公开(公告)号：WO2014011296A3

公开(公告)日：2014-03-27

申请号：PCT/US2013036750

申请日：2013-04-16

Applicant: WINTEC ARROWMAKER INC

Inventor： JONES JOHN CHARLES ,  GRIGORYEV ARTEM IGOREVICH ,  ESPINOSA LUIS CARLOS

IPC: B64F1/04

CPC classification number: B64F1/06 ,  B64C2201/084

Abstract: A man-portable unmanned aerial system launcher (UAS) launcher includes a rail assembly having an internal track and a carriage assembly having a base configured to translate within the internal track. The carriage assembly also includes a cradle configured to support a UAS and a bracket configured to support the cradle above the base. The UAS launcher includes a launch control system configured to secure the carriage assembly in the launch-ready position until the launch control system receives a launch signal. The UAS launcher also includes one or more elastic members configured to engage the carriage assembly and the rail assembly. Once the carriage assembly is translated to the launch-ready position, strain is applied to the carriage assembly by the one or more elastic members. Release of the carriage assembly enables force generated by strain of the elastic members to propel the carriage assembly toward a launch position.

Abstract translation: 便携式无人机系统发射器（UAS）发射器包括具有内部轨道的轨道组件和具有被配置为在内部轨道内平移的底座的滑架组件。 托架组件还包括支架，其构造成支撑UAS和支架，其构造成在底座上方支撑支架。 UAS发射器包括发射控制系统，其配置成将支架组件固定在发射就绪位置，直到发射控制系统接收到发射信号。 UAS发射器还包括一个或多个弹性构件，其构造成接合滑架组件和轨道组件。 一旦滑架组件被转换到发射就绪位置，则通过一个或多个弹性构件将应变施加到滑架组件。 托架组件的释放使得由弹性构件的应变产生的力能够将托架组件推向发射位置。

公开(公告)号：EP2838796A4

公开(公告)日：2016-03-23

申请号：EP13816392

申请日：2013-04-16

Applicant: WINTEC ARROWMAKER INC

Inventor： JONES JOHN CHARLES ,  GRIGORYEV ARTEM IGOREVICH ,  ESPINOSA LUIS CARLOS

IPC: B64F1/04 ,  B64F1/06

CPC classification number: B64F1/06 ,  B64C2201/084