WIMCAM

BLADE Wing Measurement Campaign

Coordinatore	BIAS - BREMER INSTITUT FUR ANGEWANDTE STRAHLTECHNIK GMBH    more  Organization address address: KLAGENFURTER STRASSE 2 city: BREMEN postcode: 28359 contact info Titolo: Dr. Nome: Jan Cognome: Burke Email: send email Telefono: +49 421 218 58014
Nazionalità Coordinatore	Germany [DE]
Totale costo	299˙840 €
EC contributo	217˙703 €
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)	2015-10-01   -   2016-12-31

 Partecipanti

#	participant	country	role	EC contrib. [€]
1	BIAS - BREMER INSTITUT FUR ANGEWANDTE STRAHLTECHNIK GMBH  Organization address address: KLAGENFURTER STRASSE 2 city: BREMEN postcode: 28359 contact info Titolo: Dr. Nome: Jan Cognome: Burke Email: send email Telefono: +49 421 218 58014	DE (BREMEN)	coordinator	132˙405.00
2	VEW VEREINIGTE ELEKTRONIK WERKSTATTEN GMBH  Organization address address: EDISONSTRASSE 19 city: BREMEN postcode: 28357 contact info Titolo: Dr. Nome: Christoph Cognome: Von Kopylow Email: send email Telefono: +49 421 271530 Fax: +49 421 273608	DE (BREMEN)	participant	85˙298.00

Mappa

 Word cloud

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 Obiettivo del progetto (Objective)

'We propose to accompany the SFWA-BLADE flight test phase with adequate wing surface metrology, to measure profile, waviness, steps, gaps, 3D disturbances, and surface roughness. The envisaged metrology system already exists and its performance to the specifications stipulated in the call has been demonstrated on relevant reference artefacts. So far, we have successfully used it for on-site BLADE wing tooling measurements, demonstrating portability besides the uncertainty required.

The measurement system is a fringe-projection system, custom built for the specific requirements of wing metrology. It can e.g. easily detect waviness of 0.1 mm and its noise limit is about 10 micrometres. The nominal field of view is 1280x800 mm², making it perfectly suited for measurements in inter-rib spaces of the BLADE wings. It can be adjusted to any orientation desired, and its position can be registered with laser tracker assistance. This makes it possible to locate unconnected surface segments correctly in 3-D space, thus eliminating the need for large overlaps between surface sub-areas. However we have also shown that very good results are achievable without laser tracker assistance by 'stitching' of sub-areas together into one combined data set for the entire wing tip surface of 9x2 m².

The applicants have decades of experience in full-field non-contact optical metrology, including three years of collaboration within the current BLADE consortium under call JTI-CS-2010-05-SFWA-03-004. The business infrastructure for a successful effort is already in place, as are evaluation methods which will be further refined during the current call and will have reached a high degree of maturity by the scheduled start time of the flight test metrology campaign.'