公开(公告)号：WO9829303B1

公开(公告)日：1999-10-07

申请号：PCT/EP9800015

申请日：1998-01-02

Applicant: INDUSTRIEANLAGEN BETRIEBSGES ,  KUENKLER HERMANN

Inventor： KUENKLER HERMANN

IPC: B64B1/06 ,  B63H5/125 ,  B64B1/30 ,  B64B1/32 ,  B64C11/02 ,  B64C27/28 ,  B64C27/52 ,  B64C29/00 ,  B64D35/00

CPC classification number: B64C29/0033 ,  B63H5/125 ,  B64B1/32 ,  B64B2201/00 ,  B64C11/02 ,  B64C27/28 ,  B64C27/52 ,  B64D35/00

Abstract: An aircraft has a fuselage substantially designed as an aerostatic lifting body and combined lifting and propelling devices joined to the fuselage, provided with propellers and forming driving units which can tilt between a lifting position, in which the plane of rotation of the respective propeller is substantially horizontal and the driven shaft of the associated drive that drives the propeller shaft is substantially vertical, and a propelling position in which the plane of rotation of the respective propeller is substantially vertical and the driven shaft of the associated drive that drives the propeller shaft is substantially horizontal. The plane of rotation of the propeller can swivel around the driven shaft of the associated drive that drives the propeller shaft.

Abstract translation: 一种飞行器具有大致设计为空气静力浮体和铰接到船体，设置有推进器，驱动成形组合升力和推进装置单元，其每一个是升程位置，在该相应的螺旋桨旋转平面基本上是水平的并偏置各个传动轴输出轴之间 相关的驱动器的基本垂直位于，和推进位置，在该相应的螺旋桨旋转平面垂直地和水平基本上位于基本上作用在相关联的驱动器的输出轴上的相应的传动轴，可以倾斜。 螺旋桨旋转相对于周围作用于相关联的驱动器的输出轴的推进器轴可倾斜的平面。

公开(公告)号：WO1993024366A1

公开(公告)日：1993-12-09

申请号：PCT/RU1993000019

申请日：1993-01-21

Applicant: NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA ... ,  SAVITSKY, Anatoly Ivanovich ,  SCHUKIN, Lev Nikolaevich ,  KARELIN, Viktor Georgievich ,  PUSHKIN, Rostislav Mikhailovich ,  MASS, Alexandr Mikhailovich ,  SHIBANOV, Anatoly Petrovich ,  SCHUKIN, Ilya Lvovich ,  KHUTSISCHVILI, Vladimir Georgievich ,  FISCHENKO, Sergei Viktorovich ,  ERMISCHIN, Alexandr Viktorovich ,  SOBKO, Alexandr Pavlovich

Inventor： NAUCHNO-PROIZVODSTVENNAYA KOOPERATIVNAYA FIRMA ...

IPC: B64C39/00

CPC classification number: B64C39/10 ,  B60V1/22 ,  B64B2201/00 ,  B64C39/00 ,  Y02T50/12

Abstract: The invention relates to aviation namely to flying vehicles adapted to ride on an air cushion and to effect a take-off and landing on aerodromes of any category. The goal of the invention is to design a flying vehicle capable of aerodynamically efficient flight both at low and high level flight, as well as take-off and landing from non-prepared aerodromes and from water under the conditions of stabilization and movement control of all flight regimes. The goal is achieved due to the fact that in a flying vehicle comprising a fuselage in the form of a carrying wing, a power installation, a take-off and landing air cushion device, a gasodynamic system of boundary layer control, a device for controlling the position of flow leaving the trailing edge as well as stabilization and flight control systems, the take-off and landing air cushion device consists of a propelling slot nozzle (12) and side skegs (17) between which are mounted rotatable flaps (21, 22, 23) controlling the flight of the vehicle and regulating the position of the pressure centre on the bottom. The fuselage has the form of a cylindrical segment conjugating at its sides with spherical fairings.

Abstract translation: 本发明涉及航空，即适用于乘坐气垫的飞行车辆，以及在任何类别的机场起飞和降落。 本发明的目标是设计一种能够在低和高水平飞行中进行空中动力学有效飞行的飞行器，以及在所有的稳定和运动控制条件下从未准备的机场和水中起飞和着陆 飞行政权 目的是实现这样的事实，即在包括机身形式的机身，动力装置，起飞和着陆气垫装置，边界层控制的气动系统，控制装置 离开后缘的流动位置以及稳定和飞行控制系统，起飞和着陆气垫装置包括推进式狭缝喷嘴（12）和侧部塞子（17），在其间安装有可旋转的翼片（21， 控制车辆的飞行并调节压力中心在底部的位置。 机身具有圆柱形段的形式，其侧面与球形整流罩共轭。

公开(公告)号：US20230286636A1

公开(公告)日：2023-09-14

申请号：US18198931

申请日：2023-05-18

Applicant: Galaxy Unmanned Systems LLC

Inventor： Antonio Roberto White ,  Jason Theodore White

IPC: B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/58 ,  B64B1/66

CPC classification number: B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/58 ,  B64B1/66 ,  B64B2201/00

Abstract: A hybrid airship-aerostat includes a hull, a motor, a fin, a controller, and a bridle system. The motor is coupled to the hull and is configured to rotate between a thrust configuration and a lift configuration. The motor is configured to generate a lift force, a thrust force, or a combination thereof. The fin is coupled to a tail of the hull and is configured to provide directional control of the hull. The controller is configured to operate the motor and the fin to pilot the hull. The bridle system is configured to removably couple to a first end of a tether.

公开(公告)号：US11685500B2

公开(公告)日：2023-06-27

申请号：US17477052

申请日：2021-09-16

Applicant: Galaxy Unmanned Systems LLC

Inventor： Antonio Roberto White ,  Jason Theodore White

IPC: B64B1/66 ,  B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/58

CPC classification number: B64B1/20 ,  B64B1/22 ,  B64B1/30 ,  B64B1/58 ,  B64B1/66 ,  B64B2201/00

Abstract: A hybrid airship-aerostat includes a hull, a motor, a fin, a controller, and a bridle system. The motor is coupled to the hull and is configured to rotate between a thrust configuration and a lift configuration. The motor is configured to generate a lift force, a thrust force, or a combination thereof. The fin is coupled to a tail of the hull and is configured to provide directional control of the hull. The controller is configured to operate the motor and the fin to pilot the hull. The bridle system is configured to removably couple to a first end of a tether.

公开(公告)号：US20190210723A1

公开(公告)日：2019-07-11

申请号：US15863018

申请日：2018-01-05

Applicant: Raytheon Company

Inventor： Gregory W. Heinen

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64B1/34 ,  B64B1/44 ,  B64B1/54 ,  B64B1/70 ,  B64B2201/00 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/12 ,  G01S7/4004 ,  G01S7/4052 ,  G01S2007/4082 ,  H01Q1/082 ,  H01Q1/2291 ,  H01Q1/28 ,  H01Q1/34

Abstract: A flight vehicle includes a drone with a pair of shaped protrusions mechanically coupled to the drone. One of the shapes is a hollow lift-producing shape, such as being a balloon filed with a lighter-than-air gas, and the other of the shapes is below the drone. The shape below the drone may be a hollow shape that does not produce lift, for example being a balloon filled with air. The shapes may be similar in size and shape, so as to provide similar drag characteristics. The shapes may be opposite ends of a support, such as a stick, rod, or other (relatively) slender structure. The vehicle includes a payload, such as radar calibration equipment or an antenna. The drone may be used to counteract wind forces on the flight vehicle, and/or to otherwise position the flight vehicle.

公开(公告)号：US20180117521A1

公开(公告)日：2018-05-03

申请号：US15342104

申请日：2016-11-02

Applicant: Mark DiCarlo

Inventor： Mark DiCarlo

IPC: B01D53/00 ,  B01D46/00 ,  B01D47/06 ,  B01D50/00

CPC classification number: B01D53/007 ,  B01D46/0023 ,  B01D46/10 ,  B01D47/06 ,  B01D50/006 ,  B01D53/14 ,  B01D53/32 ,  B01D2247/12 ,  B01D2258/06 ,  B01D2259/4575 ,  B01D2279/40 ,  B64B1/00 ,  B64B2201/00

Abstract: This disclosure relates to a system that provides an environmentally friendly method to clean air over towns and cities. The system utilizes tourmaline filters and rocks, sunlight, and water to simulate the cleaning properties of waterfalls in order to create an ionized surface within a cylindrical tube and creates raindrops and mist to simulate precipitation. The system eliminates pollutants instead of transferring them to the surrounding environment.

公开(公告)号：US20180050785A1

公开(公告)日：2018-02-22

申请号：US15675046

申请日：2017-08-11

Applicant: JG Entrepreneurial Enterprises LLC

Inventor： John GOELET

IPC: B64B1/68 ,  B64B1/34 ,  B64B1/58 ,  B64B1/22 ,  B64B1/20 ,  B64B1/60 ,  B64C25/56 ,  B64B1/12 ,  B64C25/32 ,  B64B1/00 ,  B64B1/14 ,  B64B1/06

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 ,  Y02T50/55

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.

公开(公告)号：US09852644B2

公开(公告)日：2017-12-26

申请号：US15193033

申请日：2016-06-25

Applicant: Bee Robotics Corporation

Inventor： Vladimir Salnikov ,  Anatoly Filin ,  Harm Burema

IPC: G08G5/00 ,  A01B79/00 ,  A01C21/00 ,  A01C7/00 ,  A01M9/00 ,  B64B1/40 ,  B64C39/02 ,  B64D1/16 ,  G05D1/00 ,  G08G5/04 ,  A01B79/02 ,  A01C7/04 ,  G05D1/10

CPC classification number: G08G5/0043 ,  A01B79/005 ,  A01B79/02 ,  A01C7/04 ,  A01C21/00 ,  B64B1/40 ,  B64B2201/00 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/126 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/146 ,  B64D1/00 ,  B64D1/16 ,  G05D1/104 ,  G08G5/04 ,  Y10S901/01

Abstract: Modern farming is currently being done by powerful ground equipment or aircraft that weigh several tons and treat uniformly tens of hectares per hour. Automated farming can use small, agile, lightweight, energy-efficient automated robotic equipment that flies to do the same job, even able to farm on a plant-by-plant basis, allowing for new ways of farming. A hybrid airship-drone has both passive lift provided by a gas balloon and active lift provided by propellers. A hybrid airship-drone may be cheaper, more stable in flight, and require less maintenance than other aerial vehicles such as quadrocopters. However, hybrid airship-drones may also be larger in size and have more inertia that needs to be overcome for starting, stopping and turning.

公开(公告)号：US09745042B2

公开(公告)日：2017-08-29

申请号：US15242223

申请日：2016-08-19

Applicant: LTA CORPORATION

Inventor： John Goelet

IPC: B64B1/02 ,  B64B1/68 ,  B64B1/06 ,  B64B1/12 ,  B64B1/14 ,  B64B1/20 ,  B64B1/22 ,  B64B1/34 ,  B64B1/60 ,  B64C25/32 ,  B64C25/56 ,  B64B1/00 ,  B64B1/58

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.

公开(公告)号：US09738369B2

公开(公告)日：2017-08-22

申请号：US15322933

申请日：2015-06-29

Applicant: ANTER LLC ,  RUFIUS Oy

Inventor： Timur A. Mirzeabasov ,  Lidia N. Shkolina ,  Svetlana T. Romanova ,  Dimitrii O. Belov ,  Valery M. Volynkin ,  Vadim Y. Golovan ,  Fail N. Suleymanov ,  Igor Vodyanoy

IPC: B64B1/66 ,  B64B1/22 ,  B64D27/24

CPC classification number: B64B1/66 ,  A62B5/00 ,  B64B1/06 ,  B64B1/14 ,  B64B1/22 ,  B64B1/34 ,  B64B2201/00 ,  B64C37/02 ,  B64D27/24

Abstract: The invention relates to a multipurpose airship and, more particularly, to a hybrid dirigible. The airship comprises a body (2) having a parallelepiped shape and docking means (8) comprising four rods connected by a frame and designed to be extractable from the body (2), the ends of these rods being provided each with at least one vacuum cup for adhering to a substantially vertical surface of a building. The docking means (8) are provided with grips adapted to engage with the docking means (8) of another airship of the same design. The invention also relates to a set of airships including at least two said airships. The proposed airship does not require a lot of space for its takeoff and provides fast and secure evacuation of people from tower buildings. In addition, the invention provides the possibility of varying the airship payload directly in flight depending of specific needs.