ACHEON

Aerial Coanda High Efficiency Orienting-jet Nozzle

 Coordinatore UNIVERSITA DEGLI STUDI DI MODENA E REGGIO EMILIA 

 Organization address address: VIA UNIVERSITA 4
city: MODENA
postcode: 41100

contact info
Titolo: Prof.
Nome: Eugenio
Cognome: Dragoni
Email: send email
Telefono: +39 0522 522612
Fax: +39 0522 522609

 Nazionalità Coordinatore Italy [IT]
 Totale costo 773˙196 €
 EC contributo 599˙630 €
 Programma FP7-TRANSPORT
Specific Programme "Cooperation": Transport (including Aeronautics)
 Code Call FP7-AAT-2012-RTD-L0
 Funding Scheme CP-FP
 Anno di inizio 2012
 Periodo (anno-mese-giorno) 2012-12-01   -   2014-11-30

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    UNIVERSITA DEGLI STUDI DI MODENA E REGGIO EMILIA

 Organization address address: VIA UNIVERSITA 4
city: MODENA
postcode: 41100

contact info
Titolo: Prof.
Nome: Eugenio
Cognome: Dragoni
Email: send email
Telefono: +39 0522 522612
Fax: +39 0522 522609

IT (MODENA) coordinator 148˙338.95
2    UNIVERSITY OF LINCOLN

 Organization address address: Brayford Pool
city: LINCOLN
postcode: LN6 7TS

contact info
Titolo: Prof.
Nome: Chris
Cognome: Bingham
Email: send email
Telefono: +44 07834435004

UK (LINCOLN) participant 104˙080.00
3    VRIJE UNIVERSITEIT BRUSSEL

 Organization address address: PLEINLAAN 2
city: BRUSSEL
postcode: 1050

contact info
Titolo: Mr.
Nome: Nik
Cognome: Claesen
Email: send email
Telefono: +32 2 6292210
Fax: +32 2 6293640

BE (BRUSSEL) participant 104˙080.00
4    UNIVERSIDADE DA BEIRA INTERIOR

 Organization address address: CONVENTO DE SANTO ANTONIO
city: COVILHA
postcode: 6201 001

contact info
Titolo: Ms.
Nome: Dina
Cognome: Pereira
Email: send email
Telefono: +351 275 329 146
Fax: +351 275 329 148

PT (COVILHA) participant 94˙400.00
5    REGGIO EMILIA INNOVAZIONE SCARL

 Organization address address: VIA SICILIA 31
city: REGGIO EMILIA
postcode: 42122

contact info
Titolo: Dr.
Nome: Arturo
Cognome: Tornaboni
Email: send email
Telefono: +39 0522 922 238
Fax: +39 0522 513 772

IT (REGGIO EMILIA) participant 83˙371.04
6    NIMBUS SRL

 Organization address address: VIA DEL BOSCHETTO 2/1
city: LOMBARDORE
postcode: 10040

contact info
Titolo: Mr.
Nome: Paolo
Cognome: Bellezza Quater
Email: send email
Telefono: +39 011 9956481

IT (LOMBARDORE) participant 65˙360.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

overcome    applications    physical    architectures    innovative    thrust    effect    vectoring    propulsion    acheon    jet    aerial    limits    possibility    explore    propulsive    deflection    coanda    speed   

 Obiettivo del progetto (Objective)

'The ACHEON project explores a novel propulsive system for aircrafts which overcome the main limitations of traditional systems introducing an effective and affordable vectored jet aerial propulsion with no part in move-ment. The project aims to overcome well known limits related to commonly known jet deflection system. The ACHEON system is based on the cumulated effects of three physical effects: 1. High speed jet mixing effects; 2. Coanda effect of adhesion of an high speed jet to a convex surface; 3. Coanda effect control by Electrostatic fields. The strengths of the ACHEON concept are: - Affordability: the deflection of the jet is realized without any moving part. - Simple controls: the angle formed by the jet and the nozzle axis can be regulated by varying the velocity of two incoming jets; - Precision: the Plasma Dischargers ensures an optimal control of jet attachment to the Coanda surfaces. - Possibility to be alimented by streams of any nature. The ACHEON thrust vectoring propulsive concept can produce a wide possibility of future and innovative air-crafts concepts with enhanced capabilities which could shorten take off and landing spaces, enhance manoeuvrability, explore new concepts such as diffused propulsion systems or more radical solutions for future aeronautic transport. The ACHEON Project aims to study the system and its components in a full structured systemic approach 1. to define: - the system and its control methodology identifying it possible intrinsic limits and defining exactly fields of applications; - control equations of the system as a function of both geometric and physical parameters; - system design methods which could help to obtain better results on different sizes and architectures; 2. to explore the feasibility of: - applications to traditional aerial vehicles architectures; - applications to innovative aerial vehicle designs such as distributed propulsion; - innovative aircraft optimized for thrust vectoring.'

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