COUPLING AND UNCOUPLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOJET ENGINE NACELLE
    1.
    发明申请
    COUPLING AND UNCOUPLING MECHANISM FOR AN ONBOARD DEVICE OF A TURBOJET ENGINE NACELLE 审中-公开
    用于涡轮发动机起动装置的联接和解除机构

    公开(公告)号:US20150083823A1

    公开(公告)日:2015-03-26

    申请号:US14558833

    申请日:2014-12-03

    Applicant: AIRCELLE

    Abstract: A mechanism for coupling and uncoupling a motor inlet shaft and an outlet shaft, in particular, the inlet shaft is mounted in rotation on a front frame, and the outlet shaft is mounted in rotation on a rear frame. The outlet shaft rotates an outlet pinion, and the rear frame is slidably mounted to translate between a forward compact position and a backward deployed position. The mechanism includes a coupler, and first and second lockers to couple or uncouple the inlet and outlet shafts according to the translation of the rear frame between the forward compact position and the backward deployed position. The first locker locks in rotation the inlet shaft on the front frame, the second locker locks the outlet shaft on the rear frame. In particular, the second locker automatically locks the inlet and outlet shafts in rotation respectively, according to the displacement of the rear frame.

    Abstract translation: 用于将电动机入口轴和出口轴,特别是入口轴联接和分离的机构旋转安装在前框架上,并且出口轴旋转安装在后框架上。 出口轴使出口小齿轮旋转,并且后框架可滑动地安装以在前部紧凑位置和向后展开位置之间平移。 该机构包括联接器,以及第一和第二储物柜,用于根据在前紧凑位置和向后展开位置之间的后框架的平移来连接或分离入口和出口轴。 第一个储物柜锁定前框架上的入口轴,第二个储物柜将出口轴锁定在后框架上。 特别地,第二储物柜根据后框架的位移自动将入口和出口轴锁定在旋转中。

    DE-ICING AND CONDITIONING DEVICE FOR AN AIRCRAFT
    2.
    发明申请
    DE-ICING AND CONDITIONING DEVICE FOR AN AIRCRAFT 审中-公开
    用于飞机的起动和调节装置

    公开(公告)号:US20160102610A1

    公开(公告)日:2016-04-14

    申请号:US14974427

    申请日:2015-12-18

    Applicant: AIRCELLE

    Abstract: The present disclosure provides a device for de-icing an air inlet lip of an aircraft nacelle. The device includes a pre-exchanger, an intake orifice of taking in low-pressure air downstream from a fan, and two high-pressure air intake orifices downstream from a compressor in addition to controlled valves and check valves installed in an air flow network. In particular, the pre-exchanger includes a low-pressure air outlet capable of opening into the air inlet lip of the aircraft nacelle via a pipe of the air flow network.

    Abstract translation: 本公开提供了一种用于除冰飞机机舱的进气口的装置。 该装置除了安装在空气流动网络中的受控制的阀和止回阀之外,还包括一个前置换器,一个从风扇下游吸入低压空气的进气孔和一个压缩机下游的两个高压进气口。 特别地,预交换器包括能够经由空气流动网络的管道进入飞机机舱的进气口的低压空气出口。

    METHOD FOR CONTROLLING A VARIABLE NOZZLE SECTION OF AN AIRCRAFT
    3.
    发明申请
    METHOD FOR CONTROLLING A VARIABLE NOZZLE SECTION OF AN AIRCRAFT 审中-公开
    用于控制飞机的可变喷嘴部分的方法

    公开(公告)号:US20150108235A1

    公开(公告)日:2015-04-23

    申请号:US14584435

    申请日:2014-12-29

    Applicant: AIRCELLE

    CPC classification number: F02K1/15 F02K1/763 F02K9/80 F05D2270/051

    Abstract: A method for controlling a position of a variable nozzle of an aircraft includes the following steps: setting the variable nozzle in a position P(t0) at a time t0 as a preliminary step; step A in which at each instant ti with 1

    Abstract translation: 用于控制飞行器的可变喷嘴的位置的方法包括以下步骤:将可变喷嘴设置在时间t0的位置P(t0)作为初步步骤; 步骤A,其中在每个时刻ti具有1

    TURBOJET ENGINE NACELLE
    4.
    发明申请
    TURBOJET ENGINE NACELLE 有权
    涡轮发动机NACELLE

    公开(公告)号:US20130121814A1

    公开(公告)日:2013-05-16

    申请号:US13731150

    申请日:2012-12-31

    Applicant: Aircelle Snecma

    CPC classification number: F01D25/24 B64D29/06 B64D29/08

    Abstract: A nacelle for a turbojet engine is provided that includes an air intake upstream from the turbojet engine, a middle section intended to surround a fan of the turbojet engine and its case, and a downstream section. The middle section is made from at least one aerostructure capable of ensuring external aerodynamic continuity of the nacelle, and the aerostructure is rigidly bound, so as to be able to be taken apart, to at least one surrounding fixed structure.

    Abstract translation: 提供了一种用于涡轮喷气发动机的机舱,其包括涡轮喷气发动机上游的进气口,旨在围绕涡轮喷气发动机及其壳体的风扇的中间部分和下游部分。 中间部分由能够确保机舱的外部空气动力学连续性的至少一个航空结构制成,并且航空结构刚性地结合,以便能够被分离到至少一个周围的固定结构。

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