Thrust Reverser Closure Initiator for Anti-Jamming Operation

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Solution Overview

Problem

Conventional thrust reversers experience jamming and chattering phenomena due to aerodynamic stresses, especially when actuators fail or deteriorate, leading to the external movable structure becoming stuck in the open position and causing irreversible friction and deformation.

Innovation Solution

Incorporation of a priming element separate from the actuator to exert a transient initiating force during the closing stroke, which realigns and reduces friction, combined with a mechanism to dampen and guide the movable structure, reducing the need for larger actuators and overall mass.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If actuators are sized to overcome jamming and chattering forces, then the external movable structure can be closed reliably, but the actuator dimensions and mass increase

Engineering Contradiction:
Improveclosing reliabilityVSAvoidactuator mass
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

A priming element is introduced that acts before the main actuator to initiate the closing stroke. The priming element exerts a preliminary force to start the movement of the external movable structure from the open position, overcoming the initial jamming and chattering forces without requiring the main actuator to be oversized for this purpose.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The closing force generation is divided into two segments: a priming element that provides the initial force to start closing, and a main actuator that completes the closing stroke. This segmentation allows each component to be optimized for its specific function, reducing the overall mass requirement compared to a single large actuator.

Inventive Principle:
Principle #1Segmentation

2Object-affected harmful factors

If the external movable structure is allowed to pivot under aerodynamic stresses, then the structure can accommodate flow forces, but friction and deformation increase making closure difficult

Engineering Contradiction:
Improveaerodynamic stress toleranceVSAvoidclosure ease
Core Design Contradiction:
Object-affected harmful factorsVSEase of operation

Solution Approach 1:

The priming element applies a force in the opposite direction of the aerodynamic-induced tilt before the closing stroke begins. This preliminary anti-action counteracts the tilting moment that causes jamming and chattering, realigning the external movable structure with the guide rails and reducing friction before the main closing action.

Inventive Principle:
Principle #9Preliminary anti-action

3Strength

If guide rail coatings are worn or friction increases, then the structure can withstand operational stresses, but the external movable structure becomes stuck and chattering occurs

Engineering Contradiction:
Improvestructural durabilityVSAvoidclosure reliability
Core Design Contradiction:
StrengthVSReliability

Solution Approach 1:

The priming element performs a preliminary action to overcome increased friction forces before the main actuator operates. By applying initial force to start the closing stroke, the priming element ensures that even with worn guide rail coatings, the external movable structure can begin moving without getting stuck or chattering.

Inventive Principle:
Principle #10Preliminary action

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 solution effectively mitigates jamming and chattering, facilitates easier closure of the external structure, and reduces the dimensions and mass of the thrust reverser components.

Implementation Method 1

These stresses can thus lead to the external moving structure jamming in the open position and a chattering phenomenon during the initiation of the closing stroke

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 2

When the external moving structure is in the open position, it is exposed to aerodynamic stresses that can generate a tilting moment tending to cause it to rotate

Methodology Applied
Scientific EffectAerodynamic stress: Drag

Data Source

PatentEP4010576B1Thrust reverser comprising at least one initiator to initiate the closing of a mobile external structure of this reverser
Publication Date: 2025.12.31 SAFRAN NACELLES
  • EP4010576B1 patent drawingFigure 1~2
  • EP4010576B1 patent drawingFigure 3~4
  • EP4010576B1 patent drawingFigure 5~6

AI summary

The invention relates to a thrust reverser (12) for an aircraft propulsion unit, this reverser (12) comprising a fixed structure (24) and a mobile external structure (16) able to move between a closed position and an open position so as to cause the reverser (12) to transition respectively between a direct-jet configuration and a reverse-jet configuration. The reverser (12) comprises, on the one hand, one or more actuators configured to move the mobile external structure (16) between the closed position and the open position. The reverser (12) comprises, on the other hand, at least one initiator (23) configured to apply to the mobile external structure (16) a force that initiates a closure travel in which the mobile external structure (16) is moved from the open position towards the closed position.