| 发明名称 |
Adjustable Support Structure for Aircraft Cabin Ceiling |
| 摘要 |
A system for adjusting a height of a ceiling panel in an aircraft and a corresponding method is disclosed. The system includes an arm and at least one ceiling support latch, wherein each of the at least one ceiling support latches is attached to the arm. The system further includes an adjustable fitting attached to the arm, wherein the adjustable fitting includes (i) a first sliding block attached to the arm, (ii) a second sliding block attached to a support structure, and (iii) an adjustment screw. Adjustment of the adjustment screw forces the first and second sliding blocks to move relative to one another. |
| 申请公布号 |
US2017057613(A1) |
申请公布日期 |
2017.03.02 |
| 申请号 |
US201514840245 |
申请日期 |
2015.08.31 |
| 申请人 |
The Boeing Company |
发明人 |
King Timothy Todd;Davis Kenneth G.;Thomas Matthew R.;Nadvornick Mark J.;McCune James R.;Mullins Jason W. |
| 分类号 |
B64C1/06;B64F5/00;B64D11/00 |
主分类号 |
B64C1/06 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A system for adjusting a height of a ceiling panel in an aircraft, the system comprising:
an arm; at least one ceiling support latch, wherein each of the at least one ceiling support latches is attached to the arm; and an adjustable fitting attached to the arm, wherein the adjustable fitting comprises (i) a first sliding block attached to the arm, (ii) a second sliding block attached to a support structure, and (iii) an adjustment screw, wherein adjustment of the adjustment screw forces the first and second sliding blocks to move relative to one another. |
| 地址 |
Chicago IL US |
