EP 2279280 A2 20110202 - METHOD FOR COATING A FIBER COMPOSITE COMPONENT FOR AN AIRCRAFT OR SPACECRAFT AND FIBER COMPOSITE COMPONENT PRODUCED BY SAID METHOD
Title (en)
METHOD FOR COATING A FIBER COMPOSITE COMPONENT FOR AN AIRCRAFT OR SPACECRAFT AND FIBER COMPOSITE COMPONENT PRODUCED BY SAID METHOD
Title (de)
VERFAHREN ZUM BESCHICHTEN EINES FASERVERBUNDBAUTEILS FÜR EIN LUFT- ODER RAUMFAHRZEUG UND DURCH EIN DERARTIGES VERFAHREN HERGESTELLTES FASERVERBUNDBAUTEIL
Title (fr)
PROCÉDÉ POUR APPLIQUER UN REVÊTEMENT SUR UN ÉLÉMENT COMPOSITE RENFORCÉ PAR DES FIBRES POUR UN AÉRONEF OU UN VÉHICULE SPATIAL ET ÉLÉMENT COMPOSITE RENFORCÉ PAR DES FIBRES PRODUIT SELON UN TEL PROCÉDÉ
Publication
Application
Priority
- EP 2009052902 W 20090312
- DE 102008001468 A 20080430
- US 12600308 P 20080430
Abstract (en)
[origin: WO2009132885A2] The invention relates to a method for coating a fiber composite component (1) for an aircraft or spacecraft. According to said method, a surface layer (8) of the fiber composite component (1) which is interspaced from the fibers (3) that have been introduced into the fiber composite component (1) to protect them is pretreated in at least some sections thereof to form an adhesive layer (1); at least one functional layer (17, 18) is then applied to the formed adhesive layer (13). A corresponding fiber composite component (1) comprises at least one functional layer (17, 18) which is applied to an adhesive layer (13).
IPC 8 full level
C23C 4/02 (2006.01); B64D 45/02 (2006.01)
CPC (source: EP US)
C23C 4/02 (2013.01 - EP US); C23C 4/04 (2013.01 - EP US); C23C 4/08 (2013.01 - US); C23C 4/12 (2013.01 - EP US); C23C 4/129 (2016.01 - EP US); Y10T 428/249921 (2015.04 - EP US); Y10T 428/31678 (2015.04 - EP US)
Citation (examination)
US 2007042126 A1 20070222 - PASSMAN RICHARD K [US], et al
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK TR
Designated extension state (EPC)
AL BA RS
DOCDB simple family (publication)
WO 2009132885 A2 20091105; WO 2009132885 A3 20100415; WO 2009132885 A4 20100603; BR PI0911880 A2 20170523; CA 2722108 A1 20091105; CN 102027150 A 20110420; CN 102027150 B 20130814; DE 102008001468 A1 20091112; DE 102008001468 B4 20130919; EP 2279280 A2 20110202; JP 2011518956 A 20110630; RU 2010142648 A 20120610; US 2011091709 A1 20110421; US 2011256414 A1 20111020
DOCDB simple family (application)
EP 2009052902 W 20090312; BR PI0911880 A 20090312; CA 2722108 A 20090312; CN 200980115403 A 20090312; DE 102008001468 A 20080430; EP 09737929 A 20090312; JP 2011506623 A 20090312; RU 2010142648 A 20090312; US 201113152371 A 20110603; US 91027010 A 20101022