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12 条记录 (耗时 0.048 秒)

    Deep stall aircraft landing
    1.
    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
    2.
    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。

    Inverted-landing aircraft
    3.
    发明授权
    Inverted-landing aircraft 有权
    倒地飞机

    公开(公告)号：US09511858B2

    公开(公告)日：2016-12-06

    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 ,  G05D1/06

    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。

    INVERTED-LANDING AIRCRAFT
    4.
    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。

    Foamable polyvinyl halogenated resin mass, use of polymerizates thereof as processing aids and objects formed therefrom
    8.
    发明授权
    Foamable polyvinyl halogenated resin mass, use of polymerizates thereof as processing aids and objects formed therefrom 有权
    可发泡聚乙烯基卤化树脂物质，其聚合物用作加工助剂和由其形成的物体

    公开(公告)号：US6043293A

    公开(公告)日：2000-03-28

    申请号：US174874

    申请日：1998-10-19

    申请人： Pavel Belik ,  Georg Schneider ,  Klaus Dorn ,  Stefan Forster ,  Bernd Frischkemuth

    发明人： Pavel Belik ,  Georg Schneider ,  Klaus Dorn ,  Stefan Forster ,  Bernd Frischkemuth

    IPC分类号： C08J9/04 ,  C08F2/22 ,  C08J9/00 ,  C08L27/00 ,  C08L27/06 ,  C08L33/12

    CPC分类号： C08J9/0061 ,  C08L27/06 ,  C08J2327/02 ,  C08J2433/00 ,  C08L33/12

    摘要： There are provided foamable, foamable polyvinyl halide resin masses containing: A) 1 to 25 parts relative to 100 parts of polyvinyl halide, of a polymerizate obtainable through the emulsion polymerization of i) up to 20 to not more than 75 parts of methylmethacrylate, ii) 25 to 80 parts of one or more C.sub.2 -C.sub.18 alkylmethacrylates, iii) 0 to 5 parts of one or more vinyl unsaturated monomers copolymerizable with (i) and/or (ii, wherein the components (i)-(iii) together yield 100 parts and are polymerized with up to a further 100 parts of usual additives for emulsion polymerization, wherein the emulsion polymerizate is single stepped and has a viscosity number of >700 cm.sup.3 /g and wherein copolymers are excluded which contain iv) MMA per se, or less than 20 or more than 75 parts of MMA together with either v) one or more acrylic acid esters, and/or vi) ethyl methacrylate, n-butyl-methacrylate, or ethylhexyl methacrylate. The resin mass further includes: B) 0.1-10 parts based on 100 parts of the polyvinyl halide of one or more foaming materials, C) 0-100 parts based on 100 parts polyvinyl halide of the usual additives. This polyvinyl halide resin mass, after foaming, yields a resin mass which, as well as of good surface properties, has a foam density of

    摘要翻译： 提供了可发泡的，可发泡的聚卤乙烯树脂块，其包含：A）相对于100份聚卤乙烯为1至25份，通过i）至多20至不超过75份甲基丙烯酸甲酯可获得的聚合物，ii ）25至80份一种或多种C 2 -C 18烷基甲基丙烯酸酯，iii）0至5份可与（i）和/或（ii）共聚的一种或多种乙烯基不饱和单体，其中组分（i） - （iii）共同产生 100份，再与100份常用的乳液聚合添加剂进行聚合，其中乳液聚合物为单步级，粘度为> 700cm3 / g，其中排除含有iv）MMA本身的共聚物， 或小于20或大于75份的MMA以及v）一种或多种丙烯酸酯，和/或vi）甲基丙烯酸乙酯，正丁基 - 甲基丙烯酸酯或甲基丙烯酸乙基己基酯。 树脂质量还包括：B）基于100份一种或多种发泡材料的聚卤乙烯的0.1-10份，C）基于100份常规添加剂的聚卤乙烯的0-100份。 该聚卤乙烯树脂组合物在发泡后产生具有良好表面性质的泡沫密度<0.7g / cm 3的树脂组合物。