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Combined-Cycle Engines
(CCE) for next generation
passenger aircraft
Background
The aerospace industry is exploring
novel concepts to highly increase
overall efficiency of civil aircraft
engines.
Proposed concept
Implementation of a waste recovery
unit based on supercritical CO2
technology.
Thermodynamics
• Preliminary component design
• Optimization of the ScCO2 recovery
unit
Engineering
• Weight assessment
• Investigation on novel aircraft
configurations
• CCE simulation along the entire
mission
Master Thesis: Federico Ghezze
Department: AWEP
Section: Flight Performance and Propulsion
Supervisor: L.Azzini, C.M. De Servi, A. Gangoli Rao,
Promoter: P. Colonna,
Starting date: 01/12/2014
Funding: TUDelft Aerospace faculty
Email: P.Colonna@tudelft.nl
Type: Engineering
AerospaceEngineering
Final goal
• Integrated optimization of the
CCE
Core
Nozzle
Duct
Nozzle
HPTLPC HPC LPTFAN
Fuel
Inlet
Combustion
chamber
CO2
System
TC
Electrica
l fan
MHERegenerato
r
Cooler
References
[1] Angelino, G. , Carbon dioxide condensation cycles for power
production, Journal of Engineering for Power, pages 287-295
, July 1968
Up to 15% fuel savings from the thermodynamic analysis
[2] Perullo, C. A. , Mavris, D. N. , Fonseca, E. , An integrated
assessment of an organic rankine cycle concept , Proceedings of
ASME Turbo Expo 2013, June 3-7, San Antonio, Texas, USA
Why Supercritical Carbon Dioxide?
MHECooler
A
A
Core
B
B
A-A
B-B High power density, more compact
components
 Thermal stability at high
temperatures
 High cycle efficiency
 Environmental friendly
Required:
 Innovative component design

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poster_LAzzini_co2

  • 1. Combined-Cycle Engines (CCE) for next generation passenger aircraft Background The aerospace industry is exploring novel concepts to highly increase overall efficiency of civil aircraft engines. Proposed concept Implementation of a waste recovery unit based on supercritical CO2 technology. Thermodynamics • Preliminary component design • Optimization of the ScCO2 recovery unit Engineering • Weight assessment • Investigation on novel aircraft configurations • CCE simulation along the entire mission Master Thesis: Federico Ghezze Department: AWEP Section: Flight Performance and Propulsion Supervisor: L.Azzini, C.M. De Servi, A. Gangoli Rao, Promoter: P. Colonna, Starting date: 01/12/2014 Funding: TUDelft Aerospace faculty Email: P.Colonna@tudelft.nl Type: Engineering AerospaceEngineering Final goal • Integrated optimization of the CCE Core Nozzle Duct Nozzle HPTLPC HPC LPTFAN Fuel Inlet Combustion chamber CO2 System TC Electrica l fan MHERegenerato r Cooler References [1] Angelino, G. , Carbon dioxide condensation cycles for power production, Journal of Engineering for Power, pages 287-295 , July 1968 Up to 15% fuel savings from the thermodynamic analysis [2] Perullo, C. A. , Mavris, D. N. , Fonseca, E. , An integrated assessment of an organic rankine cycle concept , Proceedings of ASME Turbo Expo 2013, June 3-7, San Antonio, Texas, USA Why Supercritical Carbon Dioxide? MHECooler A A Core B B A-A B-B High power density, more compact components  Thermal stability at high temperatures  High cycle efficiency  Environmental friendly Required:  Innovative component design