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    • 7. 发明授权
    • Two-part riveting apparatus and method for riveting barrel-shaped components such as aircraft fuselage components
    • 用于铆接诸如飞机机身部件的桶形部件的两部分铆接装置和方法
    • US06505393B2
    • 2003-01-14
    • US09905617
    • 2001-07-13
    • Udo StoewerBernd KoehlerNorbert Kosuch
    • Udo StoewerBernd KoehlerNorbert Kosuch
    • B21J1502
    • B21J15/142B21J15/10Y10T29/49956Y10T29/53065Y10T29/5377
    • An apparatus for riveting shell components to form a barrel-shaped structure such as an aircraft fuselage includes an outer part and an inner part that operate coordinated with each other under computer control. The outer apparatus part includes a riveting machine system movably carried on an annular machine guide that is supported on a stand that is movable in a length-wise X-direction. The inner apparatus part includes a multi-axis riveting robot mounted on a mounting frame that is movable along the X-direction. Instead of moving the inner and outer apparatus parts in the X-direction, it is alternatively possible to move the fuselage while keeping the apparatus parts stationary. A computer control unit provides control signals to achieve a coordinated and concurrent positioning of the inner and outer apparatus parts, and to carry out a coordinated sequence of riveting steps. Rivets can be automatically fastened even at difficult to access locations, while avoiding structural obstacles inside the aircraft fuselage. The apparatus parts are supported independently of the fuselage on the floor of the assembly hall.
    • 用于铆接外壳部件以形成诸如飞行器机身的桶形结构的装置包括在计算机控制下彼此协调操作的外部部分和内部部件。 外部装置部分包括可移动地承载在环形机器引导件上的铆接机系统,所述环形机器引导件支撑在可沿纵向X方向移动的支架上。 内部装置部件包括安装在可沿X方向移动的安装框架上的多轴铆接机器人。 代替在X方向上移动内部和外部装置部件,或者可以在保持装置部件静止的同时移动机身。 计算机控制单元提供控制信号以实现内部和外部设备部件的协调和并发定位,并且执行协调的铆接步骤序列。 即使在难以到达的位置,也可以自动固定铆钉,同时避免飞机机身内的结构性障碍物。 装置部件独立于组装大厅的地板上的机身而被支撑。
    • 9. 发明授权
    • Method and system for fabricating, equipping and outfitting an aircraft fuselage
    • 制造,装备和装备飞机机身的方法和系统
    • US06237210B1
    • 2001-05-29
    • US09366034
    • 1999-08-02
    • Udo StoewerBernd KoehlerNorbert Kosuch
    • Udo StoewerBernd KoehlerNorbert Kosuch
    • B21D3903
    • B64C1/00B64F5/10Y10T29/49829Y10T29/49831Y10T29/534Y10T29/5377
    • A fuselage is substantially simultaneously fabricated, equipped and outfitted in an assembly area including adjacent riveting, equipping and outfitting zones. The riveting zone includes an external riveting apparatus working from the outside of the aircraft fuselage, and an internal riveting apparatus working from the inside of the fuselage to fabricate and join a first fuselage section to an initial structure. The first fuselage section is moved from the riveting zone into an equipping zone, wherein equipment, such as pipes, ducts, hoses, pumps, blowers and structural components and fittings of the aircraft, is installed in the first fuselage section, while simultaneously a second fuselage section is being rivet-joined onto the first fuselage section in the riveting zone. The second fuselage section is moved from the riveting zone into the equipping zone, and the first fuselage section is moved from the equipping zone into the outfitting zone. Equipment is installed in the second fuselage section in the equipping zone, while outfitting components such as electrical cable bundles, insulation blankets, wall paneling, floors, furnishings, and cabin fittings are installed in the first fuselage section in the outfitting zone. Next, the fuselage being formed is shifted so that the second fuselage section moves from the equipping zone into the outfitting zone, while a third fuselage section is joined onto the second fuselage section in the riveting zone.
    • 机身基本上同时被制造,装配和装配在包括相邻的铆接,装备和装配区域的组装区域中。 铆接区域包括从飞机机身外部工作的外部铆接设备,以及从机身内部工作的内部铆接设备,以将第一机身部分加工成初始结构。 第一机身部分从铆接区域移动到装备区域中,其中诸如管道,管道,软管,泵,鼓风机和飞行器的结构部件和配件的设备安装在第一机身部分中,同时第二机身部分 机身部分铆接在铆接区域的第一个机身部分。 第二机身部分从铆接区域移动到装备区域中,第一机身部分从装备区域移动到装备区域中。 设备安装在装备区的第二个机身部分,而装备区域的第一个机身部分安装了电缆束,绝缘毯,墙板,地板,家具和客舱配件等部件。 接下来,正在形成的机身移动,使得第二机身部分从装备区域移动到装备区域中,而第三机身部分连接到铆接区域中的第二机身部分上。