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公开(公告)号：US20030183719A1
公开(公告)日：2003-10-02
申请号：US10112144
申请日：2002-04-01
发明人： Paul Bevilaqua , Patrick Tait
IPC分类号： B64C037/02 , B64D005/00
CPC分类号： B64D5/00
摘要： The invention is a system for ferrying at least one aircraft by a ferrying aircraft, the at least one aircraft and ferrying aircraft having vehicle management systems. In detail, the invention includes an attachment device for joining a wing tip of the at least one aircraft to one of the wing tips of the ferrying aircraft. A system is included for controlling the at least one aircraft and the ferrying aircraft such that the at least one aircraft flight characteristics are controlled by the ferrying aircraft. The method of ferrying a at least one aircraft by a ferrying aircraft from a first point to a second point includes the steps of: flying the at least one aircraft and ferrying aircraft; while in flight at the first point, joining a wing tip of the at least one aircraft to one of the wing tips of ferrying aircraft; and controlling the flight characteristics of the joined at least one aircraft such that the at least one aircraft and ferrying aircraft become a single aircraft controlled by the ferrying aircraft as the jointed aircraft fly toward the second point.
摘要翻译： 本发明是一种用于由渡轮飞行器运送至少一架飞机的系统，所述至少一架飞机和渡轮具有车辆管理系统。 详细地，本发明包括用于将至少一个飞行器的翼尖连接到渡轮飞行器的翼尖之一的附接装置。 包括用于控制至少一架飞机和飞机的系统，使得至少一架飞机飞行特性由渡轮飞机控制。 由渡轮运送至少一架飞机从第一点到第二点的方法包括以下步骤：飞行至少一架飞机和飞机; 在第一点飞行中，将至少一架飞机的翼尖连接到飞机的翼尖之一; 以及控制所连接的至少一架飞机的飞行特性，使得当联合飞机朝向第二点飞行时，至少一架飞机和渡轮飞机成为由渡轮飞机控制的单一飞机。
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公开(公告)号：US20030201362A1
公开(公告)日：2003-10-30
申请号：US10131930
申请日：2002-04-25
发明人： Fushun Yang
IPC分类号： B64C037/02 , B64D005/00
摘要： This invention provides another basic important means of transportation after motor vehicle, airplane, helicopter: helicarplane. Helicarplane can run on ground roads, take off and land in fixed-wing style or in helicopter style; can fly quickly and economically in fixed-wing airplane style. Agility, adaptability, convenience, and timesaving are helicarplane's advantages. Helicarplane enlarges the active room for human beings with significant effect of economy and society.
摘要翻译： 本发明提供了机动车，飞机，直升机：直升机之后的另一个基本重要的交通工具。 Helicarplane可以在地面道路上行驶，以固定翼风格或直升机风格起飞和降落; 可以在固定翼飞机上快速而经济地飞行。 飞机的灵活性，适应性，便利性和时间性都是螺旋桨的优点。 Helicarplane扩大了人类的活跃空间，具有显着的经济和社会效应。
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公开(公告)号：US20030080241A1
公开(公告)日：2003-05-01
申请号：US10256249
申请日：2002-09-26
IPC分类号： B64C037/02 , B64D005/00
摘要： An aircraft carrier adapted to carry and release a carried store for air launch purposes. The aircraft carrier includes a carrying station coupled to a part of the aircraft carrier and being a priori adapted to carry a load other than the carried store to be launched. The carried store to be launched is mountable to a coupling device that is mountable to the carrying station. The aircraft carrier also includes a control system capable of communicating with the coupling device for selectively releasing the carried store.
摘要翻译： 适用于携带和释放携带的商店用于空中发射目的的航空母舰。 航空母舰包括一个连接到航空母舰的一部分的承载站，并且先前适用于携带除了要启动的被携带商店以外的载荷。 要发射的携带商店可安装到可安装到承载站的联接装置。 航空母舰还包括能够与联接装置通信的控制系统，用于选择性地释放所携带的商店。
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公开(公告)号：US20040108411A1
公开(公告)日：2004-06-10
申请号：US10453777
申请日：2003-06-03
发明人： Henry August
IPC分类号： B64D005/00 , B64C037/02
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/046 , B64C2201/104 , B64C2201/121 , F42B10/16 , F42B10/62 , F42B12/58 , F42B12/62 , F42B15/00
摘要： A reusable, mach-velocity mobile platform delivers a weapons payload via vertical launch, powerless glide, weapons release, and landing operation phases. The platform includes a generally tubular shaped body having an aft and forward end, and a payload section. An arch wing is supported by the body aft end. The arch wing has an upper and a lower wing joined at distal ends by two curved end plates. A nose assembly is connected at the forward end having an upward directed fixed angle-of-attack to generate forward end lift. Thermal tiles attached under the body and the lower wing under-side radiate/dissipate heat generated during a high angle-of-attack platform reentry. Radar absorptive or radar translucent material is used. The platform preferably discharges payload from the aft end for safe separation. A landing gear is extended for the landing phase of operation.
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公开(公告)号：US20040094658A1
公开(公告)日：2004-05-20
申请号：US10615525
申请日：2003-07-07
发明人： William Dale Pas-Key
IPC分类号： B64C037/02 , B64D005/00
摘要： This machine is a mutated creature of all or most technology to produce either a platform that can be bolted to an existing power supply; as well as could be a complete unit that produces the same result of the ability to fly, hover, &/or drive. This solves many problems by offering an alternative; many parking lots already have helicopter pad(s) so being able to fly in & then hover to a parking spot is an asset. Then if you only add the ability to drive on existing streets/highways; you get the most universal transportation available. Later calculating in the factor that you can convert your existing motorcycle or ATV that is in your garage, into this highly sophisticated futuristic flying machine keeps cost down for a smooth transition is the nullPas-Keynull to the future. Imagine driving out bound on the freeway & at the fly zone limit, you flip a switch and fly right off the pavement.
摘要翻译： 该机器是所有或大多数技术的突变生物，用于生产可以螺栓连接到现有电源的平台; 以及可能是一个完整的单位，产生飞行，悬停和/或驱动能力的相同结果。 这通过提供一个替代方案来解决许多问题; 许多停车场已经有直升机垫，所以能够飞行，然后徘徊在停车位是一种资产。 那么如果你只是增加在现有的街道/高速公路上开车的能力; 你得到最普遍的交通工具。 以后，您可以将您现有的摩托车或ATV在您的车库中转换成这个高度复杂的未来派飞行器，以保持平稳过渡的成本是“Pas-Key”。 想象一下，在高速公路和飞越区域限制下，您可以翻转开关，并从路面上飞走。
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公开(公告)号：US20020092949A1
公开(公告)日：2002-07-18
申请号：US09761076
申请日：2001-01-17
发明人： Leland M. Nicolai
IPC分类号： B64C037/02 , B64D005/00 , B64C035/00
CPC分类号： B64C35/005 , B60V1/08 , B64C39/024 , B64C2201/048 , B64C2201/086 , B64C2201/088 , B64C2201/102 , B64C2201/104 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/162 , B64C2201/167 , B64C2201/187
摘要： An anti-submarine warfare system includes an unmanned nullsea-sittingnull aircraft housing submarine detecting equipment, the aircraft including a body portion having a catamaran configuration adapted for stably supporting the body portion when sitting in water, the body portion including a fuselage and laterally disposed sponsons connected to the fuselage via platforms, and submarine detecting equipment housed within the fuselage and adapted to be electronically linked to sonobuoys disposed in adjacent water locations.
摘要翻译： 一种反潜战系统包括一个无人“海坐”飞机舱潜艇检测设备，该飞机包括一个主体部分，该主体部分具有适于在坐在水中时稳定地支撑主体部分的双体船结构，该主体部分包括机身和横向 通过平台连接到机身的安装支架，以及容纳在机身内的潜艇检测设备，并且适于与设置在相邻水位的声波电子电子连接。
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公开(公告)号：US20030094536A1
公开(公告)日：2003-05-22
申请号：US10281344
申请日：2002-10-25
发明人： Mitchell G. LaBiche
IPC分类号： B64C037/02 , B64D005/00
摘要： A flyable automobile comprising a right main wing connected to the flyable automobile and comprising a right wing inner portion and a right wing outer portion, the right wing outer portion hingedly connected to the right wing inner portion so that the right wing outer portion can be folded above the right wing inner portion, and the right main wing connected to the flyable automobile so that the right main wing can pivot into a storage compartment underneath in the flyable automobile, and a left main wing connected to the flyable automobile and having a left wing inner portion and an left wing outer portion, the left wing outer portion hingedly connected to the left wing inner portion so that the left wing outer portion can be folded above the left wing inner portion, the left main wing connected to the flyable automobile so that the left main wing can pivot into the storage compartment in the flyable automobile.
摘要翻译： 一种可飞行的汽车，包括连接到可飞行汽车的右主翼，包括右翼内部和右翼外部，右翼外部铰接地连接到右翼内部，使得右翼外部可以折叠 右翼内部的右侧主翼和连接到可飞行汽车的右主翼，使得右主翼可以枢转到可飞行汽车中的下方的储藏室中，以及连接到可飞行汽车的左主翼，并具有左翼 内侧部分和左翼外部部分，左翼外部部分铰接地连接到左翼内部部分，使得左翼外部部分可以在左翼内部部分上方折叠，左主机翼连接到可飞行汽车，使得 左主翼可以枢转到可飞行汽车的储藏室。
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公开(公告)号：US20020139894A1
公开(公告)日：2002-10-03
申请号：US10057194
申请日：2002-01-25
发明人： Bradford T. Sorensen
IPC分类号： B64C037/02 , B64D005/00
CPC分类号： B60V1/08 , B64C37/00 , B64C39/066
摘要： An improved VTOL aircraft or flying car mechanism that utilizes counter-rotating blades (18) spinning inside a duct (14) causing varying speeds and volumes of atmosphere to pass across an exposed plurality of wing shaped lift generating airfoils, referred to as sucked flaps (36), at an opening in that duct (70). The volumes of atmosphere will then pass through to a lift amplifying, turbulence reducing, radial, spiral airflow generator (68) and then into thrust vector airfoils (26), which will then pass through the duct (70) again as it forms a circular path (72) back to the sucked flaps (36), where it is then re-circulated. The air pressure flowing over the top of the airfoils is reduced relative to the air pressure below the airfoils causing relatively large amounts of lift to be generated to overcome the force of gravity. Because the entire wing surface area necessary to lift the flying car or aircraft can now fit within the confines of the length, width, and height of a standard freeway-capable motor VTOL aircraft or flying car, there is no need for foldable wings, foldable control surfaces, exposed rotors, exterior wind blasts or other problems associated with prior art helicopters, flying cars, or other VTOL aircraft.
摘要翻译： 改进的垂直起伏飞行器或飞行车机构，其利用在管道（14）内部旋转的反向旋转叶片（18），使得变化的速度和体积的气氛穿过暴露的多个翼形升力产生翼型件（称为吸襟翼 36），在该导管（70）的开口处。 然后，大气量将通过升降机放大，减少湍流，径向，螺旋形气流发生器（68），然后进入推力矢量翼型件26，然后它将再次通过导管（70），因为它形成圆形 路径（72）回到吸襟翼（36），然后再次循环。 流过翼型件顶部的空气压力相对于翼型下面的空气压力减小，导致产生相对较大量的升力以克服重力。 因为提升飞行车或飞机所需的整个机翼表面区域现在可以适应标准高速公路电动机垂直起降飞机或飞行器的长度，宽度和高度的限制，所以不需要可折叠的机翼，可折叠 控制表面，暴露的转子，外部风吹或与现有技术直升机，飞行车或其他垂直起降飞机相关的其他问题。
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公开(公告)号：US20020104919A1
公开(公告)日：2002-08-08
申请号：US09820528
申请日：2001-03-30
发明人： Nick Geranio , Robert K. McBride
IPC分类号： B64C037/02 , B64D005/00 , B64C005/00 , B64C007/00
CPC分类号： B64C27/20 , B64C29/0025
摘要： A flying vehicle having a pair of counter rotating propeller blades which provide lift for the vehicle when the vehicle is in a flight mode of operation. The counter rotating blades have in flight adjustable pitch and are connected to a control and steering system in the cockpit of the vehicle. A gas turbine engine located in the aft section of the vehicle is connected through a drive shaft and transmission to the counter rotating propeller blades When the vehicle transitions to the flight mode, the user has aircraft controls available in the cockpit to make the transitions from a driver to a pilot in a short time period. Yaw pedals located on the floor board of the cockpit as well as a pitch control handle and the steering wheel allow the user to steer and control the altitude of the vehicle when the vehicle is in the flight mode.
摘要翻译： 一种具有一对反转螺旋桨叶片的飞行器，当车辆处于飞行操作模式时，该飞行器为车辆提供升降机。 反向旋转叶片具有飞行中的可调节节距并且连接到车辆驾驶舱中的控制和转向系统。 位于车辆后部的燃气涡轮发动机通过驱动轴和变速器连接到反向旋转螺旋桨叶片当车辆转换到飞行模式时，用户具有驾驶舱中可用的飞行器控制器，以从 在短时间内驾驶飞行员。 位于驾驶舱地板上的偏航踏板以及俯仰控制手柄和方向盘允许用户在车辆处于飞行模式时转向和控制车辆的高度。
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公开(公告)号：US20040108410A1
公开(公告)日：2004-06-10
申请号：US10309828
申请日：2002-12-04
发明人： Henry August
IPC分类号： B64C037/02 , B64D005/00
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/046 , B64C2201/104 , B64C2201/121 , F42B10/16 , F42B10/62 , F42B12/58 , F42B12/62 , F42B15/00
摘要： A reusable, mach-velocity mobile platform delivers a weapons payload via vertical launch, powerless glide, weapons release, and landing operation phases. The platform includes a generally tubular shaped body having an aft and forward end, and a payload section. An arch wing is supported by the body aft end. The arch wing has an upper and a lower wing joined at distal ends by two curved end plates. A nose assembly is connected at the forward end having an upward directed fixed angle-of-attack to generate forward end lift. Thermal tiles attached under the body and the lower wing under-side radiate/dissipate heat generated during a high angle-of-attack platform reentry. Radar absorptive or radar translucent material is used. The platform preferably discharges payload from the aft end for safe separation. A landing gear is extended for the landing phase of operation.
摘要翻译： 可重复使用的马赫速度移动平台通过垂直发射，无力滑翔，武器释放和着陆操作阶段提供武器有效载荷。 平台包括具有尾部和前端的大致管状的主体和有效载荷部分。 一个弓翼由身体后端支撑。 拱翼具有通过两个弯曲端板在远端连接的上翼和下翼。 前端组件在前端连接，具有向上定向的固定迎角，以产生前端提升。 安装在车体下方的散热瓦片和下部翼片下侧辐射/消散在高角度攻角平台折返期间产生的热量。 使用雷达吸收或雷达半透明材料。 该平台优选地从尾端排出有效载荷以进行安全分离。 起落架延伸到着陆阶段。
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