Methods and device for mixing airflows in environmental control systems

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Solution Overview

Problem

In aircraft environmental control systems, turbulent mixing of trim air and conditioned air does not uniformly mix airflows before temperature measurement, leading to inaccurate temperature readings and inefficient use of trim air, which affects fuel burn efficiency.

Innovation Solution

A mixing device with a duct and guide vanes is positioned within the air supply duct to induce rotation of airflows, creating a helical vortex that improves mixing between the trim air and conditioned air, allowing for more accurate temperature measurements and precise trim air injection.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Device complexity

If turbulent mixing is used to mix trim air and conditioned air, then mixing occurs without additional components, but the mixing is not uniform before temperature measurement

Engineering Contradiction:
Improvemixing device complexityVSAvoidtemperature measurement accuracy
Core Design Contradiction:
Device complexityVSMeasurement precision

Solution Approach 1:

The duct is segmented into multiple sections with guide vanes positioned at specific locations to create staged mixing. The guide vanes divide the airflow into multiple streams that are gradually mixed through rotation, ensuring uniform mixing before the temperature sensor location.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

Guide vanes are introduced as intermediary components between the trim air injection point and the temperature sensor. These vanes act as mediators that induce rotational flow and enhance mixing without requiring complex mechanical mixing devices.

Inventive Principle:
Principle #24Intermediary (Mediator)

2Measurement precision

If the duct temperature sensor is positioned far from the trim air injection point, then there is more space for mixing, but heat loss through the duct increases leading to low temperature measurements

Engineering Contradiction:
Improvetemperature measurement accuracyVSAvoidheat loss through duct
Core Design Contradiction:
Measurement precisionVSLoss of energy

Solution Approach 1:

Mixing is performed preliminarily within a compact mixing section using guide vanes that induce rapid rotational mixing. This preliminary mixing action ensures uniform temperature distribution before the air reaches the temperature sensor, eliminating the need for long duct sections and reducing heat loss.

Inventive Principle:
Principle #10Preliminary action

Solution Approach 2:

The mixing process transitions from relying on longitudinal duct length to using a transverse rotational dimension. Guide vanes create helical flow patterns that mix air in the radial direction, allowing complete mixing within a shorter axial distance and reducing heat loss opportunities.

Inventive Principle:
Principle #17Another dimension (Dimensionality change)

3Measurement precision

If additional trim air is injected to compensate for low temperature measurements, then the measured temperature increases, but bleed air usage increases and fuel efficiency decreases

Engineering Contradiction:
Improvetemperature measurement accuracyVSAvoidfuel burn efficiency
Core Design Contradiction:
Measurement precisionVSLoss of energy

Solution Approach 1:

The system implements feedback control where the temperature sensor provides accurate measurements of the mixed air temperature. This accurate feedback allows the control system to precisely adjust trim air injection to maintain the desired temperature without over-compensation, optimizing fuel efficiency.

Inventive Principle:
Principle #23Feedback

Solution Approach 2:

The guide vanes change the flow parameters by inducing rotation and enhancing turbulence. This parameter change accelerates the mixing process, ensuring uniform temperature distribution reaches the sensor quickly, which enables accurate feedback control and prevents excessive trim air injection.

Inventive Principle:
Principle #35Parameter changes

4Adaptability or versatility

If turbulent mixing is relied upon, then no additional mixing components are needed, but the position of trim air injection is limited to long straight portions of ducting

Engineering Contradiction:
Improveinjection position flexibilityVSAvoidduct configuration requirements
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The duct is divided into a mixing section with guide vanes and a measurement section. This segmentation allows the mixing function to be performed in a dedicated compact section, freeing the injection position from requiring long straight duct portions and enabling installation in various duct configurations.

Inventive Principle:
Principle #1Segmentation

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 solution facilitates uniform and complete mixing of airflows, enabling more accurate temperature measurements, reducing heat loss, and optimizing trim air usage, thereby enhancing fuel burn efficiency and minimizing ducting requirements.

Implementation Method 1

The guide vanes are configured to induce rotation of the first and second airflows flowing through the duct

Methodology Applied
Scientific EffectVortex: Vortex Ring

Implementation Method 2

the airflow turbulence in the duct mixes the airflows

Methodology Applied
Scientific EffectTurbulence: Turbulence

Data Source

PatentUS9783309B2Methods and device for mixing airflows in environmental control systems
Publication Date: 2017.10.10 THE BOEING CO
  • US9783309B2 patent drawing
  • US9783309B2 patent drawing
  • US9783309B2 patent drawing

AI summary

Methods and a device for mixing airflows in an environmental control system are provided. The device includes a duct configured to receive a first airflow and a second airflow, and a plurality of guide vanes disposed within said duct. The guide vanes are configured to induce rotation of the first and second airflows flowing through the duct.