
基本信息:
- 专利标题: SEAT BACK DECOUPLER MECHANISM
- 申请号:US16218731 申请日:2018-12-13
- 公开(公告)号:US20190112051A1 公开(公告)日:2019-04-18
- 发明人: Travis K. Finlay , Sebastián Aberastury
- 申请人: B/E Aerospace, Inc.
- 主分类号: B64D11/06
- IPC分类号: B64D11/06
摘要:
An aircraft passenger seat with dynamic seat back breakover including a pivotally-attached seat back element and a seat back breakover mechanism including an articulating weighted inertia linkage operable for coupling the seat back element in a first operating condition in which the seat back element is movable between an upright taxi takeoff and landing (TTOL) position and a reclined position, and decoupling the seat back element in a second operating condition to allow the seat back element to move forward past the upright position, the first operating condition corresponding to inertial loading below a predetermined threshold value and the second operating condition corresponding to inertial loading above the predetermined threshold value.
公开/授权文献:
- US11059587B2 Seat back decoupler mechanism 公开/授权日:2021-07-13
IPC结构图谱:
B | 作业;运输 |
--B64 | 飞行器;航空;宇宙航行 |
----B64D | 用于与飞机配合或装到飞机上的设备;飞行衣;降落伞;动力装置或推进传动装置的配置或安装 |
------B64D11/00 | 乘客或乘务员设备;其他类目不包含的飞行甲板装置 |
--------B64D11/06 | .座椅的布置或配备 |