Contoured Inlet Manifold for Uniform Subfreezing Heat Exchanger Airflow

Resolve Bottlenecks,
Find Innovative Solutions
Generate Solutions

Solution Overview

Problem

Environmental control systems face inefficiencies due to non-uniform airflow distribution and sub-freezing temperatures causing ice accumulation and blockages in heat exchangers, leading to reduced performance.

Innovation Solution

A contoured inlet manifold with a reservoir and offset flow path design that gradually increases cross-sectional area, diffusing airflow uniformly across the heat exchanger inlet, preventing ice accumulation and enhancing airflow distribution.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Speed

If high velocity airflow from turbine outlet is directed to heat exchanger inlet, then cooling efficiency is improved, but non-uniform distribution causes preferential flow to only portion of inlet face reducing heat exchanger performance

Engineering Contradiction:
Improveairflow velocityVSAvoidheat exchanger performance
Core Design Contradiction:
SpeedVSProductivity

Solution Approach 1:

The inlet manifold introduces a lateral dimension to airflow distribution by creating a reservoir that spans across the width of the heat exchanger inlet. The contoured sidewalls extend in the lateral direction, forcing the airflow to distribute across the entire inlet face width rather than concentrating in a single location, thereby resolving the non-uniform distribution problem while maintaining high velocity cooling efficiency.

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

Solution Approach 2:

The inlet manifold changes the spatial parameters of airflow distribution through its contoured geometry. The sidewalls are shaped to gradually increase cross-sectional area and offset from the longitudinal axis, transforming the concentrated turbulent flow into a laterally distributed flow pattern that covers the entire heat exchanger inlet face, improving both uniformity and performance.

Inventive Principle:
Principle #35Parameter changes

2Temperature

If sub-freezing airflow from turbine is used for cooling, then cooling capacity is improved, but ice or snow accumulates on inlet face blocking portions of heat exchanger

Engineering Contradiction:
Improveairflow temperatureVSAvoidheat exchanger operability
Core Design Contradiction:
TemperatureVSReliability

Solution Approach 1:

The inlet manifold performs preliminary action by distributing and diffusing the sub-freezing airflow before it reaches the heat exchanger inlet face. The contoured reservoir and sidewalls pre-condition the flow pattern, preventing ice accumulation by ensuring uniform distribution across the entire inlet face, which eliminates localized blockages and maintains reliable operation throughout the heat exchanger.

Inventive Principle:
Principle #10Preliminary action

3Area of stationary object

If small area turbine exhaust is directed to large area heat exchanger inlet, then system compactness is improved, but airflow is non-uniformly distributed across inlet face

Engineering Contradiction:
Improveheat exchanger inlet areaVSAvoidheat exchanger efficiency
Core Design Contradiction:
Area of stationary objectVSProductivity

Solution Approach 1:

The inlet manifold resolves the area mismatch by introducing lateral dimensionality to the airflow path. The reservoir and contoured sidewalls expand the flow distribution in the lateral direction, allowing the small turbine exhaust area to effectively serve the entire large heat exchanger inlet area through three-dimensional flow management rather than simple planar expansion.

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

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 design ensures even airflow distribution, preventing blockages and improving the operational efficiency of heat exchangers by maintaining airflow uniformity and reducing ice formation.

Implementation Method 1

The intermediate portion is contoured such that the intermediate portion is offset from the longitudinal axis at the back side of the outlet portion... diffusing airflow uniformly across the heat exchanger inlet

Methodology Applied
Scientific EffectFlow diffusion: Diffusion

Implementation Method 2

Such airflows may contain ice or snow created through the expansion cooling of air through the turbine, which can accumulate on, and may block portions of inlet face of a downstream heat exchanger... preventing ice accumulation and enhancing airflow distribution

Methodology Applied
Scientific EffectIce prevention through flow management:

Data Source

PatentUS20250334354A1Contoured inlet manifold for subfreezing heat exchanger
Publication Date: 2025.10.30 HAMILTON SUNDSTRAND CORP
  • US20250334354A1 patent drawing
  • US20250334354A1 patent drawing
  • US20250334354A1 patent drawing

AI summary

A component for use in an environmental control system includes an inlet portion having a longitudinal axis, an inlet formed at the inlet portion, and an outlet portion including a front side and a back side. The front side is arranged closer to the inlet portion than the back side. An outlet is formed at the outlet portion and is arranged at a non-parallel angle relative to the inlet. An intermediate portion extends between and fluidly couples the inlet portion and the outlet portion. The intermediate portion includes a reservoir spaced laterally from the back side of the outlet portion and offset from the longitudinal axis of the inlet portion.