Rear Spoiler with Dual Adjustable Profiles for Downforce Management

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Solution Overview

Problem

Current rear spoilers with adjustable aerodynamic profiles for high-performance road vehicles face inefficiencies in maximizing downforce while minimizing running resistance, often requiring complex and heavy actuation systems.

Innovation Solution

A rear spoiler design featuring two adjustable aerodynamic profiles with a mechanical transmission system that allows for simultaneous rotation of the profiles via a single actuator, optimizing the angle of attack to achieve high downforce at lower speeds and low resistance at higher speeds, with a compact and lightweight actuation system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Force

If a rear spoiler with adjustable aerodynamic profiles is provided to increase downforce, then the downforce is improved, but the running resistance increases

Engineering Contradiction:
ImprovedownforceVSAvoidrunning resistance
Core Design Contradiction:
ForceVSObject-generated harmful factors

Solution Approach 1:

The aerodynamic profiles are made dynamically adjustable through a mechanical transmission system that allows real-time modification of the profile angles. This enables the rear spoiler to adapt its aerodynamic characteristics based on driving conditions, optimizing the balance between downforce generation and running resistance minimization

Inventive Principle:
Principle #15Dynamics

2Adaptability or versatility

If complex actuation systems are used to adjust aerodynamic profiles, then the aerodynamic efficiency is improved, but the device complexity and weight increase

Engineering Contradiction:
Improveaerodynamic efficiencyVSAvoidactuation system complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

Multiple adjustment functions for different aerodynamic profiles are merged into a single mechanical transmission system. This integrated approach allows simultaneous adjustment of multiple profiles through one actuator, reducing the number of separate actuation mechanisms while maintaining high aerodynamic adaptability and efficiency

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The mechanical transmission system is designed with multi-functionality to perform multiple adjustment tasks. A single transmission mechanism can adjust different aerodynamic profiles at different positions, replacing what would traditionally require multiple separate actuation systems, thereby reducing overall device complexity and weight

Inventive Principle:
Principle #6Universality (Multi-functionality)

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 design achieves high aerodynamic efficiency with a simple, fast, and lightweight actuation system that maintains performance by neutralizing twisting torques, reducing additional aerodynamic resistance and enhancing response times.

Implementation Method 1

which, being impinged by the air, generate the desired lift

Methodology Applied
Scientific EffectAerodynamic lift: Aerofoil

Implementation Method 2

a mechanical transmission system that allows for simultaneous rotation of the profiles via a single actuator

Methodology Applied
Scientific EffectMechanical transmission: Gear

Data Source

PatentEP2631160B1A rear spoiler with adjustable aerodynamic profiles for a high performance road vehicle
Publication Date: 2015.11.25 FERRARI SPA
  • EP2631160B1 patent drawingFigure 1
  • EP2631160B1 patent drawingFigure 2
  • EP2631160B1 patent drawingFigure 3

AI summary

A rear spoiler (4) with adjustable aerodynamic profiles (5, 6) for a high performance road vehicle (1); the rear spoiler (4) has: at least one fin-shaped support (7); a first adjustable aerodynamic profile (5) that is mounted onto the fin-shaped support (7) and that rotates around a first rotational axis (11); and a second adjustable aerodynamic profile (6) that is mounted onto the fin-shaped support (7) at a different height than the first aerodynamic profile (5) and that rotates around a second rotational axis (12), that is parallel to the first rotational axis (11), and in an opposite direction with respect to the rotation of the first aerodynamic profile (5); wherein the first rotational axis (11) is located close to a trailing edge of the first aerodynamic profile (5) and the second rotational axis (12) is located close to a leading edge of the second aerodynamic profile (6).