Aircraft Gearbox Lubrication Segmentation for Failure Isolation

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Solution Overview

Problem

Aircraft drive systems are susceptible to losing torque, failing, and overheating due to malfunctioning or non-functioning lubrication systems, particularly when relying on a single pressurized lubrication system, which can lead to catastrophic failures and non-compliance with aviation regulations.

Innovation Solution

Implementing a compound lubrication system with multiple, independent lubrication subsystems that segregate compartments within the gearbox, preventing lubricant transfer between them, ensuring that each subsystem can operate independently to maintain lubrication even if one fails.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a single pressurized lubrication system is used, then the device complexity is reduced, but the reliability of the drive system decreases due to susceptibility to complete failure

Engineering Contradiction:
Improvelubrication system reliabilityVSAvoidlubrication system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The lubrication system is divided into multiple independent subsystems, each responsible for lubricating specific compartments. Each subsystem has its own lubricant supply and delivery mechanisms, ensuring that failure in one subsystem does not affect others. The gearbox is segmented into multiple compartments separated by barriers, with each compartment served by a dedicated lubrication subsystem.

Inventive Principle:
Principle #1Segmentation

2Reliability

If multiple independent lubrication subsystems are implemented, then the reliability improves, but the device complexity increases

Engineering Contradiction:
Improvelubrication system reliabilityVSAvoidlubrication system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The system is segmented into independent lubrication subsystems, each with dedicated components for lubricating specific compartments. This segmentation isolates failures to individual subsystems while maintaining overall system reliability.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Multiple lubrication subsystems serve universal lubrication functions across different compartments. Each subsystem performs the same basic lubrication function but operates independently to provide redundancy and reliability across the entire gearbox system.

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

3Reliability

If compartments are segregated with barriers, then the reliability increases by preventing lubricant transfer, but the manufacturing precision requirements increase

Engineering Contradiction:
Improvelubrication system reliabilityVSAvoidbarrier sealing precision
Core Design Contradiction:
ReliabilityVSManufacturing precision

Solution Approach 1:

The gearbox housing is segmented into multiple sealed compartments by barriers. These barriers create physical separations that prevent lubricant transfer between compartments, ensuring that each lubrication subsystem operates independently with its own dedicated lubricant supply.

Inventive Principle:
Principle #1Segmentation

Data Source

PatentUS11313455B2Aircraft gearbox lubrication system with multiple lubrication subsystems
Publication Date: 2022.04.26 TEXTRON INNOVATIONS INC
  • US11313455B2 patent drawing
  • US11313455B2 patent drawing
  • US11313455B2 patent drawing

AI summary

In some examples, an aircraft gearbox comprises a housing, a barrier, a rotatable drive system component, a set of gears, and a lubrication system. The barrier separates a first compartment and a second compartment within the housing. Each of the rotatable drive system component and the set of gears operable to rotate based on torque received from an engine. The rotatable drive system component is located in the first compartment. The set of gears is located in the second compartment. The lubrication system comprises a first lubrication subsystem and a second lubrication subsystem, which are, at least in part, independent from one another. The first lubrication subsystem is operable to lubricate the rotatable drive system component in the first compartment. The second lubrication subsystem is operable to lubricate the set of gears in the second compartment. The barrier inhibits lubricant from passing between the first compartment and the second compartment.