Composite Fan Case Containment System with Internal Grid
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Solution Overview
Problem
Conventional softwall fan containment systems for larger diameter gas turbine engines face challenges in achieving sufficient structural integrity and cost-effective fabrication, as aluminum honeycomb structures may not provide adequate residual stiffness and strength, and bonding processes are costly.
Innovation Solution
A cylindrical composite fan case structure with an internal and external grid pattern formed by reinforcing fiber windings in a resin matrix, where the internal grid acts as a damage-limiting substructure and the external grid provides additional strength and stiffness, potentially eliminating the need for dry containment fabric.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Weight of moving object
If aluminum honeycomb structures are used in softwall containment systems, then weight is reduced, but structural integrity (residual stiffness and strength) is insufficient
Solution Approach 1:
The patent replaces conventional aluminum honeycomb structures with a composite lattice structure made of fiber-reinforced materials. This composite lattice provides both the weight reduction benefits of softwall systems and the structural integrity needed to contain fan blade fragments, resolving the contradiction between lightweight design and structural strength.
Solution Approach 2:
The patent implements varying ply orientations and material properties at different locations within the lattice structure. Specific regions have enhanced structural properties to handle localized impact loads from blade fragments, while other regions maintain lower weight, thus achieving both weight reduction and structural integrity.
2Ease of manufacture
If bonding net shape aluminum honeycomb to composite inner shell is performed, then structural assembly is achieved, but manufacturing cost increases
Solution Approach 1:
The patent combines the lattice structure and containment shell into a single integrated composite structure manufactured in one piece using automated fiber placement. This eliminates the need for separate bonding operations between lattice and shell, reducing both manufacturing complexity and cost while maintaining structural integrity.
Solution Approach 2:
The composite lattice structure is manufactured to net shape using automated processes that lay down fibers and cure resin in a single operation. The structure serves its own structural and containment functions without requiring additional assembly steps or bonding materials, reducing manufacturing cost.
Data Source
AI summary
Composite article includes a generally cylindrical body having an internal grid structure interleaved with casing layers formed of reinforcing fibers disposed in a resin matrix. The composite article may be utilized in a fan case containment system for aircraft engine applications. Methods for fabricating the composite article are also provided.


