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公开(公告)号：US09896197B2
公开(公告)日：2018-02-20
申请号：US14723720
申请日：2015-05-28
申请人： Eugene H Vetter , James W Vetter , Paul A Vetter
发明人： Eugene H Vetter , James W Vetter , Paul A Vetter
摘要： A hybrid VTOL/high speed aircraft may comprise systems and functions for in flight configuration changes from high lift helicopter or VTOL mode to fixed or swing-wing high speed aircraft mode to accommodate a variety of functions or missions.
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公开(公告)号：US10293928B2
公开(公告)日：2019-05-21
申请号：US15863884
申请日：2018-01-06
申请人： Eugene H Vetter , James W Vetter , Paul A Vetter
发明人： Eugene H Vetter , James W Vetter , Paul A Vetter
摘要： A hybrid VTOL/high speed aircraft may comprise systems and functions for in flight configuration changes from high lift helicopter or VTOL mode to fixed or swing-wing high speed aircraft mode to accommodate a variety of functions or missions.
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3.发明授权公开(公告)号：US09061762B2
公开(公告)日：2015-06-23
申请号：US13914120
申请日：2013-06-10
申请人： James W Vetter
发明人： James W Vetter
CPC分类号： B64C37/00 , B60F5/02 , B63H1/34 , B63H2001/346 , B64C29/0008 , B64C39/003 , B64C39/005
摘要： A vertical takeoff and landing craft that utilizes lifting, propulsion and maneuvering (LPM) assemblies comprising a series of blade foils arranged along track elongated loop paths disposed at the sides of a fuselage. These LPM assemblies are provided with control mechanisms enabling lift, attitude changes, altitude changes and directional flight propulsion and control including those needed for hovering as well as vertical takeoff and landing. The LPM assemblies are configured to drive large volumes of air in a manner and scale favorably similar to conventional rotorcraft while in contrast, providing capability for faster flights by eliminating or minimizing speed limiting factors commonly associated with rotorcraft.
摘要翻译： 一种采用提升，推进和机动（LPM）组件的垂直起飞和着陆艇，包括沿着设置在机身侧面的轨道细长环路径布置的一系列叶片。 这些LPM组件设有控制机构，可实现升降，姿态变化，高度变化和定向飞行推进和控制，包括悬停以及垂直起飞和着陆所需的。 LPM组件被配置成以与常规旋翼航空器相似的方式和比例尺驱动大量空气，而相比之下，通过消除或最小化通常与旋翼航空器相关联的速度限制因素来提供更快飞行的能力。
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4.发明授权公开(公告)号：US09580171B2
公开(公告)日：2017-02-28
申请号：US15043733
申请日：2016-02-15
申请人： James W Vetter
发明人： James W Vetter
CPC分类号： B64C37/00 , B60F5/02 , B63H1/34 , B63H2001/346 , B64C29/0008 , B64C39/003 , B64C39/005
摘要： A vertical takeoff and landing craft that utilizes lifting, propulsion and maneuvering (LPM) assemblies comprising a series of blade foils arranged along track elongated loop paths disposed at the sides of a fuselage. These LPM assemblies are provided with control mechanisms enabling lift, attitude changes, altitude changes and directional flight propulsion and control including those needed for hovering as well as vertical takeoff and landing. The LPM assemblies are configured to drive large volumes of air in a manner and scale favorably similar to conventional rotorcraft while in contrast, providing capability for faster flights by eliminating or minimizing speed limiting factors commonly associated with rotorcraft.
摘要翻译： 一种采用提升，推进和机动（LPM）组件的垂直起飞和着陆艇，包括沿着设置在机身侧面的轨道细长环路径布置的一系列叶片。 这些LPM组件设有控制机构，可实现升降，姿态变化，高度变化和定向飞行推进和控制，包括悬停以及垂直起飞和着陆所需的。 LPM组件被配置成以与常规旋翼航空器相似的方式和比例尺驱动大量空气，而相比之下，通过消除或最小化通常与旋翼航空器相关联的速度限制因素来提供更快飞行的能力。
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公开(公告)号：US09315266B2
公开(公告)日：2016-04-19
申请号：US14705519
申请日：2015-05-06
申请人： James W Vetter
发明人： James W Vetter
CPC分类号： B64C37/00 , B60F5/02 , B63H1/34 , B63H2001/346 , B64C29/0008 , B64C39/003 , B64C39/005
摘要： A vertical takeoff and landing craft that utilizes lifting, propulsion and maneuvering (LPM) assemblies comprising a series of blade foils arranged along track elongated loop paths disposed at the sides of a fuselage. These LPM assemblies are provided with control mechanisms enabling lift, attitude changes, altitude changes and directional flight propulsion and control including those needed for hovering as well as vertical takeoff and landing. The LPM assemblies are configured to drive large volumes of air in a manner and scale favorably similar to conventional rotorcraft while in contrast, providing capability for faster flights by eliminating or minimizing speed limiting factors commonly associated with rotorcraft.
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