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Patent Searching and Data


Title:
REAR SECTION OF AN AIRCRAFT INCLUDING AN ENGINE MOUNTING STRUCTURE SWINGABLY MOUNTED ON THE FUSELAGE
Document Type and Number:
WIPO Patent Application WO/2010/112742
Kind Code:
A3
Abstract:
The invention relates to a rear section of an aircraft including two connecting rods (66) symmetrically arranged on either side of a vertical median plane (P), each connecting rod having an end mounted on an engine mounting structure (14) and another end mounted on the fuselage (6), said section being designed so as to enable, by rotating the connecting rods (66) about the rotational axes thereof, a limited amplitude swinging movement of the assembly (23) formed by the mounting structure and the engines, relative to the fuselage (6), through first and second openings (18) of the fuselage.

Inventors:
LAFONT LAURENT (FR)
SAUCRAY JEAN MICHEL (FR)
QUIROZ-HERNANDEZ ESTEBAN (FR)
ANTYPAS JEROME (FR)
BONNET MATHIEU (FR)
JOURNADE FREDERIC (FR)
Application Number:
PCT/FR2010/050566
Publication Date:
March 17, 2011
Filing Date:
March 29, 2010
Export Citation:
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Assignee:
AIRBUS OPERATIONS SAS (FR)
LAFONT LAURENT (FR)
SAUCRAY JEAN MICHEL (FR)
QUIROZ-HERNANDEZ ESTEBAN (FR)
ANTYPAS JEROME (FR)
BONNET MATHIEU (FR)
JOURNADE FREDERIC (FR)
International Classes:
B64C1/16; B64D27/08; B64D27/14; B64D27/26
Domestic Patent References:
WO2010031958A22010-03-25
Foreign References:
EP0884498A21998-12-16
EP0429100A11991-05-29
EP0311155A21989-04-12
US3490556A1970-01-20
Attorney, Agent or Firm:
DU BOISBAUDRY, Dominique (95 rue d'Amsterdam, Paris Cedex 8, FR)
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