Stiffened CFRP Ribs for Thermal Mismatch

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Solution Overview

Problem

Aluminum side of body ribs used in aircraft with CFRP wing boxes face thermal expansion mismatches and high fatigue loads, leading to inefficiencies and increased costs due to added weight requirements.

Innovation Solution

The use of stiffened carbon fiber reinforced polymer (CFRP) side of body ribs with a combination of aluminum and thermoplastic or thermoset stiffeners, connected via fasteners or co-bonding/co-curing, to form a CFRP rib assembly that matches the thermal expansion of the CFRP wing box while providing structural reinforcement.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If aluminum side of body ribs are used to match thermal expansion of aluminum wing boxes, then thermal expansion compatibility is improved, but thermal expansion mismatch occurs when used with CFRP wing boxes

Engineering Contradiction:
Improvethermal expansion compatibilityVSAvoidcompatibility with CFRP wing boxes
Core Design Contradiction:
Stability of the object's compositionVSAdaptability or versatility

Solution Approach 1:

The patent employs a composite structure combining CFRP rib webs with aluminum stiffeners. The CFRP portion matches the thermal expansion characteristics of the CFRP wing box, while the aluminum stiffeners provide the necessary structural reinforcement to withstand high fatigue loads. This composite approach allows the rib assembly to be compatible with both CFRP and aluminum wing box configurations.

Inventive Principle:
Principle #40Composite materials

2Strength

If aluminum side of body ribs are used to meet high fatigue load requirements, then structural strength is improved, but weight increases making it not cost effective

Engineering Contradiction:
Improvefatigue load resistanceVSAvoidrib assembly weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The patent applies local quality by using aluminum stiffeners only in specific locations where high fatigue load resistance is required, rather than making the entire rib assembly from aluminum. The CFRP rib webs provide sufficient strength for normal loading conditions, while the aluminum stiffeners are strategically placed to reinforce areas subject to high fatigue loads, thereby reducing overall weight while maintaining structural integrity.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The hybrid composite structure combines the lightweight properties of CFRP with the high strength-to-weight ratio of aluminum in critical areas. This allows the rib assembly to achieve the necessary fatigue load resistance without the penalty of using solid aluminum construction throughout, thus reducing overall weight and improving cost-effectiveness.

Inventive Principle:
Principle #40Composite materials

3Stability of the object's composition

If monolithic or built-up aluminum rib configurations are used, then structural integrity is maintained, but thermal expansion mismatch and weight issues arise with CFRP wing boxes

Engineering Contradiction:
Improvestructural integrityVSAvoidrib assembly weight
Core Design Contradiction:
Stability of the object's compositionVSWeight of moving object

Solution Approach 1:

The patent segments the rib assembly into distinct CFRP rib web portions and aluminum stiffener portions. This segmentation allows each material to be optimized for its specific function: CFRP for thermal expansion compatibility and general structural support, and aluminum for localized fatigue load resistance. The segmented design maintains structural integrity through proper connection mechanisms while avoiding the weight and thermal expansion issues of monolithic aluminum construction.

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 solution effectively addresses thermal expansion mismatches and high fatigue loads, reducing weight and costs by utilizing CFRP materials that are more efficient and cost-effective than traditional aluminum ribs, while maintaining structural integrity.

Implementation Method 1

an exterior of the interference fit fasteners may include stripes of a coating separated by non-coated stripes

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentUS11319051B2Stiffened composite ribs
Publication Date: 2022.05.03 THE BOEING CO
  • US11319051B2 patent drawing
  • US11319051B2 patent drawing
  • US11319051B2 patent drawing

AI summary

A side of body carbon fiber reinforced polymer (CFRP) composite rib assembly that is formed by connecting an aft CFRP rib web, a middle CFRP rib web, and a forward CFRP rib web together. The side of body CFRP rib assembly includes a plurality of stiffeners connected to the aft CFRP rib web, the middle CFRP rib web, or the forward CFRP rib web. A first stiffener connects the aft CFRP rib web with the middle CFRP rib web and a second stiffener connected the forward CFRP rib web to the middle CFRP rib web. The stiffeners may be connected via fasteners or may be co-bonded or co-cured with the side of body CFRP rib web. The stiffeners connected to the side of body CFRP rib assembly may include more than one shape and may be aluminum, a thermoset, and/or a thermoplastic.