公开(公告)号：US20140158817A1

公开(公告)日：2014-06-12

申请号：US13665379

申请日：2012-10-31

Applicant: TP AEROSPACE, INC.

Inventor： Paul Chambers

IPC: B64B1/08 ,  B64B1/06 ,  B64B1/16

CPC classification number: B64B1/08 ,  B64B1/16 ,  B64B1/22 ,  B64B1/32 ,  B64B2201/00

Abstract: A rigid airship comprising a hull comprising a rigid frame covered by a skin, the rigid frame comprising a plurality of high pressure inflated tubes.

Abstract translation: 一种刚性飞艇，包括一个包括被皮肤覆盖的刚性框架的船体，刚性框架包括多个高压膨胀管。

公开(公告)号：US08622337B2

公开(公告)日：2014-01-07

申请号：US13052748

申请日：2011-03-21

Applicant: Mohammed Hariri

Inventor： Mohammed Hariri

IPC: B64B1/06 ,  B64C1/14 ,  B64C1/24

CPC classification number: B64B1/06 ,  B64B1/22 ,  B64B1/30 ,  B64B2201/00

Abstract: An airship for facilitating transportation to and from one or more locations which are difficult to access or operate such as high above the ground level is disclosed. The airship can also be used in surface missions, The airship includes a cabin and a platform. The cabin is configured on a top portion of the airship. The platform is operatively connected to the cabin. The platform facilitates easy access to the cabin.

Abstract translation: 公开了一种用于便利运送到难以进入或操作的一个或多个位置的飞艇，例如高于地面高度的高度。 飞艇也可以用于地面任务，飞艇包括一个客舱和一个平台。 机舱配置在飞艇的顶部。 平台可操作地连接到机舱。 该平台便于轻松进入客舱。

公开(公告)号：US08596571B2

公开(公告)日：2013-12-03

申请号：US13430010

申请日：2012-03-26

Applicant: John Goelet

Inventor： John Goelet

IPC: B64B1/02

CPC classification number: B64B1/68 ,  B64B1/00 ,  B64B1/06 ,  B64B1/12 ,  B64B1/14 ,  B64B1/20 ,  B64B1/22 ,  B64B1/34 ,  B64B1/58 ,  B64B1/60 ,  B64B2201/00 ,  B64C25/32 ,  B64C25/56 ,  B64D2211/00

Abstract: An airship is provided. The airship includes a hull configured to contain a gas, at least one propulsion assembly coupled to the hull and including a propulsion device, and at least one aerodynamic component including a plurality of fairing structures including one or more slats, wherein the at least one aerodynamic component is associated with the hull and is configured to direct airflow around the airship.

Abstract translation: 提供飞艇。 飞艇包括构造成容纳气体的船体，耦合到船体的至少一个推进组件，并且包括推进装置，以及包括多个整流罩结构（包括一个或多个板条）的至少一个空气动力部件，其中至少一个空气动力学 组件与船体相关联，并且被配置为引导飞艇周围的气流。

公开(公告)号：US20120018571A1

公开(公告)日：2012-01-26

申请号：US13182864

申请日：2011-07-14

Applicant: John Goelet

Inventor： John Goelet

IPC: B64B1/00 ,  B64B1/06

CPC classification number: B64B1/06 ,  B64B1/005 ,  B64B1/08 ,  B64B1/10 ,  B64B1/16 ,  B64B1/20 ,  B64B1/22 ,  B64B1/28 ,  B64B1/30 ,  B64B1/58 ,  B64D9/00

Abstract: A solar-powered airship with a hull configured to contain a gas and at least one propulsion assembly with a propulsion device and electric motors configured to drive the propulsion device. The airship may also include a power supply system including solar panels operatively coupled to the electric motors and configured to supply power to the electric motors. The power supply system may also include batteries operatively coupled to the solar panels and configured to receive and store electrical energy supplied by the solar panels, the batteries being further operatively coupled to the electric motors and configured to supply power to the electric motors. The batteries may each be located within an outer envelope of the airship defined by the hull of the airship in a position selected to provide ballast. The solar-powered airship may also include a cargo system configured to contain passengers or freight.

Abstract translation: 具有构造成容纳气体的船体的太阳能飞艇和具有推进装置的至少一个推进组件和构造成驱动推进装置的电动马达。 飞艇还可以包括电源系统，其包括可操作地耦合到电动机并被配置为向电动机供电的太阳能电池板。 电源系统还可以包括可操作地耦合到太阳能电池板并且被配置为接收和存储由太阳能电池板供应的电能的电池，电池进一步可操作地耦合到电动机并且被配置为向电动机供电。 电池可以各自位于由飞艇的船体在选定为提供镇流器的位置中限定的飞艇的外部封套内。 太阳能飞艇还可以包括配置成容纳乘客或货物的货物系统。

公开(公告)号：US08052082B1

公开(公告)日：2011-11-08

申请号：US11486478

申请日：2006-07-15

Applicant: Edward Charles Herlik

Inventor： Edward Charles Herlik

IPC: B64B1/06

CPC classification number: B64B1/08 ,  B64B1/14 ,  B64B1/22 ,  B64B1/24 ,  B64B1/36 ,  B64B1/58

Abstract: An optimized lighter-than-air vehicle or airship incorporating a frame 104, internal propulsion 124, perforated covering 102 and lifting-gas cells 110 is disclosed. Optimization features include variations on a Stratford Ramp, means to control the boundary layer 210, absence of unnecessary protuberances and means to reduce the bow wave. A transportable version utilizing a flexible frame 310 and keels 314 is also disclosed along with a means for rapid descent and landing. The operating concept reduces velocity requirements which, in turn, reduce weight and size requirements.

Abstract translation: 公开了一种优化的轻型车辆或飞艇，其包括框架104，内部推进件124，穿孔盖102和提升气体单元110。 优化特征包括Stratford斜坡上的变化，控制边界层210的手段，不存在不必要的突起以及减少弓波的手段。 还公开了利用柔性框架310和龙骨314的可移动版本以及用于快速下降和着陆的装置。 操作概念降低了速度要求，从而降低了重量和尺寸要求。

公开(公告)号：US20050279880A1

公开(公告)日：2005-12-22

申请号：US10902136

申请日：2004-07-30

Applicant: Mutsuro Bundo

Inventor： Mutsuro Bundo

IPC: B64B1/02 ,  B64B1/22 ,  B64B1/28 ,  B64B1/34 ,  B64D1/18

CPC classification number: B64B1/22 ,  B64B1/02 ,  B64B1/28 ,  B64B1/34 ,  B64D1/18

Abstract: A multi-purpose airship usable for multi-purposes with less maintenance cost is provided. The multi-purpose airship comprises an operator cabin (1) to which a work device of agricultural chemical scattering device (10) or the like is fittable, a rotor (4) fitted to a top of the operator cabin (1) and having rotor blades of plural stages of which fitting angle is adjustable to generate a lifting force and propulsive force, a balloon (5) detachably fitted to a top of the rotor (4) and filled with gas lighter than air to generate a lifting force, a stabilizing wing (2) elongating horizontally from each side of the operator cabin (1) and a propulsion device (3) comprising a propeller device or jet engine fitted to a distal end of the stabilizing wing (2) to vary a thrust direction between the horizontal direction and the vertical direction.

Abstract translation: 提供可用于多目的，维护成本较低的多用途飞艇。 多用途飞艇包括操作者舱（1），农药分散装置（10）等的工作装置可装配到该操作员舱（1）上，转子（4）安装在操作员舱（1）的顶部并具有转子 多个阶段的叶片可调整以产生提升力和推进力，气囊（5）可拆卸地装配到转子（4）的顶部并且填充有比空气更轻的气体以产生提升力，稳定 翼部（2）从操作员舱（1）的每一侧水平延伸，以及推进装置（3），其包括安装在稳定翼（2）的远端的螺旋桨装置或喷气发动机，以改变水平 方向和垂直方向。

公开(公告)号：US20040019415A1

公开(公告)日：2004-01-29

申请号：US10621977

申请日：2003-07-17

Applicant: NEC Toshiba Space Systems, Ltd.

Inventor： Toshinori Hotta ,  Wakoto Akinaga

IPC: G05D003/00

CPC classification number: H01Q3/08 ,  B64B1/00 ,  B64B1/22 ,  H01Q1/18 ,  H01Q1/28 ,  H01Q21/28 ,  H04B7/18504

Abstract: A stratospheric flying object which is placed in the stratosphere of the earth has an airship-shaped flying object body, a despun platform unit mounted on the flying object body by a mount, and a controller for detecting an azimuthal angle of the despun platform unit in a horizontal plane and controlling the platform unit to face in a constant direction at all times within the horizontal plane. Preferably, directional antennas and telescopes for optical communications are mounted on the despun platform unit.

Abstract translation: 放置在地球平流层中的平流层飞行物体具有飞艇形的飞行物体，通过安装件安装在飞行物体上的解脱平台单元，以及用于检测脱水平台单元的方位角的控制器 水平面，并且在水平面内一直控制平台单元在恒定方向上面对。 优选地，用于光学通信的定向天线和望远镜安装在脱水平台单元上。

公开(公告)号：US12116102B2

公开(公告)日：2024-10-15

申请号：US17827950

申请日：2022-05-30

Applicant: Beihang University

Inventor： Kangwen Sun ,  Xinzhe Ji ,  Haoquan Liang ,  Xiao Guo

IPC: B64B1/62 ,  B60L8/00 ,  B60L58/30 ,  B64B1/22 ,  B64B1/64 ,  H01M8/04082 ,  H01M8/0656

CPC classification number: B64B1/62 ,  B60L8/003 ,  B60L58/30 ,  B64B1/22 ,  B64B1/64 ,  H01M8/04201 ,  H01M8/0656 ,  B60L2200/10 ,  H01M2250/20 ,  H01M2250/402

Abstract: An airship and its long-term floating capacity maintenance method are disclosed. The airship includes an airship capsule and a pod at bottom. A renewable fuel cell and a water tank communicated with each other are arranged in the pod. The water tank is provided with a water inlet connected with a filling aircraft outside the airship. The airship capsule is provided with a solar cell. The interior of the airship capsule is provided with a hydrogen storage bag. The solar cell is electrically connected with the renewable fuel cell. The renewable fuel cell can use electric energy provided by the solar cell to electrolyze water provided by the filling aircraft into hydrogen and supplement the hydrogen to the hydrogen storage bag. The airship can supplement hydrogen to the airship capsule by electrolyzing water to reduce the phenomenon of insufficient gas in the airship capsule.

公开(公告)号：US11753135B2

公开(公告)日：2023-09-12

申请号：US16763602

申请日：2017-11-13

Applicant: TOTAL SA ,  FLYING WHALES

Inventor： François Hervé Kuhlmann

IPC: B64B1/34 ,  B64B1/22 ,  B64D9/00 ,  G05D1/10

CPC classification number: B64B1/34 ,  B64B1/22 ,  B64D9/00 ,  G05D1/101 ,  B64B2201/00

Abstract: The method for transporting a payload to a target location, comprises the following steps of providing a hybrid airship comprises a buoyancy enclosure, a gondola carried by the buoyancy enclosure and a payload carrier, and at least one propeller; flying the hybrid airship carrying the payload to a target location, flying the hybrid airship carrying the payload comprising generating a lift force with the at least one propeller. Flying the hybrid airship carrying the payload comprises tilting the longitudinal axis of the buoyancy enclosure to a positive pitch to generate an aerodynamic lift force when the hybrid airship carrying the payload moves longitudinally.

公开(公告)号：US11731789B2

公开(公告)日：2023-08-22

申请号：US16763624

申请日：2017-11-13

Applicant: TOTAL SA ,  FLYING WHALES

Inventor： Hervé Kuhlmann

IPC: B64F5/40 ,  B64B1/22 ,  B64B1/24 ,  B64B1/32 ,  B64D9/00 ,  B64D37/04

CPC classification number: B64F5/40 ,  B64B1/22 ,  B64B1/24 ,  B64B1/32 ,  B64D9/00 ,  B64D37/04 ,  B64B2201/00

Abstract: The present invention concerns hybrid airship comprising at least one buoyancy enclosure containing a gas lighter than air, a gondola attached below the buoyancy enclosure, the gondola extending along a longitudinal axis, at least one propeller configured to propel the hybrid airship, the at least one propeller being attached to the buoyancy enclosure, at least one generator, configured to provide power to the propeller, the generator being connected to the gondola. The hybrid airship comprises an arm protruding from the gondola and connecting the generator to the gondola.