Vortex Generators for Turbine Exhaust Backpressure Reduction

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Solution Overview

Problem

Existing exhaust duct designs for turboshaft engines in rotary-wing aircraft lead to high backpressure and inefficient engine performance due to separation and inadequate diffusion of exhaust air, and the mixing with secondary cooling airflow can result in degraded performance and component loss.

Innovation Solution

The implementation of a vortex generator within the exhaust system, positioned to interrupt both primary and secondary flows, which creates vortices to enhance mixing and reduce backpressure by optimizing the diffusion process between the two flows.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Shape

If existing exhaust duct designs with large turning angles are used, then the exhaust duct can accommodate the engine outlet geometry, but airflow separation occurs causing high backpressure and reduced engine efficiency

Engineering Contradiction:
Improveexhaust duct geometryVSAvoidbackpressure
Core Design Contradiction:
ShapeVSLoss of energy

Solution Approach 1:

Vortex generators are installed upstream in the exhaust duct to pre-condition the airflow before it encounters the large turning angles. The vortex generators create controlled vortices that energize the boundary layer and prevent flow separation at the duct turns, allowing the exhaust duct to maintain its necessary geometry without suffering from airflow separation losses

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The vortex generators modify the flow parameters by creating rotational motion and enhancing mixing in the exhaust stream. This changes the velocity profile and turbulence characteristics of the flow, enabling it to better withstand the adverse pressure gradients created by the large turning angles in the exhaust duct

Inventive Principle:
Principle #35Parameter changes

2Productivity

If vortex generators are added to the exhaust system, then mixing of primary and secondary flows is enhanced and backpressure is reduced, but device complexity increases

Engineering Contradiction:
Improveengine efficiencyVSAvoidexhaust system components
Core Design Contradiction:
ProductivityVSDevice complexity

Solution Approach 1:

The vortex generators are designed to be passive components that utilize the existing exhaust flow itself to generate the required vortices. The high-speed primary exhaust flow automatically passes over the vortex generator surfaces, creating the necessary rotational flow patterns without requiring additional energy input or active control systems

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The vortex generators are designed with specific geometric parameters (size, shape, orientation, spacing) that are optimized to produce the desired flow conditioning effect. By carefully selecting these parameters, the system achieves effective flow mixing and separation prevention with minimal additional complexity

Inventive Principle:
Principle #35Parameter changes

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 vortex generator improves engine performance by reducing exhaust losses and backpressure, enhancing the mixing of primary and secondary flows, and preventing hot exhaust backflow into the engine compartment, thus maintaining efficient engine operation and component integrity.

Implementation Method 1

a vortex generator arranged within the exhaust system at a position where both the primary flow and the secondary flow are present. The vortex generator interrupts at least one of the primary flow and the secondary flow.

Methodology Applied
Scientific EffectVortex generator: Vortex Generator

Implementation Method 2

The vortex generator interrupts at least one of the primary flow and the secondary flow... creates vortices to enhance mixing

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS11268390B2Vortex generators for turbine engine exhaust
Publication Date: 2022.03.08 SIKORSKY AIRCRAFT CORP
  • US11268390B2 patent drawing
  • US11268390B2 patent drawing
  • US11268390B2 patent drawing

AI summary

An exhaust system for an engine includes an exhaust nozzle located adjacent an outlet end of the engine to receive a primary flow of exhaust gasses expelled from the engine, an inlet opening formed between the exhaust nozzle and the outlet end of the engine through which a secondary flow is provided to the exhaust nozzle, and a vortex generator arranged within the exhaust system at a position where both the primary flow and the secondary flow are present. The vortex generator interrupts at least one of the primary flow and the secondary flow.