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1. 发明公开

US20230150654A1 Novel jet-propelled lift-increasing and stability-increasing amphibious aircraft and application method thereof 审中-公开
公开(公告)号：US20230150654A1
公开(公告)日：2023-05-18
申请号：US17624358
申请日：2021-01-12
申请人： Sun Yat-sen University
发明人： Rui DENG , Fugiang LUO , Tiecheng WU , Pengnan SUN , Wanzhen LUO , Zezhen ZHANG , Siyuan CHEN
IPC分类号： B64C15/14 , B64D45/00 , B64C35/00 , G05D1/08
CPC分类号： B64C15/14 , B64C35/008 , B64D45/00 , G05D1/0816
摘要： Disclosed is a novel jet-propelled lift-increasing and stability-increasing amphibious aircraft and an application method thereof. An air intake fan connects and communicates with an air intake end of a pressurized air storage tank, an air outlet end of the pressurized air storage tank connects and communicates with a shunting pipeline, the shunting pipeline respectively connects and communicates with a plurality of air chambers, each connection of the plurality of air chambers and the shunting pipeline is provided with an adjusting valve, and the plurality of air chambers are distributed in a plurality of positions of the bottom of the aircraft, and are configured to jet air outwards. A navigation state sensing device is configured to detect navigation data of the aircraft and send the navigation data to an intelligent analysis device. The intelligent analysis device is configured to analyze the navigation data, obtain a control scheme and send to a jet control device. The jet control device controls open and closed states of the adjusting valves according to the control scheme to adjust a jet state of the plurality of air chambers. By adjusting the jet quantity of each position of the bottom of the aircraft from various positions, the aircraft is assisted to stably fly. The problems in the prior art are practically solved.

2. 发明授权

US09908613B2 Propulsion system for aircraft, in particular lightweight aircraft 有权
公开(公告)号：US09908613B2
公开(公告)日：2018-03-06
申请号：US14428654
申请日：2013-09-09
申请人： INNOVATIVE DRAGON LTD.
发明人： Herwig Fischer , Hanno Fischer
IPC分类号： B64C11/00 , B64C1/06 , B64C35/00 , B64D27/06 , B64D27/08 , B64D35/04 , B64C1/16 , B64C1/18 , B64C11/46 , B64C39/12 , B64D27/26
CPC分类号： B64C11/001 , B64C1/061 , B64C1/065 , B64C1/16 , B64C1/18 , B64C11/46 , B64C35/00 , B64C35/008 , B64C39/12 , B64D27/06 , B64D27/08 , B64D27/26 , B64D35/04
摘要： A propulsion system for aircraft, in particular lightweight aircraft, provides a low-noise and low-cost aircraft. The propulsion system includes at least two ducted propellers (3, 3′). The ducts of are provided laterally on the fuselage (4) of the aircraft in such a way that the common net thrust of the ducted propellers is substantially collinear to the net drag.

3. 发明授权

US09365088B2 UAV having hermetically sealed modularized compartments and fluid drain ports 有权
标题翻译：无人机具有气密密封的模块化隔间和排水口
公开(公告)号：US09365088B2
公开(公告)日：2016-06-14
申请号：US13730825
申请日：2012-12-28
申请人： AeroVironment, Inc.
发明人： Pavel Belik , Thomas Szarek , Gabriel E. Torres , Vernon P. Fraye
IPC分类号： B60F5/00 , B64C35/00 , B64C39/02
CPC分类号： B64C35/008 , B60F5/00 , B64C25/52 , B64C39/024 , B64C2201/042 , B64D9/00
摘要： In one possible embodiment, an amphibious unmanned aerial vehicle is provided, which includes a fuselage comprised of a buoyant material. Separators within the fuselage form separate compartments within the fuselage. Mounts associated with the compartments for securing waterproof aircraft components within the fuselage. The compartments each have drainage openings in the fuselage extending from the interior of the fuselage to the exterior of the fuselage.
摘要翻译：在一个可能的实施例中，提供了两栖无人飞行器，其包括由浮力材料构成的机身。机身内的分隔器在机身内形成独立的隔间。与机舱相关的安装件用于固定机身内的防水飞机部件。机舱各自在机身内部延伸到机身外部的机身中都有排水口。

4. 发明申请

US20150210380A1 PROPULSION SYSTEM FOR AIRCRAFT, IN PARTICULAR LIGHTWEIGHT AIRCRAFT 有权
标题翻译：特别是轻型飞机的飞机推进系统
公开(公告)号：US20150210380A1
公开(公告)日：2015-07-30
申请号：US14428654
申请日：2013-09-09
申请人： INNOVATIVE DRAGON LTD
发明人： Herwig Fischer , Hanno Fischer
IPC分类号： B64C11/00 , B64C1/06 , B64C35/00 , B64C1/18 , B64C1/16 , B64C11/46 , B64D27/26 , B64C39/12
CPC分类号： B64C11/001 , B64C1/061 , B64C1/065 , B64C1/16 , B64C1/18 , B64C11/46 , B64C35/00 , B64C35/008 , B64C39/12 , B64D27/06 , B64D27/08 , B64D27/26 , B64D35/04
摘要： A propulsion system for aircraft, in particular lightweight aircraft, provides a low-noise and low-cost aircraft. The propulsion system includes at least two ducted propellers (3, 3′). The ducts of are provided laterally on the fuselage (4) of the aircraft in such a way that the common net thrust of the ducted propellers is substantially collinear to the net drag.
摘要翻译：用于飞机，特别是轻型飞机的推进系统提供了低噪音和低成本的飞机。推进系统包括至少两个管道式推进器（3,3'）。导管横向设置在飞行器的机身（4）上，使得管道螺旋桨的共同净推力基本上与净阻力共线。

5. 发明授权

US06866224B2 Seaplane with retractable twin floats 失效
标题翻译：水上飞机与可伸缩双浮标
公开(公告)号：US06866224B2
公开(公告)日：2005-03-15
申请号：US10362436
申请日：2001-08-22
申请人： Alan John Smith , Grenfell Saxon Rudduck
发明人： Alan John Smith , Grenfell Saxon Rudduck
IPC分类号： B64C25/12 , B64C25/16 , B64C25/54 , B64C25/66 , B64C35/00
CPC分类号： B64C25/12 , B64C25/16 , B64C25/54 , B64C25/66 , B64C35/008
摘要： A twin float aircraft (1) which has a retractable float (4 and 5) for each side of a fuselage (3) providing buoyancy for the aircraft during take off and landing and reduced air resistance during flight with each of the floats (4 and 5) being articulated (12 and 13) to assist streamline alignment when retracted.
摘要翻译：一种双浮式飞机（1），其具有用于飞机在起飞和着陆期间的浮力的机身（3）的每侧的可伸缩浮子（4和5），并且在飞行期间降低空气阻力（4和5） 5）被铰接（12和13），以在缩回时辅助流线对齐。

6. 发明授权

US06592073B1 Amphibious aircraft 有权
标题翻译：两栖飞机
公开(公告)号：US06592073B1
公开(公告)日：2003-07-15
申请号：US10083081
申请日：2002-02-26
申请人： John A. Meekins
发明人： John A. Meekins
IPC分类号： B64C3500
CPC分类号： B64C25/54 , B64C11/001 , B64C25/34 , B64C35/00 , B64C35/008 , B64C39/04 , B64C39/066 , Y02T50/66
摘要： General aviation class amphibious aircraft which include two fuselages, each having a hydrodynamic surface, the fuselages connected via a primary flight surface and a ducted power plant located aft and above the fuselages. The power plant location removes the fan/propeller arc from water and spray during water-borne taxiing, takeoff and landing. The combination of fuselages, lifting surface and ducting provides an aerodynamically efficient design with a lower center of gravity and protected powerplant for yielding improved performance including increased range and airspeed, together with favorable maneuverability, stability and control characteristics both aerodynamically and hydrodynamically.
摘要翻译：通用航空级水陆两用飞机包括两个机身，每个机身均具有流体动力学表面，通过主飞行面连接的机身和位于机身后方和机身上方的管道发电厂。发电厂位置在水上滑行，起飞和着陆期间从水中除去风扇/螺旋桨电弧并喷洒。机身，提升表面和管道的组合提供了具有较低重心的空气动力学有效设计和受保护的动力装置，用于产生改善的性能，包括增加的范围和空速，以及空气动力学和流体动力学的有利的机动性，稳定性和控制特性。

7. 发明授权

US3397854A Aircraft of large wing span 失效
标题翻译：大翼跨度飞机
公开(公告)号：US3397854A
公开(公告)日：1968-08-20
申请号：US39570964
申请日：1964-09-11
申请人： WALTER REYLE
发明人： WALTER REYLE
IPC分类号： B64C11/00 , B64C35/00 , B64D27/00 , B64D27/06 , B64D39/00 , B64D45/00
CPC分类号： B64C35/008 , B64C11/00 , B64C11/001 , B64D27/00 , B64D27/06

8. 发明授权

US2383870A Amphibian aircraft 失效
标题翻译：两栖飞机
公开(公告)号：US2383870A
公开(公告)日：1945-08-28
申请号：US44993342
申请日：1942-07-06
申请人： TOWNSEND LUDINGTON CHARLES
发明人： TOWNSEND LUDINGTON CHARLES
IPC分类号： B64C35/00
CPC分类号： B64C35/008

9. 发明授权

US2184260A Linkage system 失效
标题翻译：联动系统
公开(公告)号：US2184260A
公开(公告)日：1939-12-19
申请号：US20216838
申请日：1938-04-15
申请人： FLEETWINGS INC
发明人： SUTTON WILSON L
IPC分类号： B64C25/12 , B64C35/00
CPC分类号： B64C25/12 , B64C35/008

10. 发明授权

US2053093A Amphibian landing gear 失效
公开(公告)号：US2053093A
公开(公告)日：1936-09-01
申请号：US70160533
申请日：1933-12-09
申请人： CURTISS AEROPLANE & MOTOR CO
发明人： LUBURG GUY A
IPC分类号： B64C35/00
CPC分类号： B64C35/008

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