Bearing Housing Gutter Geometry for Low-Loss Lubricant Drainage

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Solution Overview

Problem

Industrial gas turbine engines face issues with lubricant flooding and foaming due to reduced momentum of used lubricant at the base of the bearing housing, caused by sharp directional changes and narrow passageways, leading to parasitic losses and inefficient lubrication.

Innovation Solution

A low loss drain configuration is implemented in the bearing housing, featuring a gutter with sloped floor portions that maintain downward momentum and facilitate the free flow of used lubricant into a gravity-fed drain, eliminating the need for a scavenge pump and reducing sharp directional changes.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Volume of moving object

If sharp directional changes and narrow passageways are used around the base of the bearing housing, then the structure is more compact, but the momentum of used lubricant is reduced causing it to collect at the base

Engineering Contradiction:
Improvebearing housing compactnessVSAvoidlubricant flow speed
Core Design Contradiction:
Volume of moving objectVSSpeed

Solution Approach 1:

The patent applies curved surfaces and smooth transitions in the passageway geometry instead of sharp angles. The bearing housing base features curved surfaces that guide lubricant flow smoothly into the drain, maintaining momentum while achieving compact dimensions. This resolves the contradiction by using curvature to preserve flow speed despite reduced volume.

Inventive Principle:
Principle #14Spheroidality (Curvature)

2Reliability

If pumps are used to evacuate lubricant from the bearing compartment, then lubricant removal is ensured, but negative pressure is created increasing parasitic losses

Engineering Contradiction:
Improvelubricant evacuation reliabilityVSAvoidparasitic losses
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The patent extracts and eliminates the pump component from the lubricant evacuation system. Instead of using a pump to create negative pressure, the design relies on gravity-fed drainage through optimally configured passageways and drain structures. This removes the energy-consuming component while maintaining reliable lubricant removal through passive gravitational flow.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The lubricant evacuation system is designed to be self-service through gravity-driven flow. The bearing housing and drain configuration automatically guide lubricant from the bearing compartment to the drain without external power input. The system uses the lubricant's own weight and optimized flow paths to achieve evacuation, eliminating the need for active pumping and associated energy losses.

Inventive Principle:
Principle #25Self-service

3Productivity

If high oil flow rates are supplied to bearings for lubrication and cooling, then bearing performance is improved, but lubricant flooding and foaming occur if not evacuated timely

Engineering Contradiction:
Improvebearing lubrication effectivenessVSAvoidlubricant flooding and foaming
Core Design Contradiction:
ProductivityVSObject-generated harmful factors

Solution Approach 1:

The patent implements preliminary action by designing the drain and passageway configuration in advance to match the high flow rates required for bearing lubrication. The gravity-fed drain system and optimized passageways are pre-configured to handle the expected lubricant volume, ensuring that as soon as high flow rates are supplied to the bearings, the evacuation system is already positioned and sized to prevent flooding and foaming.

Inventive Principle:
Principle #10Preliminary action

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

This configuration effectively prevents lubricant flooding and foaming, ensuring efficient lubrication and cooling of turbine bearings even at high lubricant flow rates without the need for a scavenge pump, thereby minimizing parasitic losses.

Implementation Method 1

a drain disposed proximate a base of the gutter. The gutter includes a first sloped floor portion circumferentially adjacent to the drain... maintain downward momentum and facilitate the free flow of used lubricant into a gravity-fed drain

Methodology Applied
Scientific EffectGravity: Gravitation

Implementation Method 2

After being supplied to the bearings, used lubricant is flung outward to an inner wall of the bearing housing

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentEP2989300B1Low loss bearing drain
Publication Date: 2021.10.20 RTX CORP
  • EP2989300B1 patent drawingFigure 1
  • EP2989300B1 patent drawingFigure 2
  • EP2989300B1 patent drawingFigure 3

AI summary

A turbine module comprises a turbine shaft, a rotor assembly secured to the shaft, a bearing assembly rotatably supporting the turbine shaft, and a bearing housing containing the bearing assembly. The bearing housing includes a gutter at least partially circumscribing the bearing assembly, and a drain disposed proximate a base of the gutter. The gutter includes a first sloped floor portion circumferentially adjacent to the drain.