专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

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

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。

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. 外观设计

USD620838S1 Amphibious sport aircraft 有权
标题翻译：两栖运动飞机
公开(公告)号：USD620838S1
公开(公告)日：2010-08-03
申请号：US29319639
申请日：2008-06-11
申请人： Diego Miralles , Kirk Hawkins
设计人： Diego Miralles , Kirk Hawkins

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式