WISDOM

WING STRUCTURAL TEST DEVELOPMENT METHOD

Coordinatore	SERVICIOS DE TECNOLOGIA INGENIERIA E INFORMATICA SL    more  Organization address address: CALLE MORSE 3 city: GETAFE MADRID postcode: 28906 contact info Titolo: Mr. Nome: Eduardo Alberto Cognome: Cano Corral Email: send email Telefono: 34917241775 Fax: 34917903532
Nazionalità Coordinatore	Spain [ES]
Totale costo	3˙430˙272 €
EC contributo	2˙572˙704 €
Programma	FP7-JTI Specific Programme "Cooperation": Joint Technology Initiatives
Code Call	SP1-JTI-CS-2012-02
Funding Scheme	JTI-CS
Anno di inizio	2013
Periodo (anno-mese-giorno)	2013-01-14   -   2016-12-13

 Partecipanti

#	participant	country	role	EC contrib. [€]
1	SERVICIOS DE TECNOLOGIA INGENIERIA E INFORMATICA SL  Organization address address: CALLE MORSE 3 city: GETAFE MADRID postcode: 28906 contact info Titolo: Mr. Nome: Eduardo Alberto Cognome: Cano Corral Email: send email Telefono: 34917241775 Fax: 34917903532	ES (GETAFE MADRID)	coordinator	1˙561˙644.00
2	FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS  Organization address address: "Parque Tecnologico de Alava (Minano), C/ Juan de la Cierva 1" city: MINANO (ALAVA) postcode: 1510 contact info Titolo: Dr. Nome: Saez De Ocariz Cognome: Idurre Email: send email Telefono: 34945296924	ES (MINANO (ALAVA))	participant	588˙960.00
3	TESTING AND ENGINEERING OF AERONAUTICAL MATERIALS AND STRUCTURES SL  Organization address address: CALLE WILBURG Y ORVILLE WRIGHT 1 city: LA RINCONADA SEVILLA postcode: 41309 contact info Titolo: Ms. Nome: Esther Cognome: Garcia Email: send email Telefono: 34954115060	ES (LA RINCONADA SEVILLA)	participant	422˙100.00

Mappa

 Word cloud

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 Obiettivo del progetto (Objective)

'The proposal approach innovative solutions for the design and manufacturing of the test rig and the definition of the method and prformance for the structural testing of two different kinds of configuration for the outer wings within a Smart Fixed Wing Aircraft. The WISDOM proposal, understand that the test philosophy is to demonstrate that major components tests can be performed on flight test aircraft. The main requirement for this wing structural part is based on their high dimensional stability and tight geometrical tolerances to compliance with surface quality for a natural laminar flow condition, and therefore stability control and manufacturing precision over the test bench tools to be designed and manufactured shall consider this, avoiding as much as possible interfaces with the specimen surfaces. The test procedure is based in a Self-supporting test rig with flexible and adaptative plug and play loads introduction method with minimum specimen interface needs and wireless connection for data recording'