Multi-Function Fixed Structure for Compact Cascade Thrust Reversers

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Solution Overview

Problem

Existing moving-grid thrust reversers in aircraft propulsion systems have a complex and voluminous architecture, which increases mass and cost, and lack a unified structure to integrate various functional components.

Innovation Solution

A fixed structure is introduced to connect the inverter to the turbomachine, incorporating a deflection edge and sharing multiple functions, such as guiding grids and deflecting reversing flow, thereby simplifying the architecture and reducing mass and cost.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If moving grid inverters are used to reduce nacelle length and mass, then the inverter mass and drag are reduced, but the architecture becomes relatively complex and voluminous due to separate fixed components on the turbomachine

Engineering Contradiction:
Improveinverter massVSAvoidinverter architecture
Core Design Contradiction:
Weight of moving objectVSDevice complexity

Solution Approach 1:

The patent combines multiple previously separate fixed components (front frame, guide elements, deflection edges, and stop elements) into a single integrated fixed structure. This merging eliminates the need for separate components mounted on the turbomachine, simplifying the overall architecture while maintaining the mass-reduction benefits of moving grids.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fixed structure is designed to perform multiple functions simultaneously: it provides structural support, guides grid movement, deflects reversing flow, and limits grid travel through integrated stop elements. This multi-functionality reduces the number of separate components needed, addressing the complexity issue while preserving mass savings.

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

2Reliability

If multiple separate fixed components are used for grid guidance and flow deflection, then specific functions are achieved, but the overall inverter volume and complexity increase

Engineering Contradiction:
Improvegrid guidance functionVSAvoidinverter volume
Core Design Contradiction:
ReliabilityVSVolume of stationary object

Solution Approach 1:

The guide elements and deflection edges are integrated into the fixed structure itself, eliminating separate components. The fixed structure's geometry provides both guidance surfaces and flow deflection surfaces, reducing overall inverter volume while maintaining reliable grid guidance and flow control functions.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The fixed structure serves multiple purposes: it guides grid movement through integrated guide elements, deflects reversing flow through built-in deflection edges, and provides structural support. This multi-functionality achieves reliable operation without increasing inverter volume.

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

3Ease of manufacture

If a simplified fixed structure is used to reduce inverter mass, then cost and mass are reduced, but the ability to perform multiple functions may be compromised

Engineering Contradiction:
Improveinverter costVSAvoidinverter functionality
Core Design Contradiction:
Ease of manufactureVSAdaptability or versatility

Solution Approach 1:

The fixed structure is designed with multi-functionality built-in: it provides structural support, guides grid movement through integrated guide elements, deflects reversing flow through built-in deflection edges, and limits grid travel through stop elements. This single structure performs all necessary functions, maintaining versatility while simplifying manufacture and reducing cost.

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

Solution Approach 2:

By combining multiple functions into a single fixed structure, the number of separate components to manufacture and assemble is reduced. This integration simplifies the manufacturing process and reduces cost while preserving all necessary inverter functions through the multi-functional design of the fixed structure.

Inventive Principle:
Principle #5Merging (Combining)

Data Source

PatentEP4323631B1Movable-cascade thrust reverser comprising a multi-functional fixed structure
Publication Date: 2026.02.25 SAFRAN NACELLES
  • EP4323631B1 patent drawingFigure 1~2
  • EP4323631B1 patent drawingFigure 3
  • EP4323631B1 patent drawingFigure 4

AI summary

The invention relates to a movable-cascade thrust reverser comprising a multifunctional annular fixed structure (31) configured to be rigidly connected to a fan casing of a turbine engine or to an intermediate casing secured to the fan casing.