Pivotable Flow Flap for Rail Vehicle Aerodynamic Optimization

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Solution Overview

Problem

Rail vehicles face challenges in achieving optimal aerodynamics at higher speeds due to structural constraints, requiring different shapes for the front and rear but needing identical designs for both directions of travel, and existing aerodynamic aids are either ineffective or impractical to implement.

Innovation Solution

A pivotable flow flap aerodynamic aid that adjusts its position based on air flow direction, forming a stall edge in one direction and minimizing air disruption in the opposite direction, without manual intervention or power drive, using a specific angle and contact surface design to optimize airflow.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Loss of energy

If a spoiler is attached at the end of the train to reduce wake vortices, then aerodynamic performance is improved, but the device becomes complex and requires manual or power-assisted alignment which increases cost and operational complexity

Engineering Contradiction:
Improveenergy consumptionVSAvoidalignment complexity
Core Design Contradiction:
Loss of energyVSDevice complexity

Solution Approach 1:

The flow flap is designed to automatically align itself with the oncoming air flow through aerodynamic forces. The pressure differential created by the air flow itself drives the flap to the correct angle, eliminating the need for external alignment systems, motors, or manual intervention. This self-aligning mechanism resolves the contradiction by maintaining optimal aerodynamic performance without adding complex alignment infrastructure.

Inventive Principle:
Principle #25Self-service

Solution Approach 2:

The invention changes the state of the flow flap from a fixed or motor-controlled position to a dynamically adjusted position based on air flow conditions. The flap's angle of attack automatically varies with the oncoming air flow, allowing the system to adapt to different operating conditions without requiring complex control systems. This parameter change enables the device to maintain optimal aerodynamic properties across varying speeds and conditions.

Inventive Principle:
Principle #35Parameter changes

2Ease of manufacture

If identical aerodynamic shapes are used for both front and rear of the train, then the design is simplified and works for both directions, but the aerodynamic performance is suboptimal compared to direction-specific shapes

Engineering Contradiction:
Improvedesign simplicityVSAvoidaerodynamic resistance
Core Design Contradiction:
Ease of manufactureVSLoss of energy

Solution Approach 1:

The invention introduces a dynamic element (the pivotable flow flap) to an otherwise static aerodynamic design. The flow flap can pivot between different angular positions to adapt to the direction of oncoming air flow. This dynamic adjustment allows the same physical structure to provide optimal aerodynamic properties for both forward and reverse directions, resolving the contradiction between design simplicity and aerodynamic performance.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

While the overall train structure maintains symmetric identification (same shape for bow and stern), the flow flap introduces asymmetric functionality through its directional orientation. The flap's angle of attack is specifically optimized for the direction of oncoming air flow, creating asymmetric aerodynamic effects within the symmetric structure. This allows the train to achieve direction-specific aerodynamic optimization without changing the overall vehicle design.

Inventive Principle:
Principle #4Asymmetry

3Object-generated harmful factors

If the flow flap is positioned to form a stall edge for optimal aerodynamics in one direction, then wake vortex formation is reduced, but the air flow is disrupted in the opposite direction

Engineering Contradiction:
Improvewake vortex formationVSAvoidair flow disruption
Core Design Contradiction:
Object-generated harmful factorsVSObject-affected harmful factors

Solution Approach 1:

The flow flap is designed to dynamically adjust its position based on the direction of oncoming air flow. When the train moves in a particular direction, the flap pivots to form a stall edge that reduces wake vortices. When the train reverses direction, the flap automatically pivots to a position that minimizes air flow disruption. This dynamic response allows the system to optimize aerodynamic properties for each direction without compromising performance in the opposite direction.

Inventive Principle:
Principle #15Dynamics

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 allows for differential aerodynamic effects without manual operation or power assistance, reducing wake vortex formation and energy consumption, and can be retrofitted onto existing rail vehicles without impacting their appearance or requiring additional infrastructure.

Implementation Method 1

the movement between the end positions being able to be brought about exclusively by the force of the inflowing air

Methodology Applied
Scientific EffectAerodynamic force: Drag

Implementation Method 2

the flow flap is aligned in its first end position in such a way that it forms a flow separation edge and thus reduces the energy-consuming wake vortex formation

Methodology Applied
Scientific EffectFlow separation: Flow Separation

Data Source

PatentEP3247607B1Aerodynamic auxiliary means for a rail vehicle
Publication Date: 2021.06.23 SIEMENS MOBILITY AUSTRIA GMBH
  • EP3247607B1 patent drawingFigure 1~2
  • EP3247607B1 patent drawingFigure 3

AI summary

The invention relates to an aerodynamic auxiliary means (1) for a rail vehicle (2), comprising at least one flow flap (3, 3a) which is pivotably arranged about an axis of rotation (4) between two end positions, wherein the movement between the end positions can be brought about by the action of force of the inflowing air, said flow flap (3, 3a) forming a flow separation edge in a first end position and said flow flap (3, 3a) leaving the inflowing air substantially unaffected in a second end position.