Throttle Element Inlet Geometry for Uniform Flow and Lower Cavitation

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Solution Overview

Problem

Existing throttling elements in process plants suffer from cavitation and wear due to non-uniform fluid flow patterns, leading to inefficiencies and reduced service life.

Innovation Solution

The throttling element design features frustoconical inlet regions with a cone angle of 15° to 75°, followed by spherical regions, ensuring uniform fluid distribution and minimizing turbulence through seamless transitions, along with channel sections that increase in cross-section to manage fluid velocity.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If conventional throttle channels with straight or simple curved paths are used, then the structure is simple and easy to manufacture, but non-uniform fluid flow patterns occur leading to cavitation and wear

Engineering Contradiction:
Improveservice life of throttling elementVSAvoidgeometry of throttle channels
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent applies spherical curvature to the inlet region of the throttle channel, creating a spherical inlet opening instead of a conventional straight or simple curved path. This spherical geometry guides the fluid flow in a curved trajectory, ensuring uniform distribution across the channel cross-section and preventing cavitation and wear, thereby extending the service life of the throttling element.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The patent changes the geometric parameters of the throttle channel inlet by introducing a spherical shape with a specific radius (R1) and defining a cone angle (α) between the frustoconical and spherical regions. These parameter optimizations create ideal flow conditions that eliminate harmful flow patterns while maintaining manufacturing feasibility.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If the entire channel cross-section is utilized for flow, then flow distribution becomes uniform reducing cavitation and wear, but complex inlet geometry is required to achieve seamless transitions

Engineering Contradiction:
Improveuniformity of flow distributionVSAvoidmanufacturing of inlet geometry
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The spherical inlet opening with radius R1 provides a smooth, continuous curved surface that seamlessly transitions from the frustoconical region. This spherical geometry naturally guides fluid particles along curved paths, ensuring uniform flow distribution across the entire channel cross-section without creating dead zones or turbulence, while remaining manufacturable through standard machining or additive processes.

Inventive Principle:
Principle #14Spheroidality (Curvature)

Solution Approach 2:

The patent applies different geometric characteristics to different regions of the inlet: a frustoconical section with angle α for initial flow direction control, followed by a spherical section with radius R1 for uniform distribution. This local differentiation of geometric quality optimizes flow patterns in each zone while maintaining overall manufacturability.

Inventive Principle:
Principle #3Local quality

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

This design reduces cavitation and wear by optimizing fluid flow, utilizing nearly the entire channel cross-section and extending the service life of the throttling element.

Implementation Method 1

the frustoconical inlet region acts as a centering mechanism, improving the flow of the process fluid into the inlet openings

Methodology Applied
Scientific EffectFlow centering mechanism:

Implementation Method 2

the subsequent spherical region ensures a uniform distribution of the process fluid before it enters the subsequent channel sections of the throttle channels

Methodology Applied
Scientific EffectFlow distribution:

Implementation Method 3

rounded transition areas are formed between the frustoconical inlet areas and the subsequent spherical areas, according to the invention. A rounded transition area is to be understood in particular as a smooth or edgeless transition between the frustoconical inlet area and the spherical area

Methodology Applied
Scientific EffectTurbulence reduction:

Data Source

PatentEP4348087B1Throttle element for reducing the pressure of a process fluid
Publication Date: 2025.12.17 SAMSON AG
  • EP4348087B1 patent drawingFigure 1
  • EP4348087B1 patent drawingFigure 2~3
  • EP4348087B1 patent drawing

AI summary

The invention relates to a throttle element (100) for reducing the pressure of a process fluid, comprising a throttle body that has multiple throttle channels (104) through which the process fluid is to flow, wherein each throttle channel (104) has an upstream inlet opening (106), a channel section (108), and a downstream outlet opening (110) when viewed in the flow direction (S). The invention is characterized in that the inlet openings (106) are designed to have a truncated conical inlet region (106-1) which tapers in the flow direction (S) and a spherical region (106-2) adjoining said inlet region.