公开(公告)号：US09109509B2

公开(公告)日：2015-08-18

申请号：US13671233

申请日：2012-11-07

Applicant: AIRCELLE

Inventor： Christophe Thorel ,  Bertrand Desjoyeaux ,  Florent Bouillon ,  John Moutier ,  Stéphane Bardin

IPC: B64D33/02 ,  F02C7/04 ,  B64D29/06 ,  F02C7/045 ,  F02K1/80 ,  F02K1/82

CPC classification number: F02C7/04 ,  B64D29/06 ,  F02C7/045 ,  F02K1/80 ,  F02K1/827 ,  Y02T50/672 ,  Y10T29/49826 ,  Y10T403/45

Abstract: A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.

Abstract translation: 提供了一种用于飞机推进器的单元，其包括构造成附接到第二套圈的第一套圈和构造成固定到固定到第二套圈的第二对应连接凸缘的第一连接凸缘。 连接凸缘包括形成相对于第一套圈沿径向方向延伸的平面的部分。 第一套圈和对应的连接凸缘之间的连接偏移到与所述平面相对应的距离，该长度与用于阻尼通过第一套圈的力的通量产生的剪切产生弯曲力矩的长度相对应。

公开(公告)号：US20140086678A1

公开(公告)日：2014-03-27

申请号：US14093761

申请日：2013-12-02

Applicant: AIRCELLE

Inventor： Xavier CAZUC ,  Christophe Thorel ,  John Moutier

IPC: F04D29/52

CPC classification number: F04D29/52 ,  B64D29/00 ,  B64D29/06 ,  B64D2033/0286 ,  F02C7/04 ,  F05D2300/702 ,  F16B2200/50 ,  Y02T50/672

Abstract: An assembly for an aircraft nacelle includes a reinforcing plate and a flange that includes one first portion and one second portion. The first portion of the flange is attached to another flange, and the second portion extends transversely relative to the first portion and is attached onto a panel of the assembly. In particular, the reinforcing plate is attached directly, or optionally indirectly, onto the flange via an intermediate plate attached between the reinforcing plate and the flange. The reinforcing plate has a beveled portion opposite the second portion of the flange.

Abstract translation: 用于飞机机舱的组件包括加强板和包括一个第一部分和一个第二部分的凸缘。 凸缘的第一部分附接到另一凸缘，并且第二部分相对于第一部分横向延伸并且附接到组件的面板上。 特别地，加强板通过附接在加强板和凸缘之间的中间板直接地或可选地间接地附接到凸缘上。 加强板具有与凸缘的第二部分相对的斜面部分。

公开(公告)号：US20130315657A1

公开(公告)日：2013-11-28

申请号：US13671233

申请日：2012-11-07

Applicant: AIRCELLE

Inventor： Christophe Thorel ,  Bertrand Desjoyeaux ,  Florent Bouillon ,  John Moutier ,  Stéphane Bardin

IPC: F02C7/04

CPC classification number: F02C7/04 ,  B64D29/06 ,  F02C7/045 ,  F02K1/80 ,  F02K1/827 ,  Y02T50/672 ,  Y10T29/49826 ,  Y10T403/45

Abstract: A unit for an aircraft thruster is provided that includes a first ferrule configured to be attached to a second ferrule and a first connection flange configured to be secured to a second corresponding connection flange secured to the second ferrule. The connection flange includes a portion forming a plane extending along a radial direction with respect to the first ferrule. A link between the first ferrule and the corresponding connection flange is offset to a distance from said plane corresponding to a length for damping a shear-generating flexural moment, generated by fluxes of forces passing through the first ferrule.

Abstract translation: 提供了一种用于飞机推进器的单元，其包括构造成附接到第二套圈的第一套圈和构造成固定到固定到第二套圈的第二对应连接凸缘的第一连接凸缘。 连接凸缘包括形成相对于第一套圈沿径向方向延伸的平面的部分。 第一套圈和对应的连接凸缘之间的连接偏移到与所述平面相对应的距离，该长度与用于阻尼通过第一套圈的力的通量产生的剪切产生弯曲力矩的长度相对应。