公开(公告)号：US07278607B2

公开(公告)日：2007-10-09

申请号：US11202722

申请日：2005-08-12

Applicant: Howard J. Fuller

Inventor： Howard J. Fuller

IPC: B64B1/06

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.

公开(公告)号：US20070187547A1

公开(公告)日：2007-08-16

申请号：US11557378

申请日：2006-11-07

Applicant: Patrick Kelly

Inventor： Patrick Kelly

IPC: B64C27/22

CPC classification number: B64B1/20 ,  B64B1/30 ,  B64B2201/00 ,  B64G1/005

Abstract: Lifting “ferries” having rotatable wings with propeller engines can lift airplanes vertically, during takeoffs, in a quieter and safer manner with reduced fuel consumption and carbon dioxide emissions. Four rotatable wings are used, to provide balanced lifting force, and to prevent downdraft or propwash from blowing directly against the wings of an airplane being lifted. An optional buoyant aircraft such as a zeppelin can also be used to provide lifting force. Such buoyant aircraft should have adjustable internal struts, to convert it into a streamlined shape for moderate-speed flight and descent. Alternately, a zeppelin can be provided directly with four large rotatable propeller engines, to create a single-unit buoyant lifting ferry.

Abstract translation: 用螺旋桨发动机提升具有旋转翼的“渡口”可以在降低燃油消耗和二氧化碳排放的同时，以更安静和安全的方式在起飞期间垂直升降飞机。 使用四个可旋转的翼，以提供平衡的提升力，并且防止向下移动或推动剂直接吹向被提升的飞机的机翼。 一种可选的浮力飞机，如飞刀，也可以用来提供提升力。 这种浮力飞机应具有可调节的内部支柱，将其转换成流线型的中速飞行和下降形状。 或者，可以直接用四个大的可旋转螺旋桨发动机提供飞艇，以制造单一单元浮力提升渡轮。

公开(公告)号：US07137592B2

公开(公告)日：2006-11-21

申请号：US10853300

申请日：2004-05-24

Applicant: Edward Barocela ,  Patrick F. Cassidy

Inventor： Edward Barocela ,  Patrick F. Cassidy

IPC: B64B1/06 ,  B64C1/00

CPC classification number: B64B1/24 ,  B64B1/06 ,  B64B2201/00 ,  B64D2211/00 ,  Y02T50/55 ,  Y10S244/90

Abstract: In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system can have a high-aspect ratio wing shape. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The high-aspect ratio wing shape provides low drag, and can allow the hybrid airship to fly at an altitude of at least about 100,000 ft. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft for months or even years. The hybrid airship may function as a military intelligence, surveillance, and reconnaissance and communications relay platform.

Abstract translation: 一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有高纵横比的翼形。 在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。 在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。 高纵横比翼形提供了低阻力，并且可以允许混合飞艇在至少约100,000英尺的高度飞行。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以保持高空数月 甚至几年。 混合型飞艇可以作为军事情报，监视，侦察和通信中继平台。

公开(公告)号：US07108228B1

公开(公告)日：2006-09-19

申请号：US11049150

申请日：2005-02-02

Applicant: Manfred Marshall

Inventor： Manfred Marshall

IPC: B64C1/00

CPC classification number: B64G1/002 ,  B64B2201/00 ,  B64C39/001 ,  B64G1/401 ,  B64G1/443

Abstract: A spacecraft having facilities for carrying astronauts and payloads into the earth satellite orbit and space having a composite fiber body with a Kevlar exterior skin. Said craft having a substantially round shape with a portion covered with solar cells. Said solar cells powering electrical motors and a plurality of rockets using a quantity of hydrogen fuel.

Abstract translation: 具有将宇航员和有效载荷载入地球卫星轨道和空间的设备的航天器具有具有凯夫拉外部皮肤的复合纤维体。 所述工艺具有基本圆形形状，其中一部分被太阳能电池覆盖。 所述太阳能电池为使用一定数量的氢燃料的电动机和多个火箭提供动力。

公开(公告)号：US20050269441A1

公开(公告)日：2005-12-08

申请号：US10853300

申请日：2004-05-24

Applicant: Edward Barocela ,  Patrick Cassidy

Inventor： Edward Barocela ,  Patrick Cassidy

IPC: B64B1/06 ,  B64B1/24 ,  B64D27/24 ,  B64B1/00

CPC classification number: B64B1/24 ,  B64B1/06 ,  B64B2201/00 ,  B64D2211/00 ,  Y02T50/55 ,  Y10S244/90

Abstract: In one aspect, a hybrid airship including an outer shell, a plurality of helium filled gas envelopes, and an all-electric propulsion system can have a high-aspect ratio wing shape. In some embodiments, the hybrid airship may be launched using buoyancy lift alone and aerodynamic lift may be provided by the all-electric propulsion system. In one aspect, a photovoltaic array and a high energy density power storage system may be combined to power the propulsion system making the propulsion system regenerative. The high-aspect ratio wing shape provides low drag, and can allow the hybrid airship to fly at an altitude of at least about 100,000 ft. By continuously recharging the power storage system, the hybrid airship in accordance with some embodiments can stay aloft for months or even years. The hybrid airship may function as a military intelligence, surveillance, and reconnaissance and communications relay platform.

Abstract translation: 一方面，包括外壳，多个氦气填充的气体包络和全电动推进系统的混合式飞艇可以具有高纵横比的翼形。 在一些实施例中，混合式飞艇可以单独使用浮力提升机来启动，而空气动力提升可由全电动推进系统提供。 在一个方面，光伏阵列和高能量密度功率存储系统可以组合起来，为推进系统提供动力，使推进系统再生。 高纵横比翼形提供了低阻力，并且可以允许混合飞艇在至少约100,000英尺的高度飞行。通过不断地对蓄电系统充电，根据一些实施例的混合式飞艇可以保持高空数月 甚至几年。 混合型飞艇可以作为军事情报，监视，侦察和通信中继平台。

公开(公告)号：US06848647B2

公开(公告)日：2005-02-01

申请号：US10287046

申请日：2002-11-04

Applicant: H. Victoria Albrecht

Inventor： H. Victoria Albrecht

IPC: B64B1/20 ,  B64C1/00 ,  B64C37/02

CPC classification number: B64B1/20 ,  B64B2201/00 ,  B64C1/00 ,  B64C2001/0045

Abstract: A method wherein a vehicle is capable of movement on or over land, and/or on, over, or under water. Various body, wing, tail, and/or outrigger shapes facilitate movement and develop lift. Buoyancy or semi-buoyancy is developed utilizing various chambers to contain controlled volumes of gaseous or liquid substances. Motion is augmented by propulsion or repulsion mechanisms, including pressurized liquid stream jet (PJET) propulsion. The vehicle is capable of modifying its shape and/or the curvature of various parts, such as wings, tails, and/or outriggers, by manipulating the internal skeleton, the internal compartments supporting the external surfaces, and/or the internal pressure of the shape. Control Agents with mechanized or manual support manage the vehicle's operations controlling various movement particular information, as well as baseline algorithms, such as wind speed, currents, and location.

Abstract translation: 一种方法，其中车辆能够在陆地上或陆地上，和/或在水面上或水下移动。 各种身体，翼，尾和/或支腿形状有助于运动和发展升力。 利用各种室来开发浮力或半浮力以容纳受控体积的气态或液态物质。 运动通过推进或排斥机制增加，包括加压液体流喷射（PJET）推进。 车辆能够通过操纵内部骨架，支撑外表面的内部隔室和/或内部压力来改变其各种部件的形状和/或曲率，例如翼，尾和/或外伸支架 形状。 具有机械化或手动支持的控制代理管理车辆的操作，控制各种移动特定信息，以及基线算法，例如风速，电流和位置。

公开(公告)号：US20040084565A1

公开(公告)日：2004-05-06

申请号：US10287046

申请日：2002-11-04

Inventor： H. Victoria Albrecht

IPC: B64C001/00 ,  B64B001/20 ,  B64C017/00

CPC classification number: B64B1/20 ,  B64B2201/00 ,  B64C1/00 ,  B64C2001/0045

Abstract: A method wherein a vehicle is capable of movement on or over land, and/or on, over, or under water. Various body, wing, tail, and/or outrigger shapes facilitate movement and develop lift. Buoyancy or semi-buoyancy is developed utilizing various chambers to contain controlled volumes of gaseous or liquid substances. Motion is augmented by propulsion or repulsion mechanisms, including pressurized liquid stream jet (PJET) propulsion. The vehicle is capable of modifying its shape and/or the curvature of various parts, such as wings, tails, and/or outriggers, by manipulating the internal skeleton, the internal compartments supporting the external surfaces, and/or the internal pressure of the shape. Control Agents with mechanized or manual support manage the vehicle's operations controlling various movement particular information, as well as baseline algorithms, such as wind speed, currents, and location.

Abstract translation: 一种方法，其中车辆能够在陆地上或陆地上，和/或在水面上或水下移动。 各种身体，翼，尾和/或支腿形状有助于运动和发展升力。 利用各种室来开发浮力或半浮力以容纳受控体积的气态或液态物质。 运动通过推进或排斥机制增加，包括加压液体流喷射（PJET）推进。 车辆能够通过操纵内部骨架，支撑外表面的内部隔室和/或内部压力来改变其各种部件的形状和/或曲率，例如翼，尾和/或外伸支架 形状。 具有机械化或手动支持的控制代理管理车辆的操作，控制各种移动特定信息，以及基线算法，例如风速，电流和位置。

公开(公告)号：US06659403B2

公开(公告)日：2003-12-09

申请号：US10200456

申请日：2002-07-23

Applicant: Chih-Yu Hsia

Inventor： Chih-Yu Hsia

IPC: B64C330

CPC classification number: B64C3/30 ,  B64B2201/00 ,  B64C31/028 ,  B64C31/04 ,  Y10S244/903

Abstract: An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.

公开(公告)号：US20030127566A1

公开(公告)日：2003-07-10

申请号：US10200348

申请日：2002-07-23

Inventor： Chih-Yu Hsia

IPC: B64G001/62

CPC classification number: B64C3/30 ,  B64B2201/00 ,  Y10S244/903

Abstract: An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.

公开(公告)号：US06398160B1

公开(公告)日：2002-06-04

申请号：US09617765

申请日：2000-07-17

Applicant: Chih-Yu Hsia

Inventor： Chih-Yu Hsia

IPC: B64C330

CPC classification number: B64C3/30 ,  B64B2201/00 ,  B64C31/028 ,  B64C31/04 ,  Y10S244/903

Abstract: An aeronautical apparatus, the combination comprising a primary airfoil having at least one panel which is an upper panel, a lower panel, and multiple gas containing tubes associated with the airfoil and extending lengthwise thereof, the tubes including relatively larger cross-section tubes positioned chordwise of the airfoil, and relatively smaller cross-section positioners located to stabilize the relatively larger cross-section tubes.

Abstract translation: 一种航空装置，该组合包括具有至少一个面板的主要翼型件，其具有上板，下板和与翼型件相关的并且纵向延伸的多个气体，所述管包括相对较大的横截面管， 并且相对较小的横截面定位器被定位成稳定相对较大的横截面管。