Segmented Turbine Exhaust Case Thermal Expansion
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Solution Overview
Problem
The existing sheet metal turbine exhaust cases face challenges in thermal and structural mismatch, leading to potential deformation due to thermal growth of struts, which limits the choice of materials and construction methods, especially in achieving balanced stiffness between the outer and inner shrouds while maintaining lightweight design.
Innovation Solution
A turbine exhaust case design featuring a segmented inner shroud with arcuate panels and circumferentially spaced-apart struts that allow for thermal expansion and contraction, along with a unitary outer shroud of different stiffness, connected by struts that also serve as acoustic panels for sound attenuation, addressing thermal mismatch and stress relief.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Stability of the object's composition
If the inner and outer shrouds are made of the same sheet metal material to maintain balanced stiffness, then structural compatibility is improved, but the ability to accommodate thermal expansion of struts deteriorates
Solution Approach 1:
The inner shroud is divided into multiple circumferentially spaced-apart arcuate panels that can move relative to each other, allowing differential thermal expansion while maintaining overall structural integrity. This segmentation enables the shroud to accommodate strut thermal growth without requiring the entire structure to expand uniformly.
Solution Approach 2:
The inner shroud panels are designed to be movable relative to one another, transforming the static structure into a dynamic system that can adapt to thermal changes. This allows the shroud to flex and adjust its configuration in response to thermal expansion of the struts, maintaining stiffness balance while accommodating thermal growth.
2Reliability
If the inner shroud is segmented into arcuate panels to accommodate thermal expansion, then thermal growth accommodation is improved, but structural complexity increases
Solution Approach 1:
The arcuate panels serve multiple functions: they form the inner shroud structure, provide acoustic attenuation, and enable thermal expansion accommodation. By making the panels multi-functional, the design reduces the need for separate components and justifies the added complexity through functional integration.
Solution Approach 2:
The segmented panel structure allows the inner shroud to self-adjust and self-accommodate thermal expansion without requiring external mechanisms or complex control systems. The panels move relative to each other in response to thermal growth, providing automatic adaptation to thermal conditions.
3Object-affected harmful factors
If acoustic panels are integrated into the inner shroud to provide sound attenuation, then acoustic performance is improved, but manufacturing complexity increases
Solution Approach 1:
The acoustic panels are merged with the inner shroud structure, combining acoustic attenuation functionality with the structural shroud. This integration eliminates the need for separate acoustic lining components and simplifies the overall assembly process while maintaining effective sound attenuation.
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 design reduces stress levels, increases component durability, and provides effective sound attenuation by allowing the inner shroud to thermally expand and contract, while maintaining structural integrity and minimizing weight by eliminating the need for additional frame members.
Implementation Method 1
the panels being movable relative to each other to provide for thermal expansion/contraction of the radially inner annular shroud in response to thermally induced movement of the turbine exhaust struts
Implementation Method 2
a plurality of circumferentially spaced-apart exhaust struts extending radially across the gaspath between the radially outer and the radially inner annular shrouds
Data Source
AI summary
A turbine exhaust case for a turbofan engine comprises a plurality of arcuate acoustic panels assembled into a circumferentially extending inner shroud with circumferential gaps between adjacent acoustic panels. An outer shroud extends circumferentially about the inner shroud. The inner shroud and the outer shroud define an annular gaspath therebetween. A plurality of circumferentially spaced-apart exhaust struts extends radially across the annular gaspath and structurally connects the individual acoustic panels forming the inner shroud to the outer shroud.


