触皮肤（3a）的所述第一部分（10）的外表面（30），并且加强元件（5a）沿着连接装置（6）部分地延伸纵轴（X）。

5. 发明授权

US09371125B2 Fuselage element comprising a fuselage segment and joining means 有权
标题翻译：机身元件包括机身段和接合装置
公开(公告)号：US09371125B2
公开(公告)日：2016-06-21
申请号：US13381673
申请日：2010-07-02
申请人： Guillaume Gallant , Romain Delahaye , Marc Dugerie , Marc-Antoine Castanet
发明人： Guillaume Gallant , Romain Delahaye , Marc Dugerie , Marc-Antoine Castanet
IPC分类号： B64C1/12 , B64C1/06
CPC分类号： B64C1/061 , B64C1/064 , B64C1/068 , B64C1/12
摘要： A fuselage element including a fuselage segment including a skin and a junction means for connecting the skin to an adjacent fuselage segment. The fuselage segment extends along a longitudinal axis of the fuselage, and the skin includes a first section at at least one end of the fuselage segment. The fuselage segment includes at least one longitudinal stiffening element for the fuselage. A junction member is arranged so as to contact an outer surface of the first section of the skin, and the stiffening element partially extends to the junction member along the longitudinal axis.
摘要翻译：一种机身元件，包括包括皮肤的机身段和用于将皮肤连接到相邻的机身段的接合装置。机身段沿着机身的纵向轴线延伸，并且皮肤包括在机身段的至少一端的第一部分。机身部分包括用于机身的至少一个纵向加强元件。接合构件布置成接触皮肤的第一部分的外表面，并且加强元件沿着纵向轴线部分地延伸到接合构件。

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