Redundant Gearbox Assembly for Torque Transmission Failures

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Solution Overview

Problem

Gearbox assemblies in aircraft are vulnerable to catastrophic failure at specific locations, leading to loss of torque transmission and potential system failure, necessitating frequent and costly maintenance.

Innovation Solution

The implementation of redundancy measures, such as reinforcement components like plates or brackets, and secondary bearings at vulnerable points to maintain torque transmission in case of failures, thereby preventing complete system failure.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If reinforcement components are added to provide redundancy at vulnerable locations, then reliability is improved, but device complexity increases

Engineering Contradiction:
ImprovereliabilityVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Reinforcement components such as plates and brackets are pre-installed at vulnerable locations (gear meshing points, bearing supports, casing joints) before failure occurs. These components remain inactive during normal operation but automatically engage when cracks or fractures develop, maintaining torque transmission without requiring real-time detection or activation mechanisms.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The gearbox assembly is divided into critical vulnerability zones (gear meshing areas, bearing locations, casing joints), and reinforcement components are selectively applied only to these specific segments rather than the entire structure. This targeted approach provides reliability improvement at critical points while minimizing overall complexity addition.

Inventive Principle:
Principle #1Segmentation

2Reliability

If secondary bearings are provided at vulnerable locations, then reliability is improved, but device complexity increases

Engineering Contradiction:
ImprovereliabilityVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

Secondary bearings are pre-positioned at vulnerable bearing locations alongside primary bearings. During normal operation, primary bearings carry the load while secondary bearings remain inactive or lightly loaded. When primary bearings fail, secondary bearings automatically engage to maintain shaft support and torque transmission without requiring detection systems or active switching mechanisms.

Inventive Principle:
Principle #10Preliminary action

3Reliability

If reinforcement components are added to prevent catastrophic failure, then safety is improved, but manufacturing complexity increases

Engineering Contradiction:
ImprovesafetyVSAvoidease of manufacture
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The gearbox casing and components are designed as modular segments that can be manufactured separately and assembled. Reinforcement plates and brackets are manufactured as separate components that are attached to specific vulnerability zones, allowing standard manufacturing processes to be used for both the base gearbox and the reinforcement elements, simplifying production while maintaining safety.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentEP4001699A1Gearbox assembly
Publication Date: 2022.05.25 RATIER FIGEAC SAS
  • EP4001699A1 patent drawingFigure 1
  • EP4001699A1 patent drawingFigure 2
  • EP4001699A1 patent drawingFigure 3

AI summary

A gearbox assembly comprising a plurality of component parts in torque transmission connection via gear, shaft and/or housing components; the assembly further comprising means (19) for providing redundancy at selected locations where failure can lead to loss of torque transmission between component parts of the assembly.