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1.发明授权DISPOSITIF D'INVERSION DE POUSSÉE INTÉGRÉ ET NACELLE DE MOTEUR D'AÉRONEF AINSI ÉQUIPÉE 有权集成推压反转装置和飞机引擎NELELLE SOIL EQUIPED
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公开(公告)号：EP2971729A4
公开(公告)日：2016-12-07
申请号：EP14774314
申请日：2014-03-11
CPC分类号： F02K1/70 , F02C6/08 , F02C7/18 , F02K1/76 , F05D2260/608 , Y02T50/675
摘要： A gas turbine engine includes a fan duct, an inner fixed structure, and a thrust reverser assembly. The inner fixed structure forms an inner diameter of the fan duct and encloses a core compartment. The thrust reverser assembly includes a linkage assembly mounted to the inner fixed structure within the fan duct. The linkage assembly is adapted to act as a ventilation system that allows for communication between the fan duct and the core compartment.
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公开(公告)号：EP3091198A1
公开(公告)日：2016-11-09
申请号：EP16168699.3
申请日：2016-05-09
发明人： MARCOS, Juan A.
CPC分类号： F02K1/566 , F01D21/14 , F02C3/04 , F02C9/26 , F02K1/09 , F02K1/72 , F02K1/76 , F02K1/766 , F05D2270/095 , F05D2270/102 , F05D2270/114 , F05D2270/335 , Y02T50/671
摘要： A method of thrust reversal operation according to an example of the present disclosure includes, among other things, permitting an increase in engine power when at least one criterion is not met and a thrust reverser is deployed, and denying the increase in engine power when the at least one criterion is met. A system for thrust reversal is also disclosed.
摘要翻译： 根据本公开的示例的推力反转操作的方法包括，当至少一个标准不被满足并且部署推力反向器时允许增加发动机功率，并且当发动机功率增加时 至少满足一个标准。 还公开了一种用于推力反转的系统。
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4.发明授权SYSTÈME D'ACTIONNEMENT POUR ÉLÉMENT MOBILE DE NACELLE DE MOTEUR D'AÉRONEF, TEL QU'UN CAPOT D'INVERSEUR DE POUSSÉE 有权控制系统的参数便携式TRIEBWERKSGONDELEMENT飞机，比如SCHUBUMKEHRERSCHUTZ
公开(公告)号：EP2452049B1
公开(公告)日：2016-10-12
申请号：EP10745307.8
申请日：2010-06-23
申请人： Aircelle
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公开(公告)号：EP2419620B1
公开(公告)日：2016-06-15
申请号：EP10715953.5
申请日：2010-03-18
申请人： Aircelle
发明人： MAALIOUNE, Hakim
CPC分类号： F02K1/70 , F02K1/76 , F02K1/763 , F05D2270/52 , F05D2270/54 , F05D2270/62 , H02K11/33 , H02K16/04
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6.发明公开DISPOSITIF D'INVERSION DE POUSSÉE POUR UN AÉRONEF COMPRENANT AU MOINS DEUX INVERSEURS DE POUSSÉE 审中-公开反推装置上使用至少两个反推一个平面
公开(公告)号：EP2867512A1
公开(公告)日：2015-05-06
申请号：EP13744650.6
申请日：2013-06-27
申请人： Aircelle
CPC分类号： F02K1/763 , B64D33/04 , B64D41/00 , B64D2221/00 , F02K1/76 , F05D2260/901 , F05D2270/62 , H02P7/06 , Y02T50/44 , Y02T50/671
摘要： The present invention relates to a thrust-reversal device for an aircraft which includes at least two thrust reversers including a cowl which is movable between a closed position and an open position, actuated by at least one actuator (5, 5') driven by at least one electric motor powered by a single power-conversion module (100, 200, 300) supplied with electricity by a single electricity source of said aircraft. The device according to the invention is characterised in that the power-conversion module includes at least one autotransformer (301) supplied with AC electric voltage by the electricity source (3) and connected to at least one rectifier stage suitable for converting said AC voltage into DC voltage, said rectifier stage being connected to a stage for balancing and/or smoothing the current which is suitable for supplying DC voltage to said electric motor (6, 6') of said actuator (5, 5') of said cowl.
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公开(公告)号：EP2725217A2
公开(公告)日：2014-04-30
申请号：EP13005068.5
申请日：2013-10-23
发明人： Todorovic, Predrag
IPC分类号： F02K1/72
CPC分类号： F02K1/72 , F02K1/76 , F02K1/805 , F05D2240/55 , F05D2250/283 , F05D2260/96 , F05D2300/431 , F05D2300/603 , Y02T50/672
摘要： A blocker door for a gas turbine engine thrust reverser having a tray with a base and sidewalls extending about the base to define a volume, the volume being closed by a cover that extends beyond the periphery of the tray. The extension of the cover beyond the periphery provides a sealing feature.
摘要翻译： 一种用于燃气涡轮发动机推力反向器的阻塞门，其具有带有基部的托盘和围绕基部延伸的侧壁以限定容积，该体积由延伸超过托盘周边的盖封闭。 盖的延伸超过周边提供了密封特征。
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8.发明公开SYSTÈME D'ACTIONNEMENT POUR ÉLÉMENT MOBILE DE NACELLE DE MOTEUR D'AÉRONEF, TEL QU'UN CAPOT D'INVERSEUR DE POUSSÉE 有权控制系统的参数便携式TRIEBWERKSGONDELEMENT飞机，比如SCHUBUMKEHRERSCHUTZ
公开(公告)号：EP2452049A1
公开(公告)日：2012-05-16
申请号：EP10745307.8
申请日：2010-06-23
申请人： Aircelle
发明人： LE COQ, Vincent, Pierre, Germain , MORADELL-CASELLAS, Pierre , MAALIOUNE, Hakim , DESCAMPS, Alexandre
摘要： This system for actuating at least one aircraft nacelle element comprises at least two actuators (A1, A2, A3) kinematically linked together, a main hydraulic (or electric) generation circuit (1) able to operate at least one (A1) of the two actuators, and a secondary electric (or hydraulic) generation circuit (13) able to operate the other actuator (A3).
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9.发明公开SYSTEME D'ACTIONNEMENT POUR UN PANNEAU MOBILE D'UNE NACELLE DE TURBOREACTEUR 审中-公开宝贝系列FÜREINE BEWEGLICHE平底锅EINER GONDEL EINES TURBOJETS
公开(公告)号：EP2419330A1
公开(公告)日：2012-02-22
申请号：EP10723216.7
申请日：2010-04-07
申请人： Aircelle , Sagem Défense Sécurité
摘要： The invention relates to a system for actuating a plurality of actuators (15) that can move a mobile panel of an aircraft nacelle. Said system comprises at least two motors (16) that can drive the actuators (15), the two motors (16) being controlled and supplied by at least two separate control units (33, 35), and the actuators (15) being mechanically interconnected by a mechanical transmission (37). The invention also relates to a nacelle comprising such an actuating system.
摘要翻译： 本发明涉及一种用于致动能够移动飞机机舱的移动面板的多个致动器（15）的系统。 所述系统包括至少两个可驱动致动器（15）的马达（16），两个马达（16）由至少两个单独的控制单元（33,35）控制和供应，并且致动器（15）机械地 通过机械传动装置互连（37）。 本发明还涉及包括这种致动系统的机舱。
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10.发明公开THURST REVERSER SYSTEM POWER DRIVE UNIT WITH DUAL SEQUENTIAL TORQUE DECOUPLER 审中-公开与双通道器件对于连续转矩解耦反向推力系统驱动单元
公开(公告)号：EP1576273A1
公开(公告)日：2005-09-21
申请号：EP03812995.3
申请日：2003-12-12
IPC分类号： F02K1/76
摘要： A thrust reverser system that includes one or more power drive units (220) operable to supply a drive force. The power drive unit includes a motor (214) and at least two output sections (216a, 216b), each operably coupled to transmit the drive force to the trust reverser movable components. Each of the output sections is operable to decouple the motor (214) from associated trust reverser movable components upon a torque magnitude being reached in the output section. A deadband coupler (302) is provided to couple the first and second output sections together a time period after the torque magnitude is reached in one of the output sections.
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