Global Patent Index - EP 2627561 A1

EP 2627561 A1 20130821 - ASSEMBLY FOR ATTACHING THE HANGERS FROM WHICH AN AIRCRAFT PROPULSION UNIT IS SUSPENDED

Title (en)

ASSEMBLY FOR ATTACHING THE HANGERS FROM WHICH AN AIRCRAFT PROPULSION UNIT IS SUSPENDED

Title (de)

ANORDNUNG ZUR BEFESTIGUNG VON AUFHÄNGERN ZUR AUFHÄNGUNG EINER FLUGZEUGANTRIEBSANORDNUNG

Title (fr)

ENSEMBLE D'ACCROCHAGE D'UNE SUSPENSION D'UN ENSEMBLE PROPULSIF D'AÉRONEF

Publication

EP 2627561 A1 20130821 (FR)

Application

EP 11779788 A 20111004

Priority

  • FR 1058406 A 20101015
  • FR 2011052307 W 20111004

Abstract (en)

[origin: WO2012049399A1] The invention relates to an assembly for attaching the hangers from which an aircraft propulsion unit is suspended, which propulsion unit is intended to be suspended from a structural element of an aircraft, said propulsion unit comprising a turbojet engine having a longitudinal axis, said attachment assembly comprising at least one clevis mount (100) for attaching the hangers to a casing (120) of said propulsion unit, characterized in that the clevis mount (100) is fixed to said casing (120) by means designed to form a connection between said clevis mount (100) and said casing (120) at the external periphery of said casing (120).

IPC 8 full level

B64D 27/26 (2006.01)

CPC (source: EP US)

B64D 27/40 (2024.01 - EP US); B64D 27/404 (2024.01 - EP); B64D 27/404 (2024.01 - US)

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)

WO 2012049399 A1 20120419; BR 112013007208 A2 20160614; CA 2812373 A1 20120419; CN 103153789 A 20130612; EP 2627561 A1 20130821; FR 2966125 A1 20120420; FR 2966125 B1 20130426; RU 2013121274 A 20141120; US 2013227963 A1 20130905; US 8839629 B2 20140923

DOCDB simple family (application)

FR 2011052307 W 20111004; BR 112013007208 A 20111004; CA 2812373 A 20111004; CN 201180048614 A 20111004; EP 11779788 A 20111004; FR 1058406 A 20101015; RU 2013121274 A 20111004; US 201313862724 A 20130415