公开(公告)号：WO2007072045A3

公开(公告)日：2007-06-28

申请号：PCT/GB2006/004901

申请日：2006-12-22

Applicant: BRITISH AIRWAYS PLC ,  DARBYSHIRE, Martin ,  HERRING III, Asa, Dancy ,  WALDRIP, Dennis, Isaac ,  SCHATELL, Marc ,  WYSS, Alen ,  HALL, Gregory ,  SUTCAVAGE, Walter ,  LOVINGOOD, John ,  ALFORD, Dan ,  ROUND, Matthew

Inventor： DARBYSHIRE, Martin ,  HERRING III, Asa, Dancy ,  WALDRIP, Dennis, Isaac ,  SCHATELL, Marc ,  WYSS, Alen ,  HALL, Gregory ,  SUTCAVAGE, Walter ,  LOVINGOOD, John ,  ALFORD, Dan ,  ROUND, Matthew

IPC: B64D11/06 ,  B60N2/34 ,  B60N2/22 ,  B60N2/44 ,  B60N2/46 ,  B60N3/06

Abstract: An aircraft passenger seat comprises a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) so as to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4) and the secondary support surface (5) form a substantially flat and continuous surface wherein the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, said axis bein translated between the reclined and substantiall flat confi urations.

公开(公告)号：WO2007072045A2

公开(公告)日：2007-06-28

申请号：PCT/GB2006004901

申请日：2006-12-22

Applicant: BRITISH AIRWAYS PLC ,  DARBYSHIRE MARTIN ,  HERRING III ASA DANCY ,  WALDRIP DENNIS ISAAC ,  SCHATELL MARC ,  WYSS ALEN ,  HALL GREGORY ,  SUTCAVAGE WALTER ,  LOVINGOOD JOHN ,  ALFORD DAN ,  ROUND MATTHEW

Inventor： DARBYSHIRE MARTIN ,  HERRING III ASA DANCY ,  WALDRIP DENNIS ISAAC ,  SCHATELL MARC ,  WYSS ALEN ,  HALL GREGORY ,  SUTCAVAGE WALTER ,  LOVINGOOD JOHN ,  ALFORD DAN ,  ROUND MATTHEW

IPC: B60N2/34 ,  B60N2/75 ,  B60N2/90 ,  B64D11/06

CPC classification number: B64D11/06 ,  B64D11/0604 ,  B64D11/0606 ,  B64D11/064 ,  B64D11/0641 ,  B64D11/0643 ,  B64D11/0646

Abstract: An aircraft passenger seat comprises a primary seat (1) having a seat back (3) and a seat pan (4), and a secondary support surface (5) located or locatable opposite the primary seat (1), the passenger seat being able to adopt each of an upright configuration, a reclined configuration and a substantially flat configuration, such that in the reclined configuration, the primary seat (1) is reclined relative to the upright configuration and the secondary support surface (5) is angled upwardly towards the primary seat (1) so as to support the lower leg(s) of a passenger seated in the primary seat (1); and in the substantially flat configuration, the secondary support surface (5) is substantially horizontal and the seat back (3), the seat pan (4) and the secondary support surface (5) form a substantially flat and continuous surface wherein the secondary support surface (5) is rotatable about an axis between the reclined and substantially flat configurations, said axis bein translated between the reclined and substantiall flat confi urations.

Abstract translation: 一种飞机乘客座椅包括具有座椅靠背（3）和座椅底板（4）的主座椅（1）以及位于或可位于主座椅（1）对面的副支撑表面（5），乘客座椅能够 以采用竖直构型，斜躺构型和基本平坦构型中的每一种，使得在斜躺构型中，主座椅（1）相对于直立构型倾斜并且第二支承表面（5）向上朝着 主座椅（1），以支撑坐在主座椅（1）中的乘客的小腿; 并且在基本平坦的构造中，第二支撑表面（5）基本上是水平的并且座椅靠背（3），座板（4）和第二支撑表面（5）形成基本上平坦且连续的表面，其中第二支撑件 所述表面（5）可围绕所述斜躺构型和大致平坦构型之间的轴线旋转，所述轴线在所述斜躺平面和基本平坦构型之间平移。