2020:
Novel cycle concepts identification to get TRL6 in 2035 and 2050, with associated system evaluation and roadmap.
Innovative components of these novel cycles evaluation with laboratory "proof of concept" in collaboration with universities, research centers or SME.
2035:
Advanced Turbofan novel cycles needing demonstration for TRL6 in 2035:
* Intercooled and recupareted cycles with breakthrough heat exchanger device.
* Variable confluence/variable by-pass turbofan demonstration.
* Novel cycles including varable air system (cooling and sealing) for fuel consumption and emission optimlization
Advanced turboshaft/turboprop/APU novel cycles needing demonstration for TRL6 in 2035:
* Turboshaft/Turboprop/APU with exhaust thermal recovery (heat exchanger beakthrough technology, bottom cycles,)
* Constant thermodynamical cycle with variable geometry.
* Compound turbine / piston engines.
2050:
* Cycles with interturbine reheat: innovative combustion device for low pressure drop in flowpath.
* Innovative combustion cycles: constant volume deflagration, detonation, Flameless,
* Compound turbine / hot temperature fuel cell.
