Evacuation Slide Cover Release Using Magnetostriction Actuators

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Existing evacuation slide release systems in aircraft rely on gas delivery manifolds which need replacement due to the transition to electrically operated aircraft systems, necessitating a new mechanism for blowout panel and soft cover release.

Innovation Solution

Utilizing magnetostriction components, such as Terfenol-D, to actuate the release of blowout panels and soft covers through magnetic field-induced shape changes, replacing the gas-based delivery manifold system with an electrically actuated system.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If compressed gas systems are used for blowout panel and soft cover release, then reliable deployment is achieved, but the system complexity and safety risks increase due to high-pressure gas storage requirements

Engineering Contradiction:
Improvedeployment reliabilityVSAvoidsystem complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces the compressed gas mechanical system with an electrical system using magnetostriction actuators. These actuators use magnetic fields to directly actuate the release mechanisms for the blowout panel and soft cover, eliminating the need for high-pressure gas storage tanks, valves, and delivery manifolds while maintaining reliable deployment functionality

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

Solution Approach 2:

The patent eliminates the pneumatic system entirely by substituting it with electrical magnetostriction actuators that convert electrical energy directly into mechanical motion through magnetic field-induced dimensional changes in magnetostriction materials, thereby removing all gas-related components and associated safety risks

Inventive Principle:
Principle #29Pneumatics and hydraulics

2Speed

If compressed gas delivery manifolds are used, then rapid evacuation slide deployment is achieved, but safety hazards increase due to high-pressure gas storage in the aircraft

Engineering Contradiction:
Improveevacuation slide deployment speedVSAvoidsafety hazards
Core Design Contradiction:
SpeedVSObject-affected harmful factors

Solution Approach 1:

The patent substitutes the high-pressure gas system with electrical magnetostriction actuators that provide rapid, controlled actuation of release mechanisms without storing hazardous energy in the form of compressed gas, thereby eliminating safety hazards associated with gas storage and delivery systems while maintaining rapid deployment capability

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

Solution Approach 2:

The patent extracts and removes the compressed gas storage and delivery system from the evacuation slide deployment mechanism, retaining only the essential release functionality through electrical actuation, thereby eliminating the harmful factor of high-pressure gas storage while preserving the rapid deployment function

Inventive Principle:
Principle #2Taking out (Extraction)

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

Enables reliable and efficient deployment of evacuation slides without compressed gas, ensuring rapid passenger evacuation in emergency situations by using a single power source for both blowout panel and soft cover release.

Implementation Method 1

send a first signal to the first actuator that magnetizes a first magnetostriction material within the first actuator, thereby releasing the blowout panel

Methodology Applied
Scientific EffectMagnetostriction: Magnetostriction

Implementation Method 2

the solenoid generates a magnetic field in response to receiving the first signal and where the magnetic field magnetizes the first magnetostriction material

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Implementation Method 3

the compression spring provides a compression spring force that holds the spindle against the first magnetostriction material

Methodology Applied
Scientific EffectElasticity: Elasticity

Data Source

PatentEP4335751B1Off-wing evacuation packboard cover panel and soft cover release utilizing magnetostriction
Publication Date: 2026.05.06 GOODRICH CORP
  • EP4335751B1 patent drawingFigure 1
  • EP4335751B1 patent drawingFigure 2
  • EP4335751B1 patent drawingFigure 3

AI summary

A system for releasing a blowout panel (110) and softcover (206) release of an evacuation slide in an aircraft is provided. The system includes a first actuator (202), a second actuator (212); and a controller. The controller is configured to receive an indication that an evacuation event has begun; and, responsive to receiving the indication of the evacuation event beginning: send a first signal to the first actuator that magnetizes a first magnetostriction material within the first actuator, thereby releasing the blowout panel of a packboard compartment (204) in which the evacuation slide is present; and send a second signal to the second actuator that magnetizes a second magnetostriction material within the second actuator, thereby releasing a key-loop of lacing (210) associated with the softcover in which the evacuation slide is present in the packboard compartment.