公开(公告)号：US20150195947A1

公开(公告)日：2015-07-09

申请号：US14661872

申请日：2015-03-18

Applicant: THE BOEING COMPANY

Inventor： Andrew John Bayliss ,  Stephen T. Brown ,  Perry Nicholas Rea ,  Kevin Matthew Retz

IPC: H05K7/18 ,  B64D47/00

CPC classification number: B64C1/22 ,  B64C1/1446 ,  B64C3/141 ,  B64D43/00 ,  B64D47/00 ,  H05K7/1411 ,  H05K7/18 ,  Y10T292/0802 ,  Y10T292/0807

Abstract: An apparatus and method comprising a rack and a translation mechanism. The rack may be configured to hold components. The rack may comprise movable rack segments that are movable independently of each other. The translation mechanism may be configured to move a portion of the movable rack segments relative to another portion of the movable rack segments inside a platform such that internal access to at least a portion of the components is provided inside the platform.

Abstract translation: 一种包括机架和平移机构的装置和方法。 机架可能被配置为保持组件。 机架可以包括可彼此独立移动的可移动齿条段。 平移机构可以被配置为使可移动齿条段的一部分相对于可移动齿条段的另一部分移动到平台内，使得至少部分组件的内部通路设置在平台内。

公开(公告)号：US10118686B2

公开(公告)日：2018-11-06

申请号：US13628117

申请日：2012-09-27

Applicant: The Boeing Company

Inventor： Perry Nicholas Rea

IPC: B64C1/26

Abstract: A single, common, fuselage and wing design of an aircraft structure provides for two different aircraft models or configurations. A fuselage (12) has a center section cutout area (212). Each wing (16) has an airfoil over substantially its entire span. In one configuration (2A), a center section component (212), such as a wingbox, is inserted into the center section cutout and the wings are connected to opposing sides of the center section component by a side-of-body join. In another configuration (2B), the wings are moved inwardly, joined to the fuselage, and also joined to each other in a centerline join at the centerline (218) of the aircraft wherein a portion (16A) of the airfoil of each wing is then inside the fuselage. Different flaps (210, 220), spacers (222), and/or different engine mount locations (402, 404) may be provided for the wings for the two configurations.

公开(公告)号：US20140084110A1

公开(公告)日：2014-03-27

申请号：US13628117

申请日：2012-09-27

Applicant: The Boeing Company

Inventor： Perry Nicholas Rea

IPC: B64C1/26

CPC classification number: B64C1/26 ,  Y10T29/49622

Abstract: A single, common, fuselage and wing design of an aircraft structure provides for two different aircraft models or configurations. A fuselage (12) has a center section cutout area (212). Each wing (16) has an airfoil over substantially its entire span. In one configuration (2A), a center section component (212), such as a wingbox, is inserted into the center section cutout and the wings are connected to opposing sides of the center section component by a side-of-body join. In another configuration (2B), the wings are moved inwardly, joined to the fuselage, and also joined to each other in a centerline join at the centerline (218) of the aircraft wherein a portion (16A) of the airfoil of each wing is then inside the fuselage. Different flaps (210, 220), spacers (222), and/or different engine mount locations (402, 404) may be provided for the wings for the two configurations.

Abstract translation: 飞机结构的单一，通用，机身和机翼设计提供两种不同的飞机型号或配置。 机身（12）具有中心部分切断区域（212）。 每个翼（16）在其整个跨度上具有翼型。 在一个构造（2A）中，诸如翼盒的中心部分部件（212）插入到中心部分切口中，并且翼通过身体侧面连接连接到中心部分部件的相对侧。 在另一配置（2B）中，机翼向内移动，与机身相连，并且在飞行器的中心线（218）处以中心线连接处彼此接合，其中每个机翼的翼型部分（16A） 然后在机身内。 可以为这两种配置的翼提供不同的翼片（210,220），间隔件（222）和/或不同的发动机安装位置（402,404）。

公开(公告)号：US09725153B2

公开(公告)日：2017-08-08

申请号：US14661872

申请日：2015-03-18

Applicant: The Boeing Company

Inventor： Andrew John Bayliss ,  Stephen T. Brown ,  Perry Nicholas Rea ,  Kevin Matthew Retz

IPC: B64C1/22 ,  B64C1/14 ,  B64D43/00 ,  B64D47/00 ,  H05K7/14 ,  B64C3/14 ,  H05K7/18

CPC classification number: B64C1/22 ,  B64C1/1446 ,  B64C3/141 ,  B64D43/00 ,  B64D47/00 ,  H05K7/1411 ,  H05K7/18 ,  Y10T292/0802 ,  Y10T292/0807

Abstract: An apparatus and method comprising a rack and a translation mechanism. The rack may be configured to hold components. The rack may comprise movable rack segments that are movable independently of each other. The translation mechanism may be configured to move a portion of the movable rack segments relative to another portion of the movable rack segments inside a platform such that internal access to at least a portion of the components is provided inside the platform.