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CORDIS - Resultados de investigaciones de la UE
CORDIS

ELectric Innovative Commuter Aircraft

CORDIS proporciona enlaces a los documentos públicos y las publicaciones de los proyectos de los programas marco HORIZONTE.

Los enlaces a los documentos y las publicaciones de los proyectos del Séptimo Programa Marco, así como los enlaces a algunos tipos de resultados específicos, como conjuntos de datos y «software», se obtienen dinámicamente de OpenAIRE .

Resultado final

Future technical challenge and scenarios (se abrirá en una nueva ventana)

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 (se abrirá en una nueva ventana)

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 (se abrirá en una nueva ventana)

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 (se abrirá en una nueva ventana)

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 (se abrirá en una nueva ventana)

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 (se abrirá en una nueva ventana)

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.

Publicaciones

TECHNOLOGY ROADMAP AND CONCEPTUAL DESIGN OF HYBRID AND ELECTRIC CONFIGURATIONS IN THE COMMUTER CLASS

Autores: F. Nicolosi, V. Marciello, V. Cusati, F. Orefice
Publicado en: 2022
Editor: ICAS

Design of Hybrid-Electric Small Air Transports (se abrirá en una nueva ventana)

Autores: F. Orefice, V. Marciello, F. Nicolosi, Q. Zhang, G. Wortmann, J. Menu and V. Cusati
Publicado en: IOP Conference Series: Materials Science and Engineering, Edición 1226 012075, 2022
Editor: IOP Publishing Ltd
DOI: 10.1088/1757-899x/1226/1/012075

Aircraft Conceptual Design of Commuter Aircraft including Distributed Electric Propulsion (se abrirá en una nueva ventana)

Autores: Francesco Orefice, Fabrizio Nicolosi, Pierluigi Della Vecchia, Danilo Ciliberti
Publicado en: AIAA AVIATION 2020 FORUM, 2020, ISBN 978-1-62410-598-2
Editor: 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 (se abrirá en una nueva ventana)

Autores: Alp Emre Öngüt, Vincenzo Cusati, Vittorio Memmolo, Fabrizio Nicolosi, Francesco Orefice, Danyu Qiao and Yves Lemmens
Publicado en: AIAA SCITECH 2022 Forum, 2022
Editor: AIAA
DOI: 10.2514/6.2022-0169

Conceptual Design of a Hydrogen-Propelled Aircraft with Distributed Electric Propulsion (se abrirá en una nueva ventana)

Autores: Fabrizio Nicolosi, Valerio Marciello and Francesco Orefice
Publicado en: 2022
Editor: AIAA Aviation 2022 Forum
DOI: 10.2514/6.2022-3205

Economic Feasibility Study of a Hybrid-Electric 19-Passenger Commuter Aircraft (se abrirá en una nueva ventana)

Autores: G. Schuh, M. Spangenberg, Q. Zhang, B. Dannbeck, J. Stuerken
Publicado en: 2021
Editor: DGLR
DOI: 10.25967/530307

Design of hybrid-electric aircraft with fault-tolerance considerations (se abrirá en una nueva ventana)

Autores: Valerio MARCIELLO, Francesco OREFICE, Fabrizio NICOLOSI, Danilo CILIBERTI, Pierluigi DELLA VECCHIA
Publicado en: Chinese Journal of Aeronautics, Edición Vol 6, 2022, 2022, ISSN 1000-9361
Editor: 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 (se abrirá en una nueva ventana)

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

The Enabling Technologies for a Quasi-Zero Emissions Commuter Aircraft (se abrirá en una nueva ventana)

Autores: Danilo Ciliberti, Pierluigi Della Vecchia, Vittorio Memmolo, Fabrizio Nicolosi,Guido Wortmann Fabrizio Ricci
Publicado en: Aerospace, Edición Vol 9, Edición 6, 2022, ISSN 2226-4310
Editor: MDPI
DOI: 10.3390/aerospace9060319

Economically driven requirements for a hybrid-electric 19-passenger commuter aircraft (se abrirá en una nueva ventana)

Autores: G Schuh, M Spangenberg, Q Zhang
Publicado en: IOP Conference Series: Materials Science and Engineering, Edición 1024, 2021, Página(s) 012079, ISSN 1757-899X
Editor: IOP Publishing Ltd
DOI: 10.1088/1757-899x/1024/1/012079

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

Autores: Maximilian Spangenberg, Markus Wellensiek, Qinyin Zhang
Publicado en: ELICA Deliverable D2.1, 2022
Editor: ELICA Consortium

Hybrid-electric Propulsion Architecture Report

Autores: Guido Wortmann, Qinyin Zhang
Publicado en: ELICA Deliverable D3.1, 2020
Editor: ELICA Consortium

Plan for Dissemination, Exploitation and Communication of Project Results

Autores: Qinyin Zhang, Irmina Schmucker
Publicado en: ELICA Deliverable D1.3, 2020
Editor: ELICA Consortium

Enabling Technologies

Autores: Danilo Ciliberti, Pierluigi Della Vecchia, Fabrizio Nicolosi, Vittorio Memmolo, Vincenzo Cusati (Smartup), Salvatore Corcione (Smartup), Guido Wortmann (RR)
Publicado en: ELICA Deliverable D5.1, 2020
Editor: ELICA Consortium

State of the art of hybrid aircraft design projects

Autores: Valerio Marciello, Francesco Orefice, Fabrizio Nicolosi, Vincenzo Cusati (SMARTUP), Salvatore Corcione (SMARTUP)
Publicado en: ELICA Deliverable D4.1, 2020
Editor: ELICA Consortium

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