Bladderless Hat Stringer Curing via Conformal Surface

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Solution Overview

Problem

The manufacturing of composite hat stringers for aircraft structures is complex and costly, with fiber-reinforced composite materials presenting challenges such as increased complexity, expense, and waste generation due to improper curing.

Innovation Solution

A method involving the use of a rigid mold line conformal surface for coupling and curing composite hat stringers with a skin, applying pressure to compress the skin against the stringer, and using a bladder for compressive pressure during curing to form a reinforced composite structure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If fiber-reinforced composite materials are used to form structural members, then weight is reduced and mechanical strength is improved, but manufacturing complexity and cost increase

Engineering Contradiction:
ImproveweightVSAvoidmanufacturing complexity
Core Design Contradiction:
Weight of moving objectVSDevice complexity

Solution Approach 1:

The composite structure is divided into distinct modular components: hat stringers with rigid mold line conformal surfaces, skin panels, and adhesive bonding zones. This segmentation allows each component to be manufactured and cured independently before assembly, reducing overall manufacturing complexity while maintaining the weight and strength benefits of composite materials

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The hat stringers are pre-cured to form rigid mold line conformal surfaces before the skin panels are applied. This preliminary action creates ready-to-bond surfaces with precise geometric features, eliminating the need for complex real-time shaping during assembly and reducing manufacturing complexity

Inventive Principle:
Principle #10Preliminary action

2Strength

If pressure is applied to compress the skin against the hat stringer during curing, then bonding strength is improved, but additional equipment and process complexity are required

Engineering Contradiction:
Improvebonding strengthVSAvoidequipment complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

A bladder positioned within the hat stringer cavity is inflated with fluid pressure during the curing process. This pneumatic system applies uniform compressive force against the skin panel from the interior of the hat stringer, ensuring optimal bonding strength without requiring complex external mechanical pressing equipment

Inventive Principle:
Principle #29Pneumatics and hydraulics

Solution Approach 2:

The bladder is nested within the hat stringer cavity, allowing the pressure application mechanism to be contained within the structure itself rather than requiring external equipment. This nested arrangement simplifies the overall system while maintaining effective bonding pressure

Inventive Principle:
Principle #7Nested doll (Nesting)

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 approach simplifies the manufacturing process, reduces costs, and integrates the stringer and skin structure more effectively, while minimizing waste and improving mechanical strength.

Implementation Method 1

applying pressure on the skin opposite the closed hat stringer to compress the skin against the closed hat stringer

Methodology Applied
Scientific EffectCompressive pressure: Compression

Implementation Method 2

curing the skin to the rigid mold line conformal surface

Methodology Applied
Scientific EffectCuring: Chemical Bonding

Data Source

PatentUS8043554B2Manufacturing process using bladderless mold line conformal hat stringer
Publication Date: 2011.10.25 THE BOEING CO
  • US8043554B2 patent drawing
  • US8043554B2 patent drawing
  • US8043554B2 patent drawing

AI summary

Techniques for manufacturing structures that include composite hat stringers are disclosed. In one embodiment, a method of forming a composite structure includes placing a generally cured composite hat stringer on a tool, the hat stringer having a rigid mold line conformal surface for adjoining a generally uncured skin, positioning the skin adjacent to the rigid mold line conformal surface, coupling the skin to the rigid mold line conformal surface of the composite hat stringer, including applying a pressure to a surface of the skin to urge the skin into engagement with the composite hat stringer, and curing the skin.