Fast Rotorcraft

Project Information

FRC GAM 2018

Grant agreement ID: 807090

DOI

10.3030/807090

Project closed

EC signature date 1 January 2014

Start date 7 January 2014

End date 31 December 2019

Funded under

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Total cost

€ 136 809 569,16

EU contribution

€ 85 997 327,60

Coordinated by

AIRBUS HELICOPTERS
France

CORDIS provides links to public deliverables and publications of HORIZON projects.

Links to deliverables and publications from FP7 projects, as well as links to some specific result types such as dataset and software, are dynamically retrieved from OpenAIRE .

Deliverables

Documents, reports (1)

WP 2B.2: Dissemination report

Description of project dissemination and exploitation plan 2019

Publications

Conference proceedings (24)

The Challenges for the Integration of the Drive Shaft in the RACER’s Wing Conguration

Author(s): Martin Blacha, Adriana Garcia-Rios, Marc Schelcher
Published in: The vertical flight society Forum75, 2019, Page(s) 11
Publisher: The vertical flight society

RACER aero-acoustic propeller design and analysis

Author(s): Julien Decours*, Biel Ortun, Yves Delrieux, Joelle Bailly, Sylvette Canard-Caruana, Raphael Fukari, Frederic Guntzer
Published in: Vertical Flight Society Forum75, 2019
Publisher: Vertical Flight Society

Racer High-Speed Demonstrator: Tail Unit Vertical Fin Aerodynamic Design

Author(s): C.Lienard, I.S.E.Din; R.Huot; R.Fukari
Published in: AHS International 74th Annual Forum & Technology Display, 2018
Publisher: Vertical Flight Society

An overview of DLR compound rotorcraft aerodynamic activities within the CleanSky2 NACOR Project

Author(s): M.Wentrup, T.Schwarz, P.Kunze, J.H.Wendisch, J.Yin, T.Streit; R.Fukari; K.Kicker; J.P.Pinacho
Published in: AHS International 74th Annual Forum & Technology Display, 2018
Publisher: Vertical Flight Society

RACER high-speed demonstrator: Rotor and rotor-head wake interactions with tail unit

Author(s): C.Lienard, I.S.E.Din, T.Renaud; R.Fukari
Published in: AHS International 74th Annual Forum & Technology Display, 2018
Publisher: Vertical Flight Society

Aerodynamic interactions on AH compound helicopter RACER

Author(s): C. Öhrle, F. Frey, J. Thiemeier, M. Kessler, E. Krämer
Published in: The Vertical Flight Society Forum75, 2019
Publisher: Vertical Flight Society

Aerodynamics and Dynamics Analysis of the Main Rotor of the Compound Helicopter X3 in High-Speed Flight: Correlation of Simulation and Flight Test

Author(s): C. Öhrle, F. Frey, J. Thiemeier, M. Kessler, E. Krämer, P. Eglin, M. Embacher, P. Cranga
Published in: The vertigal Flight Society Forum75, 2019
Publisher: Vertical Flight Society

Simulation of Rotor-Empennage Interactional Aerodynamics in Comparison to Experimental Data

Author(s): Markus Rinker*, G. Uhl, M. Hajek, S. Platzer, Tobias Ries, Martin Embacher
Published in: the Vertical Flight Society Forum75, 2019
Publisher: Vertical Flight Society

RACER aero-acoustic propeller design and analysis

Author(s): J.Decours, B.Ortun, J.Bailly, Y.Delrieux; F.Guntzer, R.Fukari
Published in: The Vertical Flight Society Forum75, 2019
Publisher: Vertical Flight Society

Advanced concept of drive shaft system for hybrid high-speed helicopter

Author(s): MSc Dawid Cander , Dr Jerome Geneix
Published in: European Rotorcraft Forum 2019, 2019
Publisher: European Rotorcraft Forum

DLR Analysis on the Noise Emission from the RACER Configuration

Author(s): Dr Jianping Yin , Dr Thorsten Schwarz, MSc Marc Wentrup, MSc Frédéric Guntzer
Published in: European Rotorcraft Forum 2019, 2019
Publisher: European Rotorcraft Forum

Aerodynamic Design Optimization of a Helicopter Rotor Blade-Sleeve Fairing

Author(s): P. Pölzlbauer, D. Desvigne, C. Breitsamter
Published in: Proceedings of the German Aerospace Congress, 2017
Publisher: Deutsche Gesellschaft für Luft- und Raumfahrt Lilienthal-Oberth e.V.

Performance Improvement of a Compound Helicopter Rotor Head by Aerodynamic Shape Optimization

Author(s): P. Pölzlbauer, D. Desvigne, C. Breitsamter
Published in: 31st Congress of the International Council of the Aeronautical Sciences, 2018
Publisher: ICAS

Numerical simulation for the impact of frangible wing section of a tilt-rotor aircraft

Author(s): Claudio Pezzella, Salvatore Orlando, Michele Guida, Francesco Marulo
Published in: Aerospace Structural Impact Dynamics International Conference (Madrid, 6-9 June 2019), 2019
Publisher: ASIDIC conference

UNINA involvement in the CS2 JU T-WING project

Author(s): Daniele Marano, Tiziano Polito, Michele Guida, Francesco Marulo
Published in: AIDAA International Congress (Rome, 9-12 September 2019), 2019
Publisher: AIDAA, Associazione Italiana di Aeronautica e Astronautica

T-WING an Italian based aeronautical EU funded research project: objectives, status and future opportunities

Author(s): Luigi Di Palma
Published in: 8th European Aeronautics days, Issue Annual, 2019, ISSN 1869-5582
Publisher: Springer Vienna

Flutter analysis and trade-offs targeting the preliminary design of the wing of the Next Generation Civil Tilt-Rotor Technology Demonstrator

Author(s): J. Beretta, A. Cardoza, M. Belardo, N. Paletta
Published in: 8th European Aeronautics Days, 2019, ISSN 1869-5582
Publisher: Springer Vienna

On the preliminary structural design strategy of the wing of the Next Generation Civil Tilt-Rotor Technology Demonstrator

Author(s): M. Belardo, J. Beretta, G. Diodati, N. Paletta, L. Di Palma
Published in: 8th European Aeronautics Days, 2019, ISSN 1869-5582
Publisher: Springer Vienna

The Dawn of a New Rotorcraft Age

Author(s): Luca Medici, Michele Arra
Published in: European Rotorcraft Forum 45, 2019
Publisher: ERF

Next generation Civil TiltRotor

Author(s): Neil Harris
Published in: Clean Sky 2 Event, 2019
Publisher: Leonardo

Development of the Next Generation Civil Tiltrotor

Author(s): David Matthew
Published in: 11th UK Altair Technology Conference, 2019
Publisher: Leonardo

Analytical approach to develop a rotorcraft fuel system

Author(s): Luca Patricelli
Published in: 2019 SIMCENTER CONFERENCE, 2019
Publisher: Leonardo

Prototypes procurement: the RACER example (Airbus) / Workshop on advanced technologies for gears applications

Author(s): Andrea Demarin
Published in: Pisa Gears 2018, 2018
Publisher: N/A

Racer - The Future of Speed is now

Author(s): Yari M. Bovalino
Published in: Helitech 2018, 2018
Publisher: N/A

Peer reviewed articles (1)

Performance improvement of a compound helicopter rotor head by aerodynamic design optimisation of a blade-sleeve fairing

Author(s): P. Pölzlbauer, D. Desvigne, C. Breitsamter
Published in: The Aeronautical Journal, 2019, ISSN 0001-9240
Publisher: Royal Aeronautical Society

Other (4)

Italy combines capabilities for future tiltrotor

Author(s): Dominic Perry
Published in: Flight International, 2018
Publisher: FlightGlobal

Leonardo Helicopters advances on next-gen tiltrotor

Author(s): Dominic Perry
Published in: n/a, 2019
Publisher: Flight Global

GE Aviation’s Top Technologies for the RACER

Author(s): Yari M. Bovalino
Published in: YouTube, 2018
Publisher: N/A

Fast And Furious: RACER, Next-Gen Helicopter Hybrid, Could Bring Cheaper, Greener, And Speedier Air Travel

Author(s): Yari M. Bovalino
Published in: GE Reports, 2019
Publisher: N/A

Non-peer reviewed articles (1)

T-WING: sviluppo dell'ala di un convertiplano di nuova generazione

Author(s): Luigi Di Palma, Nicola Paletta, Antonio Apicella
Published in: Compisiti Magazine, Issue XIII No 49, September 2018, 2018, Page(s) pp. 8-11, ISSN 2499-6890
Publisher: Compositi Magazine

Intellectual Property Rights

Patent (40)

SYSTEME DE TRANSMISSION DE PUISSANCE ET AERONEF AYANT UNE VOITURE TOURNANTE

Application/Publication number: FR 1501920
Date: 2015-09-16
Applicant(s): AIRBUS HELICOPTERS

ORGANE DE COMMANDE, AERONEF A VOILURE TOURNANTE ET PROCEDE

Application/Publication number: FR 1601695
Date: 2016-11-30
Applicant(s): AIRBUS HELICOPTERS

Système de transmission de puissance et aéronef ayant une voilure tournante

Application/Publication number: US 2017341748
Date: 2015-09-16
Applicant(s): AIRBUS HELICOPTERS

AN ADAPTIVE FLIGHT CONTROL SYSTEM FOR THE YAW AND THRUST FLIGHT CONTROLS OF A HYBRID HELICOPTER

Application/Publication number: EP 16197906
Date: 2016-11-09
Applicant(s): AIRBUS HELICOPTERS

LUBRICATING DEVICE HAVING A PLURALITY OF VESSELS FOR RECOVERING LUBRICATING LIQUID AND OPTIMISED, RELIABLE MEANS FOR ROUTING TO A MAIN VESSEL

Application/Publication number: EP 17186759
Date: 2017-08-18
Applicant(s): AIRBUS HELICOPTERS

COMMANDE A ROULEMENT, SYSTEME MECANIQUE ET AERONEF

Application/Publication number: FR 1501841
Date: 2015-09-07
Applicant(s): AIRBUS HELICOPTERS

ELECTRIC MACHINES AND METHODS RELATED TO ASSEMBLING ELECTRIC MACHINES

Application/Publication number: EP 05807247
Date: 2005-10-04
Applicant(s): AIRBUS HELICOPTERS

ENSEMBLE SUSTENTATEUR AMOVIBLE D'UN GIRAVION ET GIRAVION

Application/Publication number: FR 1400836
Date: 2014-04-07
Applicant(s): AIRBUS HELICOPTERS

AN ELECTRICAL ARCHITECTURE WITH PAIRED SECONDARY ELECTRICAL NETWORKS FOR STARTING ENGINES OF AN AIRCRAFT

Application/Publication number: EP 17182287
Date: 2017-07-20
Applicant(s): AIRBUS HELICOPTERS

PALONNIER REGLABLE ET ROTATIF POUR UN AERONEF A VOILURE TOURNANTE

Application/Publication number: FR 1501599
Date: 2015-07-27
Applicant(s): AIRBUS HELICOPTERS

AERONEF COMBINE MUNI D'UN DISPOSITIF ANTICOUPLE COMPLEMENTAIRE

Application/Publication number: FR 1501513
Date: 2015-07-16
Applicant(s): AIRBUS HELICOPTERS

SERVOCOMMANDE, ROTOR ET AERONEF ASSOCIES

Application/Publication number: FR FR1601560
Date: 2016-10-31
Applicant(s): AIRBUS HELICOPTERS

AERONEF COMBINE MUNI D'UN DISPOSITIF ANTICOUPLE COMPLEMENTAIRE

Application/Publication number: FR 1501513
Date: 2015-07-16
Applicant(s): AIRBUS HELICOPTERS

ORGANE DE COMMANDE, AERONEF A VOILURE TOURNANTE ET PROCEDE

Application/Publication number: FR 1601695
Date: 2016-11-30
Applicant(s): AIRBUS HELICOPTERS

PALONNIER REGLABLE ET ROTATIF POUR UN AERONEF A VOILURE TOURNANTE

Application/Publication number: FR 1501599
Date: 2015-07-27
Applicant(s): AIRBUS HELICOPTERS

SERVOCOMMANDE, ROTOR ET AERONEF ASSOCIES

Application/Publication number: FR FR1601560
Date: 2016-10-31
Applicant(s): AIRBUS HELICOPTERS

Système mécanique de transmission d’un mouvement et aéronef équipé d’un système correspondant

Application/Publication number: US 2018072406
Date: 2016-09-09
Applicant(s): AIRBUS HELICOPTERS

COMPOUND HELICOPTER

Application/Publication number: EP 15400040
Date: 2015-09-11
Applicant(s): AIRBUS HELICOPTERS DEUTSCHLAND GMBH

GIRAVION MUNI D'UN DISPOSITIF STABILISATEUR

Application/Publication number: FR 1402194
Date: 2014-09-30
Applicant(s): AIRBUS HELICOPTERS

OUTRE DE QUEUE DE GIRAVION, ET GIRAVION

Application/Publication number: FR 1401589
Date: 2014-07-16
Applicant(s): AIRBUS HELICOPTERS

Système de transmission de puissance et aéronef ayant une voilure tournante

Application/Publication number: US 2017341748
Date: 2015-09-16
Applicant(s): AIRBUS HELICOPTERS

A LEAD-LAG DAMPER INTEGRATED INSIDE A BLADE OF A ROTOR

Application/Publication number: EP 17194173
Date: 2017-09-29
Applicant(s): AIRBUS HELICOPTERS

COMPOUND HELICOPTER

Application/Publication number: EP 15400040
Date: 2015-09-11
Applicant(s): AIRBUS HELICOPTERS DEUTSCHLAND GMBH

ELECTRIC MACHINES AND METHODS RELATED TO ASSEMBLING ELECTRIC MACHINES

Application/Publication number: EP 05807247
Date: 2005-10-04
Applicant(s): AIRBUS HELICOPTERS

AN ELECTRIC CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD

Application/Publication number: EP 17192890
Date: 2017-09-25
Applicant(s): AIRBUS HELICOPTERS

COMBINATEUR DES COMMANDES VOL EN LACET ET DE POUSSEE POUR UN HELICOPTERE HYBRIDE

Application/Publication number: FR 1502168
Date: 2015-10-15
Applicant(s): AIRBUS HELICOPTERS

Système mécanique de transmission d’un mouvement et aéronef équipé d’un système correspondant

Application/Publication number: US 2018072406
Date: 2016-09-09
Applicant(s): AIRBUS HELICOPTERS

AN ELECTRIC CONTROL MEMBER, A ROTARY WING AIRCRAFT, AND A METHOD

Application/Publication number: EP 17192890
Date: 2017-09-25
Applicant(s): AIRBUS HELICOPTERS

LUBRICATING DEVICE HAVING A PLURALITY OF VESSELS FOR RECOVERING LUBRICATING LIQUID AND OPTIMISED, RELIABLE MEANS FOR ROUTING TO A MAIN VESSEL

Application/Publication number: EP 17186759
Date: 2017-08-18
Applicant(s): AIRBUS HELICOPTERS

AN ELECTRICAL ARCHITECTURE WITH PAIRED SECONDARY ELECTRICAL NETWORKS FOR STARTING ENGINES OF AN AIRCRAFT

Application/Publication number: EP 17182287
Date: 2017-07-20
Applicant(s): AIRBUS HELICOPTERS

ENSEMBLE SUSTENTATEUR AMOVIBLE D'UN GIRAVION ET GIRAVION

Application/Publication number: FR 1400836
Date: 2014-04-07
Applicant(s): AIRBUS HELICOPTERS

CARENAGE DE ROTOR, ROTOR ET AERONEF

Application/Publication number: FR 1402170
Date: 2014-09-26
Applicant(s): AIRBUS HELICOPTERS

COMMANDE A ROULEMENT, SYSTEME MECANIQUE ET AERONEF

Application/Publication number: FR 1501841
Date: 2015-09-07
Applicant(s): AIRBUS HELICOPTERS

A LEAD-LAG DAMPER INTEGRATED INSIDE A BLADE OF A ROTOR

Application/Publication number: EP 17194173
Date: 2017-09-29
Applicant(s): AIRBUS HELICOPTERS

CARENAGE DE ROTOR, ROTOR ET AERONEF

Application/Publication number: FR 1402170
Date: 2014-09-26
Applicant(s): AIRBUS HELICOPTERS

AN ADAPTIVE FLIGHT CONTROL SYSTEM FOR THE YAW AND THRUST FLIGHT CONTROLS OF A HYBRID HELICOPTER

Application/Publication number: EP 16197906
Date: 2016-11-09
Applicant(s): AIRBUS HELICOPTERS

OUTRE DE QUEUE DE GIRAVION, ET GIRAVION

Application/Publication number: FR 1401589
Date: 2014-07-16
Applicant(s): AIRBUS HELICOPTERS

SYSTEME DE TRANSMISSION DE PUISSANCE ET AERONEF AYANT UNE VOITURE TOURNANTE

Application/Publication number: FR 1501920
Date: 2015-09-16
Applicant(s): AIRBUS HELICOPTERS

GIRAVION MUNI D'UN DISPOSITIF STABILISATEUR

Application/Publication number: FR 1402194
Date: 2014-09-30
Applicant(s): AIRBUS HELICOPTERS

COMBINATEUR DES COMMANDES VOL EN LACET ET DE POUSSEE POUR UN HELICOPTERE HYBRIDE

Application/Publication number: FR 1502168
Date: 2015-10-15
Applicant(s): AIRBUS HELICOPTERS