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    INVERTED-LANDING AIRCRAFT
    3.
    发明申请
    INVERTED-LANDING AIRCRAFT 有权
    反转式飞机

    公开(公告)号：US20140350748A1

    公开(公告)日：2014-11-27

    申请号：US13261813

    申请日：2012-08-16

    申请人： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    发明人： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    IPC分类号： B64C39/02 ,  G05D1/08

    CPC分类号： G01C5/005 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/18 ,  B64D47/08 ,  G05D1/0011 ,  G05D1/0676 ,  G05D1/0808 ,  G05D1/0816

    摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.

    摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视图，（2）飞机切换红色和绿色翼灯的颜色，将副翼延伸为反转翼片，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。

    UAV PAYLOAD MODULE CAMERA ASSEMBLY AND RETRACTION MECHANISM
    7.
    发明申请
    UAV PAYLOAD MODULE CAMERA ASSEMBLY AND RETRACTION MECHANISM 有权
    无人机PAYLOAD模块摄像机组件和回退机构

    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。

    Deep stall aircraft landing
    8.
    发明授权
    Deep stall aircraft landing 有权
    深停飞机着陆

    公开(公告)号：US09208689B2

    公开(公告)日：2015-12-08

    申请号：US13261814

    申请日：2012-08-16

    申请人： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    发明人： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    IPC分类号： G08G5/02 ,  B64C39/02 ,  G05D1/06 ,  B64D31/00

    CPC分类号： G08G5/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/18 ,  B64D31/00 ,  G05D1/0011 ,  G05D1/0676

    摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.

    摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视野，（2）飞机切换红色和绿色翼灯的颜色，延伸副翼作为倒转襟翼，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。

    DEEP STALL AIRCRAFT LANDING
    9.
    发明申请
    DEEP STALL AIRCRAFT LANDING 有权
    深空飞机着陆

    公开(公告)号：US20140343752A1

    公开(公告)日：2014-11-20

    申请号：US13261814

    申请日：2012-08-16

    申请人： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    发明人： Christopher E. Fisher ,  Thomas Robert Szarek ,  Justin B. McAllister ,  Pavel Belik

    IPC分类号： G08G5/02 ,  B64D31/00

    CPC分类号： G08G5/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/104 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/18 ,  B64D31/00 ,  G05D1/0011 ,  G05D1/0676

    摘要： An aircraft defining an upright orientation and an inverted orientation, a ground station; and a control system for remotely controlling the flight of the aircraft. The ground station has an auto-land function that causes the aircraft to invert, stall, and controllably land in the inverted orientation to protect a payload and a rudder extending down from the aircraft. In the upright orientation, the ground station depicts the view from a first aircraft camera. When switching to the inverted orientation: (1) the ground station depicts the view from a second aircraft camera, (2) the aircraft switches the colors of red and green wing lights, extends the ailerons to act as inverted flaps, and (3) the control system adapts a ground station controller for the inverted orientation. The aircraft landing gear is an expanded polypropylene pad located above the wing when the aircraft is in the upright orientation.

    摘要翻译： 定义直立方向和倒置方向的飞机，地面站; 以及用于远程控制飞机飞行的控制系统。 地面站具有自动地面功能，使飞机以反方向反转，失速和可控地降落，以保护从飞机向下延伸的有效载荷和舵。 在直立方向，地面站描绘从第一架飞机摄像机的视图。 当切换到倒置方向时：（1）地面站描绘从第二架飞机照相机的视图，（2）飞机切换红色和绿色翼灯的颜色，将副翼延伸为反转翼片，（3） 控制系统适应地面站控制器的倒置方向。 飞机起落架是当飞机处于直立方向时位于机翼上方的扩展的聚丙烯垫。