Curved Composite Stringer Forming via Rotatable Pallet

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Solution Overview

Problem

Aircraft stringer manufacturing faces challenges in forming curved composite charges due to the need for multiple tools and stages, which increases costs and can result in wrinkles during bending operations.

Innovation Solution

A method and device that integrate in-plane and out-of-plane bending capabilities into the stringer shaping process, using a rotatable pallet system with a bendable die to form curved composite charges, reducing the risk of wrinkles and consolidating multiple processing stages into one operation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If conventional two-stage shaping and bending is used, then stringer bends can be formed, but wrinkles are caused and manufacturing complexity increases

Engineering Contradiction:
Improvestringer bend shapeVSAvoidsurface quality (wrinkles)
Core Design Contradiction:
ShapeVSManufacturing precision

Solution Approach 1:

The patent combines the shaping and bending operations into a single integrated forming process. The forming tool includes both a die for shaping the hat portion and a cavity for receiving the bent stringer, allowing both operations to be performed simultaneously without transferring the stringer to another tool, thereby eliminating wrinkles caused by separate bending operations

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The patent performs the bending operation during the initial shaping process rather than as a subsequent step. The stringer is bent into its final configuration while still in the forming tool, before the shaping is completed, ensuring that the bending occurs under controlled conditions that prevent wrinkle formation

Inventive Principle:
Principle #10Preliminary action

2Shape

If dedicated forming tools are created for each stringer type, then specific shapes can be formed, but manufacturing costs and device complexity increase

Engineering Contradiction:
Improvestringer shape specificityVSAvoidforming tool variety
Core Design Contradiction:
ShapeVSDevice complexity

Solution Approach 1:

The forming tool is designed with a die and cavity system that can accommodate multiple stringer types and configurations. The die can be positioned at different locations within the cavity, and the cavity can receive stringers with various bends and turns, allowing a single tool to produce different stringer shapes without requiring dedicated tools for each type

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

Solution Approach 2:

The forming tool incorporates adjustable components, including a die that can be positioned at different locations within the cavity and a stringer support that can be adjusted to accommodate different stringer configurations. This dynamic adjustability allows the same tool to produce various stringer shapes and configurations

Inventive Principle:
Principle #15Dynamics

3Shape

If multiple processing stages are used, then complex shapes can be formed, but process time and productivity decrease

Engineering Contradiction:
Improvecomplex stringer shapeVSAvoidprocess throughput
Core Design Contradiction:
ShapeVSProductivity

Solution Approach 1:

The patent merges multiple processing stages into a single forming operation. The shaping of the hat portion and the bending of the stringer are performed simultaneously in one operation, eliminating the need to transfer the stringer between tools and reducing the total number of process steps, thereby increasing productivity

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP3871868B1Method and device for forming curved composite charges for stringers
Publication Date: 2023.07.05 THE BOEING CO
  • EP3871868B1 patent drawingFigure 1A~1B
  • EP3871868B1 patent drawingFigure 1C~1E
  • EP3871868B1 patent drawingFigure 1F~1G

AI summary

Described are methods and systems for manufacturing curved composite stringers. Such composite stringers may have in-plane and/or out-of-plane bends, which are formed while shaping composite charges. Specifically, a composite charge (130) is shaped using a pallet (310), comprising a plurality of independent pallet portions (319), rotatably coupled to each other. A hat portion (131) is formed when a part of this charge is conformed to a cavity (318) in the pallet. The pallet portions (319) are rotated relative to each other while forming the hat portion (131) and/or when the hat portion (131) already conforms to the cavity (318). In some examples, the die (320) is bent together with the charge (130), when the pallet portions (319) are rotated. This rotation produces one or more of in-plane and/or out-of-plane bends. In some examples, flange portions (136) of the composite charge (130) are positioned in a temporary orientation, e.g., to enable bending of the charge and reduce wrinkles.