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    INVERSEUR DE POUSSÉE POUR TURBORÉACTEUR D'AÉRONEF
    5.
    发明公开
    INVERSEUR DE POUSSÉE POUR TURBORÉACTEUR D'AÉRONEF 审中-公开
    推力反向器用于飞机发动机

    公开(公告)号：EP2697497A1

    公开(公告)日：2014-02-19

    申请号：EP12721330.4

    申请日：2012-04-12

    申请人： Aircelle

    发明人： DEZEUSTRE, Nicolas ,  KERBLER, Olivier ,  HURLIN, Hervé ,  MORADELL-CASELLAS, Pierre

    IPC分类号： F02K1/72 ,  F02K1/76

    CPC分类号： F02K1/763 ,  F02K1/625 ,  F02K1/64 ,  F02K1/72 ,  F05D2250/34 ,  Y02T50/672

    摘要： The invention relates to a thrust reverser comprising vanes for deflecting flow and a cowl (23) able to move between an open position releasing said deflecting vanes and a closed position covering said deflecting vanes (25) and furthermore comprising rails (45) able to slide in slideways (30), the rails (45) being mounted directly or indirectly on said cowl (23) and the slideways (30) being mounted directly or indirectly on either side of a suspension pylon (8) or vice versa, characterized in that it comprises at least one actuator able to slide the cowl (23) between its open and closed positions, the actuator being disposed in line with the corresponding rail (45), said actuator being: - either an actuator having a rotating nut (51) connected to an endless screw (47), for sliding the corresponding rail or corresponding slideway, as the case may be, - or an actuator suitable for pulling on the corresponding rail or on the corresponding slideway, as the case may be.

    INVERSEUR DE POUSSÉE
    6.
    发明公开
    INVERSEUR DE POUSSÉE 有权
    INVERSEUR DEPOUSSÉE

    公开(公告)号：EP2501920A1

    公开(公告)日：2012-09-26

    申请号：EP10787848.0

    申请日：2010-10-26

    申请人： Aircelle

    发明人： VAUCHEL, Guy Bernard ,  CARUEL, Pierre ,  BAILLARD, André ,  SEGAT, Peter

    IPC分类号： F02K1/72

    CPC分类号： F02K1/72 ,  B64D29/06 ,  B64D29/08 ,  F01D25/24 ,  F01D25/243 ,  F01D25/28 ,  F02C7/20 ,  F02K1/54 ,  F02K1/64 ,  F02K1/68 ,  F05D2250/34

    摘要： The present invention relates to a thrust inverter for a turbojet engine nacelle (1) including at least one outer cowl (11) that is movable between a closed position and a thrust inversion position, said movable cowl also being able to be opened into a supporting position towards which said movable cowl is hinged and guided through the use of a guiding means that is suitable to said movable cowl and located substantially on a pylon, to which the nacelle is intended to be attached and at least one front frame (15) capable of being mounted downstream from an air blower housing for said turbojet engine and directly or indirectly holds at least one flow diversion means (12). Said thrust inverter is characterized in that the front frame is detachably connected to the housing in a translatable manner along at least one related guiding member (17) once said front frame is detached from the housing.

    摘要翻译： 用于涡轮喷气发动机机舱（1）的推力逆变器技术领域本发明涉及一种用于涡轮喷气发动机机舱（1）的推力逆变器，该推力逆变器包括至少一个在关闭位置和推力反向位置之间可移动的外罩（11），所述可移动罩还能够打开成支撑 通过使用适合于所述可移动罩的导向装置将所述可移动罩铰接和引导的位置，所述导向装置基本上定位在机舱打算连接到的吊架上，以及至少一个前框架（15） 安装在所述涡轮喷气发动机的送风机壳体的下游，并直接或间接地保持至少一个分流装置（12）。 所述推力逆变器的特征在于，一旦所述前框架从所述壳体拆卸，所述前框架就可沿着至少一个相关引导构件（17）以可平移的方式可拆卸地连接至所述壳体。

    TURBINENSCHAUFEL
    7.
    发明公开
    TURBINENSCHAUFEL 有权

    公开(公告)号：EP2087207A1

    公开(公告)日：2009-08-12

    申请号：EP07821492.1

    申请日：2007-10-18

    申请人： SIEMENS AKTIENGESELLSCHAFT

    发明人： GROSS, Heinz-Jürgen

    IPC分类号： F01D5/18

    CPC分类号： F01D5/187 ,  F01D5/147 ,  F05D2250/181 ,  F05D2250/28 ,  F05D2250/34 ,  F05D2250/70 ,  F05D2260/22141

    摘要： The invention relates to a turbine blade (10) comprising a plurality of ribs (18) arranged one after the other in a cooling channel (14) extending along a flow inlet edge (12). The plurality of ribs is split into pairs of ribs (24) formed by two ribs arranged in the form of a skating step.

    摘要翻译： 本发明涉及一种涡轮机叶片（10），该涡轮机叶片包括多个沿着流入口边缘（12）延伸的冷却通道（14）中一个接一个地布置的肋（18）。 多个肋被分成由以滑行步骤的形式布置的两个肋形成的成对的肋（24）。