Assembly device for connecting cup-shaped longitudinal segments of a covering body by placing at least one longitudinal connecting joint
An assembly device, longitudinal connection technology, used in transportation and packaging, metal processing equipment, manufacturing tools, etc., can solve problems such as high costs
Inactive Publication Date: 2007-01-24
AIRBUS OPERATIONS GMBH
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Problems solved by technology
The whole structure is expensive and covers only half the fuselage circumference
Method used
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[0024] refer to figure 1 The assembly device 1 , 11 according to the invention shown in FIG. 6 comprises a mounting part 6 having a tool carrier frame 4 supported thereon. The two mounting parts, which are movable individually or together on the rail 14 in the Y-direction as required, are designed as columns or towers 61 and 62 extending in the height direction Z. The carrier frame 4 extends in the direction of the third Cartesian coordinate X and is slidable in the height direction Z by means of end pieces 43, 44 constituting frame webs and is supported by means of The device 51 is held rotatably on towers 61 and 62 about its central axis and the axis of symmetry 40 . Said assembly device 11 is used to connect a part-cylindrical shell-like longitudinal section 910 to an open face in the shape of the fuselage 9 by providing a longitudinal riveted seam 97 to the circumferentially closed shell, as shown in FIGS. 6A to 6A . Figure 6C as shown. An aircraft fuselage 9 with a cy...
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An assembly device (1) for connecting cup-shaped covering longitudinal segments (910) of a covering body (9) which forms a large component and which is provided with a cavity having an open front-surface side, used to produce a longitudinal connecting joint, comprising at least one tool pair (3), which consists of a tool (31) which is displaceably guided in a longitudinal direction (L) of the covering body (9) inside the cavity, in addition to another tool (32) which is displaceably guided in a longitudinal direction (L) outside the cavity (92). The tools (31,32) in the pair (3) interact in a direction which is perpendicular to the longitudinal direction of the body. The assembly device (1) is fitted with a pair of carriers (2) which are formed by an inner guide carrier (21), which extends inside the cavity of the covering body (9) in a longitudinal direction (L) and which displaceably guides the inner tool (31) and by an outer guide carrier (22) which extends outside the covering body (9) in a longitudinal direction (L) and which displaceably guides the outer tool (32). Each guide carrier (21,22) is rotationally and displaceably mounted about at least one longitudinal axis of rotation (50) which is oriented according to the outer longitudinal contour (980) of the covering body (9) in at least two spatial directions (Y,Z) perpendicular to the longitudinal direction (L) of the body and is fixable in such a way that the tools (31, 32) in the pair (3) assume different positions on the longitudinal periphery of the covering body (9).
Description
technical field [0001] The invention relates to a fitting device for connecting shell-shaped longitudinal shell sections of a shell forming a longitudinally extending cavity provided with an open face side by providing at least one longitudinal connecting seam on the shell And in particular closed large-scale components on the circumferential side, the assembly device comprises at least one tool pair, which includes an inner tool that can be moved and guided in the cavity in the longitudinal direction of the housing and can be moved outside the cavity. External tools guided in movement in the longitudinal direction of the shell, wherein the tools act together in pairs in a direction perpendicular to the longitudinal direction of the shell in order to produce the connecting seam. Typically, the enclosure is an aircraft fuselage assembled from a number of partially cylindrical prefabricated shell segments. These segments are arranged in position to form the fuselage and are joi...
Claims
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IPC IPC(8): B21J15/10B23P19/04B23Q1/01
CPCY10T409/308288B23P19/04B23P2700/01B21J15/142B21J15/10Y10T29/5118Y10T29/49943B23Q1/012
Inventor 赖纳·韦塞洛
Owner AIRBUS OPERATIONS GMBH