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1. 发明申请

US20030106959A1 Air vehicle 失效
标题翻译：空中车辆
公开(公告)号：US20030106959A1
公开(公告)日：2003-06-12
申请号：US10303757
申请日：2002-11-25
申请人： New Scientific R&D Institute Inc.
发明人： Koki Fukuyama
IPC分类号： B64C015/12 , B64C029/00
CPC分类号： B64C29/0033 , B64C27/20
摘要： Disclosed is an air vehicle (Z) comprising a vehicle body (1); hollow fan ducts (3A-3D) supported to and elongating through the vehicle body at least at its foreside and rear-side locations, respectively. Each fan duct communicates with air at top and bottom of the vehicle body and has a fan (9A-9D) at a top opening (6). The air vehicle further comprises rotary engines (11) each installed inside of each fan duct to rotate the fan. In a preferred embodiment, a cylinder (13) of the rotary engine is mounted to a supporting housing (25) of the fan duct via elastic means (29) which may be fitted to a boss structure (26) of the supporting housing. Each fan duct is tiltable to any directions. Preferably, the fan ducts comprise a pair of front fan ducts (3A, 3B) and another pair of rear fan ducts (3C, 3D) supported to the rear-side of the vehicle body, and the rotary engines in diagonally located fan ducts (3A and 3D; 3B and 3C) are driven to rotate in the same direction.
摘要翻译：公开了一种包括车体（1）的飞行器（Z）中空风扇管道（3A-3D）分别至少在其前侧和后侧位置处支撑并延伸穿过车体。每个风扇管道与车体的顶部和底部的空气连通，并且在顶部开口（6）处具有风扇（9A-9D）。该空中飞行器还包括旋转发动机（11），每个旋转发动机都安装在每个风扇通道内部以使风扇旋转。在优选实施例中，旋转发动机的气缸（13）通过可装配到支撑壳体的凸台结构（26）的弹性装置（29）安装到风扇导管的支撑壳体（25）上。每个风扇导管可向任何方向倾斜。优选地，风扇管道包括一对前风扇导管（3A，3B）和另一对支撑在车身后侧的后风扇导管（3C，3D）和旋转发动机在对角定位的风扇导管 3A和3D; 3B和3C）被驱动以沿相同的方向旋转。

2. 发明申请

US20020153449A1 Flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel 审中-公开
标题翻译：飞行盘形飞行/太空车辆采用新技术推动通过滚动滚轮
公开(公告)号：US20020153449A1
公开(公告)日：2002-10-24
申请号：US10089908
申请日：2002-04-05
发明人： Nikolaos C Hatzistelios
IPC分类号： B64C015/00 , B64C029/00
CPC分类号： F03H99/00 , B64C39/00 , B64C39/001
摘要： This invention called airwheel, concerns of a flying disk shaped flying/space vehicle with the use of a new technic of thrust through the rolling of a wheel. If we exercise a force from a fixed point on the edge of a turning wheel (fixed related to the main body of the vehicle) and the direction of the force is opposite to the direction of the linear speed of the edge, then we will simulate the friction force between the turning wheel of a car and the road which forces the rolling of the car wheel and not just the revolving of it. The airwheel uses to roll (fly) a wheel named in the invention rolling wheel (b) and it embraces the main body (a) of the airwheel as well as an other wheel (Angular Momentum Maintenance Wheel (c)) which turns the other way around to maintain the angular momentum. The airwheel uses nozzles (k) to manoeuvre. Airwheel ingests atmospheric air to fly and avoids/standsup against air pockets using gas saved in a cylindric tank in it which diverts gas under great pressure to the nozzles. For the interplanetary flight airwheel uses the magnetic fields of the magnetosphere, magnetotail and the magnetic fields of solar wind. It comprises T-shaped telescopic devices which on the upper side of the nullTnull contain couples of superconductor bobbins.
摘要翻译：本发明称为风轮，利用通过车轮的滚动推动的新技术的飞盘形飞行/空间车辆的问题。如果我们从转向轮边缘固定点（与车身主体相关的固定点）行使力，并且力的方向与边缘线速度的方向相反，那么我们将模拟汽车的转向轮与迫使车轮滚动的道路之间的摩擦力，而不仅仅是它的旋转。风轮用于滚动（飞行）本发明滚动轮（b）中命名的车轮，并且其包围风轮的主体（a）以及另一个转动另一个的轮（角动量维护轮（c）））方式保持角动量。风轮使用喷嘴（k）进行操纵。空气轮吸入大气空气，避免/等待气袋，使用保存在其中的圆筒形储罐中的气体，其将气体在极高的压力下转移到喷嘴。对于行星际飞行，飞轮使用磁层，磁尾和太阳风磁场的磁场。它包括T形伸缩装置，它在“T”的上侧包含一对超导线轴。

3. 发明申请

US20040065772A1 High-lift, low-drag, stall-resistant airfoil 失效
标题翻译：高升力，低阻力，失速翼型
公开(公告)号：US20040065772A1
公开(公告)日：2004-04-08
申请号：US10370740
申请日：2003-02-21
发明人： Frank S. Malvestuto JR.
IPC分类号： B64C015/02 , B64C029/00
CPC分类号： B64C23/08 , B64C21/04 , B64C29/0025 , Y02T50/166
摘要： Method and apparatus embodiments of the present invention are disclosed wherein wing-rotor configurations provide aerodynamically high lift-low drag capabilities and improvements over the prior art including increasing effective stall angles. In addition, wing-rotor-propeller configurations provide aerodynamically high lift-low drag and forward thrust capabilities and improvements over the prior art for all vehicles moving through gaseous fluids and particular including application for air vehicles and watercraft. Also, wing leading edge air blowing systems augment the example configurations for enhanced performance including substantially vertical take-off and landing of air vehicles.
摘要翻译：公开了本发明的方法和装置实施例，其中翼 - 转子构造提供了空气动力学上的高提升 - 低牵引能力和相对于现有技术的改进，包括增加有效的失速角度。此外，机翼转子 - 螺旋桨配置提供了空气动力学上的高升降低阻力和向前推力能力，并且改进了现有技术对于所有移动通过气态流体的车辆，特别是包括用于空中车辆和船舶的应用。此外，机翼前缘吹风系统增加了用于增强性能的示例配置，包括基本垂直起飞和降落的空中客车。

4. 发明申请

US20040011923A1 Efficient wings 审中-公开
标题翻译：高效的翅膀
公开(公告)号：US20040011923A1
公开(公告)日：2004-01-22
申请号：US10156205
申请日：2002-07-22
发明人： John Daniel Romo
IPC分类号： B64C015/02 , B64C029/00
CPC分类号： B64C11/001 , B64C3/00 , B64C21/00 , B64C29/0025 , Y02T50/166
摘要： To obtain an augmented lift coefficient for a given airfoil set at a maximum angle of attack (null), in a steady state airflow system, a shrouded motorized propeller is installed normal to its upper side, creating additional airflow. An outlet for the additional airflow is provided including a horizontal motorized propeller placed at the trailing edge of the airfoil. The motorized propeller converts the additional air flow into a down-wash generating additional lift. Neither the first nor the second installation alone will produce the augmented lift efficiently. Therefore, the combination of the first and the second installation is needed. The propeller-wing arrangement is implement in the airfoils.
摘要翻译：为了获得在最大迎角（α）下的给定翼型组的增强升力系数，在稳态气流系统中，被覆盖的电动螺旋桨安装在其上侧，产生额外的气流。提供了用于附加气流的出口，包括放置在翼型的后缘处的水平电动螺旋桨。电动螺旋桨将额外的空气流转换成下洗生成附加升降机。单独的第一和第二安装不能有效地产生增强升力。因此，需要第一和第二安装的组合。螺旋桨翼结构在机翼中实现。

5. 发明申请

US20030062442A1 VTOL personal aircraft 审中-公开
标题翻译： VTOL个人飞机
公开(公告)号：US20030062442A1
公开(公告)日：2003-04-03
申请号：US09968934
申请日：2001-10-02
发明人： Karl F. Milde JR.
IPC分类号： B64C015/02 , B64C029/00
CPC分类号： B64C27/20 , B64C3/56 , B64C29/0025 , Y02T50/14
摘要： A personal aircraft (PAC) capable of vertical take-off and landing (VTOL) comprises a passenger compartment having a front, a rear and two sides, and a plurality of independently powered thrusters attached to the outer periphery of the compartment. At least three thrusters are disposed on each side of the compartment. The thrusters, which are preferably ducted fan units, are capable of providing a vertically upward force to the compartment.
摘要翻译：能够垂直起飞和着陆（VTOL）的个人飞机（PAC）包括具有前，后和两侧的乘客舱，以及附接到隔室的外周的多个独立动力的推进器。至少三个推进器设置在隔室的每一侧。推进器（其优选地是风扇式风扇单元）能够向隔室提供垂直向上的力。

6. 发明申请

US20020104921A1 Electrical remote-control and remote-power flying saucer 审中-公开
标题翻译：电动遥控和遥控功率飞碟
公开(公告)号：US20020104921A1
公开(公告)日：2002-08-08
申请号：US10048091
申请日：2001-12-17
发明人： Philippe Louvel
IPC分类号： B64C015/00 , B64C029/00
CPC分类号： A63H27/12 , A63H27/002 , A63H27/04 , A63H30/02
摘要： The purpose of the invention is a light aircraft, remotely supplied and remotely controlled, propelled by electrical motors coupled to propellers, this device being able to perform stationary flight and to move in the three space dimensions in a controlled way. The system includes an aircraft (1), a control unit (3) and a handling unit (4). The aircraft comprises four propellers, each of them driven by a electric motor, a gyroscopic device, tilt sensors, a yaw sensor and an extrenal protective body. The invention also describes the method for the fliht closed loop control. The main purpose of this invention is to provide a enjoyable and educative toy, mainly intended for indoor flight. In a variant of the invention, the aircraft is fitted with a miniaturized video camera, in order to perform remote inspections on buildings or elements difficult to access.
摘要翻译：本发明的目的是远程供应和远程控制的轻型飞机，由耦合到螺旋桨的电动机驱动，该装置能够以受控的方式执行固定飞行并在三个空间维度中移动。该系统包括飞机（1），控制单元（3）和操纵单元（4）。飞机包括四个螺旋桨，每个螺旋桨由电动机驱动，陀螺装置，倾斜传感器，偏航传感器和外围保护体。本发明还描述了用于快速闭环控制的方法。本发明的主要目的是提供一种愉悦和有教育意义的玩具，主要用于室内飞行。在本发明的变型中，飞行器配备有小型化的摄像机，以便对难以进入的建筑物或元件执行远程检查。

7. 发明申请

US20040104303A1 VSTOL VEHICLE 审中-公开
标题翻译： VSTOL车辆
公开(公告)号：US20040104303A1
公开(公告)日：2004-06-03
申请号：US10012135
申请日：2001-11-29
发明人： Youbin Mao
IPC分类号： B64C029/00
CPC分类号： B64C37/00 , B64C29/0025
摘要： A VSTOL vehicle including a fuselage with two pairs of ducted rotors fully enclosed fore and aft of the fuselage respectively. The fuselage is aerodynamically shaped to generate lift in forward flight. All four ducts are configured such that their center axes are substantially parallel to each other, and at an angle tilted sufficiently forward from the vertical axis of the fuselage. Each ducted rotor is powered by one engine inside the duct behind the rotor. All four rotors and engine shafts rotates counterclockwise, generating substantial angular momentum to stabilize the vehicle through the gyroscopic effect. Variable-shape inlets of the ducted rotors and vector thrusting of the airflow out of the ducted rotors combine to provide efficient power and control during all phases of flight. The vehicle is configured to meet motor vehicle requirements to drive on streets.
摘要翻译：一款VSTOL车型，包括机身两侧分别完全封闭在机身前后的两对导管转子。机身是空气动力学形状的，用于在前进飞行中产生电梯。所有四个管道被构造成使得它们的中心轴线基本上彼此平行，并且以从机身的垂直轴线向前倾斜的角度。每个导管转子由转子后面的管道内的一个发动机供电。所有四个转子和发动机轴逆时针旋转，产生大的角动量，以通过陀螺效应来稳定车辆。导管转子的可变形入口和从导管转子传出的气流的向量推力相结合，在飞行的所有阶段提供有效的功率和控制。车辆配置为满足机动车辆要求在街道上行驶。

8. 发明申请

US20030150954A1 CONTROL SYSTEM FOR VERTICAL TAKE OFF AND LAND (VTOL) AIRCRAFT 有权
标题翻译：垂直起落架（VTOL）飞机控制系统
公开(公告)号：US20030150954A1
公开(公告)日：2003-08-14
申请号：US10074710
申请日：2002-02-13
发明人： Anthony A. duPont
IPC分类号： B64C029/00
CPC分类号： F02K1/00 , B64C15/02 , B64C29/0066 , B64D33/04 , F02K1/002 , F02K3/025
摘要： A vertical take off and land (VTOL) jet aircraft may have a jet engine mounted in a forward portion of the aircraft. A thrust deflection assembly may be provided rearward of the jet engine, and include a cascade and control box for deflecting thrust during vertical flight of the aircraft. By manipulating the cascade and control box, the roll, yaw and pitch of the aircraft during vertical flight may be controlled. In addition, ailerons, a rudder and elevators may be provided for controlling roll, yaw and pitch during forward flight. A pilot control input apparatus is also provided, which receives pilot input regarding desired roll, yaw and pitch of the aircraft. The pilot control input is operatively associated with a control mixer, which controls the control box, ailerons, rudder and elevators in accordance with the desired roll, yaw and pitch of the aircraft. As a result, the pilot uses the same control input apparatus for vertical and forward flight.
摘要翻译：垂直起飞和陆地（VTOL）喷气式飞机可能有一架喷气发动机安装在飞机的前部。推力偏转组件可以设置在喷气发动机的后方，并且包括用于在飞行器的垂直飞行期间偏转推力的级联和控制箱。通过操纵级联和控制箱，可以控制垂直飞行期间飞行器的滚动，偏航和俯仰。此外，可以提供副翼，方向舵和电梯，用于在前进飞行期间控制滚动，偏航和俯仰。还提供了一种先导控制输入装置，其接收关于飞行器的期望的滚动，偏航和俯仰的导频输入。飞行员控制输入可操作地与控制混合器相关联，控制混合器根据飞行器的期望的滚动，偏航和俯仰来控制控制箱，副翼，方向舵和电梯。因此，飞行员使用相同的控制输入装置进行垂直和前进飞行。

9. 发明申请

US20030085319A1 VTOL personal aircraft 失效
标题翻译： VTOL个人飞机
公开(公告)号：US20030085319A1
公开(公告)日：2003-05-08
申请号：US10242036
申请日：2002-09-11
发明人： Joseph Wagner , Anthony Pruszenski JR. , Karl F. Milde JR.
IPC分类号： B64C015/02 , B64C029/00
CPC分类号： B64C3/56 , B64C27/20 , B64C29/0025 , Y02T50/14
摘要： A personal aircraft (PAC) capable of vertical take-off and landing (VTOL) comprises a fixed wing and a fuselage with a passenger compartment having a front, a rear and two sides, and a plurality of independently powered thrusters, preferably integrated into the wing, on each side of the fuselage. The aircraft has a lift to drag ratio equal to or greater than 2. The thrusters, which are ducted fan units capable of providing a vertically upward force to the aircraft, are provided with such redundancy that the aircraft can hover with at one thruster inoperative on each side of the fuselage. At least one thruster on each side of the fuselage preferably comprises a nulllevitatornull which creates lift from the airfoil-like air inlet as well as from the acceleration of air from inlet to outlet.
摘要翻译：能够垂直起飞和着陆（VTOL）的个人飞机（PAC）包括一个固定翼和一个具有前，后和两侧的乘客舱的机身，以及多个独立动力的推进器，最好集成到机翼，在机身的每一侧。飞机具有等于或大于2的提升阻力比。作为能够向飞行器提供垂直向上的力的导风扇单元的推进器具有这样的冗余度，即飞行器可以在一个推进器上无法操作机身的每一边。机体每一侧至少有一个推进器最好包括一个“升降机”，它从翼型空气入口以及空气从入口到出口的加速度产生升力。

10. 发明申请

US20020109043A1 Flight vehicle having internal lift surfaces 审中-公开
标题翻译：具有内部升降面的飞行器
公开(公告)号：US20020109043A1
公开(公告)日：2002-08-15
申请号：US09781094
申请日：2001-02-12
发明人： Tianfu Li
IPC分类号： B64C015/00 , B64C029/00
CPC分类号： B64C39/001 , B64C27/06
摘要： A vehicle capable of roadway travel and flight, both in an atmosphere and in a vacuum, includes a fluid passageway, a device for producing fluid flow in the passageway, and airfoil surfaces spaced mutually along the passageway and fixed to the structure of the vehicle, to which structure lift forces produced on the airfoils are transferred. The vehicle includes lift-producing wings extending from the body of the vehicle, the fluid passageway being located within the vehicle body or the external wings. Fluid flow within the passageway is produced by a fan, propeller, or exhaust from a jet engine.
摘要翻译：能够在气氛和真空中行驶和行驶的车辆包括流体通道，用于在通道中产生流体流动的装置以及沿通道相互间隔开并固定到车辆结构的翼面，在翼型上产生的结构升力被转移到其上。车辆包括从车身延伸的升降机翼，流体通道位于车体或外翼内。通道内的流体流由风扇，螺旋桨或来自喷气发动机的排气产生。

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