Rifled Venturi for Combustor Dynamics Mitigation
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Solution Overview
Problem
Conventional rich-burn combustors with radial-radial swirlers and venturis face issues with fuel adherence and coherent liquid sheet breakup, leading to high-frequency and low-frequency spectral content in the flow, which can couple with combustion chamber modes, affecting atomization and mixing efficiency.
Innovation Solution
The introduction of rifling-type grooves on the inner surface of the venturi, varying in width, depth, and angle, to break up the coherent liquid sheet and reduce spectral content, improving fuel-air mixing and atomization.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Productivity
If a conventional venturi is used in a rich-burn combustor, then the fuel/air mixture can be delivered to the combustor, but fuel adheres to the inner surface of the venturi forming a coherent liquid sheet that reduces mixing efficiency and creates harmful spectral content
Solution Approach 1:
The patent applies segmentation by introducing multiple grooves into the venturi inner surface that divide the coherent liquid sheet into smaller segments. These grooves create multiple fuel streams instead of a single continuous sheet, enhancing mixing efficiency and reducing harmful spectral content through increased surface area and disrupted flow patterns.
Solution Approach 2:
The patent introduces grooves that add a third dimension to the fuel flow by creating depth variations in the venturi surface. This dimensional change transforms the two-dimensional liquid sheet into a three-dimensional structured flow with multiple channels, improving atomization and mixing while reducing coherent spectral content.
2Manufacturing precision
If the venturi inner surface is smooth, then fuel flow is straightforward, but the coherent liquid sheet reduces atomization quality and creates flow dynamics issues
Solution Approach 1:
The patent applies local quality by modifying only specific portions of the venturi inner surface with grooves while leaving other areas relatively smooth. This localized modification creates the necessary flow disruption for improved atomization without completely altering the overall flow path, maintaining manufacturing feasibility while enhancing performance.
Solution Approach 2:
The grooves introduce curved surfaces and varying radii into the venturi flow path, replacing the simple cylindrical geometry. This curvature variation disrupts the coherent liquid sheet formation and improves atomization quality by creating more complex flow patterns that enhance fuel-air mixing.
3Productivity
If grooves are added to the venturi inner surface, then spectral content is reduced and mixing is improved, but device complexity increases
Solution Approach 1:
The grooves are designed to be self-formed through the natural flow of fuel and air through the venturi. The geometry and positioning of the grooves allow the fluid dynamics themselves to create the desired flow patterns without requiring additional active control mechanisms or complex external systems.
Solution Approach 2:
The patent modifies geometric parameters of the venturi by introducing grooves with specific dimensions, depths, and spacing. These parameter changes are optimized to achieve the desired spectral content reduction and mixing improvement while maintaining manufacturing feasibility and avoiding excessive complexity.
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 grooves effectively reduce the flow's low-frequency spectral content and high-frequency spectral levels, enhancing the breakup of the liquid sheet and improving the mixing process within the combustor.
Implementation Method 1
The internal surface of the annular wall includes a plurality of grooves in the internal surface of the annular wall, the plurality of grooves extending in the longitudinal direction along the internal surface of the annular wall
Implementation Method 2
break up the coherent liquid sheet and reduce spectral content, improving fuel-air mixing and atomization
Implementation Method 3
an internal diameter of the forward end of the annular wall is larger than an internal diameter of a middle portion of the annular wall between the forward end of the annular wall and the aft end of the annular wall, and the internal diameter of the middle portion of the annular wall is smaller than an internal diameter of the aft end of the annular wall
Implementation Method 4
a forward oxidizer inlet swirler including a plurality of swirl vanes, the forward oxidizer inlet swirler including a fuel/oxidizer inlet arranged radially inward of the plurality of swirl vanes
Data Source
AI summary
A venturi for a swirler assembly of a combustor for a gas turbine engine. The venturi has an annular wall having internal diameter of a forward end of the annular wall that is larger than an internal diameter of a middle portion of the annular wall, which is smaller than an internal diameter of an aft end of the annular wall. The internal surface of the annular wall has a plurality of grooves extending in a longitudinal direction from the forward end of the annular wall to the aft end of the annular wall. The plurality of grooves are angled with respect to a centerline axis of the annular wall and may be spiraled about the internal surface of the annular wall.


