| 发明名称 | System and method for magnetically and aerodynamically optimized control of rotorhead | ||
| 摘要 | A rotorcraft having an operational range and a plurality of rotor blades, each rotor blade capable of assuming an angular pitch, utilizes a control apparatus a mechanism for independently controlling an angular pitch value of each of the plurality of rotor blades wherein a collective sum of the angular pitch values of the plurality of rotor blades is not constant over the operational range of the rotorcraft. | ||
| 申请公布号 | US8845290(B1) | 申请公布日期 | 2014.09.30 |
| 申请号 | US201012976687 | 申请日期 | 2010.12.22 |
| 申请人 | Sonic Blue Aerospace, Inc. | 发明人 | Lugg Richard H. |
| 分类号 | B64C27/78 | 主分类号 | B64C27/78 |
| 代理机构 | Caseiro Burke LLC | 代理人 | Caseiro Burke LLC ;Caseiro Chris A. |
| 主权项 | 1. In a rotorcraft having an operational range and a plurality of rotor blades, each rotor blade capable of assuming an angular pitch, a control apparatus comprising: a mechanism for independently controlling an angular pitch value of each of the plurality of rotor blades; wherein a collective sum of the angular pitch values of the plurality of rotor blades is not constant over the operational range of the rotorcraft. | ||
| 地址 | Mebane NC US | ||