GETREADY

HiGh spEed TuRbinE cAsing produced by powDer HIP technologY

 Coordinatore CONSORZIO INTERUNIVERSITARIO NAZIONALE PER LA SCIENZA E TECNOLOGIA DEI MATERIALI 

 Organization address address: Via Giusti 9
city: FIRENZE
postcode: 50121

contact info
Titolo: Prof.
Nome: Sara
Cognome: Biamino
Email: send email
Telefono: 390111000000
Fax: 390111000000

 Nazionalità Coordinatore Italy [IT]
 Totale costo 886˙158 €
 EC contributo 531˙484 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2013-03
 Funding Scheme JTI-CS
 Anno di inizio 2014
 Periodo (anno-mese-giorno) 2014-09-01   -   2016-02-29

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    CONSORZIO INTERUNIVERSITARIO NAZIONALE PER LA SCIENZA E TECNOLOGIA DEI MATERIALI

 Organization address address: Via Giusti 9
city: FIRENZE
postcode: 50121

contact info
Titolo: Prof.
Nome: Sara
Cognome: Biamino
Email: send email
Telefono: 390111000000
Fax: 390111000000

IT (FIRENZE) coordinator 277˙434.00
2    AUBERT & DUVAL SAS

 Organization address address: AVENUE DU MAINE 33
city: PARIS
postcode: 75755

contact info
Titolo: Dr.
Nome: Benjamin
Cognome: Picque
Email: send email
Telefono: 33534012338

FR (PARIS) participant 254˙050.00

Mappa


 Word cloud

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

efficiency    emission    nship    hot    machining    speed    raw    astroloy    reducing    route    forging    material    saving    manufacturing    isostatic    turbine    pressing    energy    respect    ca    casing   

 Obiettivo del progetto (Objective)

The objectives of the project are: 1. To apply the powder Net Shape Hot Isostatic Pressing (NSHIP) manufacturing route to the fabrication of Astroloy casing for high speed turbine. 2. To optimise the material usage reducing material waste: the specific target is to design the Hot Isostatic Pressing manufacturing step so as to provide a semi-finished part very close to the final casing profile component (aiming at achieving 2 mm or lower overstock) thus reducing as much as possible the machining efforts; 3. To fine tune a post heat treatment to fully exploit the Astroloy potential thermal/mechanical resistance for casing application. Astroloy casing cannot be manufactured by traditional processing route (forging, ring rolling, massive machining) and with respect to the currently applied process to manufacture Waspaloy casing marked material and energy efficiency improvement can be achieved as well as clear environment benefits. According to a preliminary analysis of material, energy and emission potential savings achievable by applying NSHIP with respect to the traditional forging machining route to fabricate high speed turbine casing it can be foreseen to have: • a ca. 82% raw material saving; • an energy saving of ca. 82%; • an emission reduction of ca. 81%. In terms of cost efficiency a reduction of 57% in raw materials acquisition costs.

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