公开(公告)号：US07857258B2

公开(公告)日：2010-12-28

申请号：US12108642

申请日：2008-04-24

申请人： Mathieu Normand ,  Marc Cazzola ,  Sandrine Deilhes

发明人： Mathieu Normand ,  Marc Cazzola ,  Sandrine Deilhes

IPC分类号： B64C1/00

CPC分类号： B64C1/12 ,  B64C1/069 ,  B64C2001/0072 ,  Y02T50/43

摘要： An aircraft fuselage including at least two sections kept assembled at a circumferential join, each section having at least one panel. The circumferential join includes at least one inner ring, situated on one face, called the inner face, of the fuselage. The inner ring has a width li, partially overlaps each of the two panels and is fixed to the two panels by fasteners. The fuselage also includes an outer ring, situated on one face, called the outer face, of the fuselage, opposite to the inner face. The outer ring has a width le, partially overlaps the two panels, and is fixed to the two panels and to the inner ring by some or all of the fasteners fixing the inner ring to the two panels.

摘要翻译： 包括至少两个部分的飞机机身保持组装在圆周连接处，每个部分具有至少一个面板。 圆周连接件包括位于机身的一个表面（称为内表面）上的至少一个内圈。 内圈具有宽度li，与两个面板中的每一个部分重叠，并通过紧固件固定到两个面板上。 机身还包括一个外环，位于机身的一个面，称为外表面，与内表面相对。 外圈具有宽度le，与两个面板部分重叠，并且通过将内圈固定到两个面板上的部分或全部紧固件固定到两个面板和内圈。

公开(公告)号：US20090020646A1

公开(公告)日：2009-01-22

申请号：US12108642

申请日：2008-04-24

申请人： Mathieu Normand ,  Marc Cazzola ,  Sandrine Deilhes

发明人： Mathieu Normand ,  Marc Cazzola ,  Sandrine Deilhes

IPC分类号： B64C1/00

CPC分类号： B64C1/12 ,  B64C1/069 ,  B64C2001/0072 ,  Y02T50/43

摘要： An aircraft fuselage including at least two sections kept assembled at a circumferential join, each section having at least one panel. The circumferential join includes at least one inner ring, situated on one face, called the inner face, of the fuselage. The inner ring has a width li, partially overlaps each of the two panels and is fixed to the two panels by fasteners. The fuselage also includes an outer ring, situated on one face, called the outer face, of the fuselage, opposite to the inner face. The outer ring has a width le, partially overlaps the two panels, and is fixed to the two panels and to the inner ring by some or all of the fasteners fixing the inner ring to the two panels.

摘要翻译： 包括至少两个部分的飞机机身保持组装在圆周连接处，每个部分具有至少一个面板。 圆周连接件包括位于机身的一个表面（称为内表面）上的至少一个内圈。 内圈具有宽度li，与两个面板中的每一个部分重叠，并通过紧固件固定到两个面板上。 机身还包括一个外环，位于机身的一个面，称为外表面，与内表面相对。 外圈具有宽度le，与两个面板部分重叠，并且通过将内圈固定到两个面板上的部分或全部紧固件固定到两个面板和内圈。