Undulating Fuel Injector Tube Structure for Thermal Fatigue Relief

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Solution Overview

Problem

Pressure atomizing fuel injectors for gas turbine engines experience premature fatigue failure due to thermal expansion and vibration resonance, leading to costly repairs from cracking at the metallurgical braze joints, especially in the primary fuel tube.

Innovation Solution

The fuel injector design incorporates an elongated fuel tube with an undulating surface that is in contact with another surface within the housing, reducing stress and fatigue failure by providing increased axial compliance and thermal transfer characteristics, and includes a secondary fuel tube with an undulating surface to support the primary fuel tube and reduce contact areas.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Strength

If the primary fuel tube is rigidly supported by metallurgical braze joints at both ends, then the structural support and positioning are improved, but the fatigue life deteriorates due to thermal expansion and vibration resonance stresses

Engineering Contradiction:
Improvestructural supportVSAvoidfatigue life
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The patent changes the physical state and geometric parameters of the primary fuel tube by introducing an undulating configuration instead of a straight rigid tube. This geometric parameter change allows the tube to flex and accommodate thermal expansion while maintaining structural support through the undulating shape's inherent flexibility and contact points with the secondary fuel tube.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent transforms the static rigid structure into a dynamic system where the primary fuel tube can move relative to the secondary fuel tube. The undulating tube allows controlled movement and flexing to absorb thermal expansion stresses and vibration resonance, while the contact points provide dynamic support rather than rigid fixation.

Inventive Principle:
Principle #15Dynamics

2Temperature

If the primary fuel tube is made cooler by secondary fuel flow, then the thermal stability is improved, but the thermal gradient stresses increase causing fatigue failure at braze joints

Engineering Contradiction:
Improvethermal stabilityVSAvoidthermal gradient stress
Core Design Contradiction:
TemperatureVSStress or pressure

Solution Approach 1:

The patent changes the geometric parameters of the primary fuel tube to an undulating configuration, which modifies the thermal conduction path and reduces thermal gradient stresses. The undulating shape increases the surface area and distributes thermal stresses more evenly along the tube length, preventing concentration at the braze joints while maintaining the cooling function.

Inventive Principle:
Principle #35Parameter changes

3Ease of manufacture

If straight fuel tubes are used with metallurgical joints, then the manufacturing simplicity is improved, but the resistance to fatigue failure deteriorates under thermal expansion and vibration

Engineering Contradiction:
Improvemanufacturing simplicityVSAvoidfatigue resistance
Core Design Contradiction:
Ease of manufactureVSReliability

Solution Approach 1:

The patent modifies the geometric parameter of the fuel tube from straight to undulating, which can be manufactured through forming or bending processes after assembly. This parameter change maintains manufacturing feasibility while dramatically improving fatigue resistance by allowing the tube to flex and absorb thermal and vibrational stresses without failing at the braze joints.

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 design significantly reduces fatigue failure at the metallurgical joints, minimizes resonant frequencies, and enhances the structural support of fuel delivery tubes, thereby increasing the fatigue life and reducing maintenance costs of the fuel injector.

Implementation Method 1

said undulating tube surface being in contact with another surface disposed in said housing at one or more locations of said undulating tube surface

Methodology Applied
Scientific EffectThermal transfer: Conduction (thermal)

Implementation Method 2

During high power engine operation, the fuel injector undergoes thermal expansion and vibration resonance, which generate internal stresses

Methodology Applied
Scientific EffectThermal expansion: Thermal Expansion

Data Source

PatentUS11840961B2Gas turbine engine fuel injector
Publication Date: 2023.12.12 WOODWARD INC
  • US11840961B2 patent drawing
  • US11840961B2 patent drawing
  • US11840961B2 patent drawing

AI summary

The subject matter of this specification can be embodied in, among other things, a fuel injector for a gas turbine engine includes a fuel injector housing, and an elongated fuel tube held in position in said housing by spaced apart joints and including an undulating tube surface along at least a portion of its length between said joints, said undulating tube surface being in contact with another surface disposed in said housing at one or more locations of said undulating tube surface.