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1. WO2011001121 - SYSTEM FOR ATTACHING AN IMPELLER ENGINE

Publication Number WO/2011/001121
Publication Date 06.01.2011
International Application No. PCT/FR2010/051387
International Filing Date 01.07.2010
IPC
B64D 27/26 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26Aircraft characterised by construction of power-plant mounting
CPC
B64D 2027/266
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26Aircraft characterised by construction of power-plant mounting
262Engine support arrangements or elements
266comprising suspension arrangements for supporting vertical loads
B64D 27/26
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
26Aircraft characterised by construction of power-plant mounting
Applicants
  • AIRBUS OPERATIONS (S.A.S) [FR]/[FR] (AllExceptUS)
  • BONNET, Mathieu [FR]/[FR] (UsOnly)
Inventors
  • BONNET, Mathieu
Agents
  • SCHMIT CHRETIEN
Priority Data
095458103.07.2009FR
Publication Language French (FR)
Filing Language French (FR)
Designated States
Title
(EN) SYSTEM FOR ATTACHING AN IMPELLER ENGINE
(FR) SYSTÈME D'ATTACHE D'UN MOTEUR À HÉLICES
Abstract
(EN)
The invention relates to a system for attaching an element (3) capable of vibrating onto an aircraft structure (2), comprising at least one pair of scoops (10) attached onto the element capable of vibrating, as well as onto the structure, each scoop (10a, 10b) of the pair of scoops comprising: an outer rigid element (12) attached onto the structure; an inner rigid element (13) mounted inside the outer rigid element and rigidly connected to the element capable of vibrating; and a flexible element (14) placed along each outer rigid element flank, between the outer rigid element and the inner rigid element.
(FR)
L'invention concerne un système d'attache d'un élément susceptible de vibrer (3) sur une structure (2) d'aéronef, comportant au moins une paire de pelles (10) fixée, d'une part, sur l'élément susceptible de vibrer et, d'autre part, sur la structure, chaque pelle (10a, 10b) de la paire de pelles comportant : - un élément rigide externe (12) fixé sur la structure, - un élément rigide interne (13) monté à l'intérieur de l'élément rigide externe et solidaire de l'élément susceptible de vibrer, et - un élément souple (14) placé le long de chaque flanc de l'élément rigide externe, entre l'élément rigide externe et l'élément rigide interne.
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