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公开(公告)号：EP1924494A4
公开(公告)日：2010-08-25
申请号：EP06748262
申请日：2006-02-27
申请人： MOLNARI INC
发明人： MOLNAR DEZSO , CALFEE CRAIG , GARAMSZEGI ZOLTAN
CPC分类号： B64C35/001 , B62K13/00 , B64C27/02 , B64C35/008 , B64C37/00
摘要： A vehicle that can operate as either a motorcycle or an autogiro, said vehicle having a flight mode and a motorcycle mode, said vehicle comprising: a frame having a front part and a rear part; a center-line that passes from the front of said vehicle to the rear of said vehicle through the center of said vehicle such that said vehicle's weight is distributed nearly equally to either side of said center-line; a propeller mounted to a propeller barrel that is rotatably mounted to said frame such that the junction where said frame's front part meets said frame's rear part is located within said propeller barrel; an engine mounted to the rear part of said frame, wherein said engine powers said propeller in said flight mode; a cockpit fixedly mounted to the front part of said frame, said cockpit comprising means for controlling said vehicle; at least one aircraft lift means comprising: at least one rotor that is rotatably mounted to said frame when said vehicle is in said flight mode; a front wheel steerably and rotatably mounted to the front part of said frame along the said vehicle's center-line; and a rear wheel that is rotatably mounted to the rear part of said frame along said vehicle's center-line and is powered by said engine in said motorcycle mode.
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公开(公告)号：EP1478570A4
公开(公告)日：2008-04-09
申请号：EP03709001
申请日：2003-02-06
申请人： MOLLER INT INC
发明人： MOLLER PAUL S
IPC分类号： B64C3/56 , B64C11/00 , B64C11/48 , B64C13/50 , B64C29/00 , B64C37/00 , B64D27/06 , B64D31/06
CPC分类号： B64C37/00 , B64C3/56 , B64C11/001 , B64C11/48 , B64C13/503 , B64C29/0033 , B64D27/06 , B64D31/06 , Y02T50/145
摘要： A VTOL vehicle including a fuselage with two foldable wings, two tiltable nacelles attached to the wings, a vertical stabilizer, a horizontal stabilizer, and two auxiliary thrusters. Each nacelle contains a system of vanes located at the rear opening thereof, and actuators are provided for extending and retracting the vanes in conjunction with nacelle tilting mechanisms to deflect the airflow over a predetermined range of angles from the horizontal. Each nacelle also contains two rotary engines, each of which directly drives a fan. The fans face each other and operate in counter-rotating directions at the same rotational speed. An alternative embodiment includes two additional nacelles attached to the fuselage instead of having the auxiliary thrusters. A redundant computerized flight control system maintains stability of the vehicle as it transitions from one flight mode to another.
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33.发明授权
公开(公告)号：EP1541465B1
公开(公告)日：2007-07-18
申请号：EP03028070.5
申请日：2003-12-09
申请人： Hegger, Christof
发明人： Hegger, Christof
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34.发明公开AUTOCOPTER, LAND MOTOR VEHICLE WHICH CAN BE CONVERTED INTO AN AIRMOBILE 有权IN EIN LUFTMOBIL UMWANDELBARES AUTOCOPTER-LANDMOTORFAHRZEUG
公开(公告)号：EP1512625A1
公开(公告)日：2005-03-09
申请号：EP02732764.2
申请日：2002-05-16
摘要： The invention relates to an autocopter or a half-motor vehicle which can be converted into a half-helicopter. The invention comprises: (Fig. 1) common endless screw transmission systems for a rotor, an ultralight, supercharged thermal engine or two independent engines with the same characteristics (10, 11), a fully articulated rotor (16) and a mixed clutch system comprising a centrifugal, mechanical and friction system (5, 6); (Fig. 2) two-engine option with a secondary drive shaft for the front wheel train (12), the rotor drive shaft (18) being provided with a system for connecting sections thereof to a casing tube (2); (Fig. 8) system of launching cables for folding, unfolding and stiffening the central electronic blades and small cylinder-type cable launchers (10, 20, 5, 6); (Fig. 9) a height reduction system for slide block assembly (2, 10) and runners for sliding (3, 4); and (Fig. 10) a system of contracting and stretching tails using fingers (A 1 , A 2 , B 1 , B 2 ).
摘要翻译： 本发明涉及可以转换成半直升机的自动直升机或半自动车辆。 本发明包括：（图1）用于转子，超小型，增压热引擎或具有相同特性的两个独立发动机（10,11），全关节转子（16）和混合离合器系统的共同环形螺旋传动系统 包括离心机械和摩擦系统（5,6）; （图2），具有用于前轮系（12）的辅助驱动轴的双发选项，转子驱动轴（18）设置有用于将其部分连接到套管（2）的系统; （图8）系统，用于折叠，展开和加固中央电子叶片和小型筒状电缆发射器（10,20,5,6）的电缆; （图9）用于滑块组件（2,10）的高度减小系统和用于滑动（3,4）的滑块; 和（图10）使用手指（A1，A2，B1，B2）收缩和拉伸尾巴的系统。
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35.发明公开
公开(公告)号：EP0839712A3
公开(公告)日：2000-05-24
申请号：EP97830546.4
申请日：1997-10-27
摘要： Aircraft with changeable geometry, height, weight (and also changeable carriage wheels' distance) on the ground or during flight, furnished with one or more engines mounted in the same frame and convertible into a trailer for motor vehicles. These characteristics are obtained thanks to: mechanical units mounted on the fuselage that allow fixed movements to some portions of the fuselage; adjustable front carriage's leg (4001), which can change its inclination, its length and its shape; carriage's rear portion (5000) formed by two half wings, whose roots are connected to the fuselage and their longitudinal ends to the wheels; engine casing (6001) of many shapes and sizes where various kinds of engines can be placed; fuselage's plate (6003) on which the engine casing can be placed in different positions; beams (7001 and 7004) that can be introduced in the fuselage to change the aircraft into a trailer for motor vehicles or into other types of aircrafts.
摘要翻译： 飞机在地面或飞行期间具有可变的几何形状，高度，重量（以及可更换的车轮距离），配有安装在同一车架上的一台或多台发动机，并可转换为机动车辆的拖车。 这些特性得益于：安装在机身上的机械单元，可以固定机身的某些部分; 可调节的前车厢腿（4001），可以改变其倾斜度，长度和形状; 由两个半翼形成的滑架后部（5000），其根部连接到机身并且其纵向端连接到车轮; 可放置各种发动机的多种形状和尺寸的发动机壳体（6001） 机身板（6003），其上可以放置发动机壳体的不同位置; 可以在机身中引入的横梁（7001和7004）将飞机改变为机动车辆的拖车或其他类型的飞机。
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36.发明公开Aircraft convertible into other aircrafts and into a trailer for motor vehicles 失效Luftfahrzeug，verwandelbar in andere Luftfahrzeuge und inAnhängerfürKraftfahrzeuge
公开(公告)号：EP0839712A2
公开(公告)日：1998-05-06
申请号：EP97830546.4
申请日：1997-10-27
IPC分类号： B64C37/00
CPC分类号： B64C37/00
摘要： Aircraft with changeable geometry, height, weight (and also changeable carriage wheels' distance) on the ground or during flight, furnished with one or more engines mounted in the same frame and convertible into a trailer for motor vehicles. These characteristics are obtained thanks to: mechanical units mounted on the fuselage that allow fixed movements to some portions of the fuselage; adjustable front carriage's leg (4001), which can change its inclination, its length and its shape; carriage's rear portion (5000) formed by two half wings, whose roots are connected to the fuselage and their longitudinal ends to the wheels; engine casing (6001) of many shapes and sizes where various kinds of engines can be placed; fuselage's plate (6003) on which the engine casing can be placed in different positions; beams (7001 and 7004) that can be introduced in the fuselage to change the aircraft into a trailer for motor vehicles or into other types of aircrafts.
摘要翻译： 在地面或飞行中具有可变几何形状，高度，重量（以及可更换的车轮距离）的飞机，配备一个或多个安装在同一框架中的发动机，并可转换成用于机动车辆的拖车。 这些特性得益于：安装在机身上的机械单元允许固定运动到机身的某些部分; 可调节的前支架脚（4001），可改变其倾斜度，长度和形状; 滑架后部（5000）由两个半翼形成，其根部连接到机身并且其纵向端部连接到车轮; 发动机壳体（6001），其各种形状和尺寸可放置各种发动机; 发动机壳体可以放置在不同位置的机身板（6003） 梁（7001和7004）可以引入机身，将飞机改装成用于机动车辆或其他类型飞机的拖车。
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38.发明公开
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公开(公告)号：EP4067123A1
公开(公告)日：2022-10-05
申请号：EP20893730.0
申请日：2020-11-25
发明人： HAN, Kyung Hee
IPC分类号： B60F5/02 , B64C39/02 , B64C37/00 , B64C25/36 , B64C25/62 , B64D27/24 , B64D17/80 , B60B19/02 , B60G15/06
摘要： The present invention relates to a self-powered drone flying car for land and air, in which a circular riding spherical body (110) that is a commercial space in which a person rides to fly, steer, and control the flying car is formed, a drone wing device (230) that is a flying device is mounted onto the riding spherical body, and a ground driving device for driving on the ground is mounted to a lower portion of the riding spherical body, in order to perform both flying in the air and driving on the ground. Also, an intermediate connection attaching and detaching device (210) is formed between the devices to separate and connect the devices depending on whether the flying device or the ground driving device is necessary.
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