专利检索 ap:("AIRBUS OPERATIONS LIMITED") AND inv:"Sarabpal-Singh Bhatia" 第 1 页

1.

发明授权
Spar arrangement in a wing tip device 有权

公开(公告)号：US11958597B2

公开(公告)日：2024-04-16

申请号：US18125399

申请日：2023-03-23

申请人： AIRBUS OPERATIONS LIMITED

发明人： Sarabpal-Singh Bhatia , Samuel Phillips

IPC分类号： B64C3/18 , B64C3/58 , B64C23/06 , B64F5/10

CPC分类号： B64C3/185 , B64C3/187 , B64C3/58 , B64C23/069 , B64F5/10

摘要： An aircraft wing assembly including a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13).

2.

发明授权
Spar arrangement in a wing tip device 有权

公开(公告)号：US11643183B2

公开(公告)日：2023-05-09

申请号：US16007555

申请日：2018-06-13

申请人： Airbus Operations Limited

发明人： Sarabpal-Singh Bhatia , Samuel Phillips

IPC分类号： B64C3/18 , B64C23/06 , B64F5/10 , B64C3/58

CPC分类号： B64C3/185 , B64C3/187 , B64C3/58 , B64C23/069 , B64F5/10

摘要： An aircraft (1) having a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13).