Aircraft Pressure Management Moveable Door

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Solution Overview

Problem

Aircraft interior pressure management systems face issues with high stress and component weight due to the need for frequent resetting or replacement of blowout doors and panels, which can lead to potential hazards during flight and on the ground.

Innovation Solution

A pressure management system featuring a moveable door that opens and closes in response to pressure differentials between the interior and exterior of an aircraft cavity, strategically positioned to minimize drag and reduce maintenance needs.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If blowout doors or panels are set to deploy at high pressures to prevent panel blowout hazards, then safety is improved, but stress on fairing support structure increases and component weight increases

Engineering Contradiction:
ImprovesafetyVSAvoidstress on fairing support structure
Core Design Contradiction:
ReliabilityVSStress or pressure

Solution Approach 1:

The blowout protection system is segmented into multiple independent blowout doors positioned at different pressure thresholds. This allows the structure to experience lower peak pressures in individual events while maintaining overall safety through distributed protection points, thereby reducing stress on any single support structure component.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system changes the pressure parameter threshold at which blowout doors deploy. By setting multiple doors to open at different pressure levels rather than all at once at a single high threshold, the peak pressure experienced by the structure is reduced while still providing adequate protection against panel blowout hazards.

Inventive Principle:
Principle #35Parameter changes

2Reliability

If blowout doors or panels are replaced after each blowout event, then reliability is maintained, but maintenance time and operational disruption increase

Engineering Contradiction:
ImprovereliabilityVSAvoidmaintenance time
Core Design Contradiction:
ReliabilityVSLoss of time

Solution Approach 1:

The blowout doors are designed with self-resetting mechanisms that automatically return the door to its closed position after a blowout event. This self-service capability eliminates the need for manual intervention and replacement, allowing the system to maintain reliability without requiring maintenance time or operational disruption for door replacement.

Inventive Principle:
Principle #25Self-service

3Adaptability or versatility

If multiple blowout doors are used to manage pressure differentials, then pressure control is improved, but device complexity increases

Engineering Contradiction:
Improvepressure controlVSAvoiddevice complexity
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

A pressure differential sensor acts as an intermediary between the interior and exterior pressure fields, detecting pressure differences and triggering appropriate blowout door responses. This intermediary sensing mechanism enables sophisticated pressure control across multiple doors without requiring complex mechanical linkages or control systems, thus managing adaptability while limiting complexity increase.

Inventive Principle:
Principle #24Intermediary (Mediator)

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 reduces the likelihood of panel blowout hazards, lowers peak duct burst pressure, and decreases maintenance requirements, while minimizing drag and air loads during maneuvers.

Implementation Method 1

The door opens to uncover the opening and closes to cover the opening in response to pressure differential between the exterior pressure and the interior pressure

Methodology Applied
Scientific EffectPressure differential: Pressure Gradient

Data Source

PatentUS8734211B2Aircraft pressure management system
Publication Date: 2014.05.27 THE BOEING CO
  • US8734211B2 patent drawing
  • US8734211B2 patent drawing
  • US8734211B2 patent drawing

AI summary

One embodiment of a pressure management system for an aircraft may include a cavity, an opening in a surface of the cavity, and a moveable door. An interior area within the cavity may have an interior pressure and an exterior area outside of the cavity may have an exterior pressure. The door may open to uncover the opening and may close to cover the opening in response to pressure differential between the exterior pressure and the interior pressure.