Actuator Lubricant Level Sensing Under Centrifugal Force

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Solution Overview

Problem

Detecting lubricant levels in electromechanical actuators, such as those in helicopter rotor blade control surfaces, is challenging due to substantial changes in orientation, velocity, acceleration, and vibration, which can lead to reduced performance or damage if insufficient lubrication is maintained.

Innovation Solution

A lubricant level sensing system that includes a pressure port in the actuator's outer housing, a pressure sensor, and a pathway for fluid communication with a free volume within the actuator, allowing the pressure sensor to detect changes in pressure to derive the lubricant level, with a control computer monitoring the output to determine the lubricant level accurately.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a lubricant level sensing system is implemented in an actuator subjected to substantial centrifugal force and vibration, then the reliability of lubricant level detection is improved, but the device complexity increases

Engineering Contradiction:
Improvereliability of lubricant level detectionVSAvoiddevice complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces complex mechanical level sensing mechanisms with a pressure-based detection system. A pressure sensor monitors pressure changes in a sealed cavity that communicates with the lubricant reservoir through a pathway. When lubricant level drops, air enters the cavity through the pathway, causing pressure changes that the sensor detects, eliminating the need for direct mechanical contact or complex optical systems in harsh environments

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

Solution Approach 2:

The patent introduces a sealed cavity with a pathway as an intermediary between the lubricant reservoir and the pressure sensor. This intermediary system translates lubricant level changes into pressure changes that can be reliably measured, while isolating the sensor from direct exposure to centrifugal forces, vibration, and temperature extremes that would otherwise compromise detection reliability

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If the actuator is designed to retain adequate lubricant volume under centrifugal force, then the lubrication performance is improved, but the volume of the actuator increases

Engineering Contradiction:
Improvelubrication performanceVSAvoidvolume of actuator
Core Design Contradiction:
ReliabilityVSVolume of moving object

Solution Approach 1:

The patent addresses lubricant retention under centrifugal force by designing a sealed cavity system that utilizes pressure differential rather than relying solely on gravitational retention. The pathway allows controlled air entry when lubricant level drops, creating a pressure mechanism that maintains lubricant in the required zone regardless of orientation or centrifugal acceleration, effectively adding a pressure-dimensional control mechanism to the traditional gravity-dependent lubrication system

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

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 maintains adequate lubrication levels even under high centrifugal forces, ensuring low friction and preventing damage by timely detection of lubricant loss, thus enhancing the operational reliability of the actuator.

Implementation Method 1

the pressure sensor detects changes in pressure of the free volume used to derive the lubricant level

Methodology Applied
Scientific EffectPressure detection: Pressure Gradient

Implementation Method 2

The pathway establishes fluid communication between the pressure sensor and the free volume of an internal cavity

Methodology Applied
Scientific EffectFluid communication: Pressure Gradient

Implementation Method 3

A rotor blade control surface actuator is subject to substantial centrifugal force, as well as other forces due to blade flapping

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentUS11174988B2Lubricant level sensing for an actuator
Publication Date: 2021.11.16 SIKORSKY AIRCRAFT CORP
  • US11174988B2 patent drawing
  • US11174988B2 patent drawing
  • US11174988B2 patent drawing

AI summary

According to one aspect, a lubricant level sensing system for an actuator is provided. The lubricant level sensing system includes a pressure port in an outer housing of the actuator, a pressure sensor, and a pathway from the pressure port to the pressure sensor. The pathway establishes fluid communication between the pressure sensor and a free volume of an internal cavity of the outer housing relative to a lubricant level in the internal cavity such that the pressure sensor detects a pressure of the free volume used to derive the lubricant level.