EP 2742227 A1 20140618 - EXHAUST PLUG FOR AN AIRCRAFT TURBOJET ENGINE
Title (en)
EXHAUST PLUG FOR AN AIRCRAFT TURBOJET ENGINE
Title (de)
ABGASANLAGE FÜR EIN TL-TRIEBWERK EINES FLUGZEUGES
Title (fr)
CÔNE D'ÉJECTION POUR TURBORÉACTEUR D'AÉRONEF
Publication
Application
Priority
- FR 1157322 A 20110812
- FR 2012051574 W 20120705
Abstract (en)
[origin: WO2013024216A1] This exhaust plug (1) for an aircraft turbojet engine, comprising a front part (5) intended for attachment to a rear part (7), each having an outer skin (21, 29), is characterised in that the front part and the rear part are connected by at least one connecting flange (31) common to these two parts and on which the outer skins are arranged side by side.
IPC 8 full level
F02K 1/04 (2006.01); F02K 1/44 (2006.01); F02K 1/80 (2006.01); F02K 1/82 (2006.01)
CPC (source: EP US)
F02K 1/04 (2013.01 - EP US); F02K 1/80 (2013.01 - EP US); F02K 1/82 (2013.01 - US); F05D 2230/232 (2013.01 - EP US); F05D 2250/283 (2013.01 - EP US); F05D 2260/30 (2013.01 - EP US); Y02T 50/60 (2013.01 - EP US)
Citation (search report)
See references of WO 2013024216A1
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
DOCDB simple family (publication)
FR 2978988 A1 20130215; FR 2978988 B1 20130726; BR 112014002208 A2 20170221; CA 2842871 A1 20130221; CN 103764985 A 20140430; EP 2742227 A1 20140618; RU 2014108518 A 20150920; US 2014165574 A1 20140619; WO 2013024216 A1 20130221
DOCDB simple family (application)
FR 1157322 A 20110812; BR 112014002208 A 20120705; CA 2842871 A 20120705; CN 201280039238 A 20120705; EP 12741041 A 20120705; FR 2012051574 W 20120705; RU 2014108518 A 20120705; US 201414177503 A 20140211