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1. 发明申请

US20110174930A1 FUSE LINK DEVICE BETWEEN A MOBILE PART AND A FIXED PART OF AN AIRCRAFT NACELLE 有权
标题翻译：移动部件与飞机零件固定部件之间的保险丝连接装置
公开(公告)号：US20110174930A1
公开(公告)日：2011-07-21
申请号：US13008592
申请日：2011-01-18
申请人： Alain PORTE , Jacques LALANE , Franck ALVAREZ
发明人： Alain PORTE , Jacques LALANE , Franck ALVAREZ
IPC分类号： B64C1/14 , B64D29/00
CPC分类号： B64D29/06 , B64D29/08
摘要： The object of the invention is an aircraft nacelle that comprises at least one part, called a door (14), that moves relative to a stationary part (20) and a connecting device that makes it possible to limit the offset between said door and said stationary part in a direction that corresponds to the primary direction of the flow of air outside of the nacelle during flight, whereby said device comprises, on the one hand, an indexer (40) that is connected to the door (14) that comprises an attachment surface (63) and at least one attachment element (66), and, on the other hand, at least one stop (58) that is connected to the stationary part (20) against which said indexer (40) can rest in such a way as to limit its movement in said direction, characterized in that said at least one attachment element (66), oriented in the radial direction, is arranged upstream from the stop (58) in said direction, said at least one stop (58) comprising a surface relative to the door arranged essentially at the attachment surface (63) of the indexer (40).
摘要翻译：本发明的目的是一种飞机机舱，其包括称为门（14）的至少一部分，其相对于静止部分（20）和连接装置移动，所述连接装置使得可以限制所述门和所述第二门固定部分在与飞行中的机舱外部的空气流的主要方向对应的方向上，其中所述装置一方面包括连接到门（14）的分度器（40），该分度器包括一个附接表面（63）和至少一个附接元件（66），另一方面，连接到所述固定部分（20）的至少一个止动件（58），所述分度器（40）能够抵靠所述固定部分一种限制其在所述方向上移动的方式，其特征在于，所述至少一个在径向方向上定向的连接元件（66）沿着所述方向设置在止动件（58）的上游，所述至少一个止动件）包括相对于所述门的表面，其基本上a布置 t分度器（40）的附接表面（63）。

2. 发明申请

US20120090694A1 AIRCRAFT NACELLE INCLUDING A REAR FRAME INCLINED TO THE REAR 有权
标题翻译：飞机包括后面的框架
公开(公告)号：US20120090694A1
公开(公告)日：2012-04-19
申请号：US13270536
申请日：2011-10-11
申请人： Alain PORTE , Jacques LALANE , Frederic CHELIN
发明人： Alain PORTE , Jacques LALANE , Frederic CHELIN
IPC分类号： F02K99/00
CPC分类号： B64D33/02 , B64D2033/0206 , B64D2033/0286 , Y10T137/0536
摘要： An aircraft nacelle includes a lip whose surface contacts with the aerodynamic streams extends inside the nacelle by an inside wall that delimits a layer that empties at a power plant and outside of the nacelle by an outside wall, a first front frame connects the inside and outside walls, delimiting an annular pipe with the lip, and a rear frame connects the inside and outside walls at a junction zone between the inside pipe and power plant pipe, for a given cross-section of the nacelle along a plane that contains the longitudinal axis of the nacelle, a point A at the intersection between the rear frame and the inside wall, and a point B at the intersection between the rear frame and the outside wall, with B being offset toward the rear of the nacelle relative to A over more than 50% of the rear frame's periphery.
摘要翻译：飞机机舱包括其表面与空气动力流接触的唇缘，其通过内壁在内部壁延伸，所述内壁限定通过外壁在发电厂和机舱外部排空的层，第一前框架连接内外围绕边缘限定一个环形管，并且后框架在内管和发电厂管之间的接合区连接内壁和外壁，对于机舱的给定横截面沿着包含纵向轴线的平面机舱，后框架和内壁之间的交点处的点A和后框架与外壁之间的交叉点处的点B，其中B相对于A更靠近机舱的后部超过后框架周边的50％。

3. 发明申请

US20130040117A1 WALL REINFORCED COMPOSITE MATERIAL 审中-公开
标题翻译：墙体增强复合材料
公开(公告)号：US20130040117A1
公开(公告)日：2013-02-14
申请号：US13565996
申请日：2012-08-03
申请人： Alain PORTE , Jacques LALANE
发明人： Alain PORTE , Jacques LALANE
IPC分类号： B32B3/10
CPC分类号： F02C7/045 , B29C70/088 , B29C70/688 , B29C70/865 , F02K1/827 , F05D2300/702 , Y02T50/672 , Y10T428/24851
摘要： A wall panel of composite material including at least two carbon fiber layers oriented parallel to the plane of the panel and embedded in a resin matrix. At least one reinforcement mesh is inserted between the two fiber layers. The mesh has at least a first series of linear elements with a section greater than or equal to 0.07 mm2 The reinforcement mesh is embedded in the resin matrix, and the two layers arranged on both sides of the mesh are linked in all zones situated between the linear elements of the mesh.
摘要翻译：一种复合材料的墙板，其包括至少两个平行于所述面板的平面定向并且嵌入在树脂基体中的碳纤维层。在两个纤维层之间插入至少一个加强网。网格具有至少第一系列具有大于或等于0.07mm 2的截面的线性元件。加强网被嵌入在树脂基体中，并且布置在网的两侧上的两层连接在位于网格的线性元素。

4. 发明申请

US20120090695A1 AIRCRAFT NACELLE INCLUDING AT LEAST ONE RADIAL PARTITION BETWEEN TWO CONDUCTS 有权
标题翻译：包括两个行为之间的至少一个径向分区的航空器
公开(公告)号：US20120090695A1
公开(公告)日：2012-04-19
申请号：US13270604
申请日：2011-10-11
申请人： Alain PORTE , Jacques LALANE , Frederic CHELIN , Thierry SURPLY
发明人： Alain PORTE , Jacques LALANE , Frederic CHELIN , Thierry SURPLY
IPC分类号： F02C7/04
CPC分类号： B64D33/02 , B64D2033/0206 , B64D2033/0286 , Y10T137/0536
摘要： An aircraft nacelle that makes it possible to channel a stream of air in a longitudinal direction and that includes at least two panels (50, 50′) placed end to end in the longitudinal direction, each including a so-called aerodynamic surface (52, 52′) that is in contact with the air stream and an edge (54, 54′) that is in contact with the edge of the other panel, characterized in that at least one of the panels includes—at its edge (54, 54′)—at least one partition (58) that projects relative to the edge that extends in the direction of the edge of the other panel, in a manner that is secant to the aerodynamic surface and in a plane that contains the longitudinal direction, so as to limit the circulation of air between the edges of the panels.
摘要翻译：一种飞机机舱，其使得可以沿纵向引导空气流，并且包括沿纵向方向端对端放置的至少两个面板（50,50'），每个面板（50,50'）包括所谓的空气动力学表面（52， 52'）和与所述另一面板的边缘接触的边缘（54,54'），其特征在于，至少一个所述面板包括在其边缘（54,54） '） - 至少一个相对于沿着另一个面板的边缘方向延伸的边缘突出的分隔件58，其以与空气动力学表面相切并且包含纵向方向的平面的方式，因此以限制面板边缘之间的空气循环。

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