| 发明名称 |
ENGINE INSTALLATION OF VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT |
| 摘要 |
A vertical take-off and landing (VTOL) aircraft is provided and includes a fuselage, wings extending outwardly from opposite sides of the fuselage, nacelles supportively disposed on the wings and reversely oriented, axial flow engines disposed in each of the nacelles to generate mechanical energy for driving lift and thrust generating prop-rotor rotations. |
| 申请公布号 |
US2016304196(A1) |
申请公布日期 |
2016.10.20 |
| 申请号 |
US201615132883 |
申请日期 |
2016.04.19 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Alber Mark R. |
| 分类号 |
B64C29/02;B64D33/04;B64D27/12;B64D33/02 |
主分类号 |
B64C29/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A vertical take-off and landing (VTOL) aircraft, comprising:
a fuselage; wings extending outwardly from opposite sides of the fuselage; nacelles supportively disposed on the wings; and reversely oriented, axial flow engines disposed in each of the nacelles to generate mechanical energy for driving lift and thrust generating prop-rotor rotations. |
| 地址 |
Stratord CT US |
