发明名称 ASSEMBLY FOR AN AIRCRAFT COMPRISING AN ATTACHMENT PYLON PRIMARY STRUCTURE FORMED WITH THREE INDEPENDENT ELEMENTS
摘要 In order to optimize the bulkiness of a primary structure of an aircraft engine attachment pylon and thus make it easier to install under the wing and as close as possible to the pressure face thereof, the disclosure herein provides an assembly in which the engine comprises a rear part arranged under a wing element equipped with a wing box, the primary structure being made up of the following independent elements: a first and a second side beam arranged one on each side of a vertical mid-plane of the engine; and an intermediate structure through which the vertical mid-plane of the engine passes and which is situated some distance from each of the first and second side beams.
申请公布号 US2015307199(A1) 申请公布日期 2015.10.29
申请号 US201514693545 申请日期 2015.04.22
申请人 Airbus Operations (S.A.S.) 发明人 Pautis Olivier;Blanc Jonathan
分类号 B64D29/02;B64D27/18;B64D27/26 主分类号 B64D29/02
代理机构 代理人
主权项 1. An assembly for an aircraft comprising a wing element, a bypass engine and an engine attachment pylon, the engine comprising a rear part arranged under the wing element equipped with a wing box, the pylon comprising a primary structure for transmitting loads from the engine to the wing box, and the assembly further comprising attachment structure for attaching the primary structure to the engine and attachment structure for attaching the primary structure to the wing box, wherein the primary structure is made up of the following independent elements: a first and a second side beam arranged one on each side of a vertical mid-plane of the engine; andan intermediate structure through which the vertical mid-plane of the engine passes and which is situated some distance from each of the first and second side beams.
地址 Toulouse FR