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1. 发明申请

US20110262270A1 NACELLE EQUIPPED WITH AT LEAST ONE EXCESS PRESSURE FLAP 有权
标题翻译： NACELLE装备有至少一个超压压片
公开(公告)号：US20110262270A1
公开(公告)日：2011-10-27
申请号：US12674200
申请日：2008-08-05
申请人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurélie De Sorbay , Thierry Jacques Albert Le Docte
发明人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurélie De Sorbay , Thierry Jacques Albert Le Docte
IPC分类号： F01D25/28
CPC分类号： B64D29/08 , F01D21/14 , F02C7/00 , F05D2240/14 , Y02T50/671
摘要： The present invention relates to a jet engine nacelle (1), of the type comprising an aft section forming an external structure (2) which, together with a concentric internal structure (4) comprising an internal panel (10) intended to surround a down-stream portion of the jet engine, defines an annular flow duct for a so-called secondary stream (3), characterized in that exhaust means (11) are formed in the internal panel such that any unwanted excess pressure is discharged into the annular duct.
摘要翻译：本发明涉及一种喷气式发动机舱（1），其类型包括形成外部结构（2）的后部，该外部结构与包括内部面板（10）的同心内部结构（4）一起包围下部喷气发动机的流动部分限定了用于所谓的二次流（3）的环形流动管道，其特征在于，排气装置（11）形成在内部面板中，使得任何不需要的过量压力被排放到环形管道。

2. 发明授权

US08480355B2 Nacelle comprising at least one surge trap 有权
标题翻译：至少包括一个喘振陷阱的机舱
公开(公告)号：US08480355B2
公开(公告)日：2013-07-09
申请号：US12674015
申请日：2008-07-23
申请人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurelie De Sorbay , Thierry Jacques Albert Le Docte
发明人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurelie De Sorbay , Thierry Jacques Albert Le Docte
IPC分类号： F01D11/00
CPC分类号： B64D29/08 , F01D21/14 , F02C7/00 , F05D2240/14 , Y02T50/671
摘要： The invention relates to a nacelle for a turbojet engine, comprising a rear section forming an outer structure which defines, together with a concentric inner structure (4) comprising an inner panel (10) for surrounding a downstream part of the turbojet engine, an annular flow channel for a so-called secondary flow. The invention is characterized in that the exhaust means (11) are arranged in the inner panel in such a way that any inopportune surge is exhausted in the annular channel.
摘要翻译：本发明涉及一种用于涡轮喷气发动机的机舱，包括形成外部结构的后部，该外部结构与包括用于围绕涡轮喷气发动机的下游部分的内部板（10）的同心内部结构（4）一起限定，环形所谓二次流的流动通道。本发明的特征在于，排气装置（11）以这样的方式设置在内板中，使得在环形通道中任何不合适的浪涌被排出。

3. 发明授权

US5967460A Pivoting door thrust reverser with actuating mechanism 失效
标题翻译：旋转门推力反向器与致动机构
公开(公告)号：US5967460A
公开(公告)日：1999-10-19
申请号：US942912
申请日：1997-10-02
申请人： Pierre Andre Marcel Baudu , Xavier Raymond Yves Lore
发明人： Pierre Andre Marcel Baudu , Xavier Raymond Yves Lore
IPC分类号： B64D33/00 , F02K1/32 , F02K1/70
CPC分类号： F02K1/70 , Y02T50/671
摘要： An actuating mechanism is disclosed for a thrust reverser of a turbojet engine having an engine cowling with a reverse thrust opening, a thrust reverser door pivotally connected to the engine cowling so as to pivot between forward and reverse thrust positions, and a linear actuator having a casing with an extendable and retractable piston rod. The piston rod is connected to the thrust reverser by a first connection forming a first connection point. An interface bracket is fixedly attached to the turbojet engine structure and engages a mounting flange in a connector affixed to the actuator casing at a second connection point, the mounting flange being in contact with the interface bracket at a third connection point, the first, second and third connection points lying in a straight line.
摘要翻译：公开了一种用于涡轮喷气发动机的推力反向器的致动机构，其具有具有反向推力开口的发动机整流罩，可枢转地连接到发动机整流罩以便在正向和反向推力位置之间枢转的推力反向器门以及具有外壳具有可伸缩的活塞杆。活塞杆通过形成第一连接点的第一连接件连接到推力反向器。接口支架固定地连接到涡轮喷气发动机结构，并且在第二连接点处与固定到致动器壳体的连接器中的安装凸缘接合，安装凸缘在第三连接点与接口支架接触，第一，第二并且第三连接点位于直线上。

4. 发明申请

US20110171014A1 NACELLE COMPRISING AT LEAST ONE SURGE TRAP 有权
标题翻译：包含至少一个冲击带的NACELLE
公开(公告)号：US20110171014A1
公开(公告)日：2011-07-14
申请号：US12674015
申请日：2008-07-23
申请人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurelie De Sorbay , Thierry Jacques Albert Le Docte
发明人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurelie De Sorbay , Thierry Jacques Albert Le Docte
IPC分类号： F01D25/24
CPC分类号： B64D29/08 , F01D21/14 , F02C7/00 , F05D2240/14 , Y02T50/671
摘要： The invention relates to a nacelle for a turbojet engine, comprising a rear section forming an outer structure which defines, together with a concentric inner structure (4) comprising an inner panel (10) for surrounding a downstream part of the turbojet engine, an annular flow channel for a so-called secondary flow. The invention is characterised in that the exhaust means (11) are arranged in the inner panel in such a way that any inopportune surge is exhausted in the annular channel.
摘要翻译：本发明涉及一种用于涡轮喷气发动机的机舱，包括形成外部结构的后部，该外部结构与包括用于围绕涡轮喷气发动机的下游部分的内部板（10）的同心内部结构（4）一起限定，环形所谓二次流的流动通道。本发明的特征在于，排气装置（11）以这样的方式设置在内板中，使得在环形通道中任何不合适的浪涌被排出。

5. 发明授权

US6032901A Linkage system for an aircraft turbojet engine 失效
标题翻译：飞机涡轮喷气发动机联动系统
公开(公告)号：US6032901A
公开(公告)日：2000-03-07
申请号：US969360
申请日：1997-11-28
申请人： Felix Carimali , Jean-Paul Rene Andre Hogie , Xavier Raymond Yves Lore , Pascal Gerard Rouyer
发明人： Felix Carimali , Jean-Paul Rene Andre Hogie , Xavier Raymond Yves Lore , Pascal Gerard Rouyer
IPC分类号： B64D29/06 , B64D33/00 , F01D25/24 , F02K1/60 , F02K1/80 , B64C1/14
CPC分类号： B64D29/06 , F01D25/24 , F02K1/80 , Y02T50/671 , Y10T292/0837
摘要： A linkage system is disclosed for releasably latching a thrust reverser to an engine casing having a longitudinal axis, the linkage system having a seat on the thrust reverser and a movable latching member on the engine casing movable between an open position in which the latching member is displaced away from the seat, and a closed position in which the latching member is located adjacent to the seat so as to prevent displacement of the thrust reverser away from the engine casing.
摘要翻译：公开了一种联动系统，用于可释放地将推力反向器锁定到具有纵向轴线的发动机壳体上，该联动系统在推力反向器上具有座椅，并且在发动机壳体上的可移动的闩锁构件可在打开位置之间移动，其中闩锁构件离开座椅的位置，以及闭合位置，其中闩锁构件邻近座椅定位，以防止推力反向器远离发动机壳体的位移。

6. 发明授权

US08529199B2 Locking device 有权
标题翻译：锁定设备
公开(公告)号：US08529199B2
公开(公告)日：2013-09-10
申请号：US12673716
申请日：2008-06-12
申请人： Xavier Raymond Yves Lore , Michel Christian Marie Jean
发明人： Xavier Raymond Yves Lore , Michel Christian Marie Jean
IPC分类号： F01D25/24
CPC分类号： E05C19/10 , B64D29/06 , B64D29/08 , E05B63/0056 , E05B63/14
摘要： The invention relates to a locking device (13) that includes at least one locking system (16), intended to be placed on a first moving element (11), and a retaining member (17), intended to be placed on a second moving element (12), the locking system (16) having a first hook (18) designed to engage with the retaining member so as to lock the locking device (13). The locking system (16) includes at least a second hook (19) set back from the first hook (18) so as to engage with the retaining member in the event of the first hook (18) breaking.
摘要翻译：本发明涉及一种锁定装置（13），其包括旨在放置在第一移动元件（11）上的至少一个锁定系统（16）以及旨在放置在第二移动元件（11）上的保持构件（17）所述锁定系统（16）具有设计成与所述保持构件接合以便锁定所述锁定装置（13）的第一钩（18）。锁定系统（16）包括从第一钩（18）回缩的至少第二钩（19），以便在第一钩（18）断裂的情况下与保持构件接合。

7. 发明申请

US20110103946A1 LOCKING DEVICE 有权
标题翻译：锁定设备
公开(公告)号：US20110103946A1
公开(公告)日：2011-05-05
申请号：US12673716
申请日：2008-06-12
申请人： Xavier Raymond Yves Lore , Michel Christian Marie Jean
发明人： Xavier Raymond Yves Lore , Michel Christian Marie Jean
IPC分类号： F01D25/24
CPC分类号： E05C19/10 , B64D29/06 , B64D29/08 , E05B63/0056 , E05B63/14
摘要： The invention relates to a locking device (13) that includes at least one locking system (16), intended to be placed on a first moving element (11), and a retaining member (17), intended to be placed on a second moving element (12), the locking system (16) having a first hook (18) designed to engage with the retaining member so as to lock the locking device (13). The locking system (16) includes at least a second hook (19) set back from the first hook (18) so as to engage with the retaining member in the event of the first hook (18) breaking.
摘要翻译：本发明涉及一种锁定装置（13），其包括旨在放置在第一移动元件（11）上的至少一个锁定系统（16）以及旨在放置在第二移动元件（11）上的保持构件（17）所述锁定系统（16）具有设计成与所述保持构件接合以便锁定所述锁定装置（13）的第一钩（18）。锁定系统（16）包括从第一钩（18）回缩的至少第二钩（19），以便在第一钩（18）断裂的情况下与保持构件接合。

8. 发明授权

US08529196B2 Nacelle equipped with at least one excess pressure flap 有权
标题翻译：机舱配备至少一个多余的压力皮瓣
公开(公告)号：US08529196B2
公开(公告)日：2013-09-10
申请号：US12674200
申请日：2008-08-05
申请人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurélie De Sorbay , Thierry Jacques Albert Le Docte
发明人： Xavier Raymond Yves Lore , Pascal-Marie Paul Marcel Soulier , Aurélie De Sorbay , Thierry Jacques Albert Le Docte
IPC分类号： F01D25/28
CPC分类号： B64D29/08 , F01D21/14 , F02C7/00 , F05D2240/14 , Y02T50/671
摘要： The present invention relates to a jet engine nacelle (1), of the type comprising an aft section forming an external structure (2) which, together with a concentric internal structure (4) comprising an internal panel (10) intended to surround a down-stream portion of the jet engine, defines an annular flow duct for a so-called secondary stream (3), characterized in that exhaust means (11) are formed in the internal panel such that any unwanted excess pressure is discharged into the annular duct.
摘要翻译：本发明涉及一种喷气式发动机舱（1），其类型包括形成外部结构（2）的后部，该外部结构与包括内部面板（10）的同心内部结构（4）一起包围下部喷气发动机的流动部分限定了用于所谓的二次流（3）的环形流动管道，其特征在于，排气装置（11）形成在内部面板中，使得任何不需要的过量压力被排放到环形管道。

9. 发明授权

US07007454B2 Locking system on a cascade thrust reverser 有权
标题翻译：级联推力反向器上的锁定系统
公开(公告)号：US07007454B2
公开(公告)日：2006-03-07
申请号：US10489675
申请日：2002-09-26
申请人： Michel Philippe Dehu , Xavier Raymond Yves Lore
发明人： Michel Philippe Dehu , Xavier Raymond Yves Lore
IPC分类号： F02K3/02
CPC分类号： F02K1/72 , F02K1/766 , Y02T50/672
摘要： The invention provides a locking system on a cascade thrust reverser for a bypass turbojet, the reverser (20) comprising guide means (60) for the movable parts (50), and the guide means (60) comprising rails (64) attached to the movable parts (50) and tracks (62) attached to the longitudinal members (36).According to the invention, the locking system (80) comprises locks (82) located at the end (62a) of each track (62) in the opening direction (52), each lock comprising a bolt (110) capable of preventing the rail (64) moving in the opening direction (52).
摘要翻译：本发明提供了一种用于旁通涡轮喷气发动机的级联推力反向器的锁定系统，反向器（20）包括用于可移动部件（50）的引导装置（60），并且引导装置（60）包括连接到可移动部件（50）和附接到纵向构件（36）的轨道（62）。根据本发明，锁定系统（80）包括位于每个轨道（62）沿开口方向（52）的端部（62a）处的锁（82），每个锁包括能够防止导轨（64）沿打开方向（52）移动。

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