公开(公告)号：US09663220B2

公开(公告)日：2017-05-30

申请号：US14193330

申请日：2014-02-28

申请人： The Boeing Company

发明人： Giumaa Milad ,  Edward M. Hojnacki ,  William Otto Zschoche

IPC分类号： B64C13/14 ,  B60R25/06

CPC分类号： B64C13/14 ,  Y10T70/40

摘要： Systems and methods for locking a control lever are provided. One system includes a locking device having a body configured to couple to a control lever within an aircraft to prevent the control lever from moving. The locking device also includes at least one hole defined through the body. The one hole is configured to receive one of a lock or a tag therein.

公开(公告)号：US20150246723A1

公开(公告)日：2015-09-03

申请号：US14193330

申请日：2014-02-28

申请人： The Boeing Company

发明人： Giumaa Milad ,  Edward M. Hojnacki ,  William Otto Zschoche

IPC分类号： B64C13/14 ,  B64F5/00 ,  B64D45/00

CPC分类号： B64C13/14 ,  Y10T70/40

摘要： Systems and methods for locking a control lever are provided. One system includes a locking device having a body configured to couple to a control lever within an aircraft to prevent the control lever from moving. The locking device also includes at least one hole defined through the body. The one hole is configured to receive one of a lock or a tag therein.

摘要翻译： 提供了用于锁定控制杆的系统和方法。 一个系统包括锁定装置，其具有构造成联接到飞行器内的控制杆的主体以防止控制杆移动。 锁定装置还包括至少一个通过身体限定的孔。 一个孔被配置为接收其中的一个锁或标签。