| 发明名称 |
Aircraft System for Reduced Observer Visibility |
| 摘要 |
An aircraft apparatus is disclosed that has a fuselage boom having proximal and distal ends, a wing coupled to a proximal end of the fuselage boom and at least one transparent stabilizer coupled to a distal end of the fuselage boom. |
| 申请公布号 |
US2014312169(A1) |
申请公布日期 |
2014.10.23 |
| 申请号 |
US201414184542 |
申请日期 |
2014.02.19 |
| 申请人 |
AeroVironment, Inc. |
发明人 |
Fisher Christopher Eugene;Chambers Steven Bradley;Belik Pavil;Gunder Austin Craig;Zwaan John Peter |
| 分类号 |
B64C5/02;B64C39/00;B64C9/00;B64C3/10;B64C39/12;B64C5/06 |
主分类号 |
B64C5/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft apparatus, comprising:
a fuselage boom having proximal and distal ends; a wing coupled to the proximal end of said fuselage boom; and a first transparent stabilizer coupled to a distal end of said fuselage boom. |
| 地址 |
Monrovia CA US |
