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    AIRCRAFT PROPULSION ASSEMBLY
    1.
    发明申请
    AIRCRAFT PROPULSION ASSEMBLY 审中-公开
    飞机推进装置

    公开(公告)号：US20130277454A1

    公开(公告)日：2013-10-24

    申请号：US13856038

    申请日：2013-04-03

    Applicant: AIRCELLE ,  Snecma

    Inventor： Herve Hurlin ,  Nicolas Dezeustre ,  Wouter Balk ,  Francois Gallet

    IPC: F02K1/56

    CPC classification number: F02K1/566 ,  F01D5/005 ,  F02K1/605 ,  F02K1/625 ,  F02K1/72 ,  F02K1/766 ,  F05D2230/80 ,  F05D2240/14 ,  Y02T50/672 ,  Y02T50/673

    Abstract: The disclosure relates to an aircraft propulsion assembly including a nacelle having an intermediate housing and a front frame that is to be mounted downstream of an outer envelope of the intermediate housing. The front frame includes a deviation edge and an element forming a direct or indirect support for at least one flow deviation vanes, in particular, the deviation edge and the support-forming element are built into the outer envelope of the intermediate housing.

    Abstract translation: 本发明涉及一种飞机推进组件，其包括具有中间壳体和将被安装在中间壳体的外壳的下游的前框架的机舱。 前框架包括偏离边缘和形成用于至少一个流动偏离叶片的直接或间接支撑的元件，特别地，偏转边缘和支撑形成元件被内置在中间壳体的外包层中。

    ASSEMBLY FOR ATTACHING THE HANGERS FROM WHICH AN AIRCRAFT PROPULSION UNIT IS SUSPENDED
    2.
    发明申请
    ASSEMBLY FOR ATTACHING THE HANGERS FROM WHICH AN AIRCRAFT PROPULSION UNIT IS SUSPENDED 有权
    装配飞机推进装置悬挂装置的装配

    公开(公告)号：US20130227963A1

    公开(公告)日：2013-09-05

    申请号：US13862724

    申请日：2013-04-15

    Applicant: AIRCELLE ,  SNECMA

    Inventor： Herve Hurlin ,  Nicolas Dezeustre ,  Wouter Balk ,  Gilles Charier

    IPC: B64D27/26

    CPC classification number: B64D27/26 ,  B64D2027/266

    Abstract: An assembly is designed to attach hangers from which an aircraft propulsion unit is suspended. The propulsion unit is intended to be suspended from a structural element of the aircraft. The propulsion unit includes a turbojet engine having a longitudinal axis and the attachment assembly having a clevis mount for attaching the hangers to a casing of the propulsion unit. The clevis mount is fixed to the casing by means designed to form a connection between the clevis mount and the casing at the external periphery of the casing.

    Abstract translation: 一个组件被设计成连接飞机推进装置悬挂的吊架。 推进装置旨在悬挂在飞行器的结构部件上。 推进单元包括具有纵向轴线的涡轮喷气发动机，并且附接组件具有用于将悬挂器附接到推进单元的壳体的U形夹安装件。 U形夹安装件通过设计成在壳体外周形成U形夹安装件与壳体之间的连接的方式固定在壳体上。

    Assembly for attaching the hangers from which an aircraft propulsion unit is suspended
    4.
    发明授权
    Assembly for attaching the hangers from which an aircraft propulsion unit is suspended 有权
    用于连接悬挂有飞机推进装置的吊架的组件

    公开(公告)号：US08839629B2

    公开(公告)日：2014-09-23

    申请号：US13862724

    申请日：2013-04-15

    Applicant: Aircelle ,  Snecma

    Inventor： Herve Hurlin ,  Nicolas Dezeustre ,  Wouter Balk ,  Gilles Charier

    IPC: B64D27/26

    CPC classification number: B64D27/26 ,  B64D2027/266

    Abstract: An assembly is designed to attach hangers from which an aircraft propulsion unit is suspended. The propulsion unit is intended to be suspended from a structural element of the aircraft. The propulsion unit includes a turbojet engine having a longitudinal axis and the attachment assembly having a clevis mount for attaching the hangers to a casing of the propulsion unit. The clevis mount is fixed to the casing by means designed to form a connection between the clevis mount and the casing at the external periphery of the casing.

    Abstract translation: 一个组件被设计成连接飞机推进装置悬挂的吊架。 推进装置旨在悬挂在飞行器的结构部件上。 推进单元包括具有纵向轴线的涡轮喷气发动机，并且附接组件具有用于将悬挂器附接到推进单元的壳体的U形夹安装件。 U形夹安装件通过设计成在壳体外周形成U形夹安装件与壳体之间的连接的方式固定在壳体上。

    THRUST REVERSER
    7.
    发明申请
    THRUST REVERSER 有权
    逆转器

    公开(公告)号：US20130280031A1

    公开(公告)日：2013-10-24

    申请号：US13855947

    申请日：2013-04-03

    Applicant: AIRCELLE

    Inventor： Herve Hurlin ,  Nicolas Dezeustre ,  Wouter Balk ,  Bertrand Desjoyeaux

    IPC: F01D25/24

    CPC classification number: F01D25/24 ,  F01D5/005 ,  F02K1/605 ,  F02K1/625 ,  F02K1/72 ,  F02K1/766 ,  F05D2230/80 ,  F05D2240/14 ,  Y02T50/672 ,  Y02T50/673

    Abstract: A thrust reverser for the nacelle of a turboreactor includes at least one fixed front frame that can be mounted downstream of a fan casing of the turboreactor and directly or indirectly supports at least one flow deviation vanes, in which at least part of the flow deviation vanes can be detached from the front frame and moved in translation independently therefrom when a maintenance operation is being carried out on the reverser.

    Abstract translation: 用于涡轮反应器的机舱的推力反向器包括至少一个固定的前框架，其可以安装在涡轮反应器的风扇壳体的下游，并且直接或间接地支撑至少一个流动偏离叶片，其中至少一部分流动偏离叶片 当在反向器上进行维护操作时，可以从前框架拆下并且独立地移动。

    TURBINE ENGINE SUPPORT PART OF HYBRID STRUCTURE
    8.
    发明申请
    TURBINE ENGINE SUPPORT PART OF HYBRID STRUCTURE 审中-公开
    涡轮发动机支撑部分混合结构

    公开(公告)号：US20150021455A1

    公开(公告)日：2015-01-22

    申请号：US14377644

    申请日：2013-02-05

    Applicant: SAFRAN ,  SNECMA

    Inventor： Robin Mandel ,  Wouter Balk ,  Nicolas Christian Raymond Leblond ,  Jean-Yves Picart

    IPC: F02C7/32

    CPC classification number: F02C7/32 ,  F01D25/28 ,  F02C7/25 ,  F05D2300/603

    Abstract: A turbine engine support part including a main structure made of composite material and a reinforcing secondary structure made of metal and integrated in the main structure, the secondary structure presenting a geometrical shape and dimensions configured to impart mechanical strength to the support part in event of the main structure being destroyed.

    Abstract translation: 一种涡轮发动机支撑部件，包括由复合材料制成的主结构和由金属制成并且集成在主结构中的加强二次结构，所述二次结构呈现几何形状和尺寸，其被配置为在所述主结构中发生机械强度以赋予所述支撑部分 主体被破坏。

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