| 发明名称 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH VARIABLE WING GEOMETRY |
| 摘要 |
A vertical take-off and landing (VTOL) aircraft is provided and includes a fuselage, inboard wings extending from opposite sides of the fuselage to define a support plane and engine nacelles disposed along the wings. Each of the wings includes ground alighting elements and a variable geometry such that a portion of the ground alighting elements are alignable with the support plane during in-flight conditions and displaceable from the support plane. |
| 申请公布号 |
US2015284075(A1) |
申请公布日期 |
2015.10.08 |
| 申请号 |
US201414243540 |
申请日期 |
2014.04.02 |
| 申请人 |
Sikorsky Aircraft Corporation |
发明人 |
Alber Mark R. |
| 分类号 |
B64C27/22;B64C3/42;B64C39/02;B64C29/00;B64C25/10 |
主分类号 |
B64C27/22 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A vertical take-off and landing (VTOL) aircraft, comprising:
a fuselage; wings extending from opposite sides of the fuselage to define a support plane; and engine nacelles disposed along the wings, each of the wings comprising ground alighting elements and a variable geometry such that a portion of the ground alighting elements are alignable with the support plane during in-flight conditions and displaceable from the support plane. |
| 地址 |
Stratford CT US |
