Composite Pressure Hull Joint Layout for Lightweight Strength

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Solution Overview

Problem

Conventional composite pressure hulls face challenges in reducing weight while maintaining structural efficiency, particularly in applications like aircraft components, where weight affects performance and buoyancy is desirable for submersible applications.

Innovation Solution

The method involves forming a composite pressure hull by laying up unitary halves with dome and cylindrical portions on a mandrel, creating a joint transition region using scarf joints or staggered ply splices, and joining these halves to form a continuous, closed structure without central holes, utilizing composite materials and automated fiber layup techniques.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If conventional composite pressure hulls are manufactured using traditional methods, then structural integrity can be maintained, but weight reduction is limited and manufacturing complexity increases

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

Solution Approach 1:

The pressure hull is divided into two unitary halves (first half and second half), each manufactured separately using automated fiber layup techniques. This segmentation enables weight optimization through composite materials while managing manufacturing complexity by breaking down the overall structure into manageable sections that can be produced using standardized processes.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent employs composite materials consisting of reinforcing fibers bound in polymer resin matrix to construct the pressure hull halves. These composite materials provide superior strength-to-weight ratio compared to conventional materials, achieving weight reduction while maintaining structural integrity. The automated fiber layup process further enhances efficiency in manufacturing these composite structures.

Inventive Principle:
Principle #40Composite materials

2Strength

If unitary halves are joined to form a complete pressure hull, then buoyancy and structural efficiency are improved, but manufacturing precision requirements increase

Engineering Contradiction:
Improvestructural efficiencyVSAvoidjoining precision
Core Design Contradiction:
StrengthVSManufacturing precision

Solution Approach 1:

The transition regions with joints are formed during the layup process itself, before the final curing and joining stages. This preliminary formation of joints within the transition regions allows for better integration and alignment of the unitary halves, reducing the precision demands on subsequent joining operations while maintaining structural efficiency.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The patent incorporates transition regions with joints at specific locations where the dome portion meets the cylindrical portion of each unitary half. These localized joint regions are designed with specific structural characteristics to handle stress concentrations, allowing the overall structure to achieve high structural efficiency while concentrating manufacturing precision requirements to specific manageable areas rather than the entire hull.

Inventive Principle:
Principle #3Local quality

Data Source

PatentUS20250100235A1Composite Pressure Hull and Methods of Forming
Publication Date: 2025.03.27 THE BOEING CO
  • US20250100235A1 patent drawing
  • US20250100235A1 patent drawing
  • US20250100235A1 patent drawing

AI summary

A composite pressure hull and methods of forming the composite pressure hull are presented. A unitary first half of the composite pressure hull is laid up. A unitary second half of the composite pressure hull is laid up. The unitary first half is joined to the unitary second half to form the composite pressure hull.