Orifice Pack Debris Filtration for Compressor Bleed Valve

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

In aerospace gas turbine engines, pressurized air used to control compressor bleed valves may carry debris, which is undesirable and can affect the reliability and consistency of the valve's operation.

Innovation Solution

An orifice pack system is used to deliver pressurized air to the compressor bleed valve, where a portion of the air is vented upstream of the valve to prevent debris from reaching it, ensuring cleaner air is supplied to the valve.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If pressurized air is delivered to the compressor bleed valve, then the valve can be controlled to maintain engine operability, but debris carried by the pressurized air may enter the valve and affect its reliability

Engineering Contradiction:
Improvecompressor bleed valve operation reliabilityVSAvoiddebris contamination
Core Design Contradiction:
ReliabilityVSObject-affected harmful factors

Solution Approach 1:

The orifice pack is positioned upstream of the compressor bleed valve to perform preliminary filtration of the pressurized air before it reaches the valve. The pack includes multiple orifices that create pressure drops and turbulence to separate debris particles from the air stream, ensuring cleaner air reaches the valve actuator.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The orifice pack acts as an intermediary component between the pressurized air source and the compressor bleed valve. It mediates the air flow by filtering out debris through its multi-orifice structure, preventing harmful particles from directly contacting the valve while still delivering the necessary pressurized air for valve control.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Reliability

If filtration is implemented to remove debris from pressurized air, then valve reliability improves, but system complexity increases

Engineering Contradiction:
Improvecompressor bleed valve operation reliabilityVSAvoidair delivery system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The filtration function is segmented into multiple small orifices within the orifice pack rather than using a single complex filter. Each orifice contributes to the overall filtration effect through pressure drops and flow turbulence, distributing the filtration task across multiple simple geometric features that are easy to manufacture and integrate.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The orifice pack uses simple geometric orifices that can be easily manufactured into the air delivery component. These orifices serve as a low-cost, maintenance-free filtration solution that does not require replaceable filter elements, reducing long-term operational complexity while maintaining reliable debris removal.

Inventive Principle:
Principle #27Cheap short-living objects (Disposable)

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 orifice pack effectively prevents debris from entering the compressor bleed valve, enhancing the reliability and consistency of the valve's operation by ensuring cleaner air is used for control purposes.

Implementation Method 1

an orifice pack (24) configured for delivering pressurized air to a compressor bleed valve (22) of a gas turbine engine (10)

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Data Source

PatentEP4124739B1Orifice pack for compressor bleed valve
Publication Date: 2025.06.11 PRATT & WHITNEY CANADA CORP
  • EP4124739B1 patent drawingFigure 1
  • EP4124739B1 patent drawingFigure 2
  • EP4124739B1 patent drawingFigure 3

AI summary

An orifice pack (24) is provided for delivering pressurized air to a compressor bleed valve (22) of a gas turbine engine (10). The orifice pack (24) has a diffusion chamber (34) in serial flow communication with a tapering passage (28c) and a first outlet passage (28d) for venting a first portion of the pressurized air from the diffusion chamber (34). A second outlet passage (30') branches off from the diffusion chamber (34) at an axial location between the inlet (26) and the tapering passage (28c). The second outlet passage (30') is fluidly connected to the compressor bleed valve (22) for directing a second portion of the pressurized air from the diffusion chamber (34) to the compressor bleed valve (22).