This website uses cookies
More information
Navigate directly to favourite company, aircraft and sector pages with our tracker feature.
Consortium proves the concept for fuselage wake-filling propulsion
Wednesday, 4 August 2021
The positive effect of “wake-filling” on propulsive power has long been known in marine applications. Ship propellers are typically located aft and operated within the boundary layer flow close to the ship’s surface.

The so-called Propulsive Fuselage Concept (PFC) has the potential to play a key role in developing more efficient and less polluting aircraft of the future.

After three-and-a-half years of research, the consortium of the European-funded Centreline project has managed to complete the proof of concept and experimental validation for this highly promising technology thereby maturing it to Technology Readiness Level (TRL) 3 and bringing it closer to a possible industrial uptake in the future.

The turbo-electric PFC aircraft for 340 passengers produces 4.7% less CO2 emissions compared to an equally advanced conventional aircraft. In addition to the two gas turbines on the wings, an electric fan is located at the aft-fuselage to produce thrust by ingesting and re-energising the airflow around the fuselage. The PFC configuration features excellent compatibility with other advanced technologies including hydrogen fuel technology.

The European Green Deal seeks to achieve a 90% reduction in transport emissions by 2050. This is a huge challenge for aviation requiring cutting-edge new technologies and innovations to make this happen. In enabling aviation's long-term sustainability, novel propulsion technology and propulsion-airframe integration play a key role. A yet untapped source of further efficiency improvements is associated with fuselage wake-filling propulsion integration, i.e., the ingestion and re-energisation of the fuselage boundary layer flow by the propulsion system. The positive effect of “wake-filling” on propulsive power requirements has long been known from the field of marine propulsion. Ship propellers are typically located at the aft body of the vessel and operated within the boundary layer flow close to the ship’s body surface. This physical principle is also applicable to airborne propulsion, as the 11 Centreline partners of six European countries have just proven.

"We have successfully tackled the immediate challenges that are associated with fuselage wake-filling propulsion integration. With the proof of concept performed in Centreline, we have lifted this cutting-edge technology to the next level. Our achievement may represent an important steppingstone on the way to preparing “Propulsive Fuselage” technology for a possible aircraft product development in the future”, says project coordinator Arne Seitz of Bauhaus Luftfahrt e.V. “In order to support any follow-on research and innovation activities, we have devised a roadmap for the PFC aircraft technology towards TRL 6 by the year 2030. As a further enhancement of its innovative potential, we have identified a set of further advanced technologies that feature excellent compatibility with the PFC aircraft configuration. All this was enabled by a great collaborative spirit and excellent individual contributions from the partners in the project.”

The scientific and technological development outcomes from Centreline are highly relevant for follow-on research and innovation activities. This is the result of the methodological advancements and systems design knowledge developed as well as due to the synergistic compatibility of fuselage wake-filling propulsion integration with other promising technologies, such as revolutionary core engines (such as the Composite cycle Engine, CCE), High-Temperature Superconducting (HTS) technology, ultra-efficient wing technologies (such as Natural Laminar Flow, NLF, wings as demonstrated by the BLADE demonstrator in Clean Sky, and, liquid hydrogen (LH2) fuel technology.

The Centreline partners maximised the benefits of aft-fuselage wake-filling under realistic systems design and operating conditions. A thorough understanding of the aerodynamic effects of 360° fuselage boundary layer ingestion was developed through extensive aero-numerical simulations and low-speed wind tunnel and fan rig testing. All detailed design and analysis results were incorporated in a multi-disciplinary aircraft family pre-design and the PFC technology was rigorously benchmarked against a similarly advanced but conventional aircraft. The evaluation was performed for the impactful mid-to-long range air transport task featuring 340 passengers and 6500 nmi (~12,000 km)design range in the year 2035. It shows -4.7% CO2 for the turbo-electric PFC against the advanced reference aircraft or -36% relative to a year 2000 baseline. PFC NOx (Nitrogen Oxides) emissions during the ICAO Landing and Take-off (LTO) cycle are reduced by 1.8% relative to the year 2035 reference, and by 41% compared to the year 2000 baseline. During cruise (high-level), the PFC aircraft may cut NOx emissions by 20% and 64% against year 2035 and 2000 standards, respectively.

The Centreline project stands for “ConcEpt validatioN sTudy foR fusElage wake-filLIng propulsioN intEgration” and was funded with 3.7 million euros by the European Union under the Horizon 2020 framework programme. Coordinated by Bauhaus Luftfahrt, the Centreline project consortium comprised 11 partners from six European countries. Beside Bauhaus Luftfahrt, these included four leading industry partners, namely Airbus Defence and Space, Airbus Operations, MTU Aero Engines, Rolls-Royce and Siemens, as well as four reputable European universities, namely Chalmers University of Technology, Delft University of Technology, the University of Cambridge and Warsaw University of Technology, supported by the management consulting partners ARTTIC Innovation GmbH and ARTTIC SAS.

Contact details from our directory:
Bauhaus Luftfahrt e.V. Research/Consulting Services
Airbus Defence & Space (Cassidian) Research/Consulting Services
MTU Aero Engines Additive Manufacturing, Blisks, Combustion Test Services, Compressors, Engine Parts, Final Assembly, Fuel Cells, Turbine Engine Blades, Turbine Engine Starters, Turbine Engine Vanes
Rolls-Royce Electrical (was Siemens eAircraft) Electric Batteries, Electric Engines, Electric Motors, Storage Batteries
Related directory sectors:
Design