Multi-evaporator trans-critical cooling systems

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Solution Overview

Problem

Aircraft cooling systems face inefficiencies due to significant throttling losses and thermodynamic losses from back pressure regulators in transcritical operations, limiting their ability to maintain effective cooling across varying ambient conditions.

Innovation Solution

A multi-evaporator cooling system with a compressor circuit generating multiple levels of evaporating pressures, utilizing a heat exchanger and multiple compressors to manage refrigerant pressures and temperatures, and incorporating non-isenthalpic expansion to reduce throttling losses, allowing for efficient cooling across different heat loads within an aircraft.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Temperature

If back pressure regulators are installed downstream of each evaporator to maintain different evaporating pressures, then multi-temperature cooling is achieved, but significant throttling losses occur resulting in thermodynamic loss and reduced cooling performance

Engineering Contradiction:
Improveevaporating temperatureVSAvoidthrottling loss
Core Design Contradiction:
TemperatureVSLoss of energy

Solution Approach 1:

The patent removes the back pressure regulator component from the system entirely. Instead of using traditional isenthalpic expansion devices, the invention extracts this function by allowing the evaporators to operate at different pressures naturally through their respective heat loads and refrigerant circulation patterns, eliminating the throttling losses associated with back pressure regulators.

Inventive Principle:
Principle #2Taking out (Extraction)

Solution Approach 2:

The system changes the operating parameters by allowing each evaporator to operate at its optimal evaporating pressure and temperature independently, determined by its specific heat load requirements rather than being constrained by isenthalpic expansion through back pressure regulators. This enables non-isenthalpic expansion and reduces thermodynamic losses.

Inventive Principle:
Principle #35Parameter changes

2Adaptability or versatility

If a gas-based cooling system is used to cover the wide range of ambient operating conditions, then system adaptability is improved, but system bulk and efficiency deteriorate

Engineering Contradiction:
Improveambient condition coverageVSAvoidsystem efficiency
Core Design Contradiction:
Adaptability or versatilityVSUse of energy by moving object

Solution Approach 1:

The patent implements a dynamic system where the refrigerant circulation and heat exchange processes automatically adapt to varying ambient conditions and heat loads. The system uses multiple evaporators operating at different pressures and temperatures, with refrigerant flow dynamically adjusted through the compressors and heat exchangers to match actual cooling demands, eliminating the need for oversized gas-based equipment.

Inventive Principle:
Principle #15Dynamics

Solution Approach 2:

The system changes operating parameters by allowing each evaporator to operate at its optimal evaporating pressure and temperature independently, determined by its specific heat load requirements. This enables the system to efficiently cover a wide range of ambient conditions without the bulk and inefficiency of traditional gas-based systems.

Inventive Principle:
Principle #35Parameter changes

3Temperature

If multiple evaporators operate at significantly different evaporating pressures, then specific cooling temperatures are achieved, but back pressure regulators are required downstream of each evaporator leading to throttling losses

Engineering Contradiction:
Improvecooling temperatureVSAvoidsystem configuration
Core Design Contradiction:
TemperatureVSDevice complexity

Solution Approach 1:

The patent removes the back pressure regulator component from the system entirely. Instead of using traditional isenthalpic expansion devices, the invention extracts this function by allowing the evaporators to operate at different pressures naturally through their respective heat loads and refrigerant circulation patterns, eliminating the throttling losses associated with back pressure regulators.

Inventive Principle:
Principle #2Taking out (Extraction)

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 system achieves improved cooling efficiency by tailoring mass flow rates and compressor operations to specific heat loads, reducing thermodynamic losses and enhancing overall cooling performance across a range of ambient conditions.

Implementation Method 1

a heat exchanger configured to receive the compressed refrigerant from the at least one compressor and cool the compressed refrigerant

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 2

a first evaporator circuit configured to receive the compressed refrigerant from the heat exchanger, expand the compressed refrigerant to a second pressure that is lower than the first pressure

Methodology Applied
Scientific EffectPressure expansion: Pressure Gradient

Implementation Method 3

expand the compressed refrigerant to a second pressure that is lower than the first pressure, and return the refrigerant to the compressor circuit

Methodology Applied
Scientific EffectPhase change: Phase Change

Data Source

PatentEP2889551B1Multi-evaporator trans-critical cooling systems
Publication Date: 2020.08.05 ROLLS ROYCE CORP
  • EP2889551B1 patent drawingFigure 1A~1B
  • EP2889551B1 patent drawingFigure 2
  • EP2889551B1 patent drawingFigure 3

AI summary

A multi-evaporator cooling system (200) includes a compressor circuit (204) that generates multiple levels of evaporating pressures, the circuit (204) comprising at least one compressor (220, 222, 224) configured to compress a refrigerant to a first pressure, a heat exchanger (202) configured to receive the compressed refrigerant from the at least one compressor (220, 222, 224) and cool the compressed refrigerant, a first evaporator circuit (206) configured to receive the compressed refrigerant from the heat exchanger (202), expand the compressed refrigerant to a second pressure that is lower than the first pressure, and return the refrigerant to the compressor circuit (204), and a second evaporator circuit (208) configured to receive the compressed refrigerant from the heat exchanger (202), expand the compressed refrigerant to a third pressure that is lower than the second pressure, and return the refrigerant to the compressor circuit (204).