公开(公告)号：US20130193269A1

公开(公告)日：2013-08-01

申请号：US13730828

申请日：2012-12-29

申请人： John Peter Zwaan ,  Pavel Belik ,  Manolis Dimotakis ,  Christopher J. D'Aquila

发明人： John Peter Zwaan ,  Pavel Belik ,  Manolis Dimotakis ,  Christopher J. D'Aquila

IPC分类号： B64D47/08

CPC分类号： B64D47/08 ,  B64C39/024 ,  B64C2201/127 ,  B64D9/00 ,  B64D27/24

摘要： In one possible embodiment, a UAV payload module retraction mechanism is provided including a payload pivotally attached to a housing. A biasing member is mounted to bias the payload out of the housing and a winch is attached to the payload. An elongated flexible drawing member is coupled between the housing and the winch, the elongated drawing flexible member being capable of being drawn by the winch to retract the payload within the housing.

摘要翻译： 在一个可能的实施例中，提供了一种UAV有效载荷模块缩回机构，其包括枢转地附接到壳体的有效载荷。 安装偏置构件以将有效载荷偏离壳体，并且绞盘附接到有效载荷。 细长的柔性绘图构件联接在壳体和绞盘之间，细长的拉伸柔性构件能够被绞盘牵引以将有效载荷缩回到壳体内。