Turbomachine Bleed Slide Valve for Hail Expulsion

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Solution Overview

Problem

Current compressor bleed systems in jet engines face difficulties in effectively expelling hail and preventing engine flame-out due to limited inter-flowpath height, especially in small engines, where integrating secondary-stream guide vanes into support arms complicates air expulsion.

Innovation Solution

A bleed system with a slide valve that occupies three positions – closed, intermediate, and open – allows for complete hail expulsion by controlling the bleed opening upstream and downstream of the support arms, using a flange for sealing and elastomeric or brush seals for enhanced sealing, ensuring effective hail removal and preventing engine flame-out.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If the bleed opening is positioned downstream of the support arms, then the structure is simplified, but hail cannot be completely expelled and engine flame-out risk remains

Engineering Contradiction:
Improvebleed system structureVSAvoidhail expulsion effectiveness
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The bleed opening is segmented into two distinct parts: a first bleed opening positioned upstream of the support arms and a second bleed opening positioned downstream. This segmentation allows independent control of each opening through the slide valve mechanism, enabling complete hail expulsion by opening both openings while maintaining structural organization through the intermediate casing.

Inventive Principle:
Principle #1Segmentation

2Length of moving object

If the inter-flowpath height is reduced for small engines, then the engine size is reduced, but air expulsion capability is compromised

Engineering Contradiction:
Improveengine sizeVSAvoidair expulsion capability
Core Design Contradiction:
Length of moving objectVSProductivity

Solution Approach 1:

The slide valve mechanism operates in the axial dimension to control the bleed openings, creating a three-position control system (closed, intermediate, open) that manages flow paths effectively within the limited radial space of small engines. The intermediate position with the flange provides precise control over the upstream opening while maintaining downstream opening capability.

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

3Loss of energy

If the slide valve is positioned to block the upstream bleed opening in intermediate position, then aerodynamic efficiency is improved, but hail expulsion capability is reduced

Engineering Contradiction:
Improveaerodynamic efficiencyVSAvoidhail expulsion capability
Core Design Contradiction:
Loss of energyVSReliability

Solution Approach 1:

The slide valve is designed as a dynamic component with three distinct positions that can be selected based on operational requirements. In normal operation, the valve maintains aerodynamic efficiency by positioning to block the upstream opening. When hail is detected, the valve dynamically transitions to the open position to enable complete hail expulsion, and can position in intermediate mode to selectively block only the upstream opening while maintaining downstream capability.

Inventive Principle:
Principle #15Dynamics

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 ensures complete expulsion of hail, eliminating the risk of engine flame-out and maintaining aerodynamic efficiency by strategically positioning the bleed opening and using seals to manage the air flow, particularly during low engine speeds.

Implementation Method 1

the slide valve comprises a flange which blocks off the bleed opening when the slide valve is in the intermediate position

Methodology Applied
Scientific EffectMechanical blocking: Valve

Implementation Method 2

the slide valve is equipped with elastomeric seals or with brush seals in order to provide sealing between the slide valve and the plate

Methodology Applied
Scientific EffectElastic sealing: Elasticity

Data Source

PatentUS7785066B2Bleed system for a low-pressure compressor of a turbomachine
Publication Date: 2010.08.31 SAFRAN AIRCRAFT ENGINES SAS
  • US7785066B2 patent drawing
  • US7785066B2 patent drawing
  • US7785066B2 patent drawing

AI summary

The bypass turbomachine comprises, between a primary flowpath (2) and a secondary flowpath (3), a structural intermediate casing (14). A bleed passage (29) allows the diversion of a portion of the gas stream toward the secondary flowpath (3), downstream of support arms (18) situated at the periphery of the intermediate casing. A bleed opening (28) emerges upstream of the support arms (18). A slide valve (22) slides between three positions, namely a closed position in which the slide valve (22) completely blocks off the bleed passage and opening, an intermediate position in which the bleed opening (28) emerging upstream of the support arms (18) is blocked off, while the bleed passage (29) for diverting a portion of the gas stream downstream of the support arms (18) is open, and an open position in which the bleed opening (28) emerging upstream of the support arms (18) and the bleed passage (29) emerging downstream of the support arms are both open.