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Centring assembly for a component holder

A component and component technology, applied in the field of centering components, can solve problems such as high investment cost and reduced downtime, and achieve the effect of avoiding tolerance accumulation and accurate positioning

Active Publication Date: 2015-02-11
布勒特耶自动控制设备有限责任公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The resulting long downtimes of the usually very expensive processing stations correspondingly significantly reduce their availability and thus lead to significantly higher investment costs per flying body produced

Method used

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  • Centring assembly for a component holder
  • Centring assembly for a component holder
  • Centring assembly for a component holder

Examples

Experimental program
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Embodiment Construction

[0027] exist figure 1 A component carrier 1 for an aircraft structural component, in particular a clamping frame 1a, is shown with four proposed centering assemblies. additionally, figure 1 An enlarged oblique view of one of these proposed centering arrangements in the component carrier 1 is also reflected.

[0028] The shown clamping frame 1 a is used in particular in a machining station (not shown here) for aircraft structural components. In particular, the fuselage and wings of the aircraft and their components are among the structural components of the aircraft that can be accommodated by the clamping frame 1a.

[0029] The proposed centering assembly comprises a centering pin 2 and a centering receptacle 3 for the centering pin 2, which are respectively located at figure 2 Shown enlarged in b and 2a.

[0030] The centering receptacle 3 is thus set up to accommodate the centering pin 2 in its opening. In this case, the centering receptacle 3 is arranged on the workpi...

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PUM

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Abstract

The invention relates to a centring arrangement for a component carrier, in particular for a mounting frame for structural aircraft components, having a centring pin, a centring receptacle for the centring pin, and a rotary drive for rotating the centring pin about a longitudinal axis of the centring pin, so that the centring pin can be brought into centring engagement with the centring receptacle as a result of the rotation. The invention further relates to a method for centring and locking a centring receptacle.

Description

technical field [0001] The invention relates to a centering set (Zentrieranordnung) for a component carrier (Bauteiltraeger) with the features of claim 1 and a centering assembly (Zentrieranordnung) with the features of claim 15 for centering and Method for locking the centering receptacle. Background technique [0002] Aircraft and other flying objects often have very large structural elements, such as wings, fuselages or parts thereof. During the automated production of flying bodies, these structural components are handled in correspondingly large processing stations and processed by different machine tools. The exemplary work step setting automatically sets up a series of riveted joints, which in the past often had to be carried out manually. [0003] From the prior art and in particular from the most recent document US 8,220,134, a machining station for aircraft structural components is known, in which a rectangular clamping frame (Aufspannrahmen) is used as a compone...

Claims

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Application Information

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IPC IPC(8): B23Q3/00
CPCB23Q1/015B23Q3/18B23Q1/25B23Q3/183B64F5/0009Y10T29/49998Y10T29/53983Y10T29/5177Y10T29/53091Y10T29/53687Y10T29/53961Y10T29/53978B64F5/10B25B11/00
Inventor C.奥伊斯特维曼
Owner 布勒特耶自动控制设备有限责任公司
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