Composite Outflow Valve Redundancy for Cabin Pressure Control

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Solution Overview

Problem

Aircraft outflow valves need to be lightweight, compact, and meet regulatory standards for postulated single point failures, particularly in high-altitude flight where cabin pressure control is crucial to prevent hypoxia, but existing materials like plastics and composites lack defined crack propagation properties, making it challenging to meet these requirements.

Innovation Solution

A compact and lightweight outflow valve assembly is designed with a non-metallic valve body and a metallic sleeve, featuring a dual-wall flow passage configuration and brackets for mounting to the aircraft fuselage, ensuring redundancy and compliance with regulatory standards.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Weight of moving object

If the outflow valve body is constructed from plastic or composite materials to reduce weight, then the weight is reduced, but the reliability is compromised due to undefined crack propagation properties

Engineering Contradiction:
Improveoutflow valve weightVSAvoidcrack propagation resistance
Core Design Contradiction:
Weight of moving objectVSReliability

Solution Approach 1:

The outflow valve body is constructed from a composite material consisting of a metal matrix reinforced with continuous fibers (such as carbon fiber or glass fiber). This composite structure provides both the weight reduction benefits of non-metallic materials and the defined crack propagation resistance of metal matrices, where cracks are arrested by the fiber reinforcement and metal ligaments.

Inventive Principle:
Principle #40Composite materials

Solution Approach 2:

The valve body is designed with a modular composite structure where fiber reinforcement is segmented and distributed throughout the metal matrix. This segmentation allows cracks to be contained within local regions rather than propagating through the entire structure, improving reliability while maintaining lightweight characteristics.

Inventive Principle:
Principle #1Segmentation

2Device complexity

If the outflow valve is designed to be compact and lightweight for high-altitude aircraft, then the device complexity is reduced, but meeting regulatory standards for single point failures becomes more difficult

Engineering Contradiction:
Improveoutflow valve structure complexityVSAvoidsingle point failure resistance
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The use of fiber-reinforced metal composite materials provides inherent redundancy against single point failures. The continuous fiber reinforcement creates multiple load paths, so that if one area fails, the composite structure can redistribute stresses through adjacent regions, meeting regulatory standards without increasing overall device complexity.

Inventive Principle:
Principle #40Composite materials

3Reliability

If traditional metallic outflow valves are used to ensure reliability, then the reliability is maintained, but the weight increases and compactness is reduced

Engineering Contradiction:
Improveoutflow valve reliabilityVSAvoidoutflow valve weight
Core Design Contradiction:
ReliabilityVSWeight of moving object

Solution Approach 1:

The fiber-reinforced metal composite achieves a favorable strength-to-weight ratio compared to traditional metallic valves. The continuous fiber reinforcement provides high strength and stiffness, allowing for a lighter, more compact valve design while maintaining or improving reliability through the composite's inherent crack arrest mechanisms and damage tolerance.

Inventive Principle:
Principle #40Composite materials

Data Source

PatentUS7472885B2Compact, lightweight cabin pressure control system butterfly outflow valve with redundancy features
Publication Date: 2009.01.06 HONEYWELL INTERNATIONAL INC
  • US7472885B2 patent drawing
  • US7472885B2 patent drawing
  • US7472885B2 patent drawing

AI summary

A relatively compact, lightweight outflow valve assembly includes suitable redundancy features that allow the valve assembly to meet regulatory requirements for certain postulated single point failures. The valve assembly includes a valve body that is constructed at least partially of a non-metallic material and has an outer surface and an inner surface that defines a flow passage having at least two flow ports. A sleeve is disposed within the valve body flow passage that is constructed at least partially of a metallic material. The sleeve has a flow passage formed therein that is in fluid communication with the valve body flow passage flow ports. A valve element is disposed within the sleeve flow passage and is moveable between at least an open position and a closed position. A plurality of brackets is mounted on the valve body outer surface and is coupled to the sleeve. When the valve assembly is installed in an aircraft, the plurality of brackets further couples the sleeve to the aircraft fuselage.