Staged Heat Pump Cooling Loop for Lightweight Aircraft Thermal Control

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Solution Overview

Problem

Current aircraft thermal management systems are inefficient due to standalone vapor cycle units that are heavy, power-intensive, and require multiple units to meet cooling demands, leading to increased weight and reduced aircraft efficiency.

Innovation Solution

A thermal management system with a fluid loop connecting multiple climate-controlled regions and featuring staged climate control through a series of heat pumps, allowing for distributed heating or cooling and reduced fluid volume requirements.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Adaptability or versatility

If multiple standalone vapor cycle units are used to meet cooling demands in different regions, then cooling coverage is improved, but system weight and power consumption increase

Engineering Contradiction:
Improvecooling coverageVSAvoidsystem weight
Core Design Contradiction:
Adaptability or versatilityVSWeight of moving object

Solution Approach 1:

The patent combines multiple standalone vapor cycle units into a single centralized thermal management system that serves multiple climate-controlled regions. The centralized system includes one compressor, one condenser, one expansion device, and one evaporator that collectively provide cooling to multiple regions through a shared refrigerant loop, thereby reducing overall system weight while maintaining comprehensive cooling coverage.

Inventive Principle:
Principle #5Merging (Combining)

Solution Approach 2:

The centralized thermal management system performs multiple cooling functions for different climate-controlled regions simultaneously through a single system. The refrigerant is distributed to multiple evaporators located in different regions, allowing one system to fulfill the roles of multiple standalone units, thus improving adaptability and versatility without proportionally increasing weight.

Inventive Principle:
Principle #6Universality (Multi-functionality)

2Device complexity

If centralized vapor cycle units are positioned at one location to cool multiple regions, then system complexity is reduced, but system weight increases due to larger refrigerant requirements

Engineering Contradiction:
Improvesystem complexityVSAvoidsystem weight
Core Design Contradiction:
Device complexityVSWeight of moving object

Solution Approach 1:

The patent segments the centralized thermal management system into modular components including the compressor, condenser, expansion device, evaporator, and multiple distribution loops. Each component is optimized for its specific function, and the system uses staged cooling with intermediate heat exchangers to reduce refrigerant volume requirements in each segment, thereby reducing overall system weight while maintaining centralized operation.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system employs staged cooling that changes refrigerant parameters (temperature and pressure) at different stages of the cooling process. By using intermediate heat exchangers and expansion devices at different points in the refrigerant loop, the system optimizes refrigerant density and volume at each stage, reducing the total refrigerant quantity needed compared to a single-stage centralized system.

Inventive Principle:
Principle #35Parameter changes

3Ease of operation

If standalone vapor cycle units are used for each region, then regional temperature control is improved, but aircraft efficiency decreases due to increased weight

Engineering Contradiction:
Improveregional temperature controlVSAvoidaircraft efficiency
Core Design Contradiction:
Ease of operationVSProductivity

Solution Approach 1:

The patent merges multiple regional cooling systems into a single centralized thermal management system that maintains the ability to independently control temperature in each climate-controlled region. The system uses a shared refrigerant loop with distribution to multiple evaporators, providing regional temperature control independence while consolidating system components to reduce weight and improve aircraft efficiency.

Inventive Principle:
Principle #5Merging (Combining)

4Power

If larger vapor cycle units are used to meet total cooling demand, then cooling capacity is improved, but system weight and refrigerant volume increase

Engineering Contradiction:
Improvecooling capacityVSAvoidsystem weight
Core Design Contradiction:
PowerVSWeight of moving object

Solution Approach 1:

The patent segments the total cooling capacity into multiple smaller cooling stages distributed along the refrigerant loop. Instead of using one large evaporator, the system uses multiple evaporators and intermediate heat exchangers that provide cooling in stages, allowing the total cooling capacity to be achieved with smaller, lighter components distributed throughout the system.

Inventive Principle:
Principle #1Segmentation

Solution Approach 2:

The system changes refrigerant parameters through staged expansion and cooling processes. By using multiple expansion devices and heat exchangers at different stages, the refrigerant progressively changes temperature and pressure, extracting cooling capacity incrementally at each stage. This approach achieves high total cooling capacity while using less refrigerant volume and lighter components compared to a single large-stage system.

Inventive Principle:
Principle #35Parameter changes

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 solution provides a more efficient and lighter thermal management system by maintaining a constant supply temperature across regions, reducing the overall weight of the aircraft and simplifying installation and removal of heat pump units.

Implementation Method 1

a first heat pump thermally connected to the fluid loop and disposed between the outlet of the second heat exchanger and the inlet of the first heat exchanger; and a second heat pump thermally connected to the fluid loop

Methodology Applied
Scientific EffectHeat transfer: Conduction (thermal)

Implementation Method 2

a first heat exchanger having an inlet and an outlet; a second heat exchanger having an inlet and an outlet; a fluid loop for circulating a fluid

Methodology Applied
Scientific EffectHeat exchange: Heat Exchanger

Data Source

PatentEP1849704B1Thermal management system with staged cooling
Publication Date: 2009.12.02 HAMILTON SUNDSTRAND CORP
  • EP1849704B1 patent drawingFigure 1
  • EP1849704B1 patent drawingFigure 2
  • EP1849704B1 patent drawingFigure 3

AI summary

A thermal management system (20A) comprises a first heat exchanger (66) having an inlet (30) and an outlet (32), a second heat exchanger (74) having an inlet (34) and an outlet (36), a fluid loop (25), a first heat pump (22), and a second heat pump (24). The fluid loop circulates a fluid, and forms a continuous path between the first and second heat exchangers. The first heat pump is thermally connected to the fluid loop and is disposed between the outlet of the second heat exchanger and the inlet of the first heat exchanger. The second heat pump is thermally connected to the fluid loop and is disposed between the outlet of the first heat exchanger and the inlet of the second heat exchanger.