Variable Fan Outlet Guide Vanes for Turbofan Engines

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Solution Overview

Problem

Turbofan gas turbine engines face conflicting design requirements for fan outlet guide vanes, needing high solidity and loading at take-off for high fan pressure ratio while avoiding choking at high flight Mach numbers, which limits airflow and thrust production.

Innovation Solution

A turbofan gas turbine engine design featuring a single stage of variable fan outlet guide vanes that can pivot from a nominal to an open position, minimizing weight and frontal area, and incorporating a fan bypass duct with radially outward and inward inlets and a supercharger to manage airflow efficiently across varying Mach numbers.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If fan outlet guide vanes are designed with high solidity and high loading for take-off operation, then fan pressure ratio is improved, but the vanes become choked at high flight Mach numbers limiting airflow and thrust

Engineering Contradiction:
Improvefan pressure ratioVSAvoidairflow to ramburner
Core Design Contradiction:
PowerVSProductivity

Solution Approach 1:

The patent applies variable geometry to the fan outlet guide vanes, allowing them to pivot between different angular positions. At take-off, the vanes are positioned to provide high solidity and loading for maximum fan pressure ratio. At high flight Mach numbers, the vanes pivot to an open position to prevent choking and maintain airflow to the ramburner, thus resolving the contradiction between high power at low speed and high productivity at high speed.

Inventive Principle:
Principle #15Dynamics

2Power

If fan outlet guide vanes are designed with high solidity for take-off, then thrust production is improved, but weight and frontal area increase

Engineering Contradiction:
Improvethrust productionVSAvoidfan section weight
Core Design Contradiction:
PowerVSWeight of stationary object

Solution Approach 1:

Instead of using a fixed high-solidity vane design that would permanently increase weight, the patent employs variable geometry where the vanes can adjust their angle. This allows the fan section to achieve high thrust when needed without permanently increasing weight, as the high-solidity configuration is only active during take-off operations.

Inventive Principle:
Principle #15Dynamics

3Force

If fan outlet guide vanes are designed with high solidity for take-off, then aerodynamic loading is improved, but airflow interruption increases

Engineering Contradiction:
Improveaerodynamic loadingVSAvoidairflow interruption
Core Design Contradiction:
ForceVSObject-generated harmful factors

Solution Approach 1:

The variable geometry design allows the fan outlet guide vanes to provide high aerodynamic loading during take-off when maximum thrust is required. During high Mach number operation, the vanes pivot to an open position that minimizes airflow interruption, thus resolving the contradiction between high force generation and harmful airflow disruption.

Inventive Principle:
Principle #15Dynamics

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

Enables efficient operation from take-off to high Mach number conditions without choking the fan outlet guide vanes, maintaining thrust production while reducing weight and airflow interruption, and accommodating windmilling in ram burner mode.

Implementation Method 1

The forward fan section has only a single stage of variable fan guide vanes and the fan guide vanes are variable fan outlet guide vanes located downstream or aft of and adjacent to the forward fan rotor blades

Methodology Applied
Scientific EffectAerodynamic flow control:

Implementation Method 2

A supercharger is disposed in the inlet duct. The supercharger may include radially outwardly extending blade tips of rotor blades of the core driven fan

Methodology Applied
Scientific EffectCompression: Compression

Implementation Method 3

The forward fan section has only a single stage of variable fan guide vanes and the fan guide vanes are variable fan outlet guide vanes located downstream or aft of and adjacent to the forward fan rotor blades

Methodology Applied
Scientific EffectAerodynamic propulsion:

Data Source

PatentUS7730714B2Turbofan gas turbine engine with variable fan outlet guide vanes
Publication Date: 2010.06.08 GENERAL ELECTRIC CO
  • US7730714B2 patent drawing
  • US7730714B2 patent drawing
  • US7730714B2 patent drawing

AI summary

A turbofan gas turbine engine includes a forward fan section with a row of fan rotor blades, a core engine, and a fan bypass duct downstream of the forward fan section and radially outwardly of the core engine. The forward fan section has only a single stage of variable fan guide vanes which are variable fan outlet guide vanes downstream of the forward fan rotor blades. An exemplary embodiment of the engine includes an afterburner downstream of the fan bypass duct between the core engine and an exhaust nozzle. The variable fan outlet guide vanes are operable to pivot from a nominal OGV position at take-off to an open OGV position at a high flight Mach Number which may be in a range of between about 2.5-4+. Struts extend radially across a radially inwardly curved portion of a flowpath of the engine between the forward fan section and the core engine.