Aircraft Component Machining Layout for Single-Platform Tool Service
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Solution Overview
Problem
The existing processing installations for aircraft structural components are inefficient due to the complexity and time-intensiveness of service operations, as service operators cannot easily access both the upper and lower tool units from a single service platform, requiring additional platforms and potentially disrupting the processing region.
Innovation Solution
The processing installation is designed to allow both the upper and lower tool units to be accessible from a common, fixed service platform, which can remain in a service plane, enabling service operations without the need for additional platforms and maintaining separation between the processing and service regions.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If an additional service platform is provided to access the upper tool unit, then both tools become accessible, but the processing region is disrupted and reconstruction operations are required
Solution Approach 1:
Instead of adding a static second service platform that would complicate the installation and disrupt the processing region, the upper tool unit itself is made dynamic and displaceable. This allows service access without permanent structural modifications or additional platforms
Solution Approach 2:
The upper tool unit is extracted from its fixed position in the processing region and made movable into the service region during service operations. This extraction allows service operators to work on both tool units from the original service platform without disrupting the processing region's configuration
2Device complexity
If service operations are carried out from a single fixed service platform, then service complexity is reduced, but both tools must be accessible from that platform
Solution Approach 1:
The upper tool unit's displacement capability allows it to be positioned within reach of the fixed service platform during service operations, making both tool units accessible from the same platform without requiring the platform to be movable or additional platforms to be provided
Data Source
AI summary
The disclosure relates to a processing installation for aircraft structural components having a processing station comprising a clamping frame for receiving the structural component, wherein the clamping frame extends along a station longitudinal axis which extends in a longitudinal direction and a processing unit which has an upper tool unit having an upper tool and a lower tool unit, wherein the processing installation has a processing region which is formed by a laterally delimited, first spatial portion in which the clamping frame and the processing unit are arranged during processing, wherein the processing installation has a service region for carrying out service operations, wherein the first spatial portion is separated from the second spatial portion in a transverse direction, wherein a service platform is arranged in the service region and can be positioned in a service plane which is orthogonal to the vertical direction.