| 发明名称 |
AIRCRAFT WITH INTEGRATED SINGLE SENSOR |
| 摘要 |
An aircraft is provided and includes a single sensor and wings extending outwardly in opposite directions from a fuselage. Each wing includes a main section, an engine section supported on the main section and tail surfaces extending transversely relative to the main section. The single sensor is mountable to one of the tail surfaces with a field of view (FOV) representable as a spherical wedge having a dihedral angle exceeding 180°. |
| 申请公布号 |
US2015344135(A1) |
申请公布日期 |
2015.12.03 |
| 申请号 |
US201514722921 |
申请日期 |
2015.05.27 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Alber Mark R. |
| 分类号 |
B64C29/00 |
主分类号 |
B64C29/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft, comprising:
a single sensor; and wings extending outwardly in opposite directions from a fuselage, each wing comprising a main section, an engine section supported on the main section and tail surfaces extending transversely relative to the main section, and the single sensor being mountable to one of the tail surfaces with a field of view (FOV) representable as a spherical wedge having a dihedral angle exceeding 180°. |
| 地址 |
Stratford CT US |
