公开(公告)号：US07484694B2

公开(公告)日：2009-02-03

申请号：US11532359

申请日：2006-09-15

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： B64C9/00

CPC分类号： B64C9/22 ,  Y02T50/44

摘要： An aircraft wing including a wing box and a nose flap moveably connected to the wing box by first and second folding hinges. A first transverse link is pivotally connected to first portions of the first and second folding hinges. A second transverse link is pivotally connected to second portions of the first and second folding hinges. An actuator is connected diagonally between the first and second transverse links for moving the nose flap between a retracted position and an extended position. The instant abstract is neither intended to define the invention disclosed in the specification nor intended to limit the scope of the invention in any way.

摘要翻译： 一种飞机机翼，包括翼盒和鼻翼，通过第一和第二折叠铰链可动地连接到翼盒。 第一横向连杆枢转地连接到第一和第二折叠铰链的第一部分。 第二横向连杆枢转地连接到第一和第二折叠铰链的第二部分。 致动器沿对角地连接在第一和第二横向连杆之间，用于在缩回位置和延伸位置之间移动鼻翼。 本摘要既不旨在定义说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

公开(公告)号：US07451950B2

公开(公告)日：2008-11-18

申请号：US10502559

申请日：2003-01-20

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： B64C3/44 ,  E05D1/00 ,  F16D3/00

CPC分类号： B64C9/02 ,  F16C11/12 ,  Y10T16/525 ,  Y10T16/5257 ,  Y10T403/35 ,  Y10T403/7062

摘要： A joint arrangement connects a longitudinal edge of a first component with an upper surface of a second component. At least two cooperating bands are secured with their first ends respectively on opposite sides of the first component, and are secured with their second ends respectively on clamping elements arranged on the second component, so that the bands intersect the major center plane of the first component in the joint area between the components. A pressure element is positioned on at least one clamping element for supporting the first component, and the bands extend laterally next to the pressure element and crosswise relative to one another.

摘要翻译： 联合装置将第一部件的纵向边缘与第二部件的上表面连接。 至少两个配合带的第一端分别固定在第一部件的相对侧上，并且其第二端分别固定在布置在第二部件上的夹紧元件上，使得带与第一部件的主中心平面交叉 在组件之间的联合区域。 压力元件定位在用于支撑第一部件的至少一个夹紧元件上，并且该带横向延伸靠近压力元件并相对于彼此横向延伸。

公开(公告)号：US20060226297A1

公开(公告)日：2006-10-12

申请号：US11400518

申请日：2006-04-10

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： B64C9/16

CPC分类号： B64C9/16 ,  B64C9/18 ,  Y02T50/44

摘要： A structure with at least one flap connected to a wing, including: at least one drive device; at least one actuating device including a gear device coupled to the at least one drive device and the at least one flap; and a fairing housing swivellably mounted on the wing, at least partially surrounding the gear device, and coupled to the gear device, wherein actuation of the at least one drive device causes a combined translational and rotational movement of the at least one flap and a swivelling movement of at least a portion of the fairing housing. A method for pivoting a flap is also disclosed. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.

公开(公告)号：US06729661B2

公开(公告)日：2004-05-04

申请号：US10341592

申请日：2003-01-14

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： E05C700

CPC分类号： E05B47/023 ,  B64C1/1476 ,  E05B81/10 ,  E05B83/24 ,  E05C3/06 ,  Y10T292/0825 ,  Y10T292/0826 ,  Y10T292/0828 ,  Y10T292/0831

摘要： A locking device is provided for locking two structural parts that are moveable relative to each other. A latch hook is disposed in a reference plane and is adapted to swivel on a joint with an axis center. An actuating element is provided for swivelling the latch hook about a latch hook axis. A rocking lever interacts with the actuating element for rotation about a rocking lever axis. The lever is connected with a first end of a steering arm via a first rotary joint. A second end of the steering arm is connected with the latch hook via a second rotary joint.

摘要翻译： 提供锁定装置用于锁定可相对于彼此移动的两个结构部件。 锁钩设置在参考平面中，并且适于在具有轴心的接头上旋转。 提供致动元件用于使闩锁钩绕钩钩轴线旋转。 摇摆杆与致动元件相互作用以围绕摇杆轴线旋转。 杠杆通过第一旋转接头与转向臂的第一端连接。 转向臂的第二端经由第二旋转接头与锁钩连接。

公开(公告)号：US09452823B2

公开(公告)日：2016-09-27

申请号：US14345054

申请日：2012-08-21

申请人： Tamas Havar ,  Juan Perez-Sanchez ,  Tobias Ender ,  Oliver Seack

发明人： Tamas Havar ,  Juan Perez-Sanchez ,  Tobias Ender ,  Oliver Seack

IPC分类号： B64C3/50 ,  B64C13/28 ,  B64C9/16 ,  B64C3/54 ,  B64C9/02

CPC分类号： B64C13/28 ,  B64C3/54 ,  B64C9/02 ,  B64C9/16

摘要： A lift flap bearing apparatus is improved with respect to aerodynamics, construction space and assembly, for guiding and adjusting a first lift flap and a second lift flap. The lift flap bearing apparatus comprises a first guiding device for guiding the first lift flap and a second guiding device for guiding the second lift flap. The first and the second guiding devices each have a first curved guide rail and a second curved guide rail.

摘要翻译： 相对于空气动力学，建筑空间和组装，提升翼片轴承装置得到改进，用于引导和调节第一提升翼片和第二提升翼片。 提升板轴承装置包括用于引导第一提升挡板的第一引导装置和用于引导第二提升挡板的第二引导装置。 第一和第二引导装置各自具有第一弯曲导轨和第二弯曲导轨。

公开(公告)号：US07909289B2

公开(公告)日：2011-03-22

申请号：US12340141

申请日：2008-12-19

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： B64C1/14

CPC分类号： B64C1/1446 ,  B64C1/14 ,  B64C1/36 ,  B64C25/16 ,  Y10T292/202 ,  Y10T292/212

摘要： System for opening and closing a structural part arranged on a support structure. The system includes at least one hinged joint device for flexibly connecting the structural part to the support structure. The at least one hinged joint device is arranged inside the support structure and has an axis of rotation about which the structural part can be pivoted relative to the support structure during opening and closing. A locking arrangement is structured and arranged to connect the structural part to the support structure in a form-locking manner when the structural part is in a closed position. In the closed position, the locking arrangement is arranged to relieve the at least one hinged joint device. This Abstract is not intended to define the invention disclosed in the specification, nor intended to limit the scope of the invention in any way.

摘要翻译： 用于打开和关闭布置在支撑结构上的结构部件的系统。 该系统包括用于将结构部件柔性地连接到支撑结构的至少一个铰接接头装置。 所述至少一个铰接接头装置设置在所述支撑结构的内部并且具有旋转轴线，所述结构部件可围绕所述旋转轴线相对于所述支撑结构在打开和关闭期间枢转。 锁定装置被构造和布置成当结构部件处于关闭位置时以结构形式将结构部件连接到支撑结构。 在关闭位置，锁定装置布置成减轻至少一个铰接接头装置。 本摘要不旨在限定说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

公开(公告)号：US07699270B2

公开(公告)日：2010-04-20

申请号：US10559861

申请日：2004-06-07

申请人： Hans Lonsinger ,  Juan Perez-Sanchez

发明人： Hans Lonsinger ,  Juan Perez-Sanchez

IPC分类号： B64C3/44

CPC分类号： B64C3/185 ,  B64C3/48 ,  B64C3/52

摘要： A wing has a changeable profile, and extends in a wing chord direction and perpendicularly thereto in a wingspan direction. The wing has a first cover skin and a second cover skin spaced apart from one another with spars therebetween. The wing includes a leading edge region and a trailing edge region opposite one another in the wing chord direction, and a wing tip region at the end of the wing in the wingspan direction. The wing further includes a flexible region that connects the wing tip region to the rest of the wing, and that is adapted to vary the profile of the wing in a direction that includes a component in the wing chord direction and a component in the wingspan direction.

摘要翻译： 翼具有可变轮廓，并且在翼展方向上延伸并且在翼展方向上垂直于翼翼方向延伸。 机翼具有第一盖皮肤和第二盖皮肤，彼此间隔开间隔。 机翼包括在翼弦方向上彼此相对的前缘区域和后缘区域以及翼展端部处的翼展方向的翼尖区域。 机翼还包括柔性区域，其将翼尖区域连接到机翼的其余部分，并且适于在包括机翼弦方向上的部件的方向和翼展方向上的部件的方向上改变机翼的轮廓 。

公开(公告)号：US07600718B2

公开(公告)日：2009-10-13

申请号：US11400509

申请日：2006-04-10

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： B64C3/50

CPC分类号： B64C9/18 ,  B64C9/16 ,  Y02T50/44

摘要： A pivoted flap mechanism for adjusting an aerodynamic pivotable flap associated with a wing, including: an actuating device including a gear device; a drive device including a drive arm that rotates about an axis, and which is structured and arranged to load the actuating device; and a flap support composed of a leading flap support portion and a trailing flap support portion. The aerodynamic pivotable flap is arranged on the flap support, and a steering arm of the gear device is swivellably coupled by a link to a part of the trailing flap support portion adjacent the leading flap support portion. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.

摘要翻译： 用于调节与翼相关联的空气动力学可枢转翼片的枢转翼片机构，包括：包括齿轮装置的致动装置; 驱动装置，其包括围绕轴线旋转的驱动臂，其被构造和布置成装载所述致动装置; 以及由前翼片支撑部分和后翼片支撑部分组成的翼片支撑件。 空气动力学可枢转翼片设置在翼片支撑件上，并且齿轮装置的转向臂通过与靠近翼片支撑部分的后翼片支撑部分的一部分的连杆可转动地联接。 本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

公开(公告)号：US20090127403A1

公开(公告)日：2009-05-21

申请号：US12248617

申请日：2008-10-09

申请人： Juan PEREZ-SANCHEZ ,  Gerd Schuhmacher ,  Markus Pauly ,  Siegfried Bechtle ,  Josef Mendler ,  Dieter Frank

发明人： Juan PEREZ-SANCHEZ ,  Gerd Schuhmacher ,  Markus Pauly ,  Siegfried Bechtle ,  Josef Mendler ,  Dieter Frank

IPC分类号： B64C21/00

CPC分类号： B64C9/16 ,  B64C9/22 ,  Y02T50/44

摘要： Device for carrying lift flaps arranged on the wings of an aircraft and a wing. The device includes a carrier with a U-shaped profile, a covering plate positionable over an open side of the U-shaped profile, and a fairing housing formed in an aerodynamic manner and at least in part by the carrier. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.

摘要翻译： 用于承载设置在飞机和机翼的翼上的提升襟翼的装置。 该装置包括具有U形轮廓的载体，可定位在U形轮廓的敞开侧的覆盖板以及以空气动力学方式并且至少部分地由载体形成的整流罩。 本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。

公开(公告)号：US07510151B2

公开(公告)日：2009-03-31

申请号：US11400518

申请日：2006-04-10

申请人： Juan Perez-Sanchez

发明人： Juan Perez-Sanchez

IPC分类号： B64C9/00

CPC分类号： B64C9/16 ,  B64C9/18 ,  Y02T50/44

摘要： A structure with at least one flap connected to a wing, including: at least one drive device; at least one actuating device including a gear device coupled to the at least one drive device and the at least one flap; and a fairing housing swivellably mounted on the wing, at least partially surrounding the gear device, and coupled to the gear device, wherein actuation of the at least one drive device causes a combined translational and rotational movement of the at least one flap and a swivelling movement of at least a portion of the fairing housing. A method for pivoting a flap is also disclosed. The instant abstract is neither intended to define the invention disclosed in this specification nor intended to limit the scope of the invention in any way.

摘要翻译： 一种具有至少一个翼片的结构，所述翼片连接到机翼，包括：至少一个驱动装置; 至少一个致动装置，包括联接到所述至少一个驱动装置和所述至少一个挡板的齿轮装置; 以及整流罩，其可转动地安装在所述机翼上，至少部分地围绕所述齿轮装置并且联接到所述齿轮装置，其中所述至少一个驱动装置的致动导致所述至少一个挡板的组合的平移和旋转运动， 整流罩的至少一部分的运动。 还公开了一种用于枢转翼片的方法。 本摘要既不旨在限定本说明书中公开的发明，也不旨在以任何方式限制本发明的范围。