Thrust Reverser Actuator Synchronization via Real-Time Position Feedback

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Solution Overview

Problem

Existing thrust reverser systems face challenges in synchronizing multiple electric actuators, leading to potential desynchronization, jamming, deformation, or breakage of the movable cowl during position changes between 'direct jet' and 'reverse jet' positions, which can increase braking distance and risk of mechanical failure.

Innovation Solution

A method that measures real-time position differences between adjacent actuators and adjusts their speed profiles to maintain synchronization, including acceleration or deceleration of lagging or leading actuators, and step-by-step control of healthy actuators to prevent jamming and deformation, with the option to stop the system if deviations exceed safe thresholds.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If multiple electric actuators are used to move the cowl, then the productivity and reliability of the thrust reverser system is improved, but the risk of actuator desynchronization increases, leading to potential jamming or deformation of the movable cowl

Engineering Contradiction:
Improvereliability of thrust reverser systemVSAvoidactuator desynchronization and jamming risk
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent implements a feedback mechanism where the control unit continuously monitors the position of each actuator and compares it with reference positions. When position deviations are detected, the control unit automatically adjusts the speed profile of individual actuators to maintain synchronization, thereby preventing jamming and deformation while preserving system reliability

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The patent applies dynamic speed profile adjustment to actuators based on real-time position feedback. The control unit modifies acceleration and deceleration parameters dynamically during operation, allowing actuators to adapt their motion characteristics to maintain synchronization and avoid harmful effects like jamming

Inventive Principle:
Principle #15Dynamics

2Manufacturing precision

If the speed profile of actuators is adjusted in real-time to maintain synchronization, then the position precision and operational safety are improved, but the control system complexity increases

Engineering Contradiction:
Improveactuator position synchronization precisionVSAvoidcontrol system complexity
Core Design Contradiction:
Manufacturing precisionVSDevice complexity

Solution Approach 1:

The patent changes operational parameters (speed profile, acceleration, deceleration) of actuators based on detected position deviations. The control unit adjusts these parameters dynamically to maintain synchronization precision while managing control complexity through automated feedback-based parameter modification

Inventive Principle:
Principle #35Parameter changes

3Manufacturing precision

If position deviations between actuators are corrected by accelerating lagging actuators, then the synchronization is improved, but the mechanical stress and energy consumption increase

Engineering Contradiction:
Improveactuator synchronizationVSAvoidmechanical stress on actuators
Core Design Contradiction:
Manufacturing precisionVSStress or pressure

Solution Approach 1:

The patent dynamically adjusts the speed profile of actuators based on real-time position feedback. When position deviations are detected, the control unit modifies acceleration and deceleration parameters to maintain synchronization while attempting to minimize mechanical stress through controlled, gradual adjustments rather than abrupt changes

Inventive Principle:
Principle #15Dynamics

Data Source

PatentEP2304211B1Method for synchronizing the actuators of a movable thrust reverser cowl
Publication Date: 2017.04.12 SAFRAN NACELLES
  • EP2304211B1 patent drawing
  • EP2304211B1 patent drawing
  • EP2304211B1 patent drawing

AI summary

The invention relates to a method for controlling a plurality of actuators (9a, 9b, 9c) for a movable thrust reverser cowl (1), characterized remarkable in that the position deviation between adjacent actuators is measured in real time, and in that the speed profile of the actuator or actuators in question is adjusted by a position deviation exceeding a predetermined threshold.