公开(公告)号：US20160130011A1

公开(公告)日：2016-05-12

申请号：US14537957

申请日：2014-11-11

申请人： The Boeing Company

发明人： Matthew D. Moore ,  Kelly L. Boren ,  Hao Shen ,  Chester P. Nelson

IPC分类号： F02K1/34 ,  F02K1/46

CPC分类号： B64D33/06 ,  F02K1/28 ,  F02K1/34 ,  F02K1/36 ,  F02K1/38 ,  F02K1/386 ,  F02K1/46 ,  F02K1/48 ,  F02K1/82 ,  F02K1/822 ,  F02K1/827

摘要： A jet noise suppressor including a nozzle having a front end and an opposed rear end, spokes extending radially inward from the nozzle, the spokes defining vents, and a center-body connected to the spokes and in fluid communication with the vents, the center-body being positioned centrally within the nozzle and including a closed front end and an open rear end, wherein the front end of the nozzle entrains a first ambient airflow passing through the nozzle and exiting the rear end of the nozzle proximate a periphery of the nozzle, and wherein the vents entrain a second ambient airflow passing through the center-body and exiting the rear end of the nozzle proximate a center of the nozzle.

摘要翻译： 一种喷射噪声抑制器，包括具有前端和相对的后端的喷嘴，从喷嘴径向向内延伸的辐条，辐条限定出口，以及连接到辐条并与通风口流体连通的中心体， 主体定位在喷嘴内的中心并且包括封闭的前端和敞开的后端，其中喷嘴的前端夹带穿过喷嘴的第一环境空气并且靠近喷嘴的周边离开喷嘴的后端， 并且其中所述通风口夹带穿过所述中心的第二环境空气并且在所述喷嘴的中心附近离开所述喷嘴的后端。

公开(公告)号：US09193464B1

公开(公告)日：2015-11-24

申请号：US14799884

申请日：2015-07-15

申请人： The Boeing Company

发明人： Kelly L. Boren ,  Lowell B. Campbell ,  Alan K. Prichard

IPC分类号： B64C1/10 ,  B64D11/04

CPC分类号： B64C1/10 ,  B64D11/04

摘要： An aircraft cabin has been reconfigured with a rear fuselage galley and a modified aft pressure bulkhead that enables the galley to be moved rearwardly to provide additional floor space in the aircraft cabin.

公开(公告)号：US08967723B2

公开(公告)日：2015-03-03

申请号：US13688104

申请日：2012-11-28

申请人： The Boeing Company

发明人： Kelly L. Boren

IPC分类号： A47C7/54 ,  B60N3/02 ,  B64D11/06

CPC分类号： B64D11/0693 ,  B64D11/06 ,  B64D11/062 ,  B64D11/06395 ,  B64D11/0646

摘要： An aircraft seat assembly including multiple seats together having a total seating area. The aircraft seat assembly also includes an armrest separating a first seat of the multiple seats from a second seat of the multiple seats and a sliding mechanism coupled to the armrest. The sliding mechanism enables movement of the armrest to change a portion of the total seating area that is associated with at least one seat of the multiple seats. The aircraft seat assembly also includes a controller that controls movement of the armrest responsive to a control command.

摘要翻译： 一个包括多个座位在一起的飞机座椅组件，具有总的休息区。 飞机座椅组件还包括扶手将多个座椅的第一座椅与多个座椅的第二座椅分开，以及联接到扶手的滑动机构。 滑动机构使得扶手的移动能够改变与多个座椅的至少一个座椅相关联的总座位区域的一部分。 飞机座椅组件还包括控制器，该控制器响应于控制命令来控制扶手的运动。

公开(公告)号：US20140191078A1

公开(公告)日：2014-07-10

申请号：US13736632

申请日：2013-01-08

申请人： The Boeing Company

发明人： Kelly L. Boren ,  Sergey D. Barmichev

IPC分类号： B64C25/42

CPC分类号： B64C25/42 ,  B60T1/14 ,  B64C25/32 ,  B64C25/68

摘要： A system, an apparatus, and a method for an aerospace vehicle braking system for decelerating an aerospace vehicle on a landing surface. An arm is provided having a first portion connected to the aerospace vehicle and a second portion generally distal to the first portion. The second portion of the arm includes an engagement portion configured to engage the landing surface. The arm is movable between a first position, wherein the engagement portion is substantially disengaged from the landing surface, and a second position, wherein the engagement portion engages the landing surface with a force sufficient to significantly decelerate the aerospace vehicle. The engagement portion is configured to pivot with respect to the arm in response to the direction of travel of the aerospace vehicle upon the landing surface. An actuator is connected to the arm to selectively move the arm between the first position and the second position.

摘要翻译： 一种用于航空航天车辆制动系统的系统，装置和方法，用于使航空航天器在着陆面上减速。 臂被设置有具有连接到航空航天车辆的第一部分和大致远离第一部分的第二部分。 臂的第二部分包括被配置为接合着陆表面的接合部分。 臂可在第一位置和第二位置之间移动，第一位置与接合部分基本上脱离接合表面;第二位置，其中接合部分以足以使航空航天车辆显着减速的力与着陆面接合。 接合部分构造成响应于航空航天器在着陆表面上的行进方向相对于臂枢转。 致动器连接到臂以选择性地在第一位置和第二位置之间移动臂。

公开(公告)号：US20140117156A1

公开(公告)日：2014-05-01

申请号：US13661994

申请日：2012-10-26

申请人： The Boeing Company

发明人： Kelly L. Boren

IPC分类号： B64D11/02 ,  B64D11/06

CPC分类号： B64D11/02

摘要： An aircraft cabin has a lavatory that is accessible from a cross-aisle of the aircraft and in which the toilet is moved from the typical outboard location to an inboard location where increased head room enables the toilet to be positioned in tight proximity to a back wall of the lavatory directly behind the toilet and thereby increases an open area of floor surface in front of the toilet for wheelchair access to the lavatory.

摘要翻译： 飞机机舱具有可从飞机的十字架通道进入的卫生间，其中马桶从典型的外侧位置移动到内侧位置，在该位置，增加的头部房间使得马桶能够靠近后壁定位 盥洗室直接位于马桶后面，从而增加了厕所前面的地板表面的开放面积，以便轮椅进入洗手间。

公开(公告)号：US09533761B2

公开(公告)日：2017-01-03

申请号：US14076743

申请日：2013-11-11

申请人： The Boeing Company

发明人： Kelly L. Boren ,  Paul Andrew Kinzer

IPC分类号： B64D11/00 ,  B64C1/00

CPC分类号： B64D11/00 ,  B64C2001/0027 ,  Y02T50/46

摘要： An aircraft may include a cabin having a first portion, a second portion, a first ramp and a second ramp. The first portion of the cabin may include an upper deck and a lower deck. The upper deck and the lower deck may be disposed proximate to each other with vertical separation therebetween. The second portion may include an intermediate deck disposed in a plane that is substantially parallel to planes in which the upper deck and the lower deck lie. The intermediate deck may be vertically separated from both the upper deck and the lower deck. The first ramp may extend between the lower deck and the intermediate deck to provide access therebetween. The second ramp may extend between the upper deck and the intermediate deck to provide access therebetween.

摘要翻译： 飞机可以包括具有第一部分，第二部分，第一斜坡和第二斜坡的舱室。 机舱的第一部分可以包括上甲板和下甲板。 上甲板和下甲板可以彼此靠近地设置，其间具有垂直间隔。 第二部分可以包括设置在基本上平行于上甲板和下甲板所在的平面的平面中的中间甲板。 中间甲板可以与上甲板和下甲板两者垂直分离。 第一斜坡可以在下甲板和中间甲板之间延伸以在其间提供通路。 第二斜坡可以在上甲板和中间甲板之间延伸以在其间提供通路。

公开(公告)号：US09051052B2

公开(公告)日：2015-06-09

申请号：US13661994

申请日：2012-10-26

申请人： The Boeing Company

发明人： Kelly L. Boren

IPC分类号： B64D11/02

CPC分类号： B64D11/02

摘要： An aircraft cabin has a lavatory that is accessible from a cross-aisle of the aircraft and in which the toilet is moved from the typical outboard location to an inboard location where increased head room enables the toilet to be positioned in tight proximity to a back wall of the lavatory directly behind the toilet and thereby increases an open area of floor surface in front of the toilet for wheelchair access to the lavatory.

摘要翻译： 飞机机舱具有可从飞机的十字架通道进入的卫生间，其中马桶从典型的外侧位置移动到内侧位置，在该位置，增加的头部房间使得马桶能够靠近后壁定位 盥洗室直接位于马桶后面，从而增加了厕所前面的地板表面的开放面积，以便轮椅进入洗手间。

公开(公告)号：US20140337067A1

公开(公告)日：2014-11-13

申请号：US14446207

申请日：2014-07-29

申请人： The Boeing Company

发明人： Kelly L. Boren ,  Mithra M.K.V. Sankrithi ,  Rush F. Green ,  Gregory J. Oakes ,  Sergey Barmichev

IPC分类号： G06Q50/30 ,  G06Q10/02

CPC分类号： B64D11/00 ,  B64D11/06 ,  B64D11/0601 ,  B64D11/0693 ,  B64D11/0696 ,  G06Q10/02 ,  G06Q50/30

摘要： A method and apparatus comprising a plurality of seating systems and a frame for use in a passenger aircraft. A first seating system in the plurality of seating systems may have different dimensions from a second seating system in the plurality of seating systems. A frame may be configured to be connected to the plurality of seating systems.

摘要翻译： 一种包括多个座位系统和用于客机的框架的方法和装置。 多个座位系统中的第一座椅系统可具有与多个座位系统中的第二座椅系统不同的尺寸。 框架可以被配置为连接到多个座位系统。

公开(公告)号：US20140264221A1

公开(公告)日：2014-09-18

申请号：US13797060

申请日：2013-03-12

申请人： The Boeing Company

发明人： Kelly L. Boren

IPC分类号： B64D11/00 ,  B60N3/02

CPC分类号： B64D11/00 ,  B60N3/026 ,  E04F11/1804

摘要： A handrail apparatus and method for use with vehicles are disclosed. An apparatus in accordance with the teachings of this disclosure includes a first coupling plate to be coupled to a monument of a vehicle, a second coupling plate to be coupled to the monument of the vehicle. The apparatus includes a handrail coupled to the first coupling plate and a support coupled to the second coupling plate and the handrail. The handrail is movable between a stowed position and a deployed position.

摘要翻译： 公开了一种用于车辆的扶手装置和方法。 根据本公开的教导的装置包括要耦合到车辆的纪念碑的第一联接板，要耦合到车辆的纪念碑的第二联接板。 该装置包括联接到第一联接板的扶手和联接到第二联接板和扶手的支撑件。 扶手可以在收起位置和展开位置之间移动。

公开(公告)号：US20140166807A1

公开(公告)日：2014-06-19

申请号：US14076743

申请日：2013-11-11

申请人： The Boeing Company

发明人： Kelly L. Boren ,  Paul Andrew Kinzer

IPC分类号： B64D11/00

CPC分类号： B64D11/00 ,  B64C2001/0027 ,  Y02T50/46

摘要： An aircraft may include a cabin having a first portion, a second portion, a first ramp and a second ramp. The first portion of the cabin may include an upper deck and a lower deck. The upper deck and the lower deck may be disposed proximate to each other with vertical separation therebetween. The second portion may include an intermediate deck disposed in a plane that is substantially parallel to planes in which the upper deck and the lower deck lie. The intermediate deck may be vertically separated from both the upper deck and the lower deck. The first ramp may extend between the lower deck and the intermediate deck to provide access therebetween. The second ramp may extend between the upper deck and the intermediate deck to provide access therebetween.

摘要翻译： 飞机可以包括具有第一部分，第二部分，第一斜坡和第二斜坡的舱室。 机舱的第一部分可以包括上甲板和下甲板。 上甲板和下甲板可以彼此靠近地设置，其间具有垂直间隔。 第二部分可以包括设置在基本上平行于上甲板和下甲板所在的平面的平面中的中间甲板。 中间甲板可以与上甲板和下甲板两者垂直分离。 第一斜坡可以在下甲板和中间甲板之间延伸以在其间提供通路。 第二斜坡可以在上甲板和中间甲板之间延伸以在其间提供通路。