Mechanical Surge Valve Control for Aircraft Compressors

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Solution Overview

Problem

Conventional compressor surge protection systems in aircraft pneumatic systems are costly and complex due to the need for high-bandwidth feedback control, which can lead to inefficiencies and potential damage during surge events.

Innovation Solution

A passive mechanical surge prevention system using a mechanical valve actuated by a sense line to vent excess pressure, reducing the need for complex active control systems and allowing operation at constant power.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a feedback control system with high bandwidth is used to protect compressor surge, then compressor protection is improved, but system cost and complexity increase

Engineering Contradiction:
Improvecompressor protectionVSAvoidcontrol system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent replaces complex electronic feedback control systems with a simple mechanical valve system. The mechanical valve uses a spring-loaded diaphragm mechanism that automatically opens when surge pressure is detected, eliminating the need for electronic sensors, controllers, and high-bandwidth feedback loops while maintaining effective surge protection

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

Solution Approach 2:

The mechanical valve system is self-regulating and requires no external power or control signals. The spring-loaded diaphragm automatically responds to pressure changes caused by surge conditions, opening the valve to relieve pressure without human intervention or complex control algorithms

Inventive Principle:
Principle #25Self-service

2Reliability

If conventional feedback control systems are implemented for surge protection, then compressor safety is improved, but implementation cost increases

Engineering Contradiction:
Improvecompressor safetyVSAvoidimplementation cost
Core Design Contradiction:
ReliabilityVSEase of manufacture

Solution Approach 1:

The patent employs inexpensive mechanical components (spring-loaded diaphragm valve) instead of expensive electronic control systems. The mechanical valve can be manufactured at low cost using standard aerospace mechanical components, making surge protection accessible without high implementation costs

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

3Speed

If high-bandwidth feedback control is used for surge protection, then response speed is improved, but system complexity increases

Engineering Contradiction:
Improveresponse speedVSAvoidcontrol system complexity
Core Design Contradiction:
SpeedVSDevice complexity

Solution Approach 1:

The mechanical valve provides instantaneous response to surge pressure changes through direct mechanical action on the diaphragm, eliminating electronic signal processing delays. The spring-loaded mechanism responds immediately when pressure differential exceeds the spring force, achieving high response speed without electronic complexity

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

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 mechanical surge prevention system effectively prevents compressor surge without the complexity and cost of conventional systems, providing reliable protection and improved responsiveness by passively managing pressure.

Implementation Method 1

a mechanical valve that is actuated based on a detected pressure within a sense line operably coupled to the mechanical valve

Methodology Applied
Scientific EffectPressure detection: Pressure Gradient

Implementation Method 2

the surge prevention circuit comprises a mechanical valve that is actuated based on a detected pressure within a sense line

Methodology Applied
Scientific EffectPressure venting: Depressurisation

Implementation Method 3

a heat exchanger configured to receive the compressed air as a first working fluid and a treating air as a second working fluid, the heat exchanger configured to convert the compressed air to compressed and temperature treated air

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Data Source

PatentEP4191070B1Compressor surge prevention control
Publication Date: 2025.12.24 HAMILTON SUNDSTRAND CORP
  • EP4191070B1 patent drawingFigure 1
  • EP4191070B1 patent drawingFigure 2
  • EP4191070B1 patent drawingFigure 3

AI summary

Pneumatic air systems for use onboard aircraft include a compressor (102) configured to receive air from an air supply (108) and increase a pressure of said received air to generate compressed air, a heat exchanger (112) configured to receive the compressed air as a first working fluid and a treating air as a second working fluid, the heat exchanger (112) configured to convert the compressed air to compressed and temperature treated air, one or more aircraft systems (114a-c) configured to receive the compressed and temperature treated air, and a surge prevention circuit (138) arranged to prevent surge of air at the compressor, wherein the surge prevention circuit (138) comprises a mechanical valve (140) that is actuated based on a detected pressure within a sense line (142) operably coupled to the mechanical valve (140).