Flexible assembly system for aircraft panel

An aircraft wall panel and flexible assembly technology, applied in aircraft assembly, aircraft parts, assembly machines, etc., can solve problems such as poor quality stability, low hole-making efficiency, and large gaps, and achieve flexibility, cost savings, and reduced The effect of the assembly cycle

Active Publication Date: 2014-07-16
ZHEJIANG UNIV +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, the connection assembly in the aircraft assembly process in my country is still dominated by manual drilling and riveting, the quality stabili

Method used

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  • Flexible assembly system for aircraft panel
  • Flexible assembly system for aircraft panel
  • Flexible assembly system for aircraft panel

Examples

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Embodiment Construction

[0059] The flexible assembly system for aircraft panels of the present invention will be described in detail below in conjunction with the accompanying drawings.

[0060] Such as figure 1 , 2 As shown, a flexible assembly system for aircraft panels includes:

[0061] Fixed base frame 4, fixedly installed on the ground;

[0062] The movable base frame 1 cooperates with the fixed base frame;

[0063] The pedestal base 5 is provided with a linear guide rail arranged along the X-axis direction, and the movable pedestal is slidably matched with the linear guide rail;

[0064] A number of flexible clamping board assemblies 2 are arranged on the fixed base frame and the movable base frame for clamping the aircraft wall panel 3;

[0065] Several transmission positioning units 14 are arranged on the fixed base frame and the movable base frame, and are used to adjust the position of the flexible clamp assembly;

[0066] The locator buckle 13 is arranged between the movable base fra...

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PUM

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Abstract

The invention discloses a flexible assembly system for an aircraft panel. The flexible assembly system comprises a fixed base frame, a movable base frame which is capable of moving in the X-axis direction and is matched with the fixed base frame, a plurality of flexible clamping board assemblies arranged on the fixed base frame and the movable base frame and used for clamping the aircraft panel, a plurality of transmission positioning units arranged on the fixed base frame and the movable base frame and used for adjusting the positions of the flexible clamping board assemblies and robot perforating systems. The positioning assembly requirements of different aircraft panels can be satisfied by adjusting the positions of an inside fixing clamping board and an outside fixing clamping board and replacing a replaceable internal clamping board and a replaceable skin clamping board, and therefore the flexibility of the assembly system is achieved. The two robot perforating systems arranged on the two sides of a panel assembly tool are used for simultaneously satisfying the automatic perforating connecting requirements of the two sides of the aircraft panel. The flexible assembly system is high in flexibility, high-efficiency and high-quality assembly of the aircraft panel can be achieved, the assembly period is greatly shortened, and cost is reduced.

Description

technical field [0001] The invention belongs to the technical field of aircraft digital assembly, and relates to an aircraft panel flexible assembly system. Background technique [0002] Aircraft assembly is the main link in the aircraft manufacturing process. Aircraft assembly is the process of combining and connecting parts, components or components according to design and technical requirements to form a higher-level assembly or complete machine. It is the key and core link of aircraft manufacturing. , determines the final quality, manufacturing cost and cycle of the aircraft to a large extent. In the modern aircraft manufacturing process, the assembly connection quality directly affects the fatigue resistance and reliability of the aircraft structure, and ultimately affects the life of the aircraft. It is worth noting that foreign developed countries have paid considerable attention to aircraft digital assembly technology, invested heavily in research and development, a...

Claims

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Application Information

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IPC IPC(8): B23P21/00B25B11/00B64F5/00B64F5/10
CPCB23P21/002B25B11/00B64F5/10
Inventor 蒋君侠董辉跃朱灵盛柯映林张平李少波罗水均
Owner ZHEJIANG UNIV
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