公开(公告)号：US20150101695A1

公开(公告)日：2015-04-16

申请号：US14069928

申请日：2013-11-01

Applicant: Joannes Jozef Antonius Maria Van Aspert

Inventor： Joannes Jozef Antonius Maria Van Aspert

IPC: F16L55/11

CPC classification number: F16L55/1125 ,  B64D37/005 ,  B64F1/005 ,  B64F5/50 ,  F02C7/22 ,  F05D2240/55 ,  F16L55/1141

Abstract: The present invention relates to a sealing device designed for sealing a fuel inlet opening of an aircraft engine and to an aircraft engine provided with such a sealing device. The invention further relates to a method for sealing a fuel inlet opening of an aircraft engine.

Abstract translation: 本发明涉及一种设计用于密封飞机发动机的燃料入口和密封装置的飞机发动机的密封装置。 本发明还涉及一种用于密封飞机发动机的燃料入口的方法。

公开(公告)号：US20140327184A1

公开(公告)日：2014-11-06

申请号：US14294794

申请日：2014-06-03

Applicant: The Boeing Company

Inventor： Li C. Chang ,  Richard M Coleman ,  Ronald J. Steckman ,  Andrew M. Huckey ,  Nicholas A. Norman

IPC: B64F5/00 ,  B23Q3/00

CPC classification number: B64F5/50 ,  B23Q3/00 ,  B64C1/068 ,  Y10T29/49826 ,  Y10T29/53961

Abstract: A barrel assembly for a composite structure includes a barrel of composite material, a first end ring, and a mid support. The barrel of composite material has a first end, an interior surface and an outer surface, and the first end ring is removably attached to the first end. The first end ring has a perimeter that is substantially congruent with the first end, and is configured to maintain a shape of the barrel. The mid support is removably disposed within the barrel, and has a plurality of spokes extending outwardly from a central hub to contact the interior surface, to maintain a shape of the barrel.

Abstract translation: 用于复合结构的桶组件包括复合材料桶，第一端环和中间支撑。 所述复合材料桶具有第一端，内表面和外表面，并且所述第一端环可移除地附接到所述第一端。 第一端环具有与第一端基本一致的周边，并且构造成保持筒的形状。 中间支撑件可移除地设置在筒体内，并且具有从中心毂向外延伸以接触内表面的多个辐条，以保持筒的形状。

公开(公告)号：US08840364B2

公开(公告)日：2014-09-23

申请号：US13344367

申请日：2012-01-05

Applicant: Jordan Scott Warton ,  Robert Allen Baten

Inventor： Jordan Scott Warton ,  Robert Allen Baten

IPC: F01D25/00

CPC classification number: F01D25/285 ,  B64F5/50 ,  F05D2230/51 ,  F05D2230/64 ,  F05D2260/02 ,  F05D2260/36 ,  Y02B10/30

Abstract: A system includes a turbomachine platform including a first docking guide. The turbomachine platform supports a turbomachine skid, and the skid includes a second docking guide. The first docking guide is configured to interface with the second docking guide in order to guide the turbomachine skid between a docked position and an undocked position relative to other equipment supported by the platform.

Abstract translation: 一种系统包括包括第一对接引导件的涡轮机平台。 涡轮机平台支撑涡轮机防滑装置，并且防滑装置包括第二对接引导件。 第一对接引导件被配置为与第二对接引导件相接合，以便相对于由平台支撑的其他设备引导涡轮机械在对接位置和离开位置之间的滑动。

公开(公告)号：US08789837B2

公开(公告)日：2014-07-29

申请号：US13622035

申请日：2012-09-18

Applicant: Li C Chang ,  Richard M Coleman ,  Ronald J Steckman ,  Andrew M Huckey ,  Nicholas A Norman

Inventor： Li C Chang ,  Richard M Coleman ,  Ronald J Steckman ,  Andrew M Huckey ,  Nicholas A Norman

IPC: B62B1/00 ,  B65D85/68

CPC classification number: B64F5/50 ,  B23Q3/00 ,  B64C1/068 ,  Y10T29/49826 ,  Y10T29/53961

Abstract: A barrel assembly for a composite structure includes a barrel of composite material, a first end ring, and a mid support. The barrel of composite material has a first end, an interior surface and an outer surface, and the first end ring is removably attached to the first end. The first end ring has a perimeter that is substantially congruent with the first end, and is configured to maintain a shape of the barrel. The mid support is removably disposed within the barrel, and has a plurality of spokes extending outwardly from a central hub to contact the interior surface, to maintain a shape of the barrel.

Abstract translation: 用于复合结构的桶组件包括复合材料桶，第一端环和中间支撑。 所述复合材料桶具有第一端，内表面和外表面，并且所述第一端环可移除地附接到所述第一端。 第一端环具有与第一端基本一致的周边，并且构造成保持筒的形状。 中间支撑件可移除地设置在筒体内，并且具有从中心毂向外延伸以接触内表面的多个辐条，以保持筒的形状。

公开(公告)号：US20140090252A1

公开(公告)日：2014-04-03

申请号：US13837750

申请日：2013-03-15

Applicant: THE BOEING COMPANY

Inventor： Farahnaz Tanni Sisco ,  Daniel R. Smith ,  Jayson J. Aquino ,  Edward John Batt ,  James N. Buttrick ,  Antonio C. Micale ,  Darrell D. Jones ,  Clayton L. Munk ,  Chris G. Couevas ,  Mario Ramos ,  Azita N. Namdaran ,  Noman S. Noor ,  Donald A. Mottaz

IPC: B23P23/00

CPC classification number: B23P23/00 ,  B21J15/142 ,  B23P21/004 ,  B23P23/06 ,  B23P2700/01 ,  B64F5/10 ,  B64F5/50 ,  Y10T29/49622 ,  Y10T29/51

Abstract: A system and method are provided to automate the assembly of a wing panel, such as utilized by commercial aircraft. In the context of a system, a tacking cell is provided that is configured to tack one or more stringers to a skin plank. The system also includes a riveting cell configured to receive a tacked plank from the tacking cell and to rivet the one or more stringers to the skin plank. The system also includes a splicing cell configured to receive a plurality of riveted planks from the riveting cell and to attach one or more splice stringers to the plurality of riveted planks. Further, the system includes a side of body cell configured to receive a spliced panel from the splicing cell and to attach a side of body chord thereto to produce a wing panel.

Abstract translation: 提供了一种系统和方法，用于使诸如由商用飞机使用的翼板的组装自动化。 在系统的上下文中，提供了一种定位单元，其被配置成将一个或多个纵梁固定到皮肤板。 该系统还包括铆接单元，其被配置为从固定单元接收固定板，并将一个或多个纵梁铆接到皮质板。 该系统还包括拼接单元，该拼接单元被配置为从铆接单元接收多个铆接板，并且将一个或多个接头纵梁附接到多个铆接板。 此外，该系统包括身体单元的一侧，其被配置为从拼接单元接收拼接面板并且将主体弦的一侧附接到其上以产生翼板。

公开(公告)号：US20140061382A1

公开(公告)日：2014-03-06

申请号：US13597717

申请日：2012-08-29

Applicant: Brian E. Tucker

Inventor： Brian E. Tucker

IPC: B64F5/00

CPC classification number: B64F5/50 ,  G07C5/008 ,  G07C5/085 ,  G07C2205/02

Abstract: According to one embodiment, an aircraft part storage system includes a first storage device and a second storage device. The first storage device is configured to be coupled to an aircraft part and operable to store and transmit a first set of information about the aircraft part. The second storage device is configured to be coupled to the same aircraft part and operable to store and transmit a second set of information about the aircraft part. The second storage device has a larger storage capacity than the first storage device but a shorter transmission range than the first storage device.

Abstract translation: 根据一个实施例，飞行器部件存储系统包括第一存储装置和第二存储装置。 第一存储设备被配置为耦合到飞行器部件并且可操作以存储和发送关于飞行器部件的第一组信息。 第二存储设备被配置为耦合到相同的飞行器部件并且可操作以存储和发送关于飞行器部件的第二组信息。 第二存储装置具有比第一存储装置更大的存储容量，但是比第一存储装置更短的传输范围。

公开(公告)号：US20130241130A1

公开(公告)日：2013-09-19

申请号：US13990002

申请日：2012-01-13

Applicant: Ichiro Ozu ,  Kentaro Irie ,  Kazunori Kamiya ,  Daisuke Kinugasa ,  Junji Nagata ,  Sachio Takeyama

Inventor： Ichiro Ozu ,  Kentaro Irie ,  Kazunori Kamiya ,  Daisuke Kinugasa ,  Junji Nagata ,  Sachio Takeyama

IPC: B25B11/02

CPC classification number: B25B11/02 ,  B62B3/08 ,  B64F5/10 ,  B64F5/50

Abstract: An assembly jig includes an upper jig frame that is provided above a longitudinal outer edge of a large structure, a lower jig frame that is provided below a longitudinal outer edge of the large structure, a connecting jig frame that connects the upper jig frame and the lower jig frame to each other, three supporting parts for supporting the lower jig frame from below, and a jig leg portion that is provided perpendicular to the direction in which the lower jig frame extends and parallel to a ground surface. The supporting parts are provided at three portions that are respectively located under two end portions of the jig leg portion and under the lower jig frame, and arrangement positions of the supporting parts provided at the three portions form a substantially triangular shape when seen from above.

Abstract translation: 组装夹具包括设置在大结构的纵向外边缘上方的上夹具框架，设置在大结构的纵向外边缘下方的下夹具框架，连接上夹具框架和 下夹具框架彼此相连，用于从下方支撑下夹具框架的三个支撑部件和垂直于下夹具框架延伸并平行于地面的方向设置的夹具腿部。 支撑部分设置在分别位于夹具腿部的两个端部下方和下部夹具框架下方的三个部分处，并且当从上方观察时，设置在三个部分处的支撑部件的布置位置形成大致三角形形状。

公开(公告)号：US20130158697A1

公开(公告)日：2013-06-20

申请号：US13326996

申请日：2011-12-15

Applicant: Paul Reed Stone ,  Clayton Lynn Munk ,  Eric M. Reid

Inventor： Paul Reed Stone ,  Clayton Lynn Munk ,  Eric M. Reid

IPC: G06F19/00 ,  B65G49/00 ,  B23P19/00 ,  B23Q41/02 ,  B23P15/00

CPC classification number: B64F5/0036 ,  B25J9/1682 ,  B64F5/10 ,  B64F5/50 ,  G05B19/41895 ,  G05B2219/31008 ,  G05B2219/45071 ,  Y02P90/285 ,  Y02P90/60 ,  Y10T29/49616 ,  Y10T29/49622 ,  Y10T29/534

Abstract: A method and apparatus for manufacturing a structure. A part for the structure may be supported on a plurality of mobile fixtures configured to control an orientation of the part. The part for the structure may be moved using the plurality of mobile fixtures to a number of stations for performing a number of operations for manufacturing the structure using the part. The plurality of mobile fixtures may be configured to move in a coordinated manner and substantially maintain a desired orientation for the part while moving the part to a station in the number of stations. The number of operations for manufacturing the structure may be performed at the number of stations while the plurality of mobile fixtures supports the part.

Abstract translation: 一种用于制造结构的方法和装置。 用于结构的部件可以被支撑在被配置成控制部件的取向的多个移动夹具上。 结构的部件可以使用多个移动固定装置移动到多个工位，用于执行用于使用该部件制造结构的多个操作。 多个移动固定装置可以被配置为以协调的方式移动并且在将零件移动到台站数目的站的同时基本保持该零件的期望取向。 用于制造结构的操作的数量可以在多个移动固定装置支撑该部件的情况下以台数进行。

公开(公告)号：US08439337B2

公开(公告)日：2013-05-14

申请号：US12789286

申请日：2010-05-27

Applicant: Horst Kott

Inventor： Horst Kott

IPC: B25B1/24

CPC classification number: B23P19/10 ,  B23P2700/01 ,  B64F5/10 ,  B64F5/50

Abstract: A positioning system is provided for mounting a wing of an aircraft to a fuselage of the aircraft. The positioning system includes, but is not limited to a programmable mounting unit that can perform a final adjustment and alignment of the wing with respect to the fuselage without user interaction.

Abstract translation: 提供了一种定位系统，用于将飞行器的翼片安装到飞行器的机身上。 定位系统包括但不限于可编程安装单元，其可以在没有用户交互的情况下执行机翼相对于机身的最终调整和对准。

公开(公告)号：US08313131B2

公开(公告)日：2012-11-20

申请号：US12449165

申请日：2008-01-14

Applicant: Richard Lester Hallett ,  Peter William Spence

Inventor： Richard Lester Hallett ,  Peter William Spence

IPC: B66C1/62 ,  B66C1/34 ,  B64C1/20

CPC classification number: B66C1/66 ,  B64F5/50 ,  B66C1/24 ,  Y10T403/32631

Abstract: A method of lifting an aircraft at a lifting location, the method comprising: securing a fitting (10) to the aircraft when the aircraft is at the lifting location; engaging the fitting with a crane hook (100); transmitting lifting load from the crane hook to the aircraft via the fitting; and removing the fitting from the aircraft. A fitting (10) for transmitting lifting loads from a crane hook (100) to an item, the fitting comprising: an attachment member (11) configured to be secured to the item; and a lifting member (12) which is pivotally coupled to the attachment member and configured to be engaged by the crane hook (100) so as to transmit lifting loads from the crane hook to the item. A crane hook (100) with a ball-and-socket connection is provided. The crane hook has an attachment link (106) having a first pivot point (107) attached to the hook forward of its center of gravity, and a second pivot point (109) configured to be lifted by a crane, —and a biasing system which applies a biasing force to the attachment link causing the attachment link to rotate about the first pivot-point whereby the second pivot point moves towards the rear of the hook when the hook is unloaded.

Abstract translation: 一种在提升位置提升飞机的方法，所述方法包括：当飞机处于提升位置时，将配件（10）固定到飞行器; 将配件与吊钩（100）接合; 通过配件将提升负载从起重机吊钩传递到飞行器; 并从飞机上拆下配件。 一种用于将提升负载从起重机钩（100）传送到物品的配件（10），所述配件包括：被配置为固定到所述物品上的附接构件（11） 以及提升构件（12），其枢转地联接到所述附接构件并且构造成与所述起重机吊钩（100）接合，以便将提升负载从所述起重机吊钩传递到所述物品。 提供具有球窝连接的起重机吊钩（100）。 起重机吊钩具有附接连杆（106），该连接连杆（106）具有附接到其重心前方的钩的第一枢转点（107）和构造成由起重机提升的第二枢转点（109），以及偏置系统 其向联接连接件施加偏压力，从而使附接连杆围绕第一枢转点旋转，由此当钩被卸载时，第二枢轴点朝钩的后方移动。