Cabin Altitude Alerting System with Dynamic Acoustic Feedback

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Solution Overview

Problem

Aircraft pilots face challenges in quickly diagnosing the cause of a single horn activation, leading to potential misdiagnosis of cabin issues due to the lack of intelligent alerts for specific problems.

Innovation Solution

A cabin pressure alerting system that uses a cabin altimeter, processing device, and alerting device to determine issues with cabin pressure, set alert volumes or frequencies based on pressure changes, and issue alerts, including terrain and altitude data to provide accurate notifications.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Reliability

If a single horn is used to alert the flight crew of various problems, then the alerting device is simple, but the flight crew cannot quickly diagnose the cause leading to misdiagnosis

Engineering Contradiction:
Improvediagnosis accuracyVSAvoidalerting system complexity
Core Design Contradiction:
ReliabilityVSDevice complexity

Solution Approach 1:

The patent divides the single horn alert into multiple distinct alert types (cabin pressure alert, terrain alert, glide slope alert, configuration alert), where each alert type corresponds to a specific problem category. This segmentation allows the flight crew to immediately identify the nature of the problem without misdiagnosis, while maintaining manageable system complexity through modular alert design.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent applies different alert characteristics (sound frequency, volume, pattern) to different problem types. For example, cabin pressure alerts use specific acoustic patterns distinct from terrain alerts. This local differentiation in alert quality enables the flight crew to quickly diagnose the specific problem type without increasing overall system complexity.

Inventive Principle:
Principle #3Local quality

2Loss of time

If multiple alert types are introduced to improve diagnosis accuracy, then the alerting system becomes more complex

Engineering Contradiction:
Improvediagnosis timeVSAvoidalerting system complexity
Core Design Contradiction:
Loss of timeVSDevice complexity

Solution Approach 1:

The alerting system is segmented into distinct alert types with unique characteristics, allowing the flight crew to immediately identify the problem category without time-consuming diagnosis. Each alert type (cabin pressure, terrain, glide slope, configuration) is pre-defined with specific acoustic patterns, eliminating the need for pilots to analyze and diagnose the problem type.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent uses acoustic pattern differentiation (analogous to color changes in visual systems) to encode problem type information in the alerts. Different problem types produce distinct acoustic patterns that are easily distinguishable by the flight crew, enabling rapid diagnosis without increasing operational complexity.

Inventive Principle:
Principle #32Color changes

3Loss of information

If alert volume and frequency are set based on rate of change of cabin pressure, then the alert provides more information, but the processing requirements increase

Engineering Contradiction:
Improvepressure change informationVSAvoidprocessing device complexity
Core Design Contradiction:
Loss of informationVSDevice complexity

Solution Approach 1:

The patent varies alert parameters (volume and frequency) based on the rate of change of cabin pressure. When pressure changes rapidly, the alert uses higher volume and/or frequency to convey urgency. This parameter modulation provides the flight crew with information about the severity and progression of the pressure problem without requiring complex processing systems.

Inventive Principle:
Principle #35Parameter changes

Solution Approach 2:

The processing device continuously monitors cabin pressure and adjusts alert characteristics in real-time based on the rate of pressure change. This feedback mechanism provides the flight crew with dynamic information about the developing situation, allowing them to assess the urgency and progression of the problem without requiring sophisticated processing equipment.

Inventive Principle:
Principle #23Feedback

Data Source

PatentUS9809313B2Cabin altitude alerting systems and methods
Publication Date: 2017.11.07 HONEYWELL INTERNATIONAL INC
  • US9809313B2 patent drawing

AI summary

Systems and methods for intelligently alerting the flight crew of a cabin depressurization. An example system includes a cabin altimeter that generates a cabin pressure value, an alerting device, such as a speaker system and a processing device in data communication with the cabin altimeter and the alerting device. The processing device determines if there is a problem with the cabin pressure received from the cabin altimeter, determines rate of change of the cabin pressure, and sets at least one of an alert volume or an alert frequency based on the cabin pressure and the rate of change of the cabin pressure if it was determined that a problem exists with the cabin pressure. The processing device also issues a cabin depressurization alert over the alerting device based on at least one of the set alert volume or alert frequency, if there is a problem with the cabin pressure value.