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1. 发明申请

US20120301681A1 LAYING-UP METHOD FOR NON-PLANAR COMPOSITE COMPONENTS 有权
标题翻译：非平面复合材料的层叠方法
公开(公告)号：US20120301681A1
公开(公告)日：2012-11-29
申请号：US13235570
申请日：2011-09-19
申请人： Alberto Lozano Sevilla , José Orencio Granado Macarrilla , Vicente Martínez Valdegrama , Raúl Burgos Gallego
发明人： Alberto Lozano Sevilla , José Orencio Granado Macarrilla , Vicente Martínez Valdegrama , Raúl Burgos Gallego
IPC分类号： B32B3/00 , G06F17/50
CPC分类号： B29C70/386 , Y02T50/43 , Y10T428/24479 , Y10T428/24628 , Y10T428/24669
摘要： A method for laying-up the tapes of a prepeg composite material in the 0° direction of a non-planar composite component on a suitable mould using an ATL machine comprising steps of: a) determining the trajectories of said tapes as modified trajectories of geodesic trajectories complying with the following conditions in their projections in an horizontal plane: that the curvature radius R2 of their curved segments is bigger than a predetermined value Rmin; that the gap G2p between two contiguous tapes is comprised between 0 and a predetermined value Gmax; b) providing said modified trajectories to said ATL machine. The invention also refers to a non-planar composite component such as an skin of an aircraft wing having the tapes in the 0° direction following trajectories complying with said conditions.
摘要翻译：一种用于使用ATL机器在合适的模具上在非平面复合部件的0°方向上铺设预制复合材料带的方法，所述方法包括以下步骤：a）将所述带的轨迹确定为测地线的修改轨迹在水平面的突起中符合以下条件的轨迹：曲线段的曲率半径R2大于预定值Rmin; 两个连续带之间的间隙G2p在0和预定值Gmax之间; b）向所述ATL机器提供所述修改的轨迹。本发明还涉及一种非平面复合构件，例如机翼的皮肤，其具有沿着符合所述条件的轨迹之后的0°方向的带。

2. 发明授权

US08649897B2 Laying-up method for non-planar composite components 有权
标题翻译：非平面复合构件的铺设方法
公开(公告)号：US08649897B2
公开(公告)日：2014-02-11
申请号：US13235570
申请日：2011-09-19
申请人： Alberto Lozano Sevilla , José Orencio Granado Macarrilla , Vicente Martínez Valdegrama , Raúl Burgos Gallego
发明人： Alberto Lozano Sevilla , José Orencio Granado Macarrilla , Vicente Martínez Valdegrama , Raúl Burgos Gallego
IPC分类号： G06F19/00 , B32B3/00
CPC分类号： B29C70/386 , Y02T50/43 , Y10T428/24479 , Y10T428/24628 , Y10T428/24669
摘要： A method for laying-up the tapes of a prepeg composite material in the 0° direction of a non-planar composite component on a suitable mold using an ATL machine includes the steps of: a) determining the trajectories of the tapes as modified trajectories of geodesic trajectories complying with the following conditions in their projections in an horizontal plane: that the curvature radius R2 of their curved segments is bigger than a predetermined value Rmin; that the gap G2p between two contiguous tapes is comprised between 0 and a predetermined value Gmax; and b) providing modified trajectories to the ATL machine. The invention also refers to a non-planar composite component such as an skin of an aircraft wing having the tapes in the 0° direction following trajectories complying with conditions described.
摘要翻译：使用ATL机在合适的模具上在非平面复合部件的0°方向上铺设预制复合材料的带的方法包括以下步骤：a）确定带的轨迹为修改的轨迹在水平面的投影中符合以下条件的测地轨迹：曲线段的曲率半径R2大于预定值Rmin; 两个连续带之间的间隙G2p在0和预定值Gmax之间; 和b）向ATL机器提供改进的轨迹。本发明还涉及一种非平面复合构件，例如飞行器机翼的皮肤，其具有在遵循所述条件的轨迹之后的0°方向上的带。

3. 发明授权

US08597770B2 Composite material part with stringer on ramp 有权
标题翻译：复合材料部分带斜边斜坡
公开(公告)号：US08597770B2
公开(公告)日：2013-12-03
申请号：US12981635
申请日：2010-12-30
申请人： Vicente Martínez Valdegrama , José Orencio Granado Macarrilla , Manuel Recio Melero , Antonio Blázquez Ajenjo
发明人： Vicente Martínez Valdegrama , José Orencio Granado Macarrilla , Manuel Recio Melero , Antonio Blázquez Ajenjo
IPC分类号： B32B3/00 , B64C1/00 , B64C3/00
CPC分类号： B29C70/30 , B29C70/386 , B29L2031/3076 , B29L2031/7738 , Y02T50/43 , Y10T428/24612
摘要： Composite material part (11) with stringer (31) on ramp, manufactured from a stack of fabrics, which comprises at least one zone (13) with two sectors (17, 19) having a greater thickness than that of the surrounding zones and with the stringer (31) situated on an edge (21) of said zone (13) in which: a) each group of fabrics (27, 27′ . . . ; 29, 29′, . . . ) of said sectors (17, 19) has the dimensions to form on said edge (21) a ramp with an acceptable gradient 1/p so that the stringer (31) remains situated on the ramp; b) the stacking of the zone (13) is carried out firstly by placing the fabrics (27, 27′, . . . ) of the first sector (17) and on these the fabrics (29, 29′, . . . ) of the second sector (19) in such a way that in the coinciding section (35) of said edge (21) the gradient of the resulting ramp is 1/(p/2).
摘要翻译：复合材料部件（11），其具有在斜面上的纵梁（31），由一叠织物制成，其包括具有两个扇区（17,19）的至少一个区域（13），该区域具有比周围区域的厚度更大的厚度，位于所述区域（13）的边缘（21）上的纵梁（31），其中：a）所述区段（17）的每组织物（27,27'...，29,29'，...），19）具有在所述边缘（21）上形成具有可接受的梯度1 / p的斜面的尺寸，使得所述桁条（31）保持位于所述斜坡上; b）首先通过放置第一扇区（17）的织物（27,27'...）并且在这些织物（29,29'...）上进行区域（13）的堆叠，第二扇区（19）的方式使得在所述边缘（21）的重合部分（35）中，所得到的斜坡的斜率为1 /（p / 2）。

4. 发明申请

US20130026294A1 MANUFACTURING PROCEDURE OF A COMPOSITE PART OF A CLOSED COMPARTMENT WITH AN INTEGRATED ACCESS ASSEMBLY 有权
标题翻译：一体化集装箱组合件的复合部件的制造程序
公开(公告)号：US20130026294A1
公开(公告)日：2013-01-31
申请号：US13348170
申请日：2012-01-11
申请人： Teresa Latorre Plaza , Vicente Martínez Valdegrama , José Orencio Granado Macarrilla
发明人： Teresa Latorre Plaza , Vicente Martínez Valdegrama , José Orencio Granado Macarrilla
IPC分类号： B64C3/00 , B32B37/12 , B23P17/04 , B32B38/10
CPC分类号： B29C70/30 , B29C70/545 , B29L2031/3085 , Y02T50/43 , Y10T29/49826 , Y10T156/1062
摘要： Procedure for the manufacture of a composite part (13) of a closed compartment, said part (13) having an access assembly to said compartment through an opening (11) in said part (13), said access assembly comprising a cover (27) for said opening (11) and a housing panel (25) for said cover (27), comprising steps of: a) providing common laminates (31, 31′, 31″) of a composite material for said cover (27) and said housing panel (25) in an uncured state; b) cutting said common laminates (31, 31′, 31″) by the perimeter foreseen for said cover (27) and separating the cover laminates (33, 33′, 33″) and the housing panel laminates (35, 35′, 35″); c) manufacturing separately, on the one side, the cover (27) using said cover laminates (31, 31′, 31″) and, on the other side, the part (13) together with said housing panel (25) using said housing panel laminates (35, 35′, 35″).
摘要翻译：用于制造封闭隔室的复合部件（13）的步骤，所述部件（13）具有通过所述部件（13）中的开口（11）到所述隔间的进入组件，所述进入组件包括盖（27）对于所述开口（11）和用于所述盖（27）的壳体板（25），包括以下步骤：a）为所述盖（27）和所述盖（27）提供用于复合材料的常见层压板（31,31'，31“），未固化状态的住房面板（25）; b）通过所述盖（27）预见的周边切割所述普通层压板（31,31'，31“），并将所述盖层压板（33,33'，33”）和所述壳板层压板（35,35'，33“ 35“）; c）使用所述盖层压板（31,31'，31“）在一侧单独制造所述盖（27），并且在另一侧上使用所述盖板（31,31'，31”）与所述壳体面板（25）一起制造所述部件外壳板层压板（35,35'，35“）。

5. 发明申请

US20130001363A1 FILLER PANELS FOR THE SKINS OF AIRCRAFT FUEL TANKS 审中-公开
标题翻译：飞机燃油箱皮肤填充面板
公开(公告)号：US20130001363A1
公开(公告)日：2013-01-03
申请号：US13339101
申请日：2011-12-28
申请人： José Orencio Granado Macarrilla , Vicente Martínez Valdegrama , Daniel Casares Rodríguez , Manuel Recio Melero
发明人： José Orencio Granado Macarrilla , Vicente Martínez Valdegrama , Daniel Casares Rodríguez , Manuel Recio Melero
IPC分类号： B64D37/08
CPC分类号： B64C3/182 , B64C3/34
摘要： An aircraft lifting surface structured as a torsion box comprising upper and lower skins (19, 21) stiffened by span wise stringers (25, 25′, 25″), said aircraft lifting surface comprising one or more fuel tanks (31, 33, 35, 37) arranged inside of said torsion box and separated by bulkheads (41), the stringers (25, 25′, 25″) having extended feet in the intersection areas with said bulkheads (41), also comprising filler panels (45) of said skins (19, 21) covering the holes that remain between said skins (19, 21) and said bulkheads (41) outside said intersection areas, whose configuration is adapted for covering the space between the extended feet (26, 26′) of stringers (25, 25′), leaving a gap with them of a predetermined width (W1), thereby providing a self-fastening capability over each skin plane that facilitates the attachment of said filler panels (45) to said skins (19, 21).
摘要翻译：一种构造为扭转箱的飞机提升表面，包括由跨越纵梁（25,25'，25“）加固的上表皮和下表皮（19,21），所述飞行器提升表面包括一个或多个燃料箱（31,33,35 ，37），其布置在所述扭转箱的内部并由隔板（41）分隔，在与所述隔板（41）的交叉区域中具有延伸的脚的桁条（25,25'，25“）还包括填充板（45）所述表面（19,21）覆盖保留在所述外表面（19,21）和所述隔壁（41）之间的所述交叉区域外部的孔，其构造适于覆盖延伸的脚（26,26'）之间的空间（25,25'），与预定宽度（W1）留下间隙，从而在每个皮肤平面上提供便于将所述填充板（45）附接到所述外壳（19,21）的自固定能力）。

6. 发明授权

US09073271B2 Manufacturing procedure of a composite part of a closed compartment with an integrated access assembly 有权
标题翻译：具有集成进入组件的封闭隔室的复合部件的制造程序
公开(公告)号：US09073271B2
公开(公告)日：2015-07-07
申请号：US13348170
申请日：2012-01-11
申请人： Teresa Latorre Plaza , Vicente Martínez Valdegrama , José Orencio Granado Macarrilla
发明人： Teresa Latorre Plaza , Vicente Martínez Valdegrama , José Orencio Granado Macarrilla
IPC分类号： B29C70/30 , B29C70/54 , B29L31/30
CPC分类号： B29C70/30 , B29C70/545 , B29L2031/3085 , Y02T50/43 , Y10T29/49826 , Y10T156/1062
摘要： Procedure for the manufacture of a composite part (13) of a closed compartment, said part (13) having an access assembly to said compartment through an opening (11) in said part (13), said access assembly comprising a cover (27) for said opening (11) and a housing panel (25) for said cover (27), comprising steps of: a) providing common laminates (31, 31′, 31″) of a composite material for said cover (27) and said housing panel (25) in an uncured state; b) cutting said common laminates (31, 31′, 31″) by the perimeter foreseen for said cover (27) and separating the cover laminates (33, 33′, 33″) and the housing panel laminates (35, 35′, 35″); c) manufacturing separately, on the one side, the cover (27) using said cover laminates (31, 31′, 31″) and, on the other side, the part (13) together with said housing panel (25) using said housing panel laminates (35, 35′, 35″).
摘要翻译：用于制造封闭隔室的复合部件（13）的步骤，所述部件（13）具有通过所述部件（13）中的开口（11）到所述隔间的进入组件，所述进入组件包括盖（27）对于所述开口（11）和用于所述盖（27）的壳体板（25），包括以下步骤：a）为所述盖（27）和所述盖（27）提供用于复合材料的常见层压板（31,31'，31“），未固化状态的住房面板（25）; b）通过所述盖子（27）预见的周边切割所述普通层压板（31,31'，31“），并将盖板层压板（33,33'，33”）和壳体板层压板（35,35'，33“ 35“）; c）使用所述盖层压板（31,31'，31“）在一侧单独制造所述盖（27），并且在另一侧上使用所述盖板（31,31'，31”）与所述壳体面板（25）一起制造所述部件外壳板层压板（35,35'，35“）。

7. 发明授权

US08733689B2 Device for providing electrical continuity between aeronautical components with relative movement 有权
标题翻译：用于在航空部件之间提供相对运动的电气连续性的装置
公开(公告)号：US08733689B2
公开(公告)日：2014-05-27
申请号：US12882251
申请日：2010-09-15
申请人： Vicente Martínez Valdegrama , José Luis Lozano García , Gonzalo Ramírez Blanco
发明人： Vicente Martínez Valdegrama , José Luis Lozano García , Gonzalo Ramírez Blanco
IPC分类号： B64D3/00
CPC分类号： H01R4/64 , B64C1/26 , B64C5/02 , B64C7/00 , B64D45/02 , H01R35/04 , H01R41/00 , H01R2201/26
摘要： A device provides electrical continuity between aeronautical components including a first fixed component and a second component displaceable with respect to the first component. The first and second components include electrically conducting surfaces. A first conductive piece is fixed to the first component and a second conductive piece is fixed to the second component. The first and second pieces are joined together with the possibility of sliding one on the other, in such a way that the first piece is connected to the conductive surface of the first component and the second piece is connected to the conductive surface of the second component, so that, when displacements take place of the second component with respect to the first component, the first piece slides on the second piece maintaining the electrical conductivity between the first and second components.
摘要翻译：一种装置提供包括第一固定部件和可相对于第一部件移动的第二部件的航空部件之间的电连续性。第一和第二部件包括导电表面。第一导电片被固定到第一部件，第二导电片固定到第二部件。第一和第二部件以可能性彼此滑动的方式接合在一起，使得第一部件连接到第一部件的导电表面，并且第二部件连接到第二部件的导电表面使得当相对于第一部件发生第二部件的位移时，第一部件在第二部件上滑动，保持第一和第二部件之间的导电性。

8. 发明授权

US08746058B2 Liquid fuel tank for measuring fuel volume 有权
标题翻译：用于测量燃油量的液体燃料箱
公开(公告)号：US08746058B2
公开(公告)日：2014-06-10
申请号：US13315890
申请日：2011-12-09
申请人： Vicente Martínez Valdegrama , Luis Manuel Rodríguez Urbina
发明人： Vicente Martínez Valdegrama , Luis Manuel Rodríguez Urbina
IPC分类号： G01F23/00
CPC分类号： G01F23/2922 , G01F23/292
摘要： Its object is to allow measurement of the volume of fuel (2) using optic fiber cables (3); it is characterized in that, adhered to one or more of the inner faces of the tank (1) there is at least one sheet (4) in which a plurality of optic fiber cables (3) with different lengths are included, located between the inner face of the tank and the sheet (4). One set of the ends (10) of the optic fiber cables (3) are disposed so that they are in contact with the fuel (2) when it reaches their level, thereby allowing measurement of the fuel level at all times.The preferred embodiment distributes the optic fiber cables (3) on two opposing lateral faces of the tank (1) so that they cross over one another and in opposite directions to measure any fuel level.It is applied in aeronautics.
摘要翻译：其目的是允许使用光纤电缆（3）测量燃料（2）的体积; 其特征在于，粘附到罐（1）的一个或多个内表面的是至少一个片（4），其中包括具有不同长度的多根光纤电缆（3），位于罐体和片材（4）的内表面。一组光纤电缆（3）的端部（10）被布置成使得它们在达到其水平时与燃料（2）接触，从而允许始终测量燃料液位。优选实施例将光纤电缆（3）分配在罐（1）的两个相对的侧面上，使得它们彼此交叉并且沿相反的方向测量任何燃料水平。它适用于航空。

9. 发明授权

US08375978B2 Fastening system for drainage valves 有权
标题翻译：排水阀紧固系统
公开(公告)号：US08375978B2
公开(公告)日：2013-02-19
申请号：US12712312
申请日：2010-02-25
申请人： Vicente Martínez Valdegrama , Luis Manuel Rodríguez Urbina , Olaf Andreas Dietrich Carreño
发明人： Vicente Martínez Valdegrama , Luis Manuel Rodríguez Urbina , Olaf Andreas Dietrich Carreño
IPC分类号： F16K1/42
CPC分类号： F16K24/00 , F16K27/07 , Y10T137/598
摘要： Provided herein are drainage valves for removing water accumulated in the lower part of fuel tanks of an aircraft. The valves can be affixed in correspondence with a lower skin forming part of the tanks. The lower skin includes recesses for the complementary housing of the heads of the valves that, in combination with some axial fastening nuts, immobilize the valves to that skin. The recesses can comprise a conical structure obtained by deformation of the lower skin, and with the deformation an inner elevated seat is further obtained, on which seat the axial fastening nuts press, maintaining the thickness of the skin in the area where the valves are located, thus preventing the area from weakening as it happens conventionally.
摘要翻译：本文提供了用于去除积聚在飞行器的燃料箱下部的水的排水阀。阀可以与形成部分罐的下部皮肤相对应地固定。下部皮肤包括用于阀头的互补壳体的凹槽，其与一些轴向紧固螺母组合，将阀固定到该皮肤上。凹槽可以包括通过下皮的变形而获得的锥形结构，并且随着变形，进一步获得内部升高的座位，轴向紧固螺母在该座位上被压住，从而保持皮肤在阀所在的区域中的厚度，从而防止该区域在常规情况下变弱。

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