Aircraft Component Machining with Backup Upper Tool Units

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Solution Overview

Problem

Existing processing installations for aircraft structural components face challenges with service operations on upper tools, leading to complex and time-intensive procedures, resulting in prolonged downtimes due to the need for manual removal of jammed rivet elements and other service operations.

Innovation Solution

The implementation of a second upper tool unit allows for continued processing of aircraft structural components by enabling another upper tool to take over operations in case of failure, thereby reducing downtimes. This is achieved by positioning the second upper tool unit to cooperate with the common lower tool, allowing for uninterrupted processing and simplified service operations.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of operation

If a service platform is moved into position below the upper tool for service operations, then service personnel can access the upper tool, but the processing operation must be interrupted and the service operation becomes complex and time-intensive

Engineering Contradiction:
ImproveService accessibilityVSAvoidService downtime
Core Design Contradiction:
Ease of operationVSLoss of time

Solution Approach 1:

The upper tool unit is divided into separable components that can be quickly detached and replaced. The upper tool can be rapidly exchanged with a backup tool without requiring complex service operations, thereby reducing service downtime while maintaining accessibility.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A second upper tool unit is prepared in advance as a backup. When service is needed on the first upper tool, the pre-positioned second upper tool can immediately take over the processing operation, eliminating the need to interrupt processing for service access.

Inventive Principle:
Principle #10Preliminary action

2Productivity

If the upper tool is positioned several meters above ground for processing operations, then the processing installation can accommodate large aircraft structural components, but service personnel cannot readily reach the upper tool

Engineering Contradiction:
ImproveProcessing capabilityVSAvoidService accessibility
Core Design Contradiction:
ProductivityVSEase of operation

Solution Approach 1:

The upper tool unit is designed as a modular, separable system. The upper tool can be quickly detached from its elevated position and replaced with a backup tool, allowing service operations to be performed on the ground level while maintaining high processing capability during normal operation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A second upper tool unit serves as a duplicate backup system. When the first upper tool requires service, the second upper tool can immediately assume the processing function from the elevated position, while service personnel work on the first tool from ground level.

Inventive Principle:
Principle #26Copying

3Device complexity

If a single upper tool unit is used for processing, then the processing installation is simpler, but any failure or service need stops the entire processing operation

Engineering Contradiction:
ImproveTool unit configurationVSAvoidProcessing continuity
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The upper tool system is segmented into multiple independent upper tool units that can operate separately. This modular configuration allows one unit to continue processing while another undergoes maintenance, improving reliability without significantly increasing overall system complexity.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system employs a backup upper tool unit that remains standby ready to take over if the primary unit fails or requires service. This redundancy ensures processing continuity while keeping the additional complexity minimal, as the backup unit is only activated when needed.

Inventive Principle:
Principle #34Discarding and recovering

Data Source

PatentUS12337993B2Machining facility for aircraft structural components
Publication Date: 2025.06.24 BROETJE AUTOMATION
  • US12337993B2 patent drawing

AI summary

The disclosure relates to a processing installation for aircraft structural components having a processing station comprising a clamping frame, wherein the clamping frame extends along a station longitudinal axis, and a processing unit which has a first upper tool unit having an upper tool which is orientated along a first tool axis and a lower tool unit having a lower tool which is orientated along a second tool axis, wherein the first tool axis and the second tool axis can be orientated parallel with a vertical direction which is angled with respect to the longitudinal direction, and wherein in at least one processing position of the upper tool of the first upper tool unit and in at least one processing position of the lower tool of the lower tool unit the first tool axis and the second tool axis are orientated coaxially relative to each other.