WP1.1 Overall specification and assessment

Current activities

The cooperation process between SPs defined in 2009 has been successfully tested on SP3 reference direct drive engine.

A close cooperation between Airbus and SP1 OEMs is ongoing to ensure a fair and complete understanding of fuel burn computations regarding advanced turbofan engine linked to SP4 activities.

Results & achievements

Through an active cooperation involving all SPs partners, a detailed assessment process was defined to make a clear, fair and complete comparison of all engine architectures benefits vs Year 2000 engine configurations.

This assessment process covers fuel burn (metrics for pollutioin and economis), and noise on the certification points.

WP1.2 TERA2020

The W1.2 activities were focused on the adaptation of the TERA2020 techno-environment assessment tool to the novel concepts studied, particularly open rotor engines.

Results & achievements

The final DREAM TERA2020 simulation platform was successfully completed and integrated in iSight.

It includes innovative simulation modules capable of estimating engine performance, noise (on FAR points), engine weight, aircraft mission and gaseous emissions for different geared and direct drive open rotor engine designs.

The models were successfully verified against available data and OEM experience.

The TERA2020 platform is currently being used to perform sensitivity analysis and trade off studies regarding fuel burn, emissions and noise.

The noise module (called TENOR) is based on unsteady CFD calculations and captures the interaction between propellers.

The picture on the left shows the pressure field between rotors and we can see the wakes of the front rotor impacting in the rear rotor.

The picture on the right shows the noise spectrum in the 3 FAR certification points. It can be seen that both tone and broaband noise are captured by the model.

 The high-level objective of SP1 is to ensure the overall consistency of DREAM results and to assess the DREAM engine technologies and architectures benefits to mature technologies that offer the potential to go beyond the ACARE objectives for SFC. SP1 will federate both specification and assessment of each architecture concept, from the common point of view of aircraft environmental technical and economic objectives.
 
 
The technical objectives of SP1 are to :
  • Define the aircraft application context for DREAM engine concepts, both for innovative open rotors architectures and advanced conventional turbofan technologies
  • Provide peak requirement and objectives of each different DREAM engine technology
  • Compare, assess and rank the advanced propulsion systems investigated within DREAM by their techno-economic potential whilst achieving environmental goals
  • Establish how the propulsion system compare to the ACARE goals
  • Assess the possible shortfalls
  • Develop and adjust a previously created software tool (TERA2020) to compare the technical and environmental impact of the various engine architectures studied in DREAM, and use it to advise industry and public bodies, such as legislators.