Exhaust Nozzle Vane Support for Thermal Expansion

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Solution Overview

Problem

Gas turbine engine exhaust nozzles face challenges in managing high temperatures, which affect the structural integrity and operational efficiency due to thermal expansion and contraction of components.

Innovation Solution

The design incorporates an expansion-permissive link system that includes an inner plug, support vanes, and a vane-support frame, allowing for thermal expansion and contraction by adjusting the distance between components, ensuring stability and efficient operation across temperature changes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Stability of the object's composition

If rigid support structures are used to hold the inner plug, then structural stability is improved, but thermal expansion causes stress and potential damage

Engineering Contradiction:
Improvestructural stabilityVSAvoidthermal stress
Core Design Contradiction:
Stability of the object's compositionVSStress or pressure

Solution Approach 1:

The support vanes are designed with dynamic characteristics that allow them to flex and adapt to thermal expansion. The vanes can change their structural state from rigid to flexible depending on temperature conditions, enabling the inner plug to expand and contract without generating excessive stress while maintaining structural stability during normal operation.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The support vanes change their physical parameters (flexibility, stiffness) in response to temperature changes. As temperature increases, the vanes become more flexible to accommodate thermal expansion of the inner plug. This parameter change allows the structure to adapt to varying thermal conditions without compromising structural integrity or generating damaging stress.

Inventive Principle:
Principle #35Parameter changes

2Stability of the object's composition

If the inner plug is firmly constrained, then positional stability is improved, but operational efficiency decreases due to restricted thermal movement

Engineering Contradiction:
Improvepositional stabilityVSAvoidoperational efficiency
Core Design Contradiction:
Stability of the object's compositionVSProductivity

Solution Approach 1:

The support vanes provide dynamic positioning rather than static constraint. They maintain the inner plug in a stable position during normal operation but allow controlled movement when thermal expansion occurs. This dynamic behavior ensures both positional stability for operational efficiency and adequate thermal movement capability.

Inventive Principle:
Principle #15Dynamics

3Strength

If heavy-duty support structures are used, then structural integrity at high temperature is improved, but weight increases

Engineering Contradiction:
Improvestructural integrityVSAvoidnozzle assembly weight
Core Design Contradiction:
StrengthVSWeight of moving object

Solution Approach 1:

The support vanes are designed as thin, flexible structures rather than heavy-duty rigid components. These thin-film-like vanes provide adequate structural integrity to support the inner plug while accommodating thermal expansion through their flexibility. This approach achieves the required strength without the weight penalty of conventional heavy-duty support structures.

Inventive Principle:
Principle #30Flexible shells and thin films

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 enables the exhaust nozzle to maintain structural integrity and operational efficiency by accommodating thermal growth, reducing stress and enhancing performance under varying temperature conditions.

Implementation Method 1

The expansion-permissive link may allow for thermal expansion and contraction of the inner plug and the support vane relative to one another as a temperature of the exhaust nozzle changes

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentUS11274630B2Exhaust nozzle with vane support structure for a gas turbine engine
Publication Date: 2022.03.15 ROLLS ROYCE CORP
  • US11274630B2 patent drawing
  • US11274630B2 patent drawing
  • US11274630B2 patent drawing

AI summary

An exhaust nozzle for use with a gas turbine engine includes an outer shroud and a nozzle-plug assembly coupled to the outer shroud. The nozzle-plug assembly includes an inner plug and at least one support vane that is coupled to the outer shroud to support the inner plug in an exhaust nozzle flow path.