Vortex Disruption Devices for Trailer Drag Reduction

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Solution Overview

Problem

Existing devices fail to effectively disrupt the trailing vortex created by air flow around vehicles with non-tapered rear ends, leading to significant pressure drag and reduced vehicle efficiency, which increases transportation costs.

Innovation Solution

The use of vortex disruption devices positioned beyond the fluid dynamic laminar boundary layer, extending from the trailing edge of vehicles, dispersing airflow and preventing the formation of low-pressure vortices, with both fixed and mechanically actuated configurations available for installation on various vehicle types.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If vortex disruption devices are positioned beyond the boundary layer to prevent vortex formation, then drag is reduced and fuel efficiency is improved, but device complexity and installation requirements increase

Engineering Contradiction:
Improvefuel efficiencyVSAvoiddevice complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The vortex disruption device is divided into multiple independent elements (10) that can be individually positioned and adjusted. Each element consists of simple planar surfaces that can be separately secured to the trailer, allowing the system to achieve complex flow disruption patterns through simple modular components rather than a single complex structure.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The device transitions from two-dimensional surface-mounted vortex generators to three-dimensional structures that extend beyond the boundary layer. The planar surfaces are oriented at specific angles and positioned at various heights to create three-dimensional flow disruption patterns that effectively prevent vortex formation in the wake region.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

2Object-affected harmful factors

If vortex disruption devices extend well beyond the boundary layer, then vortex formation is effectively prevented, but the devices create additional structural requirements and installation complexity

Engineering Contradiction:
Improvevortex formationVSAvoidease of manufacture
Core Design Contradiction:
Object-affected harmful factorsVSEase of manufacture

Solution Approach 1:

The vortex disruption elements utilize thin planar surfaces that can be easily manufactured and installed. These flexible-looking structures (which may be rigid or flexible materials) extend beyond the boundary layer to disrupt vortex formation while maintaining simplicity in manufacturing and installation through their thin-film-like construction.

Inventive Principle:
Principle #30Flexible shells and thin films

Solution Approach 2:

The planar surfaces are oriented at specific angles and curved configurations to optimize flow disruption. The surfaces may be flat or slightly curved to achieve the desired aerodynamic effect while maintaining manufacturing simplicity, avoiding complex three-dimensional curved surfaces that would be difficult to manufacture.

Inventive Principle:
Principle #14Spheroidality (Curvature)

3Object-affected harmful factors

If multiple vortex disruption devices are positioned in spaced relation, then airflow convergence is effectively prevented, but device complexity and installation time increase

Engineering Contradiction:
Improveairflow convergenceVSAvoidinstallation time
Core Design Contradiction:
Object-affected harmful factorsVSLoss of time

Solution Approach 1:

The system uses multiple segmented vortex disruption elements positioned in spaced relation along the trailer. Each element is independently installable and positioned to disrupt airflow convergence at different locations, preventing vortex formation through distributed rather than centralized intervention.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The vortex disruption elements are pre-positioned and pre-oriented at specific angles and spacings to optimally disrupt airflow convergence before vortex formation can occur. This preliminary configuration of multiple elements ensures effective drag reduction while allowing for standardized installation procedures that reduce on-site installation time.

Inventive Principle:
Principle #10Preliminary action

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 solution significantly reduces drag and enhances fuel efficiency by inhibiting the formation of low-pressure vortices behind vehicles, thereby minimizing transportation costs and improving vehicle performance.

Implementation Method 1

The vortex disruption devices are disposed in adjacently spaced relation and extend away from the vehicle or trailer surface well beyond the fluid dynamic laminar boundary layer formed as the vehicle passes through the air. Once installed the vortex disruption devices disperse the air flowing over the disrupter while allowing air to flow normally through the spaces between the devices. The vortex disruption devices thereby inhibit the natural convergence of airflow and prevent the formation of a low-pressure vortex beyond the trailing edge of the vehicle.

Methodology Applied
Scientific EffectVortex disruption: Turbulence

Data Source

PatentUS10843746B1Vortex drag disruption apparatus
Publication Date: 2020.11.24 STINCHCOMB JOSEPH
  • US10843746B1 patent drawing
  • US10843746B1 patent drawing
  • US10843746B1 patent drawing

AI summary

Vortex disruption apparatus are permanently or removably installed or attached to cargo and passenger vans, busses, box-trucks, tractor-trailer combinations, or any other vehicle to increase transportation efficiency by reducing drag by minimizing the formation of trailing end vortex flow. A plurality of vortex disruption devices is disposed in proximity to the trailing end of a cargo trailer and in adjacently spaced relation whereby they extend away from the vehicle or trailer surface well beyond the fluid dynamic laminar boundary layer formed as the vehicle passes through the air. Once installed the vortex disruption devices disperse the air flowing over the disrupter while allowing air to flow normally through the spaces between the devices. The vortex disruption devices thereby inhibit the natural convergence of airflow and prevent the formation of a low-pressure vortex beyond the trailing edge of the vehicle.