Reciprocating sCO2 Piston System for Sub-Megawatt Power Generation

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Solution Overview

Problem

The design and manufacturing of sub-megawatt turbomachinery for supercritical carbon dioxide (sCO2) systems pose significant challenges due to complex blade geometry, high-speed rotor dynamics, and high costs, making them commercially unviable.

Innovation Solution

A system for generating mechanical power using supercritical carbon dioxide, comprising a twin cylinder reciprocating system with a larger expansion cylinder and a smaller compression cylinder, connected by heat exchangers to manage the high-temperature and high-pressure CO2, optimizing the thermodynamic Brayton cycle for efficient power generation.

Engineering Contradictions & Design Principles

VSEngineering Contradiction Analysis

1Power

If sCO2 turbines are designed to operate at high rpms (50-100 k rpm) to compensate for low blade heights, then adequate power can be produced, but the complexity of blade geometry increases and manufacturing costs skyrocket

Engineering Contradiction:
Improvepower outputVSAvoidblade geometry complexity
Core Design Contradiction:
PowerVSDevice complexity

Solution Approach 1:

The patent replaces the traditional high-speed rotating turbine mechanism with a reciprocating piston-cylinder mechanism. This substitution eliminates the need for complex high-speed rotor dynamics, critical speed considerations, and intricate blade geometries. The reciprocating system operates at lower speeds while producing adequate power through volumetric displacement, thereby simplifying manufacturing and reducing costs.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

2Power

If sCO2 turbines spin at very high rpms to produce adequate power, then power generation is achieved, but shaft seals, bearings, and rotor dynamics become severe constraints

Engineering Contradiction:
Improvepower generationVSAvoidrotor dynamics reliability
Core Design Contradiction:
PowerVSReliability

Solution Approach 1:

The patent substitutes the high-speed rotating turbine with a reciprocating piston system that operates at much lower speeds. This eliminates the severe constraints associated with high-speed rotor dynamics, including shaft seal reliability, bearing life, and critical speed issues. The reciprocating mechanism achieves reliable power generation through simple, robust components that operate within acceptable mechanical limits.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

3Power

If sub-megawatt sCO2 turbomachinery is designed with watchmaker's precision, then adequate power can be produced, but the cost skyrockets making it commercially unviable

Engineering Contradiction:
Improvepower outputVSAvoidmanufacturing cost
Core Design Contradiction:
PowerVSEase of manufacture

Solution Approach 1:

The patent replaces the precision-critical high-speed turbine with a reciprocating piston system that tolerates standard manufacturing variations. The reciprocating mechanism does not require the same level of dynamic balancing, shaft alignment, and component precision as high-speed turbines. This substitution dramatically reduces manufacturing costs and improves commercial viability while maintaining adequate power output.

Inventive Principle:
Principle #28Mechanics substitution (Replace mechanical system)

4Shape

If sCO2 expands from 210 bar to 0.05 bar in a steam turbine, then large change in density occurs facilitating larger blade heights, but the turbine size becomes very large

Engineering Contradiction:
Improveblade heightVSAvoidturbine size
Core Design Contradiction:
ShapeVSVolume of moving object

Solution Approach 1:

The patent changes the operating parameters of the sCO2 cycle, specifically operating at higher minimum pressures (avoiding expansion to 0.05 bar). This parameter change results in smaller density ratios across the expansion device, which allows for more compact reciprocating cylinder designs. The reciprocating system accommodates these parameter changes efficiently, achieving compact sizes suitable for sub-megawatt applications.

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

The proposed system achieves efficient mechanical power generation with improved thermal efficiencies and reduced costs by optimizing the design of the twin cylinder system and heat exchanger configuration, addressing the challenges of sub-megawatt sCO2 turbomachinery.

Implementation Method 1

A heat exchanger is provided between the compression cylinder and the expansion cylinder. The heat exchanger cools the CO2 received from the expansion cylinder.

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Implementation Method 2

The compression cylinder pressurizes the CO2 cooled by the first heat exchanger.

Methodology Applied
Scientific EffectCompression: Compression

Implementation Method 3

The sCO2 received from the outlet port of the compression cylinder expands in the expansion cylinder to drive a piston to generate mechanical energy.

Methodology Applied
Scientific EffectThermal energy conversion to mechanical energy: Heat Engine

Implementation Method 4

A second heat exchanger is provided between the compression cylinder and the expansion cylinder. The second heat exchanger heats the sCO2 received from the outlet port of the compression cylinder.

Methodology Applied
Scientific EffectHeat transfer: Heat Exchanger

Data Source

PatentUS12270319B2System and a method for generating mechanical power using super critical carbon dioxide
Publication Date: 2025.04.08 INDIAN INSTITUTE OF SCIENCE
  • US12270319B2 patent drawing
  • US12270319B2 patent drawing
  • US12270319B2 patent drawing

AI summary

A system for generating mechanical power using super critical carbon dioxide (sCO2) is disclosed. The system includes at least one expansion cylinder (5) housing a first piston (5a) and at least one compression cylinder (6) housing a second piston (6a). A first heat exchanger (C) is fluidically connected to the compression cylinder (6) and the expansion cylinder (5), and a second heat exchanger (H) is fluidically connected to the compression cylinder (6) and the expansion cylinder (5). The first heat exchanger (C) cools the CO2 received from the expansion cylinder (5), and the compression cylinder (6) pressurizes the CO2 cooled by the first heat exchanger (C). The second heat exchanger (H) heats the CO2 from the compression cylinder (6) and supplies to the expansion cylinder (5). The high temperature and high-pressure CO2 drives the first piston (5a) housed inside the expansion cylinder (5) to generate mechanical energy.