公开(公告)号：US20160343467A1

公开(公告)日：2016-11-24

申请号：US14726964

申请日：2015-06-01

Applicant: Aurora Flight Sciences Corporation

Inventor： ED WEN ,  DAN COTTRELL ,  ADAM EHRMANTRAUT ,  MARK BLEHAR ,  DAVID KORDONOWY

IPC: H01B7/00 ,  C23C16/44 ,  H01B13/012 ,  C23C16/06

CPC classification number: C23C16/06 ,  B29C70/885 ,  B29L2031/3076 ,  B64C3/185 ,  B64C3/20 ,  B64C3/26 ,  B64C2001/0072 ,  B64D15/12 ,  B64D45/00 ,  H01B7/0018 ,  H01B7/0823 ,  H01B7/0838 ,  H01B7/0861 ,  H01L2924/01079 ,  H01L2924/14 ,  H05K1/0393 ,  H05K3/281 ,  H05K3/321 ,  Y02T50/54

Abstract: A multi-functional composite system generally comprises a core, a plurality of structural composite fiber layers, a matrix material, a connector configured to interface with one or more electrical devices and a composite conductor assembly, the composite conductor assembly having one or more conductors disposed between two or more insulating layers.

Abstract translation: 多功能复合系统通常包括芯，多个结构复合纤维层，矩阵材料，被配置为与一个或多个电气装置和复合导体组件相接合的连接器，所述复合导体组件具有一个或多个导体， 在两个或更多个绝缘层之间。

公开(公告)号：US20150344138A1

公开(公告)日：2015-12-03

申请号：US14727060

申请日：2015-06-01

Applicant: Aurora Flight Sciences Corporation

Inventor： ED WEN ,  DAN COTTRELL ,  ADAM EHRMANTRAUT ,  MARK BLEHAR ,  DAVID KORDONOWY

IPC: B64D15/12 ,  H05B3/28

CPC classification number: H05B3/286 ,  B64C1/12 ,  B64D45/00 ,  H05B2214/02 ,  H05B2214/04 ,  Y02T50/54 ,  Y10T29/49085

Abstract: A multi-functional composite system, the multi-functional composite system comprising a core, a plurality of structural composite fiber layers, a matrix material, a composite conductor assembly, the composite conductor assembly having one or more conductors disposed between two or more insulating layers, and an electric power source electronically coupled with said composite conductor assembly, the electric power source is configured to pass electric current through at least one of said one or more conductors.

Abstract translation: 一种多功能复合系统，所述多功能复合系统包括芯，多个结构复合纤维层，基体材料，复合导体组件，所述复合导体组件具有设置在两个或多个绝缘层之间的一个或多个导体 以及与所述复合导体组件电连接的电源，所述电源被配置为使电流通过所述一个或多个导体中的至少一个。

公开(公告)号：US20160137311A1

公开(公告)日：2016-05-19

申请号：US14213450

申请日：2014-03-14

Applicant: Aurora Flight Sciences Corporation

Inventor： JAMES PEVERILL ,  ADAM WOODWORTH ,  BENJAMIN FREUDBERG ,  DAN COTTRELL ,  TERRENCE MCKENNA

IPC: B64F1/02 ,  B64C39/02 ,  B60L11/18 ,  B64D45/08 ,  G05D1/10 ,  B64C25/68 ,  B64D47/08

CPC classification number: B64F1/02 ,  B60L11/1816 ,  B60L11/1838 ,  B60L2200/10 ,  B64C25/68 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/066 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/182 ,  B64D47/04 ,  B64D47/08 ,  B64F1/362 ,  G05D1/101 ,  G06K9/0063

Abstract: An aerial vehicle system for gathering data may comprise a Waypoint Location, wherein the Waypoint Location comprises an arresting cable; a Ground Control Station, wherein the Ground Control Station comprises a charging cable; and an aerial vehicle, wherein the aerial vehicle comprises an onboard battery, a capturing hook and a sensor payload for generating surveillance data. The aerial vehicle may be configured to autonomously travel between the Waypoint Location and the Ground Control Station. The aerial vehicle may be configured to couple with the arresting cable via the capturing hook. The aerial vehicle may be configured to electronically couple with the charging cable via the capturing hook to facilitate charging the aerial vehicle's onboard battery.

Abstract translation: 用于收集数据的飞行器系统可以包括航点位置，其中航点位置包括拦阻缆线; 地面控制站，其中地面控制站包括充电电缆; 以及飞行器，其中所述空中飞行器包括车载电池，捕获钩和用于产生监视数据的传感器有效载荷。 航空器可以被配置为在路点位置和地面控制站之间自主行进。 飞行器可以被配置成经由捕获钩与阻止电缆耦合。 飞行器可以被配置为经由捕获钩与充电电缆电子耦合，以便于对飞行器的车载电池充电。