Sustainable Water-Injecting Turbofan Comprising Hybrid-electrics

Informazioni relative al progetto

SWITCH

ID dell’accordo di sovvenzione: 101102006

DOI

10.3030/101102006

Data della firma CE 9 Dicembre 2022

Data di avvio 1 Gennaio 2023

Data di completamento 31 Dicembre 2026

Finanziato da

• Climate, Energy and Mobility

Costo totale

€ 67 635 029,08

Contributo UE

€ 48 501 871,65

Coordinato da

MTU AERO ENGINES AG
Germany

CORDIS fornisce collegamenti ai risultati finali pubblici e alle pubblicazioni dei progetti ORIZZONTE.

I link ai risultati e alle pubblicazioni dei progetti del 7° PQ, così come i link ad alcuni tipi di risultati specifici come dataset e software, sono recuperati dinamicamente da .OpenAIRE .

Risultati finali

Demonstrators, pilots, prototypes (2)

High Voltage EWIS for Powertrain testing at the Collins UK, GRID and Airbus facility

1st prototype hardware to support integration efforts(T6.7.2)

Delivery of prototype development hardware to Collins US for integration testing

Delivery of the following 1st build standard hardware to support integration testing in Collins US and Airbus FR:• Electrical motor (T6.2.1)• Motor controller (T6.3.1)• Output filter (T6.4)• DC panel (T6.5.2)

Documents, reports (4)

Data Management Plan (DMP)

Develop a detailed data management plan based on the EC template. (T1.1.4)

Updated Dissemination and Communication Plan

Updated plan for dissemination including communication activities. (T1.2)

Dissemination and Communication Plan

Plan for dissemination including communication activities. (T1.2)

Electric Oil Pump Specification

Deliverable provided by Collins US:Oil pump specification available (T6.6.1)

Pubblicazioni

Conference proceedings (11)

Early results from the design of an integrated steam vaporizer for hybrid aero engine applications

Autori: Michal Nitulescu, Sonny Andersson and Jonathan Berg, Isak Jonsson
Pubblicato in: 26th Conference of the International Society for Air Breathing Engines, 2024
Editore: International Society for Air Breathing Engines

Investigation of Impact of Steam Addition on Combustion Behavior and Pollutant Emissions in an RQL Combustor at High Pressure

Autori: J. Gray, O. Lammel, H. Ax, R. Lückerath, KP Geigle, G. Boardman, W. Kim, M. Haeringer
Pubblicato in: ASME Turbo Expo, 2025, ISBN 978-0-7918-8879-7
Editore: ASME
DOI: 10.1115/GT2025-153904

Condenser Design in the Sustainable Water Injecting Turbofan Comprising Hybrid Electrics

Autori: Hariharan Kallath, Jeong Hoon Heo, Majid Bhinder, Changmin Cao and El Hassan Ridouane
Pubblicato in: Transport Research Arena (TRA) 2024, Dublin, Ireland, 2024, ISBN 978-3-031-89444-2
Editore: Transport Research Arena
DOI: 10.1007/978-3-031-89444-2_109

Modeling and Analysis of a Water Recovery Unit for the Water-Enhanced Turbofan

Autori: Tim Hertwig, Jonathan Gloger, Alexander Woitalka, Arnold Herrgen
Pubblicato in: 26th Conference of the International Society for Air Breathing Engines, 2024
Editore: International Society for Air Breathing Engines

Aero-Thermo Analysis of a Waste Heat Recovery Heat Exchanger

Autori: Jonsson, Isak; Bredberg, Jonas; Vikhorev, Valentin; Alrifrai, Yasser; Bergh, Jonathan
Pubblicato in: Volume 1: Aircraft Engine; Ceramics and Ceramic Composites, 2025, ISBN 978-0-7918-8876-6
Editore: ASME
DOI: 10.1115/1.4070341

Design, implementation and setup of a condenser test-rig for the Water Enhanced Turbofan aero engine concept

Autori: Dimitriadou et al., I. Bolgar
Pubblicato in: 12th National (Hellenic) conference on Fluid and Flow Phenomena, Thessaloniki, Greece, 2024
Editore: 12th National (Hellenic) conference on Fluid and Flow Phenomena, Thessaloniki, Greece

EXPERIMENTAL SETUP FOR THE INVESTIGATION OF WATER SEPARATION IN ANNULAR FLOW WITHIN A CIRCULAR CHANNEL

Autori: Richard Haidl, Bernhard Weigand
Pubblicato in: 34th Congress of the International Council of the Aeronautical Sciences, 2024, ISSN 2958-4647
Editore: The International Council of the Aeronautical Sciences

Experimental Investigation of Components Influencing Annular Flow within a Circular Channel to Optimize Water Separation Processes

Autori: Richard Haidl, Georgios Iosifidis, Benjamin Lang, Alexander Woitalka, Bernhard Weigand
Pubblicato in: 26th Conference of the International Society for Air Breathing Engines, 2024
Editore: International Society for Air Breathing Engines

Water-Enhanced Turbofan Condenser Sizing Considering Configuration and Operating Conditions

Autori: Paul Ziegler, Christopher Simson, Thorsten Arzberger, Alexander Woitalka, Fabian Nöske, Sascha Kaiser, Volker Gümmer
Pubblicato in: 26th Conference of the International Society for Air Breathing Engines, 2024
Editore: International Society for Air Breathing Engines

COMPUTATIONAL MODELLING OF TWO-PHASE FLOW AND HEAT TRANSFER IN THE PRESENCE OF NON-CONDENSABLE GASES

Autori: Paraskevopoulos et al.
Pubblicato in: 12th National (Hellenic) conference on Fluid and Flow Phenomena, Thessaloniki, Greece, 2024
Editore: Proceedings of 12th National (Hellenic) conference on Fluid and Flow Phenomena, Thessaloniki, Greece

Numerical Simulation of Two-Phase Turbulent Flow in a 90deg. Pipe Bend with an Eulerian-Lagrangian Approach

Autori: Georgios Iosifidis, Richard Haidl, Bernhard Weigand, Arnold Herrgen
Pubblicato in: 26th Conference of the International Society for Air Breathing Engines, 2024
Editore: International Society for Air Breathing Engines

Peer reviewed articles (2)

Preliminary Investigation of the Heat Transfer and Pressure Drop of a Plate-Fin Heat Exchanger for Aero Engine Applications

Autori: Maria Dimitriadou, Vasilis Karaiskos, Zinon Vlahostergios, Dimitrios Misirlis, Kyros Yakinthos , Christopher McNab, Berwyn Pollard
Pubblicato in: Chemical Engineering Transactions, Numero 120, 2025, ISSN 2283-9216
Editore: AIDIC
DOI: 10.3303/CET25120091

Aero–Thermo Analysis of a Waste Heat Recovery Heat Exchanger

Autori: Isak Jonsson, Jonas Bredberg, Valentin Vikhorev, Yasser Alrifai, Jonathan Bergh
Pubblicato in: Journal of Engineering for Gas Turbines and Power, Numero 148, 2026, ISSN 0742-4795
Editore: ASME International
DOI: 10.1115/1.4070341