Aircraft Gearbox Lubricant-Out Detection in Splash-Lubricated Systems

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Solution Overview

Problem

Aircraft gearboxes face challenges in detecting lubricant-out conditions effectively, particularly in splash lubricated systems where pressure-based detection methods are not applicable, potentially leading to unforeseen system failures and unsafe flight conditions.

Innovation Solution

A lubricant-out sensor system that detects non-pressure based parameters such as lubricant temperature and conductivity, or a combination of both, within the lubricant return passages to provide accurate alerts for lubricant loss, ensuring reliable detection and timely warnings for pilots or ground controllers.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If pressure-based detection methods are used in aircraft gearboxes, then detection reliability is improved, but applicability is worsened because these methods cannot be used in splash lubricated systems

Engineering Contradiction:
Improvedetection reliabilityVSAvoidapplicability
Core Design Contradiction:
ReliabilityVSAdaptability or versatility

Solution Approach 1:

The patent changes the detection parameter from pressure-based to non-pressure-based parameters such as temperature and conductivity. This allows the detection system to be applicable to splash lubricated systems while maintaining reliable detection capability. The temperature sensor detects lubricant temperature changes and the conductivity sensor detects lubricant conductivity changes, both of which occur when lubricant level is low, providing reliable detection without requiring pressure.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The patent replaces the mechanical pressure-based detection system with non-mechanical sensing methods using temperature and conductivity sensors. This substitution eliminates the need for pressure mechanisms while achieving equivalent or superior detection reliability across different lubrication systems including splash lubricated systems.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Adaptability or versatility

If non-pressure based parameters are detected, then adaptability is improved for splash lubricated systems, but measurement precision may be worsened compared to pressure-based methods

Engineering Contradiction:
Improveapplicability to splash lubricated systemsVSAvoiddetection precision
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The patent creates a universal detection system that can be applied to both pressure-based and splash lubricated systems by using temperature and conductivity sensors. These sensors detect multiple parameters (temperature and conductivity) that change when lubricant level is low, providing precise detection across different system types. The multi-functional sensors monitor both thermal and electrical properties of the lubricant to ensure accurate detection.

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

Solution Approach 2:

The patent uses temperature and conductivity as intermediary parameters to indirectly detect lubricant level. Instead of directly measuring lubricant presence, the sensors measure temperature and conductivity changes that occur when lubricant level drops, providing precise indirect measurement that works reliably in splash lubricated systems.

Inventive Principle:
Principle #24Intermediary (Mediator)

3Measurement precision

If multiple sensors are used to detect both temperature and conductivity, then detection accuracy is improved, but device complexity is worsened

Engineering Contradiction:
Improvedetection accuracyVSAvoidsensor system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The patent combines temperature and conductivity sensing capabilities into a single integrated sensor assembly that is fluidically connected to the lubricant return passage. This merged sensor design detects both temperature and conductivity parameters simultaneously, improving detection accuracy while minimizing the increase in device complexity through a unified sensing structure rather than separate independent sensors.

Inventive Principle:
Principle #5Merging (Combining)

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 system effectively detects lubricant loss in aircraft gearboxes, enabling timely interventions and preventing gearbox failures, thus ensuring sustained safe flight even after ballistic impacts or other system failures.

Implementation Method 1

the lubricant-out sensor comprises a temperature sensor, wherein the non-pressure based parameter comprises lubricant temperature

Methodology Applied
Scientific EffectTemperature sensing:

Implementation Method 2

the lubricant-out sensor comprises a conductivity sensor, wherein the non-pressure based parameter comprises lubricant conductivity

Methodology Applied
Scientific EffectConductivity sensing:

Data Source

PatentUS11512811B2System and method for detecting a lubricant-out condition in an aircraft gearbox
Publication Date: 2022.11.29 SIKORSKY AIRCRAFT CORP
  • US11512811B2 patent drawing
  • US11512811B2 patent drawing

AI summary

A gearbox includes a housing including a lubricant reservoir, at least one gear system arranged in the housing, at least one lubricant delivery passage operable to direct a flow of lubricant from a lubricant reservoir onto the at least one gear system, at least one lubricant return passage operable to guide the flow of lubricant to the lubricant reservoir, and a lubricant-out sensor fluidically connected to the at least one lubricant return passage. The lubricant-out sensor is operable to detect a non-pressure based parameter of the lubricant.