Layered Turbofan Blade Containment Arrangement

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Solution Overview

Problem

Turbofan gas turbine engine blade containment arrangements face challenges in withstanding ice impacts, accommodating radial variations and vibrations, and maintaining the trajectory of detached fan blades during failures, while also aiming to reduce weight and maintain structural integrity.

Innovation Solution

A layered containment arrangement comprising a first and second layer of cellular material, a strong and ductile layer with chopped glass fibers, and an abradable layer, where the cellular materials can be honeycomb or foam, and the strong and ductile layer is designed to absorb energy from impacts without rupturing, allowing for efficient energy absorption and distribution across the containment system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If a metallic fan casing with thicker regions is used to contain detached fan blades, then the containment strength is improved, but the weight of the fan casing increases

Engineering Contradiction:
Improvecontainment strengthVSAvoidfan casing weight
Core Design Contradiction:
StrengthVSWeight of stationary object

Solution Approach 1:

The patent employs a composite containment arrangement consisting of multiple material layers including cellular material (honeycomb or foam), strong and ductile material with chopped glass fibres, and abradable material. This composite structure achieves the required containment strength while reducing overall weight compared to solid metallic casings, as each layer contributes specific properties (energy absorption, structural strength, adaptability) without requiring excessive thickness throughout.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The containment arrangement uses different materials with specific properties positioned at different radial locations to address local requirements. The cellular material provides initial energy absorption, the strong and ductile layer with chopped glass fibres provides structural integrity and blade containment, and the abradable layer accommodates radial variations. This localized material distribution optimizes strength where needed while minimizing unnecessary weight in other areas.

Inventive Principle:
Principle #3Local quality

2Strength

If the fan blade containment arrangement is made stronger to withstand ice impacts, then the impact resistance is improved, but the ability to accommodate radial position variation and vibrations deteriorates

Engineering Contradiction:
Improveimpact resistanceVSAvoidaccommodation of radial variation and vibrations
Core Design Contradiction:
StrengthVSAdaptability or versatility

Solution Approach 1:

The containment arrangement assigns different functional properties to different material layers at different locations. The abradable material layer is specifically positioned to accommodate radial position variations and vibrations through its compliant nature, while the strong and ductile layer with chopped glass fibres provides impact resistance. This spatial differentiation of material properties allows simultaneous achievement of impact resistance and adaptability without compromise.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The multi-material composite structure enables dissociation of functions: the cellular material and strong and ductile layer handle impact forces, while the abradable material layer handles radial variations and vibrations. This functional separation within the composite system allows each layer to optimize its performance for its specific purpose without interfering with the other requirements.

Inventive Principle:
Principle #40Composite materials

3Weight of stationary object

If the fan blade containment arrangement is made thinner to reduce weight, then the weight is reduced, but the ability to contain detached fan blades deteriorates

Engineering Contradiction:
Improvefan casing weightVSAvoidblade containment capability
Core Design Contradiction:
Weight of stationary objectVSStrength

Solution Approach 1:

The patent uses a composite structure with multiple functional layers that together provide adequate blade containment capability at reduced thickness. The cellular material layer absorbs impact energy, the strong and ductile layer with chopped glass fibres provides structural containment strength, and the abradable layer ensures adaptability. This composite approach achieves containment performance comparable to or exceeding solid metallic structures while significantly reducing weight due to the lower density and optimized thickness of each layer.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The containment arrangement is segmented into multiple functional layers, each contributing to the overall containment capability. This segmentation allows the system to achieve the required containment performance through the combined effect of multiple thinner layers rather than requiring a single thick metallic structure, thereby reducing overall weight while maintaining or improving containment effectiveness.

Inventive Principle:
Principle #1Segmentation

4Loss of energy

If a layered containment arrangement with multiple materials is used to reduce weight and improve energy absorption, then the weight is reduced and energy absorption is improved, but the structural complexity increases

Engineering Contradiction:
Improveenergy absorptionVSAvoidcontainment arrangement complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The containment arrangement is divided into distinct functional layers (cellular material, strong and ductile material with chopped glass fibres, abradable material), where each layer is optimized for a specific function. This segmentation enables weight reduction and improved energy absorption by using lightweight materials in non-critical areas while maintaining structural integrity. The modular layered structure, while appearing complex, simplifies manufacturing and assembly compared to monolithic designs, as each layer can be independently selected and installed based on its specific function.

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

The solution effectively absorbs and distributes the energy from fan blade impacts, preventing penetration through the containment arrangement, reduces the weight of the fan casing, and maintains the structural integrity necessary to withstand ice impacts and vibrations, while allowing for reduced weight and independent operation from the fan casing design.

Implementation Method 1

a first layer of cellular material, a septum layer arranged within the first layer of cellular material, a second layer of cellular material arranged within the septum layer

Methodology Applied
Scientific EffectCompression: Compression

Implementation Method 2

the strong and ductile layer is designed to absorb energy from impacts without rupturing

Methodology Applied
Scientific EffectEnergy absorption: Absorption (physical)

Implementation Method 3

the strong and ductile layer is designed to absorb energy from impacts without rupturing

Methodology Applied
Scientific EffectDeformation: Deformation

Implementation Method 4

The strong and ductile layer may comprise chopped fibres in a resin. The strong and ductile layer may comprise chopped glass fibres

Methodology Applied
Scientific EffectComposite materials: Composite Materials

Implementation Method 5

a layer of abradable material arranged within the strong and ductile layer

Methodology Applied
Scientific EffectAbrasion: Abrasion

Data Source

PatentEP2458162B1Blade containment arrangement for a turbofan
Publication Date: 2020.03.04 ROLLS ROYCE PLC
  • EP2458162B1 patent drawingFigure 1~2
  • EP2458162B1 patent drawingFigure 3~5

AI summary

A gas turbine engine blade containment arrangement (32) comprises a casing (30), a first layer of cellular material (36) arranged within the casing (30), a septum layer (38) within the first layer of cellular material (36), a second layer of cellular material (40) within the septum layer (38), a strong and ductile layer (42) within the second layer of cellular material (40) and a layer of abradable material (44) within the strong and ductile layer (42).