公开(公告)号：US09121429B2

公开(公告)日：2015-09-01

申请号：US13856875

申请日：2013-04-04

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Timm E. Hartman ,  Casey Hanlon ,  Mitchell Laidlaw ,  Kellan Geck

IPC: F16B39/02 ,  F16H48/42

CPC classification number: F16B39/02 ,  F16B39/10 ,  F16H48/10 ,  F16H48/42 ,  F16H57/0025

Abstract: An apparatus includes a shaft, a device, a fastener, and an anti-rotation clip. The shaft is configured for rotation. The device is mounted on, and surrounds at least a portion of, the shaft, and has first and second protrusions that are formed on one side and are spaced apart to define a tab space. The fastener is rotationally mounted relative to the shaft, and includes a tab slot formed in its outer surface that extends radially inwardly and is disposed radially inwardly of the tab space. The anti-rotation clip includes a main body portion and a head portion that has a first tab portion and a second tab portion. At least a portion the main body portion is disposed between the device and the fastener, the first tab is disposed in the tab space, and the second tab is disposed in the tab slot.

Abstract translation: 一种装置包括轴，装置，紧固件和防旋转夹。 轴配置为旋转。 该装置安装在轴上并且围绕该轴的至少一部分，并且具有第一和第二突起，其形成在一侧上并且间隔开以限定突出部空间。 紧固件相对于轴旋转地安装，并且包括形成在其外表面中的径向向内延伸并且设置在凸片空间的径向内侧的凸片槽。 防旋转夹具包括主体部分和具有第一突出部分和第二突出部分的头部部分。 主体部分的至少一部分设置在装置和紧固件之间，第一突出部设置在突出部空间中，第二突片设置在突片槽中。

公开(公告)号：US20140302960A1

公开(公告)日：2014-10-09

申请号：US13856875

申请日：2013-04-04

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Timm E. Hartman ,  Casey Hanlon ,  Mitchell Laidlaw ,  Kellan Geck

IPC: F16B39/02 ,  F16H48/42

CPC classification number: F16B39/02 ,  F16B39/10 ,  F16H48/10 ,  F16H48/42 ,  F16H57/0025

Abstract: An apparatus includes a shaft, a device, a fastener, and an anti-rotation clip. The shaft is configured for rotation. The device is mounted on, and surrounds at least a portion of, the shaft, and has first and second protrusions that are formed on one side and are spaced apart to define a tab space. The fastener is rotationally mounted relative to the shaft, and includes a tab slot formed in its outer surface that extends radially inwardly and is disposed radially inwardly of the tab space. The anti-rotation clip includes a main body portion and a head portion that has a first tab portion and a second tab portion. At least a portion the main body portion is disposed between the device and the fastener, the first tab is disposed in the tab space, and the second tab is disposed in the tab slot.

Abstract translation: 一种装置包括轴，装置，紧固件和防旋转夹。 轴配置为旋转。 该装置安装在轴上并且围绕该轴的至少一部分，并且具有第一和第二突起，其形成在一侧上并且间隔开以限定突出部空间。 紧固件相对于轴旋转地安装，并且包括形成在其外表面中的径向向内延伸并且设置在凸片空间的径向内侧的凸片槽。 防旋转夹具包括主体部分和具有第一突出部分和第二突出部分的头部部分。 主体部分的至少一部分设置在装置和紧固件之间，第一突出部设置在突出部空间中，第二突片设置在突片槽中。

公开(公告)号：US20160312511A1

公开(公告)日：2016-10-27

申请号：US14803305

申请日：2015-07-20

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Kevin K. Chakkera ,  Timm E. Hartman ,  Ron Vaughan ,  Stephen Birn

IPC: E05F11/02 ,  E05F15/00 ,  B64D29/08 ,  F16H1/20

CPC classification number: F16H1/203 ,  B64C1/1446 ,  B64D29/06 ,  B64D29/08 ,  F02K1/763 ,  F16H1/22 ,  F16H25/2454

Abstract: An aircraft engine nacelle door operating system locking manual drive unit includes a housing, an input drive shaft, an output drive shaft, a lock shaft, and a lock spring. The input drive shaft, the output drive shaft, and the lock shaft are all rotationally mounted in the housing. The output drive shaft continuously engages and mates with the input drive shaft, and he lock shaft extends at least partially into and engages the input drive shaft. The lock shaft is movable between a lock position, in which it engages and mates with the output drive shaft, and an unlock position, in it is disengaged from the output drive shaft. The lock spring supplies a bias force to the lock shaft that urges the lock shaft toward the lock position.

Abstract translation: 飞机发动机舱门操作系统锁定手动驱动单元包括壳体，输入驱动轴，输出驱动轴，锁定轴和锁定弹簧。 输入驱动轴，输出驱动轴和锁定轴都旋转地安装在外壳中。 输出驱动轴与输入驱动轴连续地接合并配合，并且其锁定轴至少部分地延伸并接合输入驱动轴。 锁定轴可在其与输出驱动轴接合并配合的锁定位置之间移动，并且解锁位置在其中与输出驱动轴分离。 锁定弹簧向锁定轴提供偏压力，以将锁定轴朝向锁定位置。