| 发明名称 |
Remotely-Activated Self-Centering Cable Latch |
| 摘要 |
A hidden latch system for an interior structure of an aircraft is disclosed. The hidden latch system includes at least two engagement features coupled to an interior structure of an aircraft. Each of the at least two engagement features includes an engagement portion, an engagement rod, and a self-centering feature. The engagement portion is configured to engage and release the engagement rod, and the self-centering feature is configured to self-center the engagement rod in at least one direction. Further, the engagement portion is configured to release the engagement rod using a cable pull system. |
| 申请公布号 |
US2017058561(A1) |
申请公布日期 |
2017.03.02 |
| 申请号 |
US201514840188 |
申请日期 |
2015.08.31 |
| 申请人 |
The Boeing Company |
发明人 |
Terry Troy N.;Schoales Jasen P. |
| 分类号 |
E05B15/02;B64C1/14;E05C1/08;E05C3/12;E05B17/00;E05B65/00 |
主分类号 |
E05B15/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A hidden latch system for an interior structure of an aircraft, the hidden latch system comprising:
at least two engagement features coupled to an interior structure of an aircraft, wherein each of the at least two engagement features comprises:
an engagement portion;an engagement rod; anda self-centering feature, wherein the engagement portion is configured to engage and release the engagement rod, wherein the self-centering feature is configured to self-center the engagement rod in at least one direction, and wherein the engagement portion is configured to release the engagement rod using a cable pull system. |
| 地址 |
Chicago IL US |
