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HUC SIGNED

Development and validation of a powder HIP route for high temperature Astroloy to manufacture Ultrafan® IP Turbine Casings

Total Cost €

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EC-Contrib. €

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Partnership

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Project "HUC" data sheet

The following table provides information about the project.

Coordinator
ASOCIACION CENTRO TECNOLOGICO CEIT-IK4 

Organization address
address: PASEO MANUEL DE LARDIZABAL 15
city: SAN SEBASTIAN
postcode: 20018
website: www.ceit.es

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Spain [ES]
 Total cost 1˙557˙700 €
 EC max contribution 1˙499˙781 € (96%)
 Programme 1. H2020-EU.3.4.5.5. (ITD Engines)
 Code Call H2020-CS2-CFP07-2017-02
 Funding Scheme CS2-IA
 Starting year 2018
 Duration (year-month-day) from 2018-10-01   to  2021-09-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    ASOCIACION CENTRO TECNOLOGICO CEIT-IK4 ES (SAN SEBASTIAN) coordinator 659˙836.00
2    UNIVERSIDAD DEL PAIS VASCO/ EUSKAL HERRIKO UNIBERTSITATEA ES (LEIOA) participant 400˙000.00
3    FUNDACION IMDEA MATERIALES ES (GETAFE) participant 224˙801.00
4    AUBERT & DUVAL SAS FR (PARIS CEDEX 15) participant 135˙143.00
5    CONSORZIO INTERUNIVERSITARIO NAZIONALE PER LA SCIENZA E TECNOLOGIA DEI MATERIALI IT (FIRENZE) participant 80˙000.00

Map

 Project objective

This is a response to the Call for Proposal under Clean Sky 2 and JU to manufacture IP Turbine casings for the new generation Ultrafan® engine from Astroloy using Net Shape Hot Isostatic Pressing of powder (NSHIP). Astroloy with high γ’ volume fraction have the required high temperature properties but it is unforgeable. Thus, Powder-HIP is the most promising process route for this alloy though this technique presents several challenges such as presence of PPBs in the HIPped microstructure, the high cost of powder and HIP-tooling. HUC, making usage of the background technology will face and overcome these challenges and will take a step further tackling technology gaps alongside the material capability, basic mechanical behaviour and impact in the presence of the exposure with the ultimate goal for this technology to be fully tested in the relevant UltraFan® Demonstrator engine environment. The main objective of HUC is to improve the buy to fly ratio from the typically achieved 9 through the conventional cast and wrought route to less than 3 through NNSHIP being the material developed able to withstand engine relevant conditions with and without exposure guaranteeing its ability to contain. The work plan includes the following main activities: 1. Development and Optimisation of a powder HIP processing for Astroloy 2. Characterisation of mechanical properties to generate a database which supports the component design 3. Development of experiments and numerical simulations to assess the material´s behaviour under dynamic and ballistic conditions 4. Characterisation and understanding of mechanical properties with exposure at high temperatures 5. Development of low cost tooling for HIPping high temperature superalloy casings 6. Development and validation of process modelling capabilities 7. Manufacturing of canning/tooling to guarantee the compliance of the finish product with the requirements 8. Project progress Management, Dissemination, Communication and Exploitation

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The information about "HUC" are provided by the European Opendata Portal: CORDIS opendata.

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