Outlet Cone Cooling Layout for Turbomachine Component Integration

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The high temperature of the primary flow around the outlet cone in turbomachines limits the integration of components due to excessive heat, creating a large unused space.

Innovation Solution

A double-flow turbomachine design with a hollow radial arm conveying a cooling flow from a secondary flow to cool components in the outlet cone, utilizing a cover to channel the cooling flow around and through components, and a thermal insulation space to maximize heat exchange.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Productivity

If components are integrated in the outlet cone, then the productivity is improved by utilizing previously unused space, but the temperature becomes excessively high making component integration impossible

Engineering Contradiction:
Improvecomponent integrationVSAvoidtemperature in outlet cone
Core Design Contradiction:
ProductivityVSTemperature

Solution Approach 1:

The outlet cone is divided into distinct functional zones: a thermal insulation space separated by an inner wall, and component mounting regions. This segmentation allows the cone to simultaneously provide thermal protection for components while maintaining structural integrity and aerodynamic function.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A cooling flow is introduced as an intermediary substance between the hot primary flow and the components to be cooled. This cooling flow, circulated through the thermal insulation space, acts as a thermal mediator that absorbs excess heat from components without requiring direct contact with the hot primary flow.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Temperature

If a cooling flow is circulated to cool components, then the temperature is reduced enabling component installation, but the device complexity increases due to additional cooling systems

Engineering Contradiction:
Improvecomponent temperatureVSAvoidcooling system complexity
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The cooling flow serves multiple functions simultaneously: it cools components mounted in the outlet cone, it provides thermal insulation by circulating in the dedicated insulation space, and it can be integrated with existing engine air systems. This multi-functionality reduces the need for separate dedicated cooling systems for each function.

Inventive Principle:
Principle #6Universality (Multi-functionality)

Solution Approach 2:

The cooling system is merged with the thermal insulation structure by circulating the cooling flow through the thermal insulation space defined by the inner and outer walls of the outlet cone. This integration combines the cooling function with the structural insulation function, reducing overall system complexity.

Inventive Principle:
Principle #5Merging (Combining)

3Device complexity

If the cooling flow simply ventilates the entire inner space of the cone, then the device complexity is minimized, but the cooling effectiveness is insufficient for component cooling

Engineering Contradiction:
Improvecooling system simplicityVSAvoidcooling effectiveness
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

Instead of uniform ventilation throughout the entire cone, the cooling flow is directed to specifically target regions where components are mounted. The inner wall creates a dedicated thermal insulation space that channels cooling flow locally around components, providing enhanced cooling effectiveness precisely where needed rather than diffuse cooling throughout the entire volume.

Inventive Principle:
Principle #3Local quality

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

Effective cooling allows for the installation of components like electrical machines in the outlet cone, with optimized heat exchange and thermal protection, even during engine shutdown.

Implementation Method 1

a cooling flow passes from upstream to downstream through this space before being discharged

Methodology Applied
Scientific EffectConvection: Convection

Implementation Method 2

an inner wall which runs alongside the outer wall and is radially spaced therefrom to delimit a thermal insulation space

Methodology Applied
Scientific EffectThermal insulation: Thermal Insulation

Data Source

PatentUS12560104B2Turbomachine comprising an outlet cone incorporating components cooled by circulation of a cooling flow
Publication Date: 2026.02.24 SAFRAN AIRCRAFT ENGINES SAS
  • US12560104B2 patent drawing
  • US12560104B2 patent drawing
  • US12560104B2 patent drawing

AI summary

A double-flow turbomachine has an exhaust casing through which a hot primary flow passes and surrounded by a cold secondary flow, and a cone carried by the exhaust casing. The exhaust casing has a hollow radial arm passing through the primary flow to convey air into the cone in order to form a cooling flow for components located in the cone. The cone has an outer wall and an inner wall which runs alongside the outer wall and is radially spaced therefrom to delimit a thermal insulation space through which the cooling flow passes from upstream to downstream before it is discharged through an outlet opening at the end of the cone. It has an inner cover surrounding a component to channel the cooling flow so that it runs along the component to cool it before passing through the thermal insulation space to be discharged there.