| 发明名称 |
Structure and Method for Reducing Air Flow in a Wall Volume of an Aircraft |
| 摘要 |
An aircraft including a fuselage defining an upper lobe and a lower lobe, the fuselage including a wall structure that includes an outboard boundary and an inboard boundary spaced from the outboard boundary, wherein the outboard boundary and the inboard boundary define a wall volume therebetween, and a barrier sheeting member extending into the wall volume. |
| 申请公布号 |
US2015274304(A1) |
申请公布日期 |
2015.10.01 |
| 申请号 |
US201514616885 |
申请日期 |
2015.02.09 |
| 申请人 |
The Boeing Company |
发明人 |
Gray John C.;Black Roger B. |
| 分类号 |
B64D13/02;B64C1/10;B64C1/40;B64C1/18;B64D45/00;B64D11/04 |
主分类号 |
B64D13/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft comprising:
a fuselage defining an upper lobe and a lower lobe, said fuselage comprising a wall structure that comprises:
an outboard boundary; andan inboard boundary spaced from said outboard boundary,wherein said outboard boundary and said inboard boundary define a wall volume therebetween; and a barrier sheeting member extending into said wall volume. |
| 地址 |
Chicago IL US |
