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1. 发明申请

US20090309328A1 AMPHIBIOUS SPORT AIRCRAFT TRAILER 有权
标题翻译：大型运动飞行员
公开(公告)号：US20090309328A1
公开(公告)日：2009-12-17
申请号：US12482277
申请日：2009-06-10
申请人： Matthew Gionta , Kirk Hawkins , Paul Nicholas
发明人： Matthew Gionta , Kirk Hawkins , Paul Nicholas
IPC分类号： B60P3/11 , B60P3/10
CPC分类号： B60P3/1033 , B60P3/11
摘要： An amphibious aircraft trailer includes a frame supported on a wheel/suspension bearing axle for movements over a roadway surface. Incorporated into the trailer is a cradle configured to engage a hull of the amphibious aircraft when it is loaded and unloaded in water conditions. A lift mechanism interposed between and coupled to the frame and the cradle is operable to displace the cradle vertically with respect to the frame such that landing gear associated with the amphibious aircraft can be extended or retracted while on the trailer. The trailer may also include a plurality of wheel tracks aligned with the landing gear to facilitate the aircraft's loading and unloading in its ground based mode of operation.
摘要翻译：水陆两用飞机拖车包括支撑在车轮/悬架轴承轴上的框架，用于在道路表面上移动。挂在拖车中的是支架，配置为当水陆两用飞机的装载和卸载时在水中接合。插入在框架和托架之间并联接到框架和托架的提升机构可操作以相对于框架垂直地移动托架，使得与水陆两用飞机相关联的起落架可以在拖车上延伸或缩回。拖车还可以包括与起落架对准的多个轮轨，以便于飞机在其基于地面的操作模式下的装载和卸载。

2. 发明授权

US08152100B2 Amphibious sport aircraft trailer 有权
标题翻译：两栖运动飞机拖车
公开(公告)号：US08152100B2
公开(公告)日：2012-04-10
申请号：US12482277
申请日：2009-06-10
申请人： Paul Nicholas , Kirk Hawkins , Matthew Gionta
发明人： Paul Nicholas , Kirk Hawkins , Matthew Gionta
IPC分类号： B60P3/11
CPC分类号： B60P3/1033 , B60P3/11
摘要： An amphibious aircraft trailer includes a frame supported on a wheel/suspension bearing axle for movements over a roadway surface. Incorporated into the trailer is a cradle configured to engage a hull of the amphibious aircraft when it is loaded and unloaded in water conditions. A lift mechanism interposed between and coupled to the frame and the cradle is operable to displace the cradle vertically with respect to the frame such that landing gear associated with the amphibious aircraft can be extended or retracted while on the trailer. The trailer may also include a plurality of wheel tracks aligned with the landing gear to facilitate the aircraft's loading and unloading in its ground based mode of operation.
摘要翻译：水陆两用飞机拖车包括支撑在车轮/悬架轴承轴上的框架，用于在道路表面上移动。挂在拖车中的是支架，配置为当水陆两用飞机的装载和卸载时在水中接合。插入在框架和托架之间并联接到框架和托架的提升机构可操作以相对于框架垂直地移动托架，使得与水陆两用飞机相关联的起落架可以在拖车上延伸或缩回。拖车还可以包括与起落架对准的多个轮轨，以便于飞机在其基于地面的操作模式下的装载和卸载。

3. 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.

4. 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。

5. 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。

6. 发明授权

US08157206B2 Two-motion wing-fold mechanism with independent load path 有权
标题翻译：具有独立载荷路径的双运动翼折机构
公开(公告)号：US08157206B2
公开(公告)日：2012-04-17
申请号：US12482308
申请日：2009-06-10
申请人： Matthew Gionta , James Crocoll , Jon Karkow , Paul Nicholas , Scott Bledsoe
发明人： Matthew Gionta , James Crocoll , Jon Karkow , Paul Nicholas , Scott Bledsoe
IPC分类号： B64C3/56
CPC分类号： B64C3/56 , Y02T50/14
摘要： An aircraft wing folding system folds an outboard wing section relative to an inboard wing section between a deployed position and a stored position in two discrete motions where each motion has an independent load path separate of the loading of the wing experienced by in-flight aerodynamic forces. The wing-fold mechanism of the present invention includes a fold assembly comprising a twist component and a fold component operable to fold the outboard wing section from the deployed position to the stored position that remains substantially unloaded with respect to in-flight aerodynamic forces when the wing is in the deployed or flight configuration.
摘要翻译：飞机机翼折叠系统相对于在两个离散运动中的展开位置和存储位置之间的内侧翼部分折叠外侧翼部分，其中每个运动具有独立的负载路径，其分离由飞行中的空气动力。本发明的机翼折叠机构包括折叠组件，该折叠组件包括扭转部件和折叠部件，该折叠部件可操作以将外侧机翼部分从展开位置折叠到相对于飞行中的空气动力力基本上被卸载的存储位置，机翼正在部署或飞行配置中。

7. 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。

8. 发明申请

US20110180657A1 TWO-MOTION WING-FOLD MECHANISM WITH INDEPENDENT LOAD PATH 有权
标题翻译：具有独立负载路径的双动力机身
公开(公告)号：US20110180657A1
公开(公告)日：2011-07-28
申请号：US12482308
申请日：2009-06-10
申请人： Matthew Gionta , James Crocoll , Jon Karkow , Paul Nicholas
发明人： Matthew Gionta , James Crocoll , Jon Karkow , Paul Nicholas
IPC分类号： B64C3/56
CPC分类号： B64C3/56 , Y02T50/14
摘要： An aircraft wing folding system folds an outboard wing section relative to an inboard wing section between a deployed position and a stored position in two discrete motions where each motion has an independent load path separate of the loading of the wing experienced by in-flight aerodynamic forces. The wing-fold mechanism of the present invention includes a fold assembly comprising a twist component and a fold component operable to fold the outboard wing section from the deployed position to the stored position that remains substantially unloaded with respect to in-flight aerodynamic forces when the wing is in the deployed or flight configuration.
摘要翻译：飞机机翼折叠系统相对于在两个离散运动中的展开位置和存储位置之间的内侧翼部分折叠外侧翼部分，其中每个运动具有独立的负载路径，其分离由飞行中的空气动力。本发明的机翼折叠机构包括折叠组件，该折叠组件包括扭转部件和折叠部件，该折叠部件可操作以将外侧机翼部分从展开位置折叠到相对于飞行中的空气动力力基本上被卸载的存储位置，机翼正在部署或飞行配置中。

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