Turbine Fuel Injector Polygonal Nozzle Additive Manufacturing

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing fuel injectors for turbine engines face challenges in reducing manufacturing costs, assembly time, and achieving precision fuel injection.

Innovation Solution

A fuel injector assembly with a nozzle passage featuring a non-annular, non-circular cross-sectional geometry, such as a square or diamond shape, and a tapered design to minimize surface finish variations, allowing for additive manufacturing with reduced dimensional and geometric deviations, thereby enhancing fuel metering precision.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Ease of manufacture

If traditional fuel injector designs are used, then manufacturing and assembly are simpler, but manufacturing costs are higher and assembly time is longer

Engineering Contradiction:
Improvemanufacturing costVSAvoidnozzle passage geometry
Core Design Contradiction:
Ease of manufactureVSDevice complexity

Solution Approach 1:

The fuel nozzle and fuel injector body are merged into a single integrated component manufactured via additive manufacturing. This eliminates separate machining operations and assembly steps, reducing manufacturing cost and assembly time despite the complex polygonal internal geometry of the nozzle passage.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The nozzle passage cross-sectional geometry is changed from traditional circular or annular shapes to polygonal shapes (triangle, square, rectangle). This parameter change enables additive manufacturing advantages while maintaining functional performance, resolving the contradiction between manufacturing ease and geometric complexity.

Inventive Principle:
Principle #35Parameter changes

2Manufacturing precision

If conventional nozzle passages are used, then manufacturing is easier, but dimensional and geometric deviations are higher

Engineering Contradiction:
Improvedimensional deviationVSAvoidmanufacturing process
Core Design Contradiction:
Manufacturing precisionVSEase of manufacture

Solution Approach 1:

The cross-sectional geometry parameter is changed to polygonal shapes, which inherently reduce surface finish variations and dimensional deviations compared to curved geometries. This parameter change improves manufacturing precision while the additive manufacturing process maintains ease of production.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The invention deliberately avoids curved geometries in favor of polygonal shapes with straight edges and flat surfaces. This inverse application of the curvature principle reduces surface finish variations and dimensional deviations in additive manufactured components, improving manufacturing precision.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Measurement precision

If precise fuel injection is achieved through traditional methods, then fuel metering is accurate, but manufacturing costs and assembly time increase

Engineering Contradiction:
Improvefuel metering precisionVSAvoidassembly time
Core Design Contradiction:
Measurement precisionVSProductivity

Solution Approach 1:

Multiple components (fuel nozzle, injector body, passage) are merged into a single additive manufactured part. This integration achieves precise fuel metering through the polished internal surfaces and accurate geometries of additive manufacturing, while eliminating multiple assembly steps to reduce assembly time.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The nozzle passage internal surfaces are polished and finished during the additive manufacturing process itself, before final assembly. This preliminary action ensures precise fuel metering characteristics are built-in during manufacturing, eliminating the need for post-assembly adjustments or additional machining operations.

Inventive Principle:
Principle #10Preliminary action

Data Source

PatentEP4067747B1Turbine engine fuel injector with polygonal nozzle passage
Publication Date: 2025.06.25 RTX CORP
  • EP4067747B1 patent drawingFigure 1~2
  • EP4067747B1 patent drawingFigure 3
  • EP4067747B1 patent drawingFigure 4~5

AI summary

An apparatus (20) is provided for a turbine engine. This turbine engine apparatus (20) includes a fuel nozzle (26). The fuel nozzle (26) includes a nozzle passage (42) and a nozzle orifice (52). The nozzle passage (42) extends longitudinally along a centerline (50) within the fuel nozzle (26) to the nozzle orifice (52). The nozzle passage (42) has a solid polygonal cross-sectional geometry at the nozzle orifice (52).