ALEA

Accelerated Life tests for Electric drives in Aircrafts

 Coordinatore UNIVERSITA DEGLI STUDI DI PARMA 

 Organization address address: VIA UNIVERSITA 12
city: PARMA
postcode: 43100

contact info
Titolo: Prof.
Nome: Stefano
Cognome: Selleri
Email: send email
Telefono: +39 0521 905763
Fax: +39 0521 905758

 Nazionalità Coordinatore Italy [IT]
 Totale costo 799˙676 €
 EC contributo 599˙757 €
 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) 2014-10-01   -   2016-07-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    UNIVERSITA DEGLI STUDI DI PARMA

 Organization address address: VIA UNIVERSITA 12
city: PARMA
postcode: 43100

contact info
Titolo: Prof.
Nome: Stefano
Cognome: Selleri
Email: send email
Telefono: +39 0521 905763
Fax: +39 0521 905758

IT (PARMA) coordinator 521˙681.70
2    RAW POWER SRL

 Organization address address: VIA PANSA 47
city: Reggio Emilia
postcode: 42124

contact info
Titolo: Mr.
Nome: Andrea Stefano
Cognome: Crinto
Email: send email
Telefono: +39 0522 334042
Fax: +39 0522 513772

IT (Reggio Emilia) participant 78˙075.38

Mappa


 Word cloud

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

software    voltage    life    motor    actual    bed    line    moreover    data    reliability    realize    accelerated    converter    electric   

 Obiettivo del progetto (Objective)

'Reliability in electronics is nowadays one of the most important subjects of study, as the range of its application is very wide. At the moment, the lifetime problems have been addressed by analysing separately the causes of failure and accelerated tests were proposed for the single components. This proposal aims at realizing a test bed able to apply multiple age accelerating stresses and to realize the on-line test of the machine under different operating conditions. The test rig will embed an environmental chamber able to replicate the ambient conditions at 50000ft, moreover, a custom converter able to vary the voltage stress at the motor’s terminal will be developed, in order to test the reliability of the motor with the converters of the future, that will employ always faster devices. In the aerospace industry, reliability is an extremely important and researched feature for the electric drive systems. Given the life-span of an actual aircraft and the costs of unplanned maintenance, the results of this research are potentially of great impact in how designers now realize electric drives. The procedures to realize the test bed, the data acquisition software and the post-processing software that will be developed during the project will be helpful to further push the technology limits. Moreover, the test of actual motors and the data acquired will constitute a database that will improve the existing knowledge of life time models. The ability to modify the actual voltage waveform characteristics of the converter driving the motor under test, in conjunction with the other test facilities, constitutes a great improvement on the existing testing methodology, that usually imply off-line accelerated testing of the twisted pairs.'

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