Aircraft Duct Velocity Mapping for Sensor Placement

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Solution Overview

Problem

Complex duct systems in aircrafts with varying airflow velocities and eddy currents lead to inaccurate airflow measurements, resulting in suboptimal performance of environmental control systems, where equipment may overheat and cabin temperature control issues arise due to inconsistent airflow distribution.

Innovation Solution

A velocity mapping system comprising a sensor system and an airflow mapper that generates data on airflow velocities across duct systems, creating profiles to accurately map airflow velocities and account for variations, enabling better sensor placement and airflow management.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If an airflow sensor is placed in a location where an eddy current occurs, then the sensor can be installed in complex duct configurations, but the velocity measurement accuracy deteriorates

Engineering Contradiction:
Improvesensor placement flexibilityVSAvoidvelocity measurement accuracy
Core Design Contradiction:
Adaptability or versatilityVSMeasurement precision

Solution Approach 1:

The system performs preliminary velocity measurements at multiple candidate locations before final sensor placement. By预先 measuring velocity profiles across the duct cross-section and identifying eddy current regions, the system can select optimal sensor locations that avoid measurement errors while maintaining placement flexibility in complex duct configurations

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The system uses velocity profile measurements to provide feedback on measurement quality at different locations. By continuously monitoring velocity data and comparing it against expected flow patterns, the system can identify locations with eddy currents or measurement errors and adjust sensor placement or data weighting accordingly

Inventive Principle:
Principle #23Feedback

2Measurement precision

If multiple velocity measurements are taken across the duct cross-section, then measurement accuracy improves, but system complexity increases

Engineering Contradiction:
Improveairflow velocity measurement accuracyVSAvoidmeasurement system complexity
Core Design Contradiction:
Measurement precisionVSDevice complexity

Solution Approach 1:

The duct cross-section is divided into multiple measurement zones or segments, with velocity measurements taken at representative points in each segment. This segmentation approach captures the velocity profile variation across the duct while using a manageable number of measurement points, avoiding the need for continuous or excessively dense measurement networks

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system uses velocity profile data from one or more measurement planes to create representative models or copies of the overall flow pattern. By analyzing velocity ratios and profile shapes at strategic locations, the system can infer characteristics of the entire duct flow without requiring direct measurement at every point, reducing system complexity while maintaining accuracy

Inventive Principle:
Principle #26Copying

Data Source

PatentUS9523703B2Velocity profile mapping system
Publication Date: 2016.12.20 THE BOEING CO
  • US9523703B2 patent drawing
  • US9523703B2 patent drawing
  • US9523703B2 patent drawing

AI summary

A velocity mapping system comprising a sensor system and an airflow mapper. The sensor system is configured to generate data about a velocity of airflow for a location in a duct system. The airflow mapper is configured to receive the data from the sensor system and generate a profile of the velocity of the airflow at the location in the duct system.