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91. 发明专利

JPS6250297A TAKEOFF AND LANDING DEVICE FOR HYDROAEROPLANE 失效
公开(公告)号：JPS6250297A
公开(公告)日：1987-03-04
申请号：JP18853085
申请日：1985-08-29
申请人： K SEVEN KK
发明人： KURIBAYASHI SADATOMO
IPC分类号： B64C25/54 , B64C35/00 , B64C35/02

92. 发明专利

JPS58218499A Air cushion vehicle 失效
标题翻译： AIR CUSHION VEHICLE
公开(公告)号：JPS58218499A
公开(公告)日：1983-12-19
申请号：JP9390683
申请日：1983-05-27
申请人： Paul Kjoelseth , Rolf Jan Mowill
发明人： KJOELSETH PAUL , MOWILL ROLF JAN
IPC分类号： B64C35/02 , B60V1/08 , B60V3/08
CPC分类号： B60V1/08

93. 发明专利

JPS5643099A PREVENTIVE DEVICE FOR JUMP OF AEROBOAT 失效
公开(公告)号：JPS5643099A
公开(公告)日：1981-04-21
申请号：JP11672779
申请日：1979-09-13
申请人： SHIN MEIWA IND CO LTD
发明人： SAKOHATA TAKESHI
IPC分类号： B63B1/22 , B63B1/18 , B64C35/00 , B64C35/02

94. 发明专利

JPS5477996A FLYING BOAT BODY 失效
公开(公告)号：JPS5477996A
公开(公告)日：1979-06-21
申请号：JP14037478
申请日：1978-11-14
申请人： LABONIA MICHELINO
发明人： MITSUCHIERIINO RABONIA
IPC分类号： B63B1/16 , B63B1/18 , B63B3/16 , B63B39/06 , B64C35/02

95. 实用新型

JPS5218560Y2 失效
公开(公告)号：JPS5218560Y2
公开(公告)日：1977-04-26
申请号：JP8436672
申请日：1972-07-19
IPC分类号： B64C25/54 , B64C35/00 , B64C35/02

96. 发明专利

JPS5239296A FLYING BOAT HAVING A GLIDING SURFACE PROJECTING FROM BOW 失效
公开(公告)号：JPS5239296A
公开(公告)日：1977-03-26
申请号：JP11431075
申请日：1975-09-23
申请人： SHIN MEIWA IND CO LTD
发明人： OZAKI ATSUSHI
IPC分类号： B64C25/54 , B64C25/52 , B64C35/00 , B64C35/02
摘要： PURPOSE:To improve wave resistance and minimize water resistance by providing a gliding surface protruding downward and forward to the bow section and locating a step in the rear of the center of gravity of a flying boat.

97. 发明授权

US10458341B2 Turboshaft engine for an aircraft equipped with an automatically-activated centraliser 有权
公开(公告)号：US10458341B2
公开(公告)日：2019-10-29
申请号：US15568742
申请日：2016-04-26
申请人： SAFRAN HELICOPTER ENGINES
发明人： Olivier Lafargue , Sébastien Brotier
IPC分类号： F02C7/36 , B64C27/12 , B64C35/02 , F02C3/10 , F01D15/12 , F16H57/02 , B64D35/02
摘要： A turboshaft engine includes a casing in which is arranged a gas generator and a free turbine fitted to a power shaft. The power shaft is configured to be mechanically connected to/disconnected from a reduction gearbox.The turboshaft engine includes at least one centralizer movable between an active position, in which the centralizer forms a bearing for the power shaft and which corresponds to a mechanical disconnection between the power shaft and the reduction gearbox, and a passive position, in which the centralizer is distanced from the power shaft and which corresponds to a mechanical connection between the power shaft the reduction gearbox.

98. 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。

99. 发明授权

US6098927A Multi-purpose aircraft 失效
标题翻译：多功能飞机
公开(公告)号：US6098927A
公开(公告)日：2000-08-08
申请号：US195920
申请日：1998-11-19
申请人： David E. Gevers
发明人： David E. Gevers
IPC分类号： B64C1/00 , B64C3/38 , B64C3/54 , B64C3/56 , B64C25/52 , B64C25/54 , B64C25/66 , B64C35/00 , B64C35/02 , B64D27/00 , B64D27/02 , B64D27/08 , B64D29/04 , B64D35/04 , B64C3/00
CPC分类号： B64D35/04 , B64C1/00 , B64C25/52 , B64C25/54 , B64C25/66 , B64C3/38 , B64C3/54 , B64C3/56 , B64C35/00 , B64C35/002 , B64C35/008 , B64D27/00 , B64D27/08 , B64D29/04 , B64C2001/0045 , Y02T50/12 , Y02T50/145 , Y02T50/44
摘要： Several innovative systems for an aircraft, and aircraft incorporating them, are disclosed. Features include inboard-mounted engine(s) with a belt drive system for turning wing-situated propellers; compound landing gear integrating ski, pontoon and wheel subcomponents; pivotal mounting armatures for landing gear and/or propellers which provide a plurality of possible landing gear and/or propeller configurations; and a compound wing structure featuring extendable wing panels that permit the wing span of the aircraft to be nearly doubled while in flight. Aircraft incorporating such features will enjoy several safety advantages over conventional multi-engine aircraft and will be capable of modifications during flight which permit landings on any of snow, hard surfaces (runways) and water.
摘要翻译：披露了一些飞机的创新系统，以及包含它们的飞机。特征包括内置式发动机，带有用于转动翼位螺旋桨的皮带传动系统; 复合起落架整合滑雪，浮桥和车轮子部件; 用于起落架和/或螺旋桨的枢转安装衔铁，其提供多个可能的起落架和/或螺旋桨结构; 以及具有可延伸翼板的复合翼结构，其允许飞行器的机翼跨度在飞行中几乎翻倍。结合这种特征的飞机将比传统的多引擎飞机享有几个安全优势，并且能够在飞行期间进行修改，这些飞行器允许在雪，硬表面（跑道）和水中的任一个上着陆。

100. 发明授权

US6042052A Retractable step fairing for amphibian airplane 失效
标题翻译：两栖飞机伸缩步进整流罩
公开(公告)号：US6042052A
公开(公告)日：2000-03-28
申请号：US160140
申请日：1998-09-25
申请人： Donald E. Smith
发明人： Donald E. Smith
IPC分类号： B64C35/00 , B64C35/02
CPC分类号： B64C35/007
摘要： The invention comprises an improved seaplane having a retractable step. The term retractable step, however, is a misnomer. The step portion of the seaplane float includes a panel which may be extended once the plane is airborne to reduce aerodynamic drag created by such hydrodynamic steps. The panel may be hinged at a rear portion of the aircraft and extended and retracted using a hydraulic strut or the like. Side panels may also be provided which would hinge via a piano type hinge or the like to the sides of the extendable panel. The side panels may be provided with an end pin or pins which would travel in a track within the step cavity such that the side panels would be pushed into position as the step cover panel is extended. The apparatus of the present invention may be employed in both conventional and tunnel type hulls.
摘要翻译：本发明包括具有可缩回步骤的改进的水上飞机。然而，术语可伸缩的步骤是一个误会。水上飞机浮体的台阶部分包括一旦平面空气传播就可延伸的面板，以减少由这种流体力学步骤产生的气动阻力。面板可以铰接在飞机的后部，并使用液压支柱等延伸和缩回。还可以提供侧板，其可以经由钢琴型铰链等铰链到可延伸面板的侧面。侧板可以设置有将在台阶腔内的轨道中行进的端部销或销，使得当台阶盖板延伸时侧板将被推入到位。本发明的装置可以用于常规的和隧道式的船体。

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