Development of a High Efficiency Axial Inflow Turbine for Application on a Downsized Gasoline Engine

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Title
Development of a High Efficiency Axial Inflow Turbine for Application on a Downsized Gasoline Engine

CoPED ID
af6208be-ff88-4eaa-aeb0-56277a7a347d

Status
Closed

Funders

Value
No funds listed.

Start Date
Sept. 30, 2018

End Date
Sept. 29, 2021

Description

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Project Aim:
The research proposed aims to bring an integrated approach to deliver innovation through two novel concepts (a Variable Geometry Turbine and a Fixed Geometry Turbine), both based on axial turbine technology. The two concepts proposed aim to offer a unique gasoline engine variable geometry and dedicated pulsating flow energy recovery benefits, leading in both cases to improved turbine total-to-static efficiency, lower inertia, improved "time to torque", and improved fuel consumption and emissions, compared to conventional designs. As such the specific aims of the project are:
To understand the fundamental limits of exploitation of the inherent advantages of the two novel, axial turbine concepts and ensure that the underlying science is applied in their design process to achieve higher levels of gasoline engine exhaust energy recovery and reduced fuel consumption compared to established technologies.
To assess the viability of the concepts in providing VGT capability and superior pulsating flow performance for modern gasoline engines but also beyond and across the range of turbocharged ICE applications.
Project objectives:
1. To achieve levels of fuel efficiency equal to or higher than 2% for both of the proposed systems compared to established radial and mixed-flow turbines.
2. To evaluate the viability of the concepts and understand the real-world issues that will affect advanced axial turbocharger turbine concepts, through realistic on-engine testing.
3. To evaluate the validity of methods and viability of the concepts through standalone testing of the two concept turbochargers at the standalone test facility
4. To optimise the design of the two proposed, advanced axial turbocharger turbine concepts prior to experimental validation.
5. To inform and further develop the modelling methodologies applied in the in-house code to better predict axial turbocharger turbine performance.
6. To understand the issues affecting axial turbine efficiency under realistic (pulsating, hot) exhaust flow and to understand the issues affecting the scaling of the technologies proposed

APOSTOLOS PESYRIDIS SUPER_PER
Gregory Guarda STUDENT_PER

Subjects by relevance
  1. Turbines
  2. Fuels
  3. Energy consumption (energy technology)
  4. Motors and engines
  5. Petrol engines
  6. Emissions
  7. Optimisation
  8. Gas turbines
  9. Projective geometry
  10. Energy efficiency
  11. Combustion engines
  12. Innovations

Extracted key phrases
  1. High Efficiency Axial Inflow Turbine
  2. Advanced axial turbocharger turbine concept
  3. Axial turbine concept
  4. Axial turbocharger turbine performance
  5. Axial turbine efficiency
  6. Variable Geometry Turbine
  7. Axial turbine technology
  8. Gasoline engine exhaust energy recovery
  9. Concept turbocharger
  10. Novel concept
  11. Unique gasoline engine variable geometry
  12. Flow turbine
  13. Development
  14. Project aim
  15. Flow energy recovery benefit

Related Pages

UKRI project entry

UK Project Locations