EP 2084063 A1 20090805 - JET ENGINE NACELLE MEMBER
Title (en)
JET ENGINE NACELLE MEMBER
Title (de)
TRIEBWERKSGONDELEMENT
Title (fr)
ELEMENT DE NACELLE DE TURBOREACTEUR
Publication
Application
Priority
- FR 2007001580 W 20070927
- FR 0609608 A 20061103
Abstract (en)
[origin: WO2008053088A1] The invention relates to an nacelle member (1) comprising at least one mobile cowling (2) pivotally or slidably mounted in an essentially longitudinal direction of the nacelle, capable of displacement between an expanded position and a closed position relative to a fixed structure of the nacelle member (1) through at least one pivoting or translation guiding sleeve (4, 7) that receives a guiding shaft (5, 6). An electric heating de-icing device (9, 13) is provided inside the guiding shaft or defines an interface between the guiding shaft (5, 6) and the guiding sleeve (4, 7).
IPC 8 full level
B64D 29/06 (2006.01); B64D 15/12 (2006.01); F02K 1/72 (2006.01)
CPC (source: EP US)
B64D 15/12 (2013.01 - EP US); B64D 29/06 (2013.01 - EP US); F02K 1/72 (2013.01 - EP US)
Citation (search report)
See references of WO 2008053088A1
Designated contracting state (EPC)
AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HU IE IS IT LI LT LU LV MC MT NL PL PT RO SE SI SK TR
DOCDB simple family (publication)
WO 2008053088 A1 20080508; BR PI0717965 A2 20131105; CA 2666747 A1 20080508; CN 101528542 A 20090909; EP 2084063 A1 20090805; FR 2908109 A1 20080509; FR 2908109 B1 20081212; RU 2009120114 A 20101210; US 2010064660 A1 20100318
DOCDB simple family (application)
FR 2007001580 W 20070927; BR PI0717965 A 20070927; CA 2666747 A 20070927; CN 200780039105 A 20070927; EP 07848291 A 20070927; FR 0609608 A 20061103; RU 2009120114 A 20070927; US 51343207 A 20070927