发明名称 |
Release and Capture of a Fixed-Wing Aircraft |
摘要 |
In one embodiment, a system includes an unmanned, multirotor helicopter and a fixed-wing aircraft. The multirotor helicopter may couple to the fixed-wing aircraft to support and hold the fixed-wing aircraft. The multirotor helicopter may then elevate the fixed-wing aircraft from a launch site to a release altitude. The multirotor helicopter may also accelerate the fixed-wing aircraft to a release speed and upon reaching the release speed, release the fixed-wing aircraft. The unmanned, multirotor helicopter may then return to the launch site. |
申请公布号 |
US2017036762(A1) |
申请公布日期 |
2017.02.09 |
申请号 |
US201514816318 |
申请日期 |
2015.08.03 |
申请人 |
Gamble Dustin;Curran Matthew |
发明人 |
Gamble Dustin;Curran Matthew |
分类号 |
B64D5/00;B64C27/08;B64C39/02 |
主分类号 |
B64D5/00 |
代理机构 |
|
代理人 |
|
主权项 |
1. A system, comprising:
an unmanned, multirotor helicopter; a fixed-wing aircraft; wherein the unmanned, multirotor helicopter is configured to:
couple to the fixed-wing aircraft to support and hold the fixed-wing aircraft;elevate the fixed-wing aircraft from a launch site to a release altitude;accelerate the fixed-wing aircraft to a release speed;release the fixed-wing aircraft upon reaching the release speed; andreturn to the launch site. |
地址 |
San Luis Obispo CA US |