Multi-Zone Aircraft Cooling Loops Without Large Air Ducting

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Solution Overview

Problem

Existing environmental control systems in vehicles, such as aircraft, face limitations in the number and spatial distribution of zones due to the size and complexity of ducting required for temperature control, and inefficiencies in cooling air to specific temperature targets.

Innovation Solution

The system employs a refrigerant circuit with a pump segment and an evaporator, along with a coolant circuit that has parallel segments for heat transfer between zones, using a controller to throttle coolant flow independently to each zone, and utilizes heat recovery from other vehicle systems to improve efficiency.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If air is cooled to the temperature required for the zone with the lowest temperature requirement and then mixed with warmer air for other zones, then temperature control for multiple zones is achieved, but ducting size and pressure drop increase, limiting the number and spatial distribution of zones

Engineering Contradiction:
Improvenumber of zonesVSAvoidducting size
Core Design Contradiction:
Adaptability or versatilityVSDevice complexity

Solution Approach 1:

The coolant circuit is divided into multiple independent loops, with each loop serving a specific zone. Each loop includes its own pump, heat exchanger, and flow control valve, allowing independent temperature control for each zone without requiring large ducting systems to distribute conditioned air.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The patent transitions from air-based thermal management to liquid coolant-based systems. Liquid coolant circuits with pumps and heat exchangers replace traditional air ducting, enabling more efficient heat transfer and eliminating the need for large-volume air distribution ducts throughout the vehicle.

Inventive Principle:
Principle #29Pneumatics and hydraulics

2Adaptability or versatility

If air is cooled to the temperature required for the zone with the lowest temperature requirement, then all zones can be served, but efficiency losses occur due to over-cooling and subsequent mixing with warmer air

Engineering Contradiction:
Improvetemperature control capabilityVSAvoidcooling efficiency
Core Design Contradiction:
Adaptability or versatilityVSLoss of energy

Solution Approach 1:

Each zone has its own dedicated coolant loop with independent flow control, allowing each zone to receive coolant at the specific temperature and flow rate required for its local thermal conditions. This eliminates the need to over-cool air for the coldest zone and then mix it with warmer air for other zones.

Inventive Principle:
Principle #3Local quality

Solution Approach 2:

The system employs dynamically controllable flow rates and temperatures in each coolant loop through electronic control of pumps and flow control valves. This allows real-time adjustment of cooling parameters for each zone based on actual thermal demands, optimizing energy efficiency while maintaining adaptability.

Inventive Principle:
Principle #15Dynamics

3Temperature

If traditional environmental control systems are used with ducting, then temperature control is provided, but the spatial distribution and number of controllable zones are limited

Engineering Contradiction:
Improvetemperature controlVSAvoidspatial distribution of zones
Core Design Contradiction:
TemperatureVSAdaptability or versatility

Solution Approach 1:

Liquid coolant circuits with flexible hoses and compact heat exchangers replace rigid air ducting systems. This hydraulic approach enables coolant delivery to multiple zones throughout the vehicle interior without the spatial constraints of air duct routing, significantly improving the spatial distribution capability and number of controllable zones.

Inventive Principle:
Principle #29Pneumatics and hydraulics

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

This approach allows for temperature control in multiple zones without the need for ducts, reduces efficiency losses by throttling coolant flow, and powers the refrigeration segment using waste heat, enhancing overall system efficiency.

Implementation Method 1

an evaporator arranged along the evaporator segment and in fluid communication with of the refrigerant circuit, and a coolant circuit. The coolant circuit extends through the evaporator and is thermally coupled to refrigerant circuit by the evaporator

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 2

The refrigerant is in a liquid state in a first portion of the refrigerant circuit, and that the refrigerant is in a vapor state in a second portion of the refrigerant circuit

Methodology Applied
Scientific EffectPhase change: Phase Change

Implementation Method 3

the coolant circuit including a first segment and a second segment arranged in parallel with one another to transfer heat from a first zone to a first portion of liquid coolant traversing the coolant circuit, and transfer additional heat from a second zone to a second portion of coolant traversing the coolant circuit

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Data Source

PatentUS11780295B2Aircraft multi-zone environmental control systems
Publication Date: 2023.10.10 HAMILTON SUNDSTRAND CORP
  • US11780295B2 patent drawing
  • US11780295B2 patent drawing
  • US11780295B2 patent drawing

AI summary

An environmental control system includes a refrigerant circuit with a pump segment and an evaporator segment, an evaporator arranged along the evaporator segment and in fluid communication with of the refrigerant circuit, and a coolant circuit. The coolant circuit extends through the evaporator and is thermally coupled to refrigerant circuit by the evaporator, the coolant circuit including a first segment and a second segment arranged in parallel with one another to transfer heat from a first zone to a first portion of liquid coolant traversing the coolant circuit and transfer additional heat from a second zone to a second portion of coolant traversing the coolant circuit. Aircraft and environmental control systems are also described.