Composite Stringer Splicing and Vacuum Compaction

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Solution Overview

Problem

The assembly of stiffened composite structures, such as aircraft fuselages, is labor-intensive and requires large, customized tooling, making it difficult to handle and transport long stringers and resulting in inefficient production processes.

Innovation Solution

The use of a trunnion with a rotatable chuck and stiffener trays allows for the indexing, splicing, and vacuum compaction of stringer segments, enabling efficient assembly and transportation of stringers in segments, and accommodating multiple stringer types with a single trunnion, along with a transfer tool for efficient loading onto an inner mold line layup mandrel.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If stringers are handled and assembled in their entirety, then the structural integrity is maintained, but the handling and transportation becomes difficult due to their length

Engineering Contradiction:
Improvestructural integrityVSAvoidhandling and transportation
Core Design Contradiction:
Stability of the object's compositionVSEase of operation

Solution Approach 1:

The stringer is divided into multiple segments that can be handled and transported separately. These segments are then joined together using a splice fixture to form the complete stringer assembly, combining the benefits of easier handling with maintained structural integrity.

Inventive Principle:
Principle #1Segmentation

2Manufacturing precision

If customized tooling is used for each stringer type, then the assembly precision is improved, but the device complexity and space requirements increase

Engineering Contradiction:
Improveassembly precisionVSAvoidtooling complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

A universal splice fixture is designed that can accommodate multiple stringer types through adjustable components and interchangeable fixtures. This single multi-functional device replaces the need for multiple customized tooling sets, maintaining assembly precision while reducing device complexity and space requirements.

Inventive Principle:
Principle #6Universality (Multi-functionality)

3Ease of operation

If manual positioning of stringers is used, then the flexibility in positioning is maintained, but the productivity decreases due to labor-intensive processes

Engineering Contradiction:
Improvepositioning flexibilityVSAvoidproduction efficiency
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

A splice fixture serves as an intermediary device that guides and positions stringer segments during assembly. This fixture maintains the positioning flexibility previously achieved through manual methods while enabling more efficient assembly operations and improving overall productivity.

Inventive Principle:
Principle #24Intermediary (Mediator)

4Length of moving object

If large tooling is used to accommodate long stringers, then the assembly capability is improved, but the space requirements increase

Engineering Contradiction:
Improvestringer lengthVSAvoidtooling space
Core Design Contradiction:
Length of moving objectVSArea of stationary object

Solution Approach 1:

By segmenting the stringer into smaller sections, the assembly process can be performed on a compact splice fixture that occupies less space. The segments are joined in-place, eliminating the need for large tooling that could accommodate the full length of the completed stringer.

Inventive Principle:
Principle #1Segmentation

Applied Scientific Principles

This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.

Function Achieved in This Case

This method improves production efficiency by allowing for the assembly of stiffened composite structures with reduced labor and tooling requirements, enabling the handling and transportation of long stringers in segments and accommodating various stringer types, thus streamlining the manufacturing process.

Implementation Method 1

applying a vacuum chuck to the trunnion to compact the stiffener assembly

Methodology Applied
Scientific EffectVacuum: Vacuum

Implementation Method 2

moving the vacuum chuck together with the stiffener assembly from the trunnion to a transfer tool

Methodology Applied
Scientific EffectVacuum: Vacuum

Data Source

PatentUS10807737B2Process for handling, installing, compacting, splicing, and/or assembling composite stringers
Publication Date: 2020.10.20 THE BOEING CO
  • US10807737B2 patent drawing
  • US10807737B2 patent drawing
  • US10807737B2 patent drawing

AI summary

Methods of assembling stiffened composite structures are disclosed. Some methods include forming a stiffener assembly by compacting it within a trough formed in a trunnion. A single trunnion may accommodate two or more different types of stiffeners, thereby avoiding the need for multiple sets of tooling. In some methods, a plurality of stiffener segments may be spliced together, thereby avoiding the need to transport and handle an entire stiffener. A vacuum chuck may be utilized in some examples to transfer the stiffener assembly from the trunnion to a transfer tool. The same vacuum chuck may be transferred along with the stiffener assembly on the transfer tool and loaded onto an inner mold line layup mandrel, where the vacuum chuck may be used to compact the stiffener assembly to the inner mold line layup mandrel.