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ELectric Innovative Commuter Aircraft

Risultati finali

Future technical challenge and scenarios

The report will identify scientific and technical challenges for the successful of a 19 passengers commuter aircraft specifying gaps from the current SOTA A potential update will be voted to required performance for a viable commuter size aircraft UNINA Finally advise on the required steps towards the progress needed in improving individual system components performance RRD

Enabling technologies

The report will point out all the main innovative technologies available to be pursued on aircraft systems to make feasible a near-zero CO2 commuter aircraft. The advisory will be addressed not only to power train architectures components produced by RRD and SISW, on-board-systems components and airframes, but also on the alternative mobility scenarios (as forecasted in WP2 by ASP), aircraft requirements, regulations, costs and emissions.

Hybrid-electric propulsion architecture report

Distributed propulsion systems require to operate each propulsor individually, so that the propulsion power flow and split vary throughout the mission. This power variability and possible failure cases are the key drivers for synthesizing suitable architectures. In this task, hybrid-electric architectures of hybrid ships and proposed architectures for future aircraft are reviewed and assessed with respect to the aircraft requirements, operational characteristics and failure cases.

Dissemination, comunication and exploiation Plan

The dissemination and exploitation of achieved results. UNINA will cooperate in administrative items and will coordinate dissemination and exploitation activities.

State-of-the-art (SOTA) of hybrid aircraft design projects

UNINA will review the SOTA of recent research projects and literature on the design and applications for light, commuter, general aviation and large turboprop aircraft.

Economic feasibility study for a 19 PAX hybrid-electric commuter aircraft

The successful introduction of a new aircraft into the transportation market is highly dependent on the economic feasibility which includes the forecasted market volume, the profitable routes, and the specific cost of transport. In a first step, the transportation demand based on socio-economic factors and available transportation options will be analysed. In a second step, the competitive range of the operating costs for the identified demand will be analysed in comparison to the other existing transportation options. The analysis will be verified with the views of the airframers from the Industrial Advisory Board.



Autori: F. Nicolosi, V. Marciello, V. Cusati, F. Orefice
Pubblicato in: 2022
Editore: ICAS

Design of Hybrid-Electric Small Air Transports

Autori: F. Orefice, V. Marciello, F. Nicolosi, Q. Zhang, G. Wortmann, J. Menu and V. Cusati
Pubblicato in: IOP Conference Series: Materials Science and Engineering, Issue 1226 012075, 2022
Editore: IOP Publishing Ltd
DOI: 10.1088/1757-899x/1226/1/012075

Aircraft Conceptual Design of Commuter Aircraft including Distributed Electric Propulsion

Autori: Francesco Orefice, Fabrizio Nicolosi, Pierluigi Della Vecchia, Danilo Ciliberti
Pubblicato in: AIAA AVIATION 2020 FORUM, 2020, ISBN 978-1-62410-598-2
Editore: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.2020-2627

A Design Chain for Distributed Electric Propulsion with Increased Fidelity Structural Strength Assessment and Mass Estimation

Autori: Alp Emre Öngüt, Vincenzo Cusati, Vittorio Memmolo, Fabrizio Nicolosi, Francesco Orefice, Danyu Qiao and Yves Lemmens
Pubblicato in: AIAA SCITECH 2022 Forum, 2022
Editore: AIAA
DOI: 10.2514/6.2022-0169

Conceptual Design of a Hydrogen-Propelled Aircraft with Distributed Electric Propulsion

Autori: Fabrizio Nicolosi, Valerio Marciello and Francesco Orefice
Pubblicato in: 2022
Editore: AIAA Aviation 2022 Forum
DOI: 10.2514/6.2022-3205

Economic Feasibility Study of a Hybrid-Electric 19-Passenger Commuter Aircraft

Autori: G. Schuh, M. Spangenberg, Q. Zhang, B. Dannbeck, J. Stuerken
Pubblicato in: 2021
Editore: DGLR
DOI: 10.25967/530307

Design of hybrid-electric aircraft with fault-tolerance considerations

Autori: Valerio MARCIELLO, Francesco OREFICE, Fabrizio NICOLOSI, Danilo CILIBERTI, Pierluigi DELLA VECCHIA
Pubblicato in: Chinese Journal of Aeronautics, Issue Vol 6, 2022, 2022, ISSN 1000-9361
Editore: Press of Acta Aeronautica et Astronautica Sinica
DOI: 10.1016/j.cja.2022.05.014

Preliminary Design to Fulfil Future Market Demand of Electric Aircraft

Autori: Francesco Orefice, Pierluigi Della Vecchia, Danilo Ciliberti, Fabrizio Nicolosi
Pubblicato in: International Review of Aerospace Engineering (I.RE.AS.E.), Issue Vol 14, No 6 (2021), 2021, ISSN 1973-7459
Editore: Praise Worthy Prize
DOI: 10.15866/irease.v14i6.20814

The Enabling Technologies for a Quasi-Zero Emissions Commuter Aircraft

Autori: Danilo Ciliberti, Pierluigi Della Vecchia, Vittorio Memmolo, Fabrizio Nicolosi,Guido Wortmann Fabrizio Ricci
Pubblicato in: Aerospace, Issue Vol 9, Issue 6, 2022, ISSN 2226-4310
Editore: MDPI
DOI: 10.3390/aerospace9060319

Economically driven requirements for a hybrid-electric 19-passenger commuter aircraft

Autori: G Schuh, M Spangenberg, Q Zhang
Pubblicato in: IOP Conference Series: Materials Science and Engineering, Issue 1024, 2021, Page(s) 012079, ISSN 1757-899X
Editore: IOP Publishing Ltd
DOI: 10.1088/1757-899x/1024/1/012079

Economic feasibility study for a 19 PAX hybrid-electric commuter aircraft

Autori: Maximilian Spangenberg, Markus Wellensiek, Qinyin Zhang
Pubblicato in: ELICA Deliverable D2.1, 2022
Editore: ELICA Consortium

Hybrid-electric Propulsion Architecture Report

Autori: Guido Wortmann, Qinyin Zhang
Pubblicato in: ELICA Deliverable D3.1, 2020
Editore: ELICA Consortium

Plan for Dissemination, Exploitation and Communication of Project Results

Autori: Qinyin Zhang, Irmina Schmucker
Pubblicato in: ELICA Deliverable D1.3, 2020
Editore: ELICA Consortium

Enabling Technologies

Autori: Danilo Ciliberti, Pierluigi Della Vecchia, Fabrizio Nicolosi, Vittorio Memmolo, Vincenzo Cusati (Smartup), Salvatore Corcione (Smartup), Guido Wortmann (RR)
Pubblicato in: ELICA Deliverable D5.1, 2020
Editore: ELICA Consortium

State of the art of hybrid aircraft design projects

Autori: Valerio Marciello, Francesco Orefice, Fabrizio Nicolosi, Vincenzo Cusati (SMARTUP), Salvatore Corcione (SMARTUP)
Pubblicato in: ELICA Deliverable D4.1, 2020
Editore: ELICA Consortium

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