Aircraft Nacelle Thrust Reverser With Longitudinal Deflectors

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

The existing cascades in thrust reversal devices of aircraft nacelles have a non-negligible mass, which affects their efficiency and operational performance.

Innovation Solution

The introduction of longitudinal deflectors that are secant to transverse deflectors, oriented at an angle of less than 25° to the longitudinal direction, reduces the mass and enhances the efficiency of the orientation system by improving airflow diversion and orientation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If traditional cascades are used in the orientation system, then the structural strength and rigidity are sufficient, but the mass of the orientation system becomes non-negligible, reducing efficiency

Engineering Contradiction:
Improvemass of orientation systemVSAvoidstructural strength
Core Design Contradiction:
Weight of moving objectVSStrength

Solution Approach 1:

The orientation system is divided into multiple transverse deflectors and longitudinal deflectors that work together. Each deflector is a separate component that segments the airflow control function, allowing for reduced mass of individual components while maintaining overall structural effectiveness through their coordinated arrangement.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The deflectors are designed to be movable rather than fixed rigid structures. The transverse and longitudinal deflectors can adjust their positions dynamically to control airflow, replacing heavy static cascade structures with lighter dynamic components that achieve the same airflow orientation function with reduced mass.

Inventive Principle:
Principle #15Dynamics

2Weight of moving object

If the number of cascades is reduced to lower mass, then the mass of the orientation system decreases, but the efficiency of airflow orientation may be compromised

Engineering Contradiction:
Improvemass of orientation systemVSAvoidairflow orientation efficiency
Core Design Contradiction:
Weight of moving objectVSProductivity

Solution Approach 1:

The system transitions from traditional two-dimensional cascade arrangements to a three-dimensional configuration involving both transverse and longitudinal deflectors. This adds a longitudinal dimension to the airflow control mechanism, enabling more efficient airflow orientation with fewer components by utilizing spatial arrangement in multiple dimensions.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

Solution Approach 2:

The longitudinal deflectors act as intermediaries that work in conjunction with the transverse deflectors. These intermediary components guide and refine the airflow between the primary transverse deflectors, enhancing the overall orientation efficiency without requiring a proportional increase in the number of main deflectors.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 configuration reduces the mass of the orientation system while maintaining or improving the efficiency of airflow diversion and orientation, enhancing the thrust reversal device's performance.

Implementation Method 1

at least one longitudinal deflector which is secant to the transverse deflector(s) and which is orientated in a direction which forms an angle of less than 25° with the longitudinal direction

Methodology Applied
Scientific EffectFluid diversion and orientation:

Data Source

PatentUS12492668B2Aircraft nacelle provided with at least one thrust reversal device comprising at least one longitudinal deflector, aircraft comprising at least one propulsion assembly composed of such a nacelle
Publication Date: 2025.12.09 AIRBUS OPERATIONS (SAS)
  • US12492668B2 patent drawing
  • US12492668B2 patent drawing
  • US12492668B2 patent drawing

AI summary

An aircraft nacelle provided with a thrust reversal device which comprises at least one diversion system which is configured to divert, in the activated state, an airflow channeled in the nacelle toward a lateral opening of the nacelle, at least one orientation system comprising at least one transverse deflector which is configured to orientate the airflow diverted by the diversion system in the radial directions and toward the upstream end of the nacelle, and at least one longitudinal deflector which is secant to the transverse deflector(s) and which is oriented in a direction which forms an angle of less than 25° with the longitudinal direction.