Title (en)

TURBOJET ENGINE NACELLE COMPRISING A UNIT ASSEMBLY CAPABLE OF MOVING ALONG A GUIDE ASSEMBLY

Title (de)

TURBOSTRAHL-TRIEBWERKSGONDEL MIT EINER EINHEITENBAUGRUPPE ZUR BEWEGUNG ENTLANG EINER SCHIENENBAUGRUPPE

Title (fr)

NACELLE POUR TURBOREACTEUR COMPRENANT UN ENSEMBLE UNITAIRE MOBILE LE LONG D'UN ENSEMBLE DE GUIDAGE

Publication

EP 2917109 A1 20150916 (FR)

Application

EP 13803117 A 20131108

Priority

• FR 1260623 A 20121109
• FR 2013052685 W 20131108

Abstract (en)

[origin: WO2014072655A1] The present invention relates to an assembly comprising at least one nacelle (1) unit assembly (9) for a turbojet engine, capable of moving relative to a fixed structure along at least one associated guide element (15), said guide assembly comprising: - at least one guiding element (17, 20) secured to the fixed structure; - at least one guided element (19) secured to the unit assembly, shaped to move along the guiding element; - at least one contact surface (21, 25) common to said guiding and guided elements.

IPC 8 full level

B64D 29/06 (2006.01); F02K 1/72 (2006.01); F02K 1/80 (2006.01)

CPC (source: EP US)

B64D 29/06 (2013.01 - EP US); F01D 25/24 (2013.01 - US); F02K 1/54 (2013.01 - US); F05D 2220/323 (2013.01 - US); F05D 2260/50 (2013.01 - US)

Citation (search report)

See references of WO 2014072655A1

Designated contracting state (EPC)

AL 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 RS SE SI SK SM TR

Designated extension state (EPC)

BA ME

DOCDB simple family (publication)

WO 2014072655 A1 20140515; BR 112015008204 A2 20170704; CA 2887470 A1 20140515; CN 104781144 A 20150715; EP 2917109 A1 20150916; FR 2997925 A1 20140516; FR 2997925 B1 20160304; RU 2015121970 A 20170110; US 2016208738 A1 20160721

DOCDB simple family (application)

FR 2013052685 W 20131108; BR 112015008204 A 20131108; CA 2887470 A 20131108; CN 201380058766 A 20131108; EP 13803117 A 20131108; FR 1260623 A 20121109; RU 2015121970 A 20131108; US 201514703144 A 20150504