公开(公告)号：US20030094542A1

公开(公告)日：2003-05-22

申请号：US09990462

申请日：2001-11-21

Inventor： John Williamson

IPC: B64D011/06 ,  B64D025/02 ,  B64D025/102

CPC classification number: B64D11/0696 ,  B60N2/015 ,  B60N2/062 ,  B60N2/231 ,  B60N3/004 ,  B64D11/0638 ,  B64D11/064

Abstract: A passenger seat which includes a seat bottom chassis assembled from a plurality of leg modules attached to fixed, spaced-apart attachment points on a supporting surface, and a plurality of beam elements for being carried by the leg modules. A plurality of clamp joints are positioned on a first side of the leg modules in a first laterally-offset relation thereto in a first spaced-apart relation to the attachment points of the supporting surface and for receiving the plurality of beam elements for defining a ladder frame assembly having a first specified width and seat spacing. The plurality of clamp joints are removable from the first side of the leg modules can positioned on a second, opposite side of the leg modules in a second laterally-offset relation for defining a ladder frame assembly having a second specified width and seat spacing while the plurality of leg modules maintain the same position relative to each other and thus to the fixed, spaced apart attachment points whereby the location of the seats may be altered while using the same beam elements.

Abstract translation: 一种乘客座椅，其包括由多个支腿模块组装的座底底盘，所述多个腿模块附接到支撑表面上的固定的间隔开的附接点，以及多个用于由腿部模块承载的梁元件。 多个夹紧接头以与支撑表面的附接点成第一间隔开的关系以与其相对的第一横向偏移关系定位在腿模块的第一侧上，并且用于容纳多个用于限定梯子的梁元件 框架组件具有第一特定宽度和座椅间距。 所述多个夹紧接头可从所述腿部模块的第一侧移除，所述腿部模块可以位于所述腿部模块的第二相对侧上，以第二横向偏移关系来限定具有第二特定宽度和座椅间距的梯形框架组件， 多个腿模块相对于彼此保持相同的位置，并因此保持相对于固定的间隔开的连接点，由此座椅的位置可以在使用相同的梁元件时改变。

公开(公告)号：US20030226934A1

公开(公告)日：2003-12-11

申请号：US10454889

申请日：2003-06-05

Inventor： Bruno Saint-Jalmes

IPC: B64D025/02 ,  B64D025/102

CPC classification number: B64D11/064 ,  A47C7/024 ,  A47C7/506 ,  B60N2/3061 ,  B60N2/3065 ,  B60N2205/30 ,  B64D11/0607 ,  B64D11/0643

Abstract: An aircraft seat includes a seat cushion and a seat back. The seat cushion has a rear portion along the seat back and a front portion of complementary shape to the rear portion to form a complete seat cushion. The rear portion moves between a raised position and a lowered position. A coupling arrangement connects the front portion to the rear portion so that when the front portion is in the raised position along the seat back the front portion is in the lowered position, in which at least part of it is retracted under the rear portion. When the rear portion is in its lowest position along the seat back the front portion is in a raised, advanced position at the same height as the rear portion to form therewith the seat cushion of the seat for receiving a seated passenger.

Abstract translation: 飞机座椅包括座垫和座椅靠背。 座垫具有沿着座椅靠背的后部和与后部互补的前部，以形成完整的座垫。 后部在升高位置和下降位置之间移动。 联接装置将前部连接到后部，使得当前部沿着座椅靠背处于升高位置时，前部处于降低位置，其中至少一部分在其后部缩回。 当后部沿着座椅靠背处于其最低位置时，前部处于与后部相同高度的升高的前进位置，以与其一起形成用于接收座位乘客的座椅座垫。

公开(公告)号：US20010023908A1

公开(公告)日：2001-09-27

申请号：US09804582

申请日：2001-03-09

Inventor： Jens Romca ,  Jochen Mueller ,  Markus Schumacher

IPC: B64D011/06 ,  B64D025/02 ,  B64D025/102

CPC classification number: B64D11/0647 ,  B64D11/00 ,  B64D11/06 ,  B64D45/00 ,  B64D2045/007

Abstract: A seating space such as an aircraft passenger cabin has rows of seats along an aisle, identified by a row number and a seat location letter. A seat row indicator is arranged on the side flank of the seat back of each aisle seat, at the corner where the side flank and upper edge of the seat back meet. A seat location indicator is arranged at the middle of the upper edge of the seat back of each seat. The row numbers and seat letters are indicated on or in the indicators by paint, printing, engraving, inserts, illumination or tactile indicia. The indicators are conspicuous and easily visible to a passenger standing or walking in the aisle without bending or leaning over. Boarding of the aircraft is facilitated and expedited. Emergency evacuation is assisted by appropriate illumination of the indicators.

Abstract translation: 诸如飞机乘客舱的座位空间具有沿着通道的一排座位，由行号和座位位置字母标识。 座位排指示器设置在每个通道座椅的座椅靠背的侧面，座椅靠背的侧面和上边缘相交的拐角处。 座椅位置指示器布置在每个座椅的座椅靠背的上边缘的中间。 行号和座位字母通过油漆，印刷，雕刻，插入，照明或触觉标记在指示器上或其中指示。 这些指示灯对于站立或走在通道中的乘客而言不会弯曲或倾斜，显而易见。 飞机的登机方便和加快。 通过适当照明指示灯辅助紧急疏散。

公开(公告)号：US20040031883A1

公开(公告)日：2004-02-19

申请号：US10222291

申请日：2002-08-15

Inventor： Gregory M. Schmidt

IPC: B64D011/06 ,  B64D025/02 ,  B64D025/102 ,  B64D025/112 ,  B64D025/118

CPC classification number: B64D11/064 ,  B60N2/0292 ,  B60N2/995 ,  B60N2002/247 ,  B64D11/062 ,  B64D11/0643 ,  B64D11/0696

Abstract: Multiple-position seating units, methods for operating seating units, and methods for installing seating units are disclosed herein. In one embodiment, the seating unit includes a first seat portion and a second seat portion. The first seat portion has a first upper surface with a front extremity. The first seat portion can be moveable between first and second positions. In the second position, the first seat portion is tilted forwardly downwardly. The second seat portion has a second upper surface that can be configured to support at least one shin of a person. The second seat portion can be moveable between a stowed position and a deployed position. In the deployed position, the second upper surface is spaced apart from the front extremity of the first seat portion.

Abstract translation: 本文公开了多位置座椅单元，操作座椅单元的方法以及安装座椅单元的方法。 在一个实施例中，座椅单元包括第一座椅部分和第二座椅部分。 第一座部分具有前端的第一上表面。 第一座椅部分可以在第一和第二位置之间移动。 在第二位置，第一座部向前倾斜。 第二座部分具有第二上表面，该第二上表面可被构造成支撑人的至少一个胫骨。 第二座椅部分可以在收起位置和展开位置之间移动。 在展开位置，第二上表面与第一座部分的前端间隔开。

公开(公告)号：US20030052229A1

公开(公告)日：2003-03-20

申请号：US10155445

申请日：2002-05-24

Inventor： Raymond W. Mort

IPC: B64D011/06 ,  B64D025/02 ,  B64D025/102

CPC classification number: B64D11/0619 ,  B64D11/06 ,  B64D11/0698

Abstract: A crashworthy aircraft seat for protecting a passenger during a crash of the aircraft includes a support structure coupled to the aircraft, a seat assembly slidingly associated with the support structure, guide means coupled to the support structure for guiding upright members of the seat assembly as the seat assembly slides relative to the support structure, and means for variably attenuating kinetic energy as the seat assembly and the passenger move downward relative to the support structure from an initial static start position to an end position during the crash.