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11. 发明授权

EP2411686B1 BIELLE COUDEE EQUIPEE D'AU MOINS UN MOYEN D'AUTO-ALIGNEMENT 有权
标题翻译：与至少一个自对准指配备BENT VERBINDUNGSSTANGE
公开(公告)号：EP2411686B1
公开(公告)日：2014-12-10
申请号：EP10715310.8
申请日：2010-03-09
申请人： Aircelle
发明人： VAUCHEL, Guy, Bernard , SEGAT, Peter , BAILLARD, André , BOURET, Georges, Alain
IPC分类号： F16C7/06 , F16C7/04 , F02K1/12 , F02K1/70 , F02K1/72
CPC分类号： F16C7/04 , F02K1/1261 , F02K1/70 , F02K1/72 , F16C7/06 , Y10T74/2142

12. 发明公开

EP2501920A1 INVERSEUR DE POUSSÉE 有权
标题翻译： 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。

13. 发明公开

EP2238032A2 SYSTÈME DE GUIDAGE POUR LA MAINTENANCE D'UNE NACELLE D'AÉRONEF 审中-公开
标题翻译：管理系统的维护飞机发动机GONDEL的
公开(公告)号：EP2238032A2
公开(公告)日：2010-10-13
申请号：EP09716458.6
申请日：2009-01-21
申请人： Aircelle
发明人： CARUEL, Pierre , JORET, Jean-Philippe , SEGAT, Peter
IPC分类号： B64D29/08
CPC分类号： B64D29/08
摘要： The invention relates to a nacelle (100) for the turbojet of an aircraft that comprises a downstream structure including: an outer structure (106), a concentric inner structure (109) surrounding a downstream portion (111) of the turbojet and including an upstream section having a relatively small diameter (113) and a downstream section having a relatively large diameter (114), wherein said inner structure (109) defines together with the outer structure (106) an annular flow channel (108); and a guiding system (140) for connecting the inner structure (109) and the downstream portion (111) of the turbojet engine or a portion of a suspension mast; characterised in that the guiding system (140) includes a means for combining a translation and rotation movement of at least a portion of said inner structure (109) between a working position, in which the inner structure (109) is used as a cowling for the turbojet downstream portion (111), and a maintenance position in which the inner structure (109) exposes said turbojet downstream portion (111), thus enabling the movement of said portion if the inner structure (109) along the profile of the upstream section having a relatively small diameter (113), and then of the downstream section having a relatively large diameter (114).

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