Brush Seal Oil Flow for Jet Engine Coking

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Solution Overview

Problem

Labyrinth seals in turbojet engines are inefficient due to excessive gas flow during high phases of flight, leading to reduced engine efficiency and increased oil leakage, while brush seals suffer from coking and wear issues.

Innovation Solution

A brush seal design where an oil flow is created along the strands to prevent degradation, with oil supply mechanisms to maintain freshness and lubrication, reducing coking and enhancing durability.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If labyrinth seals are used with high gas flow rate, then oil leakage is reduced, but engine efficiency decreases and oil is carried out of the enclosure

Engineering Contradiction:
Improveoil tightnessVSAvoidengine efficiency
Core Design Contradiction:
ReliabilityVSLoss of energy

Solution Approach 1:

The patent changes the physical parameters of the seal by transitioning from traditional labyrinth seals to brush seals with specific brush configuration, allowing optimal gas flow rates that maintain both oil tightness and engine efficiency across different flight phases

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The seal design incorporates dynamic adaptation through brush seal elements that can adjust to varying operating conditions, maintaining effective sealing performance whether the engine is at idle or in high-power phases

Inventive Principle:
Principle #15Dynamics

2Reliability

If brush seals are used with low gas flow rate, then oil tightness is improved, but coking occurs on the fibers

Engineering Contradiction:
Improveoil tightnessVSAvoidcoking
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The patent introduces oil as an intermediary substance that flows through the brush seal, serving dual functions: maintaining oil tightness and preventing coking by continuously renewing the oil film on the fibers, thus eliminating the harmful thermal degradation effect

Inventive Principle:
Principle #24Intermediary (Mediator)

Solution Approach 2:

The seal system performs self-maintenance through the continuous flow of oil that automatically renews itself as it passes through the brush seal, preventing accumulation of degraded oil and eliminating coking without external intervention

Inventive Principle:
Principle #25Self-service

3Reliability

If brush seals are used with contact friction, then sealing effectiveness is improved, but wear reduces durability

Engineering Contradiction:
Improvesealing effectivenessVSAvoiddurability
Core Design Contradiction:
ReliabilityVSDuration of action of stationary object

Solution Approach 1:

The continuous oil flow through the brush seal provides automatic lubrication, reducing friction and wear on the fibers while maintaining contact with the rotating component, thus preserving sealing effectiveness over extended operational periods

Inventive Principle:
Principle #25Self-service

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 solution improves the oil tightness and durability of the seal by maintaining oil freshness and lubrication, reducing coking and wear, thereby enhancing the seal's effectiveness and longevity.

Implementation Method 1

an oil flow is created along the strands of the brush seal, which ensures renewal of the oil on contact with them, since the latter is driven in motion along the strands

Methodology Applied
Scientific EffectLubrication: Lubrication

Implementation Method 2

the friction of the bristles on the track of the rotating part intended to be in contact with their ends causes their wear

Methodology Applied
Scientific EffectFriction: Friction

Implementation Method 3

the gases are evacuated in 'oil separators' generally formed by radial chimneys made in the low pressure shaft and on the wall of which the oil is collected to be reinjected into the corresponding enclosure, by centrifugal effect

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Data Source

PatentEP2553221B1Sealing device for jet engine oil chamber
Publication Date: 2016.05.18 SAFRAN AIRCRAFT ENGINES SAS
  • EP2553221B1 patent drawingFigure 1
  • EP2553221B1 patent drawingFigure 2~3
  • EP2553221B1 patent drawingFigure 4

AI summary

The invention relates to a sealing device for a chamber (4, 5) that is formed of at least one rotary member (3, 15) and at least one static member (12, 13) of a jet engine (1) and is intended to contain a lubricating oil droplet suspension (h). The sealing device comprises at least one brush seal (14) that has juxtaposed strands (17) and is set up so as to ensure sealing between at least one rotary member (15) and at least one stationary member (12). Said device is characterized in that it comprises a means (12, 19, 25, 30) for recovering part of the oil suspended within the inner space (V) of the chamber (4, 5) and comprises a means (20, 22, 23, 24, 26) for delivering said recovered oil (h), said delivery means being set up so as to generate a flow of oil (h) along the strands (17) of said brush seal (14), said oil flow being oriented in the direction of the rotary member (3, 15). The brush seal (14) thus provides better resistance to coking.