Electromechanical Actuator SAW Sensor Integration

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Solution Overview

Problem

Existing electromechanical actuators (EMAs) used in safety-critical applications, such as aircraft flight control surfaces, require additional sensors for performance monitoring, which increases the overall size and weight of the actuators.

Innovation Solution

Integration of a surface acoustic wave (SAW) sensor and an inductive position sensor within the actuation element of the EMA, utilizing a pair of interface components to transmit signals and determine the position of the movable body portion relative to the stationary body portion, thereby reducing the need for external sensors.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Measurement precision

If output position sensors are attached to EMA inside a gearbox, then the position of rotary EMAs can be monitored, but the overall size of the EMAs increases and thus the weight increases

Engineering Contradiction:
Improveposition monitoringVSAvoidEMA weight
Core Design Contradiction:
Measurement precisionVSWeight of moving object

Solution Approach 1:

The patent combines the position sensor functionality with the existing interface components (antennas) of the SAW sensor system. The first interface component (stationary antenna) and second interface component (movable antenna) serve dual purposes: transmitting signals to/from the SAW sensor and functioning as an inductive position sensor. This merging eliminates the need for separate position sensors, thereby avoiding additional weight while maintaining position monitoring capability.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The interface components of the SAW sensor system are designed to perform multiple functions. Besides their primary role in signal transmission for the SAW sensor, they also function as an inductive position sensor to determine the position of the movable body portion. This multi-functionality reduces the overall component count and weight while achieving both sensor operation monitoring and position monitoring.

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

2Reliability

If additional sensors are integrated for performance monitoring, then safety and reliability are improved, but the device complexity and size increase

Engineering Contradiction:
Improvesafety critical monitoringVSAvoidsensor integration complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent merges the position sensing function with the existing SAW sensor interface components, creating a multi-functional system. The first and second interface components serve both as communication interfaces for the SAW sensor and as an inductive position sensor, thereby reducing device complexity while maintaining comprehensive monitoring capabilities for safety-critical applications.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The interface components are designed with universal functionality to perform both signal transmission for operational monitoring and position determination. This multi-functionality approach allows the system to achieve enhanced reliability through multiple monitoring capabilities without proportionally increasing device complexity.

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

This solution allows for the reduction of the EMA's weight and size while maintaining performance monitoring capabilities, thereby addressing the challenge of reducing aircraft emissions and improving safety without compromising reliability.

Implementation Method 1

a surface acoustic wave, SAW, sensor disposed on the actuation element

Methodology Applied
Scientific EffectSurface acoustic wave: Surface Acoustic Wave

Implementation Method 2

the first interface component and the second interface component define an inductive position sensor, such that the first interface component produces a signal suitable for determination of the position of the second interface component

Methodology Applied
Scientific EffectElectromagnetic induction: Electromagnetic Induction

Data Source

PatentEP4542176A1Electromechanical actuator with operational sensors
Publication Date: 2025.04.23 GOODRICH ACTUATION SYST
  • EP4542176A1 patent drawingFigure 1
  • EP4542176A1 patent drawingFigure 2
  • EP4542176A1 patent drawingFigure 3

AI summary

An electromechanical actuator, EMA, (1) is provided comprising: a stationary body portion (11); a movable body portion (13) configured to move relative to the stationary body portion (11); an actuation element (19) connecting the stationary body portion (11) and the movable body portion (13) and configured to actuate the movable body portion (13) relative to the stationary body portion (11); a surface acoustic wave, SAW, sensor (4) disposed on the actuation element (19); a first interface component (2) disposed on the stationary body portion (11) at an interface (17) between the stationary body portion (11) and the movable body portion (13); and a second interface component (3) disposed on the movable body portion (13) at the interface (17) between the stationary body portion (11) and the movable body portion (13); wherein the second interface component (3) is configured to transmit signals between the SAW sensor (4) and the first interface component (2); and wherein the first interface component (2) and the second interface component (3) define an inductive position sensor (6), such that the first interface component (2) produces a signal suitable for determination of the position of the second interface component (3).