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：US08464977B2

公开(公告)日：2013-06-18

申请号：US12677917

申请日：2008-08-12

Applicant: Masahiko Suzuki

Inventor： Masahiko Suzuki

IPC: B64C39/00

CPC classification number: B64C39/04 ,  B60V1/08 ,  B64B2201/00

Abstract: A positive-pressure floating type airplane comprising an airfoil portion, left-right fuselages, a central fuselage, an elevator and a rudder disposed at the back of the airfoil portion, a thruster disposed at the back of the central fuselage, and a horizontal stabilizer disposed at the rear ends of the left-right fuselages. The individual front ends of the airfoil portion, the left-right fuselages and the central fuselage are formed into arcuate shapes in longitudinal sections. On the lower side of the airfoil portion, a recessed air capture is formed from the front end to the rear end. As a result, the positive-pressure floating type airplane is floated by the reaction from the air at the time when the air to pass the air capture through the airfoil portion is pushed by the thrust of the thruster, and is propelled forward by the component of that thrust.

Abstract translation: 一种正压浮式飞机，其包括设置在翼型部分的后部的机翼部分，左右机身，中央机身，电梯和方向舵，设置在中央机身后部的推进器和水平稳定器 设置在左右机身的后端。 机翼部分，左右机身和中央机身的各个前端在纵向部分形成为弓形。 在翼型部分的下侧，从前端到后端形成凹陷的空气捕获。 结果，正压浮式飞机在通过空气捕获通过翼型部的空气被来自空气的反作用力推动推动器的推力而被推动时被部件 的推力。

公开(公告)号：US08418952B2

公开(公告)日：2013-04-16

申请号：US13342373

申请日：2012-01-03

Applicant: Pierre Balaskovic

Inventor： Pierre Balaskovic

IPC: B64B1/12 ,  B64B1/10

CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

公开(公告)号：US20120273608A1

公开(公告)日：2012-11-01

申请号：US12999309

申请日：2009-05-21

Applicant: Peter E. Jess ,  Ken Laubsch

Inventor： Peter E. Jess ,  Ken Laubsch

IPC: B64B1/34

CPC classification number: B64B1/30 ,  B64B1/08 ,  B64B1/34 ,  B64B2201/00

Abstract: A hybrid lift air vehicle for carrying and transporting a load, comprising an envelope having a generally ellipsoidal shape adapted to receive a volume of lighter-than-air gas, at least two variable thrust vertical thrusters in secure engagement with the envelope and at least two variable thrust lateral thrusters in secure engagement with the envelope, means for temporarily securely engaging the load to the envelope wherein the volume of lighter-than-air gas has a buoyancy that offsets at least 25% of the weight of the air vehicle when unloaded, wherein the thrust from the at least two vertical thrusters may be varied to raise and lower the air vehicle and the load when engaged, and wherein the thrust from the at least two lateral thrusters may be varied to maneuver and transport the raised air vehicle and the load when engaged.

Abstract translation: 一种用于承载和运输负载的混合动力提升空气车辆，包括具有适于接纳一定体积的轻质气体的大致椭圆形状的外壳，至少两个可变推力垂直推进器，其与所述外壳牢固接合，并且至少两个 可变推力横向推进器与信封牢固地接合，用于将负载暂时牢固地接合到信封的装置，其中轻质空气气体的体积具有在卸载时抵消空中交通工具的重量的至少25％的浮力， 其中来自所述至少两个垂直推进器的推力可以变化以在接合时升高和降低空中车辆和负载，并且其中来自所述至少两个横向推进器的推力可以变化以调节和运输升高的空气车辆， 接合时加载

公开(公告)号：US08177159B2

公开(公告)日：2012-05-15

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: B64B1/20 ,  B64B1/26

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

Abstract: A rescue aircraft having a rigid body with gas-filled envelopes and propulsion devices located inside rotatable aerodynamic toroidal modules. A longitudinal through passage in the lower part of the aircraft connects a crew cabin, a cargo-and-passenger compartment, fuel tanks, and accessories. The aircraft has exit hatches, mooring devices, and a gangway with railings and a removable cart. The aircraft also has a cross passage with exits onto its wings and a vertical passage with a pulley and other devices for lowering and lifting people and cargo. The lower part of the aircraft and hollow wings are filled with a foamed plastic for buoyancy and strength.

Abstract translation: 一架救援飞机具有刚性体，气体充满的信封和推进装置位于可旋转的空气动力学环形模块内。 飞机下部的纵向通道连接船员舱，货舱和货舱，燃油箱和附件。 这架飞机有出口舱口，系泊装置和一个带栏杆和可移动推车的通道。 飞机还有一个十字通道，出口到其翼上，一个垂直通道，带有滑轮和其他用于降低和提升人员和货物的装置。 飞机的下部和空心翼充满泡沫塑料，用于浮力和强度。

公开(公告)号：US20110163200A1

公开(公告)日：2011-07-07

申请号：US12957989

申请日：2010-12-01

Applicant: Pierre Balaskovic

Inventor： Pierre Balaskovic

IPC: B64B1/06 ,  B64B1/22 ,  B64B1/24 ,  B64B1/12

CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

公开(公告)号：US07866601B2

公开(公告)日：2011-01-11

申请号：US11907883

申请日：2007-10-18

Applicant: Pierre Balaskovic

Inventor： Pierre Balaskovic

IPC: B64B1/12 ,  B64B1/10

CPC classification number: B64B1/06 ,  B64B1/10 ,  B64B1/12 ,  B64B1/30 ,  B64B1/34 ,  B64B2201/00 ,  B64C2201/00

Abstract: An airship may include a hull substantially shaped as an oblate spheroid, one or more frame members defining a support structure, wherein the support structure forms at least a partial support for the hull, at least one horizontal stabilizing member operably coupled to a lower surface of the airship, and at least one horizontal stabilizing member having a first end and a second end. The at least one horizontal stabilizing member may define an anhedral configuration. The airship may also include a vertical stabilizing member having a first end pivotally coupled to the airship and a second end oriented to remain below an upper surface of the airship. The vertical stabilizing member may be configured to pivot within a vertical plane, and the first end of the vertical stabilizing member and the first end of the at least one horizontal stabilizing member may be operably coupled to one another.

Abstract translation: 飞艇可以包括基本上成形为扁圆球体的船体，限定支撑结构的一个或多个框架构件，其中所述支撑结构至少形成用于船体的部分支撑件，至少一个水平稳定构件可操作地联接到船体的下表面 所述飞艇以及具有第一端和第二端的至少一个水平稳定构件。 所述至少一个水平稳定构件可以限定一个双面构型。 飞艇还可以包括垂直稳定构件，其具有枢转地联接到飞艇的第一端和定向成保持在飞艇的上表面下方的第二端。 垂直稳定构件可以构造成在垂直平面内枢转，并且垂直稳定构件的第一端和至少一个水平稳定构件的第一端可以可操作地彼此连接。

公开(公告)号：US20100276546A1

公开(公告)日：2010-11-04

申请号：US12384802

申请日：2009-04-09

Applicant: Sunstar Im

Inventor： Sunstar Im

IPC: B64B1/20 ,  B64G1/26 ,  B64B1/06

CPC classification number: B64B1/08 ,  B64B1/005 ,  B64B1/16 ,  B64B1/18 ,  B64B1/20 ,  B64B1/28 ,  B64B1/58 ,  B64B2201/00 ,  B64C2201/00 ,  B64G1/005

Abstract: The structure provided multi-Levels of the center fuselage, two front wings, Extended mid-two wings and two rear wings with two vertical winglets.The fuselage has a cross section of half circle shaped fuselage.The first level comprises multi-fuel tanks, water tanks, Helium gas tanks, hydraulic, Pneumatic systems and plurality of the multi-landing gear bays and multi-cargo Compartments.The first level comprises a top cockpit and the plurality of the multi-passenger Cabins.The second level is comprises multi-central posts, multi-guy wires on the top center Beams, mid level, lower level center beams, leak proof sealed floor gates for the Multi-gas envelopes structure, under belly multi-pontoon air bags.The first level further comprises multi-jet power plants with multi-chute flaps.The second level may comprises, carbon fiber honey comb sandwich composite Multi-envelopes and multi-level soft gas envelopes.

Abstract translation: 该结构提供了中央机身的多层次，两个前翼，扩展中二翼和两个后翼与两个垂直的小翼。 机身有半圆形的机身横截面。 第一级包括多燃料箱，水箱，氦气罐，液压，气动系统和多个起落架舱和多货舱。 第一级包括顶部驾驶舱和多个多乘客舱。 第二级包括多中心柱，多中心柱，多中心杆，顶级中心梁，中级，下级中心梁，多气体信封结构的防漏密封地板门，腹部多浮桥气囊。 第一级还包括具有多溜槽襟翼的多喷射发电厂。 第二级可以包括碳纤维蜂蜜夹心复合多信封和多层软气体包络。

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。