Variable Width Flange Stringers for Aircraft Load Transfer

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Solution Overview

Problem

Existing elongated structures for aircraft, such as stringers, face challenges in attaching to adjacent structures with adequate load transfer without increasing weight and cost, and require complex designs to achieve desired weight and performance characteristics, leading to increased manufacturing time and cost.

Innovation Solution

The development of elongated structures with variable width flanges that can be tailored to provide varying levels of stability and load-bearing capacity along their length, allowing for efficient attachment to frame members using a mounting clip, reducing the need for multiple stringers and attachment fittings.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If traditional elongated structures are used with constant cross-section, then manufacturing is simpler, but load-bearing capacity and stability are insufficient for highly loaded structures

Engineering Contradiction:
Improveload-bearing capacityVSAvoidstructural complexity
Core Design Contradiction:
StrengthVSDevice complexity

Solution Approach 1:

The patent applies local quality by varying the cross-sectional properties of the elongated structure along its length. The flange width changes from a first width at the first end to a second width at the second end, allowing different sections to have optimized properties for their specific loading conditions. This enables the structure to achieve higher load-bearing capacity without requiring uniform complexity throughout, as each section is tailored to its local requirements.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The patent implements dynamics by transitioning from a static, constant cross-section design to a dynamic, variable cross-section design. The cross-sectional properties are not fixed but vary continuously or in steps along the length of the structure, allowing the structural characteristics to adapt to changing load conditions along the span, thereby improving overall load-bearing capacity.

Inventive Principle:
Principle #15Dynamics

2Strength

If more stringers are used to achieve desired weight and performance characteristics, then structural performance is improved, but manufacturing time and cost increase

Engineering Contradiction:
Improvestructural performanceVSAvoidmanufacturing efficiency
Core Design Contradiction:
StrengthVSProductivity

Solution Approach 1:

The patent applies universality by designing a single elongated structure that can perform multiple functions that would traditionally require multiple separate stringers. The variable cross-sectional design allows one structure to provide the necessary structural performance across different loading zones, replacing multiple constant-cross-section stringers and reducing the number of attachment fittings needed, thereby improving manufacturing efficiency.

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

Solution Approach 2:

The patent utilizes parameter changes by varying the cross-sectional dimensions (flange width) along the length of the elongated structure. This continuous or stepped variation in geometric parameters allows the structure to achieve desired weight and performance characteristics in a single component, eliminating the need for multiple stringers and reducing manufacturing complexity.

Inventive Principle:
Principle #35Parameter changes

3Reliability

If attachment fittings are machined for proper attachment, then load transfer is adequate, but weight and cost increase

Engineering Contradiction:
Improveload transfer capabilityVSAvoidattachment weight
Core Design Contradiction:
ReliabilityVSWeight of stationary object

Solution Approach 1:

The patent applies the extraction principle by removing the need for separate, complex machined attachment fittings. The variable cross-section design of the elongated structure itself provides the necessary attachment surfaces and load transfer capabilities directly on the structure, eliminating or reducing the need for additional attachment components, thereby reducing weight while maintaining adequate load transfer.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The patent merges the functions of the elongated structure and attachment fittings into a single integrated component. The variable cross-sectional design incorporates attachment surfaces and load transfer features directly into the structure body, combining what would traditionally be separate elements (structure plus attachment fittings) into one unified component, reducing overall weight and complexity.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentUS10207786B2Elongated structures and related assemblies
Publication Date: 2019.02.19 THE BOEING CO
  • US10207786B2 patent drawing
  • US10207786B2 patent drawing
  • US10207786B2 patent drawing

AI summary

An elongated structure comprising a web extending along a length of the elongated structure and a flange comprising a first flange portion, the first flange portion extending away from an area of the web. The first flange portion comprises a variable width along at least a portion of the length of the elongated structure. The first flange portion of the elongated structure may comprise the variable width the length of the elongate structure. The first flange portion may comprise a constant width along at least a portion of the length of the elongated structure. The elongated structure may further comprise a second flange portion. The second flange portion may comprise a variable width along at least a portion of the length of the elongate structure. The first flange portion may comprise a first top flange portion.