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1. 发明授权

US08286912B2 Wingtip and sponson interaction on an amphibious aircraft 有权
公开(公告)号：US08286912B2
公开(公告)日：2012-10-16
申请号：US13372150
申请日：2012-02-13
申请人： Jon Karkow , Krik Hawkins , Matthew Gionta , Steen Strand
发明人： Jon Karkow , Krik Hawkins , Matthew Gionta , Steen Strand
IPC分类号： B64C35/00
CPC分类号： B64C35/001 , B64C3/56 , B64C35/006 , Y02T50/14
摘要： A system for enhanced lateral stability of an amphibious aircraft includes a buoyancy system laterally displaced from opposite sides of the fuselage of the aircraft and wingtip system having a hydrodynamic planing surface associated with each wingtip. The hydrodynamic planing surface on each wingtip prevents the submersion of an associated buoyancy structure. By supplementing the lateral stability of the buoyancy structures using hydrodynamic planing surfaces, the combined lateral width of the fuselage and buoyancy structures can be reduced without detrimentally impacting operational performance. This reduced lateral width enables the amphibious aircraft to be configured for storage and transportation on a trailer or shipping container.

2. 发明申请

US20120187242A1 WINGTIP AND SPONSON INTERACTION ON AN AMPHIBIOUS AIRCRAFT 有权
标题翻译：在大型飞机上的WINGTIP和SPONSON相互作用
公开(公告)号：US20120187242A1
公开(公告)日：2012-07-26
申请号：US13372150
申请日：2012-02-13
申请人： Jon Karkow , Krik Hawkins , Matthew Gionta , Steen Strand
发明人： Jon Karkow , Krik Hawkins , Matthew Gionta , Steen Strand
IPC分类号： B64C25/54 , B64C35/02
CPC分类号： B64C35/001 , B64C3/56 , B64C35/006 , Y02T50/14
摘要： A system for enhanced lateral stability of an amphibious aircraft includes a buoyancy system laterally displaced from opposite sides of the fuselage of the aircraft and wingtip system having a hydrodynamic planing surface associated with each wingtip. The hydrodynamic planing surface on each wingtip prevents the submersion of an associated buoyancy structure. By supplementing the lateral stability of the buoyancy structures using hydrodynamic planing surfaces, the combined lateral width of the fuselage and buoyancy structures can be reduced without detrimentally impacting operational performance. This reduced lateral width enables the amphibious aircraft to be configured for storage and transportation on a trailer or shipping container.
摘要翻译：一种用于增强水陆两用飞机的侧向稳定性的系统包括从飞行器的机身的相对侧面横向偏移的浮力系统和具有与每个翼尖相关联的流体动力学平面的翼尖系统。每个翼尖上的流体力学刨削表面防止相关浮力结构的浸没。通过使用流体动力学刨削表面补充浮力结构的横向稳定性，可以减小机身和浮力结构的组合横向宽度，而不会不利地影响操作性能。这种减小的横向宽度使得两栖飞机能够被配置为在拖车或运输容器上存储和运输。

3. 发明申请

US20100314493A1 WINGTIP AND SPONSON INTERACTION ON AN AMPHIBIOUS AIRCRAFT 有权
标题翻译：在大型飞机上的WINGTIP和SPONSON相互作用
公开(公告)号：US20100314493A1
公开(公告)日：2010-12-16
申请号：US12482336
申请日：2009-06-10
申请人： Jon Karkow , Kirk Hawkins , Matthew Gionta , Steen Strand
发明人： Jon Karkow , Kirk Hawkins , Matthew Gionta , Steen Strand
IPC分类号： B64C35/00
CPC分类号： B64C35/001 , B64C3/56 , B64C35/006 , Y02T50/14
摘要： A system for enhanced lateral stability of an amphibious aircraft includes a buoyancy system laterally displaced from opposite sides of the fuselage of the aircraft and wingtip system having a hydrodynamic planing surface associated with each wingtip. The hydrodynamic planing surface on each wingtip prevents the submersion of an associated buoyancy structure. By supplementing the lateral stability of the buoyancy structures using hydrodynamic planing surfaces, the combined lateral width of the fuselage and buoyancy structures can be reduced without detrimentally impacting operational performance. This reduced lateral width enables the amphibious aircraft to be configured for storage and transportation on a trailer or shipping container.
摘要翻译：一种用于增强水陆两用飞机的侧向稳定性的系统包括从飞行器的机身的相对侧面横向偏移的浮力系统和具有与每个翼尖相关联的流体动力学平面的翼尖系统。每个翼尖上的流体力学刨削表面防止相关浮力结构的浸没。通过使用流体动力学刨削表面补充浮力结构的横向稳定性，可以减小机身和浮力结构的组合横向宽度，而不会不利地影响操作性能。这种减小的横向宽度使得两栖飞机能够被配置为在拖车或运输容器上存储和运输。

4. 发明授权

US08177162B2 Wingtip and sponson interaction on an amphibious aircraft 有权
标题翻译： Wingtip和赞助在两栖飞机上的互动
公开(公告)号：US08177162B2
公开(公告)日：2012-05-15
申请号：US12482336
申请日：2009-06-10
申请人： Jon Karkow , Kirk Hawkins , Matthew Gionta , Steen Strand
发明人： Jon Karkow , Kirk Hawkins , Matthew Gionta , Steen Strand
IPC分类号： B64C35/00
CPC分类号： B64C35/001 , B64C3/56 , B64C35/006 , Y02T50/14
摘要： A system for enhanced lateral stability of an amphibious aircraft includes a buoyancy system laterally displaced from opposite sides of the fuselage of the aircraft and wingtip system having a hydrodynamic planing surface associated with each wingtip. The hydrodynamic planing surface on each wingtip prevents the submersion of an associated buoyancy structure. By supplementing the lateral stability of the buoyancy structures using hydrodynamic planing surfaces, the combined lateral width of the fuselage and buoyancy structures can be reduced without detrimentally impacting operational performance. This reduced lateral width enables the amphibious aircraft to be configured for storage and transportation on a trailer or shipping container.
摘要翻译：一种用于增强水陆两用飞机的侧向稳定性的系统包括从飞行器的机身的相对侧面横向偏移的浮力系统和具有与每个翼尖相关联的流体动力学平面的翼尖系统。每个翼尖上的流体力学刨削表面防止相关浮力结构的浸没。通过使用流体动力学刨削表面补充浮力结构的横向稳定性，可以减小机身和浮力结构的组合横向宽度，而不会不利地影响操作性能。这种减小的横向宽度使得两栖飞机能够被配置为在拖车或运输容器上存储和运输。

5. 发明授权

US09169003B2 Self-orienting aircraft landing gear 有权
标题翻译：自主定向飞机起落架
公开(公告)号：US09169003B2
公开(公告)日：2015-10-27
申请号：US14333791
申请日：2014-07-17
申请人： Byron Young , Jon Karkow , Steen Strand
发明人： Byron Young , Jon Karkow , Steen Strand
IPC分类号： B64C25/50 , B64C25/36
CPC分类号： B64C25/36 , B64C25/50
摘要： An aircraft landing gear self-orients so to align itself within a plane parallel to the plane defined by the aircraft's roll and yaw axis. A nose gear of a tricycle landing gear configuration includes the ability to not only caster 360 degrees but also self-orient itself to be aligned parallel with the plane defined by the aircraft's roll and yaw axis once removed from any interaction with the ground. A simple and efficient mechanical design provides the landing gear with a substantially constant centering torque that neither impedes nor impairs ground movement yet returns the nose gear to a proper alignment for retraction and stowage.
摘要翻译：飞机起落架自我定位，使其在平行于由飞机的侧倾和偏转轴限定的平面的平面内对准。三轮车起落架配置的起落架包括不仅能够将脚轮360度的自动定向本身与由飞机的侧倾和偏航轴定义的平面对准的能力，一旦从与地面的任何相互作用中被去除，一种简单有效的机械设计为起落架提供了基本上恒定的定心转矩，既不妨碍也不损害地面运动，而是使起落架返回正确的对齐方式以缩回和装载。

6. 发明申请

US20150021434A1 SELF-ORIENTING AIRCRAFT LANDING GEAR 有权
标题翻译：自主研发飞机起落架
公开(公告)号：US20150021434A1
公开(公告)日：2015-01-22
申请号：US14333791
申请日：2014-07-17
申请人： Byron Young , Jon Karkow , Steen Strand
发明人： Byron Young , Jon Karkow , Steen Strand
IPC分类号： B64C25/36
CPC分类号： B64C25/36 , B64C25/50
摘要： An aircraft landing gear self-orients so to align itself within a plane parallel to the plane defined by the aircraft's roll and yaw axis. A nose gear of a tricycle landing gear configuration includes the ability to not only caster 360 degrees but also self-orient itself to be aligned parallel with the plane defined by the aircraft's roll and yaw axis once removed from any interaction with the ground. A simple and efficient mechanical design provides the landing gear with a substantially constant centering torque that neither impedes nor impairs ground movement yet returns the nose gear to a proper alignment for retraction and stowage.
摘要翻译：飞机起落架自我定位，使其在平行于由飞机的侧倾和偏转轴限定的平面的平面内对准。三轮车起落架配置的起落架包括不仅能够将脚轮360度的自动定向本身与由飞机的侧倾和偏航轴定义的平面对准的能力，一旦从与地面的任何相互作用中被去除，一种简单有效的机械设计为起落架提供了基本上恒定的定心转矩，既不妨碍也不损害地面运动，而是使起落架返回正确的对齐方式以缩回和装载。

7. 发明申请

US20190255422A1 LATERALLY-SLIDING BOARD WITH BIFURCATED TRUCKS 审中-公开
公开(公告)号：US20190255422A1
公开(公告)日：2019-08-22
申请号：US16404229
申请日：2019-05-06
申请人： Steen Strand
发明人： Steen Strand
IPC分类号： A63C17/00 , A63C17/01
摘要： A bifurcated truck in a laterally-sliding board wheel assembly enables the “freeboard” to seamlessly transition from “carving”—as associated with a traditional skateboard—to new omnidirectional motions, in which the board can easy travel forward, backwards, sideways or in any other directional combination. The wheel assembly of this invention employs a bifurcated truck system having two independent suspension arms, both operating independently from one another and from the board's castering wheels. The wheel assemblies are mirrored at each longitudinal end of the board, resulting in the board's ability to carve, slide or skid—and easily transition back and forth among each of these modes—providing the rider a sense of stability and freedom commonly associated only with snowboarding.

8. 发明授权

US5833252A Lateral sliding roller board 失效
公开(公告)号：US5833252A
公开(公告)日：1998-11-10
申请号：US717406
申请日：1996-09-20
申请人： Steen Strand
发明人： Steen Strand
IPC分类号： A63C17/01 , A63C17/04
CPC分类号： A63C17/0033 , A63C17/01 , A63C17/012 , A63C17/014 , A63C17/04 , Y10T16/196
摘要： A roller board allowing the rider to slide laterally in a manner similar to a snowboard. The roller board is comprised of a platform having four fixed wheels, and two pivoting rollers positioned along the platform's longitudinal axis. The fixed wheels function similarly to conventional skateboard trucks. The pivoting rollers rotate to align themselves with the direction of force exerted on the platform. The pivoting rollers are spring biased to align themselves with the longitudinal axis of the platform. A height differential between the two types of rollers enables the rider to transfer weight from one type of roller to the other, alternating between the carving and sliding characteristics of a snowboard.

9. 发明授权

US10661151B2 Laterally-sliding board with bifurcated trucks 有权
公开(公告)号：US10661151B2
公开(公告)日：2020-05-26
申请号：US16404229
申请日：2019-05-06
申请人： Steen Strand
发明人： Steen Strand
IPC分类号： A63C17/04 , A63C17/00 , A63C17/01
摘要： A bifurcated truck in a laterally-sliding board wheel assembly enables the “freeboard” to seamlessly transition from “carving”—as associated with a traditional skateboard—to new omnidirectional motions, in which the board can easy travel forward, backwards, sideways or in any other directional combination. The wheel assembly of this invention employs a bifurcated truck system having two independent suspension arms, both operating independently from one another and from the board's castering wheels. The wheel assemblies are mirrored at each longitudinal end of the board, resulting in the board's ability to carve, slide or skid—and easily transition back and forth among each of these modes—providing the rider a sense of stability and freedom commonly associated only with snowboarding.

10. 外观设计

USD620392S1 Amphibious sport aircraft with wing-fold 有权
标题翻译：两栖运动飞机与翼折
公开(公告)号：USD620392S1
公开(公告)日：2010-07-27
申请号：US29319641
申请日：2008-06-11
申请人： Randy Rodriguez , Diego Miralles , Steen Strand
设计人： Randy Rodriguez , Diego Miralles , Steen Strand

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