Centrifugal Compressor Bleed Flow Splitter Design

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Solution Overview

Problem

Centrifugal compressors often require a bleed flow that is not readily available from a single source, as the pressure upstream of the impeller is too low for auxiliary use, necessitating a complex bleed flow control arrangement involving multiple sources.

Innovation Solution

An impeller with a plurality of vanes around a hub, featuring a flow stream split that creates an offset between the leading edge and trailing edge, allowing for a mid-impeller bleed location facilitated by a flow splitter, which efficiently captures a desired quantity of bleed flow without complex redesigns.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If a single bleed source is used upstream of the impeller, then the device complexity is reduced, but the pressure is too low for auxiliary use

Engineering Contradiction:
Improvebleed flow control arrangementVSAvoidbleed flow pressure
Core Design Contradiction:
Device complexityVSStress or pressure

Solution Approach 1:

The impeller vanes are segmented with an offset between leading and trailing edges, creating distinct flow paths that enable a single source to provide both high and low pressure bleed flows through different extraction points

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

A flow splitter is introduced as an intermediary component that interfaces with the offset impeller vanes to define a mid-impeller bleed location, enabling efficient capture of bleed flow at the desired pressure level

Inventive Principle:
Principle #24Intermediary (Mediator)

2Stress or pressure

If multiple bleed sources are used, then the pressure requirement is met, but the device complexity increases

Engineering Contradiction:
Improvebleed flow pressureVSAvoidbleed flow control arrangement
Core Design Contradiction:
Stress or pressureVSDevice complexity

Solution Approach 1:

The offset impeller vane design creates a multi-functional single source that can provide bleed flow at multiple pressure levels (high pressure from trailing edge, low pressure from leading edge) and intermediate levels from the mid-impeller location, eliminating the need for multiple separate bleed sources

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

Solution Approach 2:

The offset between leading and trailing edges creates a new spatial dimension in the flow path, allowing the flow splitter to access bleed flow at different radial positions and pressure levels from a single impeller source

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

3Use of energy by moving object

If bleed flow is removed from the impeller, then the dynamic head is improved, but diffusion effects may become detrimental

Engineering Contradiction:
Improvedynamic headVSAvoiddiffusion effects
Core Design Contradiction:
Use of energy by moving objectVSObject-generated harmful factors

Solution Approach 1:

The flow splitter is positioned to extract bleed flow locally at the mid-impeller location where the flow conditions are optimal, removing only the necessary amount of flow (1% to 10%) without disrupting the overall diffusion process in other critical areas of the impeller

Inventive Principle:
Principle #3Local quality

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 solution enables efficient and low-loss bleed flow recovery, providing a consistent 1% to 10% bleed flow, improving the dynamic head and reducing detrimental diffusion effects, while allowing for significant bleed turndown without lip separation.

Implementation Method 1

a centrifugal compressor assembly generally includes an impeller and a diffuser. The impeller, fixed to a central shaft, rotates about an axis within a stationary impeller shroud

Methodology Applied
Scientific EffectCentrifugal force: Centrifugal Force

Implementation Method 2

The flow splitter 52 closely follows the shape of a radial forward surface downstream of the offset to define a mid-impeller bleed path

Methodology Applied
Scientific EffectFlow separation: Flow Separation

Data Source

PatentUS8935926B2Centrifugal compressor with bleed flow splitter for a gas turbine engine
Publication Date: 2015.01.20 RTX CORP
  • US8935926B2 patent drawing
  • US8935926B2 patent drawing
  • US8935926B2 patent drawing

AI summary

An impeller includes a plurality of vanes formed around a hub, each of the plurality of vanes defines an offset between a leading edge and a trailing edge.