Cooling Air Flap Actuation Using Shape-Memory Alloy

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Solution Overview

Problem

Existing devices for regulating hot air flow in vehicle compartments, such as engine compartments, are inefficient due to the need for complex electrohydraulic or electromechanical activating mechanisms, which are cumbersome and less reliable.

Innovation Solution

A device comprising a wing connectable to an air inflow opening, a drive module with a shape-memory alloy actuator that applies a thrust force when reaching a predetermined temperature, and a transmission apparatus to move the wing between closed and open positions, allowing for efficient heat exchange without the need for complex activating systems.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If electrohydraulic or electromechanical activating mechanisms are used to control wing movement, then the device can reliably regulate cooling air flow, but the device complexity and weight increase significantly

Engineering Contradiction:
Improvereliability of cooling air flow regulationVSAvoidcomplexity of activating mechanisms
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces complex electrohydraulic or electromechanical activating mechanisms with a purely mechanical thermal expansion-based actuation system. The bimetallic strip or thermal expansion element directly converts temperature changes into mechanical motion to open or close the cooling air flow passages, eliminating the need for motors, sensors, control circuits, and hydraulic systems while maintaining reliable automatic regulation.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The device uses the heat from the engine compartment itself to activate the cooling mechanism. The thermal expansion element is positioned to sense the ambient temperature and automatically opens the cooling passages when the temperature exceeds a predetermined threshold, without requiring external power sources or control systems. The system serves itself by using the problem (heat) as the solution (activation energy).

Inventive Principle:
Principle #25Self-service

2Reliability

If electrohydraulic or electromechanical activating mechanisms are used to control wing movement, then the device can reliably regulate cooling air flow, but the weight of the device increases

Engineering Contradiction:
Improvereliability of cooling air flow regulationVSAvoidweight of activating mechanisms
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The patent replaces heavy electrohydraulic or electromechanical components with lightweight thermal expansion elements. The actuation mechanism consists of simple mechanical elements such as bimetallic strips or thermal expansion bars that convert temperature changes directly into mechanical motion, reducing the weight by eliminating motors, batteries, control electronics, and hydraulic fluids.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The system uses the thermal energy already present in the engine compartment to drive the cooling mechanism, eliminating the need for external power sources and heavy actuating components. The thermal expansion element uses the ambient heat to directly open or close the cooling passages, making the system both lightweight and self-powered.

Inventive Principle:
Principle #25Self-service

3Manufacturing precision

If complex electromechanical systems are used to control cooling air flow, then precise temperature regulation can be achieved, but the device becomes structurally complicated and less manageable

Engineering Contradiction:
Improveprecision of temperature regulationVSAvoidstructural complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent achieves temperature regulation precision by carefully selecting and adjusting the physical parameters of the thermal expansion element, such as the composition and dimensions of the bimetallic strip or the coefficient of thermal expansion of the material. By optimizing these parameters, the device can open or close the cooling passages at specific temperature thresholds, providing precise temperature control through simple material properties rather than complex control systems.

Inventive Principle:
Principle #35Parameter changes

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 device provides a structurally simple, lightweight, and reliable means to regulate cooling air flow, effectively managing heat exchange by using temperature-responsive shape-memory alloy actuators to control wing movement, reducing the risk of overheating or excessive cooling without complex electromechanical systems.

Implementation Method 1

The drive module comprises at least one actuator made of a shape-memory alloy such that the thrust force is applied when the actuator reaches a predetermined temperature

Methodology Applied
Scientific EffectShape-memory alloy: Shape Memory Alloy

Data Source

PatentUS11890925B2Device for regulating a cooling air flow in a vehicle
Publication Date: 2024.02.06 AUTOMOBILI LAMBORGHINI SPA
  • US11890925B2 patent drawing
  • US11890925B2 patent drawing

AI summary

A device for controlling a hot air flow, for example in an engine compartment of a motor car, includes at least one wing connectable to an air inflow opening of an engine compartment of a motor car and movable between a position for closing and a position for opening the air inflow opening. A drive module is configured to apply a predetermined thrust force and a transmission apparatus is capable of transmitting the thrust force from the drive module to the wing to move the wing from the closed position to the open position and vice versa. The drive module includes at least one actuator made of a shape-memory alloy such that the thrust force is applied when the actuator reaches a predetermined temperature.