Pressure Sensor Drift Detection in Cabin Control

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Solution Overview

Problem

Pressure sensors in environments like aircraft cabins experience signal drift and noise over time, leading to inaccurate pressure control, potential safety issues, and eventual failure, which can cause occupant discomfort and safety risks.

Innovation Solution

A pressure control system that calculates and compares pressure sensor rate of change errors and errors with predefined control limits, using ambient and environmental air pressure signals to predict sensor failure and provide maintenance alerts, with computations performed externally to reduce resource requirements on embedded controllers.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Duration of action of stationary object

If pressure sensors are used for long-term pressure control, then pressure control function is maintained, but sensor drift and noise increase leading to degraded signal quality and control accuracy

Engineering Contradiction:
Improvesensor operational durationVSAvoidpressure measurement accuracy
Core Design Contradiction:
Duration of action of stationary objectVSMeasurement precision

Solution Approach 1:

The system performs preliminary detection of sensor drift and noise trends before complete failure occurs. By continuously monitoring sensor output quality metrics and comparing against thresholds, the system predicts imminent failure and triggers maintenance actions in advance, preventing catastrophic pressure control loss while extending effective sensor operational duration.

Inventive Principle:
Principle #10Preliminary action

2Device complexity

If pressure sensor drift is allowed to progress, then system complexity is reduced, but control inaccuracy increases causing erroneous BIT failures and safety valve oscillations

Engineering Contradiction:
Improvesystem complexityVSAvoidpressure control reliability
Core Design Contradiction:
Device complexityVSReliability

Solution Approach 1:

The system implements feedback monitoring of sensor output quality by continuously analyzing pressure signals for drift and noise patterns. When quality metrics degrade beyond acceptable thresholds, the system generates alerts and predicts failure, enabling timely maintenance interventions that prevent control inaccuracies, erroneous BIT failures, and safety valve oscillations without requiring overly complex redundant sensor systems.

Inventive Principle:
Principle #23Feedback

3Measurement precision

If pressure sensor degradation is monitored continuously, then sensor failure prediction accuracy is improved, but computational resource requirements increase

Engineering Contradiction:
Improvefailure prediction accuracyVSAvoidcomputational energy consumption
Core Design Contradiction:
Measurement precisionVSUse of energy by moving object

Solution Approach 1:

The system applies partial monitoring by focusing computational resources on detecting specific degradation patterns (drift trends and noise levels) rather than analyzing all sensor parameters continuously. Quality metrics are evaluated at strategic intervals and compared against pre-established thresholds, achieving accurate failure prediction while minimizing unnecessary computational energy consumption on the embedded controller.

Inventive Principle:
Principle #16Partial or excessive action

Data Source

PatentUS10934004B2Detection of noise in pressure sensor and prediction of pressure sensors drift in cabin pressure control system/air data computer system/environmental control systems
Publication Date: 2021.03.02 HONEYWELL INTERNATIONAL INC
  • US10934004B2 patent drawing
  • US10934004B2 patent drawing
  • US10934004B2 patent drawing

AI summary

A pressure control system for an environment to be pressurized includes a controller configured to calculate at least one of: a calculated pressure sensor rate of change error; and a calculated pressure sensor error. The calculated sensor rate of change error is based on a plurality of first environment air pressure signals over a first time period; and the calculated sensor error is based, over a second period of time, a difference between ambient air pressure signals and second environment air pressure signals. A processor in communication with the controller is configured to compare at least one of: the calculated pressure sensor rate of change error with at least one pressure sensor rate of change error control limit; and the calculated pressure sensor error with at least one pressure sensor error control limit. The at least one pressure sensor rate of change error control limit is based on past pressure sensor rate of change errors; and the at least one pressure sensor error control limit is based on past pressure sensor errors.