公开(公告)号：US20100096493A1

公开(公告)日：2010-04-22

申请号：US12507592

申请日：2009-07-22

Applicant: Boris V. KHAKIMOV ,  Alexandr N. CHERNIKOV ,  German V. DEMIDOV ,  Rustem Z. KHAMITOV

Inventor： Boris V. KHAKIMOV ,  Alexandr N. CHERNIKOV ,  German V. DEMIDOV ,  Rustem Z. KHAMITOV

IPC: B64B1/00

CPC classification number: A62C29/00 ,  A62B5/00 ,  B64B1/20 ,  B64B1/36 ,  B64B2201/00

Abstract: The invention relates to lighter-than-air vehicles. The inventive aircraft comprises a rigid body with carrier gas-containing shells and propulsers arranged inside aerodynamic modules which are embodied in the form of aerodynamically shaped toroidal bodies of revolution. A longitudinal through passage in embodied in the lower part of the body in such a way that it communicates a crew cabin, a cargo-and-passenger compartment, fuel tanks and accessories and is provided with exit hatches and devices for docking to external objects, an extensible stairway with fences and a demountable carriage. The aircraft also comprises a transversal passage with overwing exits and a vertical passage provided with a cable hoist and devices for lowering and lifting people and cargo. The lower part of the body and hollow wings are filled with a foamed plastic which is used for providing the aircraft with floatability and strength. The aim of the invention is to extend the list of technical means.

Abstract translation: 本发明涉及轻型轻型车辆。 本发明的飞行器包括具有载气容纳壳体的刚体和布置在空气动力学模块内部的推进器，其以空气动力学形式的环形旋转体形式体现。 身体的下部具有纵向通过通道，以使其与乘员舱，货物和乘客舱，燃料箱和附件通信，并且设置有用于对接到外部物体的出口舱口和装置， 带有围栏的可扩展楼梯和可拆卸的车厢。 该飞机还包括一个具有俯仰出口的横向通道和一个设有缆索起重机的垂直通道和用于降低和提升人员和货物的装置。 身体的下部和空心翼充满泡沫塑料，用于为飞机提供浮动性和强度。 本发明的目的是扩大技术手段的清单。

公开(公告)号：US20090200416A1

公开(公告)日：2009-08-13

申请号：US12068667

申请日：2008-02-08

Applicant: Yee-Chun Lee

Inventor： Yee-Chun Lee

IPC: B64B1/02

CPC classification number: B64B1/30 ,  B64B1/32 ,  B64B2201/00 ,  B64C23/00 ,  B64C2230/04 ,  Y02T50/166

Abstract: Systems, method, devices and apparatus are provided for reducing drag and increasing the flight efficiency characteristics of aircraft and airships including hybrid aircraft utilizing distributed boundary layer control and propulsion means. Boundary layer control includes passive systems such as riblet films and boundary layer propulsion means includes a divided and distributed propulsion system disposed in the curved aft sections of aircraft and airships including hybrid aircraft susceptible to boundary layer drag due to degree of curvatures, speed and density of the surrounding air. Distributed propulsion propulsion means includes constructing propellers and riblets from shape memory alloys, piezoelectric materials and electroactive polymer (EAP) materials to change the shape and length of the distributed propulsion means.

Abstract translation: 提供了系统，方法，装置和装置，用于减少使用分布式边界层控制和推进装置的飞机和飞艇（包括混合动力飞机）的飞行效率特性。 边界层控制包括被动系统，例如肋状膜，边界层推进装置包括分布和分布的推进系统，其设置在飞机和飞艇的弯曲后部，包括由于曲率程度，速度和密度而易受边界层拖动的混合飞机 周围的空气。 分布式推进推进装置包括从形状记忆合金，压电材料和电活性聚合物（EAP）材料构建螺旋桨和肋，以改变分布式推进装置的形状和长度。

公开(公告)号：US20090108135A1

公开(公告)日：2009-04-30

申请号：US12157600

申请日：2008-06-11

Applicant: Donald Orval Shaw

Inventor： Donald Orval Shaw

IPC: B64G1/00 ,  B64B1/02

CPC classification number: B64C3/30 ,  B64B2201/00 ,  B64C31/036 ,  B64D27/24 ,  B64G2001/1071 ,  Y02T50/62

Abstract: The invention is an aircraft having an inflatable wing connected to a base unit, with the inflatable wing inflated with a lifting gas such as helium. The inflatable wing has a series of cell structures, and may be configured with ballonets to selectively introduce and expel outside air within the inflatable wing to vary the buoyancy and/or airfoil properties of the inflatable wing. The aircraft is particularly useful at low speeds and in thin atmospheres (such as at high Earth altitudes and on Mars), and can be used for interplanetary missions to explore planetary bodies, such as moons and planets, having atmospheres.

Abstract translation: 本发明是一种具有连接到基座单元的可充气翼的飞行器，充气翼用诸如氦气的提升气体充气。 充气翼具有一系列的细胞结构，并且可以配置有气球，以选择性地引入和排出可充气翼内的外部空气，以改变可充气翼的浮力和/或翼型性质。 该飞机在低速和薄弱的气氛（如高地球高度和火星上）特别有用，可用于行星际飞行任务，以探索具有气氛的行星体，如卫星和行星。

公开(公告)号：US20090108126A1

公开(公告)日：2009-04-30

申请号：US11922506

申请日：2005-07-07

Applicant: Alfredo Capuani

Inventor： Alfredo Capuani

IPC: B64B1/02

CPC classification number: B64C31/032 ,  B64B1/02 ,  B64B2201/00

Abstract: The aircraft (10) comprises an elongated framework (26) provided with propelling means and direction-control planes. The framework is coupled to a pneumatic chamber (16) suited to be filled with lighter-than-air gas and comprising two tubular branches (12, 14) joined to form a V-shaped profile, with an aerodinamic-lift surface (22, 24) extending therebetween.

Abstract translation: 飞行器（10）包括设置有推进装置和方向控制平面的细长框架（26）。 该框架联接到适于填充轻于空气气体的气动室（16），并且包括两个连接以形成V形轮廓的管状分支（12,14），其具有气动提升表面（22， 24）。

公开(公告)号：US20070114326A1

公开(公告)日：2007-05-24

申请号：US11561392

申请日：2006-11-18

Applicant: Francis Gentile

Inventor： Francis Gentile

IPC: B64B1/06

CPC classification number: B64C39/06 ,  B64B2201/00

Abstract: Integration of structure and aerodynamic shape results in a Damage Resistant Unmanned Aircraft, Capable of surviving ground handling and impacts with plants, wires, solid objects and water. The structure dismantles for transport and storage into a small space, that is resistant to damage. The aerodynamic arrangement has a improved ability to fly controllably in the gusty environment that causes difficulty for small light weight aircraft. A method of mounting pneumatic and fabric shapes onto a Damage Resistant Aircraft with parts facilitating a round structure. Use of the pneumatic shapes to adjust the length and stiffness of the post. The post produces tension on the structure that It presses against. Inflatable post ends and an attachment system. Multi piece removable wing tips which allow deflation, access and small folding volume of the inflatable structure. All tension rudders are formed inside the net structure where it is protected from damage.

Abstract translation: 结构和空气动力学形状的结合形成了一种耐损伤的无人驾驶飞机，能够幸存地面处理和对植物，电线，固体物体和水的冲击。 结构拆除运输和储存在一个小空间，这是耐损坏。 空气动力学装置具有改善的能力，可控制地在气候环境中飞行，这导致小重型飞机的困难。 将气动和织物形状安装在耐损伤飞机上，方便圆形结构的部件的方法。 使用气动形状来调节柱的长度和刚度。 该柱在其压紧的结构上产生张力。 充气后端和附件系统。 多片可移动的翼尖，其可充气结构的放气，通道和小折叠体积。 所有张力舵都形成在网状结构内，防止受到损坏。

公开(公告)号：US20070034741A1

公开(公告)日：2007-02-15

申请号：US11202722

申请日：2005-08-12

Applicant: Howard Fuller

Inventor： Howard Fuller

IPC: B64D41/00 ,  B64B1/24

CPC classification number: B64B1/14 ,  B64B2201/00 ,  B64D27/24 ,  B64D2041/005 ,  B64D2211/00 ,  Y02T50/55 ,  Y02T50/62 ,  Y02T90/36

Abstract: A solar-powered aircraft uses solar energy to electrolyze on-board water to produce hydrogen. The hydrogen fills various on-board tanks, causing the aircraft to become lighter than air. The hydrogen is also used to operate a fuel cell which provides power for electrical equipment, including a motor for turning a propeller. Water produced as waste by the fuel cell is recycled for use in the production of hydrogen. When hydrogen is removed from the tanks, either because it is consumed by the fuel cell or because it is compressed and pumped out of the tanks, air returns to the tanks, and the aircraft becomes heavier than air. The aircraft can thus be made to climb and descend by making it lighter than air, or heavier than air. The aircraft emits no harmful substances into the environment. The aircraft can remain aloft indefinitely, limited only by an insignificant amount of leakage of hydrogen and water.

Abstract translation: 太阳能飞机使用太阳能来电化船上水以产生氢气。 氢气填充各种车载坦克，使飞机变得比空气轻。 氢还用于操作为电气设备提供动力的燃料电池，包括用于转动螺旋桨的电动机。 由燃料电池作为废物生产的水被再循环用于生产氢气。 当从罐中取出氢气时，由于燃料电池被消耗或被压缩并从罐中抽出，所以空气返回到罐中，飞机变得比空气重。 因此，飞机可以通过使其比空气轻，或比空气重，使其爬升和下降。 飞机在环境中不会产生有害物质。 飞机可以无限期地保持高空，仅受到氢和水的泄漏量的微不足道的限制。

公开(公告)号：US06880783B2

公开(公告)日：2005-04-19

申请号：US10175237

申请日：2002-06-18

Applicant: Jeffery Roger Munk

Inventor： Jeffery Roger Munk

IPC: B60V3/08 ,  B64B1/00 ,  B64C1/00 ,  B64B1/20

CPC classification number: B60V3/08 ,  B64B1/005 ,  B64B2201/00

Abstract: A hybrid air vehicle having a gas-filled contoured flattened hull including a pair of longitudinally extending side lobes defining, on the underside of the hull, a longitudinally extending central recess, a payload module received in the central recess and air cushion landing gear units on the underside of the side lobes of the hull. The landing gear units are spaced apart on either side of the payload module. The hybrid air vehicle has characteristics of an airplane, a lighter-than-air airship and a hovercraft.

Abstract translation: 一种混合动力车辆，其具有气体填充的轮廓平坦的船体，包括一对纵向延伸的侧翼，其在船体的下侧上限定纵向延伸的中心凹部，容纳在中央凹部中的有效载荷模块和气垫起落架单元 船体旁瓣的下侧。 起落架单元在有效载荷模块的任一侧间隔开。 混合动力车辆具有飞机，轻型空中飞艇和气垫船的特征。

公开(公告)号：US20030001044A1

公开(公告)日：2003-01-02

申请号：US10175237

申请日：2002-06-18

Inventor： Jeffery Roger Munk

IPC: B64B001/00

CPC classification number: B60V3/08 ,  B64B1/005 ,  B64B2201/00

Abstract: A hybrid air vehicle having a gas-filled contoured flattened hull including a pair of longitudinally extending side lobes defining, on the underside of the hull, a longitudinally extending central recess, a payload module received in the central recess and air cushion landing gear units on the underside of said side lobes of the hull. The landing gear units are spaced apart on either side of the payload module. The hybrid air vehicle has characteristics of an airplane, a lighter-than-air airship and a hovercraft.

Abstract translation: 一种混合动力车辆，其具有气体填充的轮廓平坦的船体，包括一对纵向延伸的侧翼，其在船体的下侧上限定纵向延伸的中心凹部，容纳在中央凹部中的有效载荷模块和气垫起落架单元 船体旁瓣的下侧。 起落架单元在有效载荷模块的任一侧间隔开。 混合动力车辆具有飞机，轻型空中飞艇和气垫船的特征。

公开(公告)号：US4606515A

公开(公告)日：1986-08-19

申请号：US614819

申请日：1984-05-29

Applicant: John J. Hickey

Inventor： John J. Hickey

IPC: B64B1/26 ,  B64B1/36

CPC classification number: B64B1/26 ,  B64B1/36 ,  B64B2201/00

Abstract: A hybrid annular airship of the kind including an annulus containing at least one gas containing portion is disclosed which is characterized by improved maneuverability, stability and speed. This improvement is effected by combined means comprising a pair of tubes mounted diametrically within the annulus and normal one to the other. A plurality of doors are provided for selectively closing off one or the other of the pair of tubes. Each tube is provided with a propulsion unit, having an access port, and preferably reversibly mounted therein. The tubes either are mounted on the same level or at different levels. Preferably, the propulsion units are jet engines which are individually operable. An elevator and a walkway preferably are provided communicating with each of the access ports leading to the propulsion units. Preferably, each access port has its own opening and closing mechanism.

Abstract translation: 公开了一种包括包含至少一个气体容纳部分的环空的混合环形飞艇，其特征在于改进的机动性，稳定性和速度。 这种改进通过组合装置来实现，所述组合装置包括一对直径安装在环形空间内并且彼此正常安装的管。 提供多个门以选择性地关闭该对管中的一个或另一个。 每个管设置有具有进入端口的推进单元，并且优选地可逆地安装在其中。 管或者安装在相同的水平或不同的水平上。 优选地，推进单元是单独可操作的喷气发动机。 优选地提供与通向推进单元的每个进入端口通信的电梯和走道。 优选地，每个进入端口具有其自己的打开和关闭机构。

公开(公告)号：US4365772A

公开(公告)日：1982-12-28

申请号：US331414

申请日：1981-12-16

Applicant: Frederick D. Ferguson

Inventor： Frederick D. Ferguson

IPC: B64B1/00 ,  B64B1/56 ,  B64B1/66

CPC classification number: B64B1/00 ,  B64B2201/00

Abstract: An aircraft is provided utilizing a spherical balloon filled with buoyant gas such as helium at a pressure substantially greater than atmospheric so that its dimensions are substantially unaffected by changes in atmospheric pressure or temperature. The aircraft may take the form of a self-propelled and self-contained airship, or may be merely a passive device for providing lift and intended to be towed by and controlled from a helicopter. The spherical balloon is mounted on a normally horizontal axle having end portions projecting from opposite sides of the balloon, and includes a rigid load supporting yoke including two arms extending upwardly from a central load supporting structure and each with an upper end suspended from the axle.

Abstract translation: 使用充满浮力气体（例如氦气）的球形气囊，其压力基本上大于大气压，使其尺寸基本上不受大气压力或温度变化的影响。 飞机可以采取自行式和独立式飞艇的形式，或者可以仅仅是用于提供升降机的被动装置，并且意图被直升机牵引和控制。 球形球囊安装在正常水平的轴上，其具有从球囊的相对侧突出的端部，并且包括刚性负载支撑轭，其包括从中心负载支撑结构向上延伸的两个臂，并且每个具有悬挂在车轴上的上端。