OREAT II

Open Rotor Engines Advanced Technologies II

 Coordinatore GE AVIATION SYSTEMS LTD 

 Organization address address: Cheltenham Road
city: Bishops Cleeve
postcode: GL52 8SF

contact info
Titolo: Mr.
Nome: Paul
Cognome: Myers
Email: send email
Telefono: 441453000000

 Nazionalità Coordinatore United Kingdom [UK]
 Totale costo 1˙964˙531 €
 EC contributo 940˙371 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2011-01
 Funding Scheme JTI-CS
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-12-01   -   2013-07-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    GE AVIATION SYSTEMS LTD

 Organization address address: Cheltenham Road
city: Bishops Cleeve
postcode: GL52 8SF

contact info
Titolo: Mr.
Nome: Paul
Cognome: Myers
Email: send email
Telefono: 441453000000

UK (Bishops Cleeve) coordinator 27˙000.00
2    GENERAL ELECTRIC COMPANY POLSKA

 Organization address address: Aleja Krakowska 110/114
city: Warszawa
postcode: 02-256

contact info
Titolo: Mr.
Nome: Miroslaw
Cognome: Sobaniec
Email: send email
Telefono: +48 22 112 3272
Fax: +48 22 868 5666

PL (Warszawa) participant 553˙199.00
3    INSTYTUT LOTNICTWA

 Organization address address: KRAKOWSKA 110/114
city: WARSZAWA
postcode: 02 256

contact info
Titolo: Mr.
Nome: Grzegorz
Cognome: Szymanowski
Email: send email
Telefono: 48225773401

PL (WARSZAWA) participant 360˙172.00

Mappa


 Word cloud

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

maturation    rotor    cs    benches    sage    plans    engine    blade    definition    packages    selected    manufacturing    pitch    components    aviation    pcm    jt    ge   

 Obiettivo del progetto (Objective)

'A principal contributor to affordable and sustainable public air transportation will be the introduction of more fuel-efficient propulsion systems, one of which is the Open Rotor Engine concept. Unlike turbofans, open rotors must vary blade pitch to accommodate power and aircraft speed range, so a key element to the viability of the concept is the actuation and control of the blade pitch via the Pitch Change Mechanism (PCM). GE Company Polska, Warsaw Institute of Aviation and GE Aviation Systems Ltd (trading as Dowty Propellers) propose to build on the background of JT1-CS-2009-1-SAGE-02-001 as support for the SAGE 2 engine PCM. The work packages proposed via this application will focus on the design, manufacturing and testing of key components associated with the down selected PCM concepts from JT1-CS-2009-1-SAGE-02-001. The proposal contains detailed design, manufacturing and assembly of key components and test benches, design and procurement of required instrumentation, key components maturation test plans, description of the test support and test data post processing. The deliverables from the programme will be the definition of the selected key components with 3D models, complete definition of test benches, evaluation of vendors and suppliers. All activities will be summarized in comprehensive reports. The work packages will be closely aligned to the key technologies maturation plans, in preparation for the ground demonstration of the open rotor engine.'

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