Project Details
Description
OFELIA is a Project, which deals with "Ultra Efficient Propulsion" for short and short-medium-range aircraft. The following topics shall be dressed:
• Demonstrate one engine architecture compatible with SR/SMR aircraft architecture.
• Fuel-efficiency improvement of no less than 20% at the engine level, with a quantified reduction in installed TSFC (if applicable), CO2 and all other relevant GHG emissions, and full adaptability to 100% (non-blended) SAF.
• Activities are expected to achieve TRL 5 by the end of the project.
• Synergies with other EC/CAJU initiatives/programs are expected.
A number of top-level goals will be the basis for performance targets.
• No less than a 20% reduction in fuel burn and related emissions at an overall propulsion system level
• Engine/installed performance compliant with the aircraft performance
• The target of 30% fuel burn reduction (to be extended as much as possible to a target of 30% GHG emissions reduction at aircraft level
• All noise and emission levels resulting from the projects are consistent with currently foreseen regulations and standards.
• Weight constraints of the overall propulsion system so as to minimize the propulsion weight ratio to the operation empty weight.
• Compatible with safety as an overarching requirement.
The task of TU-Graz is to study and evaluate novel turbine architectures for these highly efficient aircraft designs. In particular, the large-scale test rigs, which are unique in Europe, will be used.
Status | Active |
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Effective start/end date | 1/11/22 → 31/12/25 |
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