STAGEDIS

Electrical Starter / Generator disconnect system

Coordinatore	CT INGENIEROS AERONAUTICOS DE AUTOMOCION E INDUSTRIALES SL    more  Organization address address: AVENIDA LEONARDO DA VINCI 22 PARQUE EMPRESARIAL LA CARPETANIA LA ATALAYUELA city: GETAFE (MADRID) postcode: 28906 contact info Titolo: Mr. Nome: Rubén Cognome: Piornedo Email: send email Telefono: 34609826320
Nazionalità Coordinatore	Spain [ES]
Totale costo	565˙600 €
EC contributo	282˙800 €
Programma	FP7-JTI Specific Programme "Cooperation": Joint Technology Initiatives
Code Call	SP1-JTI-CS-2013-03
Funding Scheme	JTI-CS
Anno di inizio	2015
Periodo (anno-mese-giorno)	2015-07-01   -   2016-12-31

 Partecipanti

#	participant	country	role	EC contrib. [€]
1	CT INGENIEROS AERONAUTICOS DE AUTOMOCION E INDUSTRIALES SL  Organization address address: AVENIDA LEONARDO DA VINCI 22 PARQUE EMPRESARIAL LA CARPETANIA LA ATALAYUELA city: GETAFE (MADRID) postcode: 28906 contact info Titolo: Mr. Nome: Rubén Cognome: Piornedo Email: send email Telefono: 34609826320	ES (GETAFE (MADRID))	coordinator	196˙000.00
2	INDRA SISTEMAS S.A.  Organization address address: Avenida de Bruselas 35 city: ALCOBENDAS-MADRID postcode: 28108 contact info Titolo: Mr. Nome: Luis Cognome: Verdugo Martín Email: send email Telefono: 34918948732	ES (ALCOBENDAS-MADRID)	participant	86˙800.00

Mappa

 Word cloud

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 Obiettivo del progetto (Objective)

'StaGeDis will establish new conceptual designs for a dual-use starter/generator disconnect system. New generation aircraft require higher level of electrical power, increasing weight and volume of the electrical machines. In order to compensate this increase of weight and volume the generator will be able to operate as an electric starter, eliminating the need of pneumatic starter. Due to safety reasons, the starter/generator requires a disconnection system to protect the machines and engine gearbox This disconnection system shall be able to separate mechanically the gearbox from the starter/generator with the electrical machine operating whether as starter or generator. This system will be commanded by an electrical pulse. Different technologies and architectures will be studied, evaluated and compared in order to define a proper disconnection system. Criteria of compactness, weight reduction and conformity with harsh aeronautic engine environment will be also an important part of the study. The selected solution will require a detailed design and the definition and methodology of the verification tests.'