公开(公告)号：WO2013112198A3

公开(公告)日：2013-10-31

申请号：PCT/US2012049790

申请日：2012-08-06

Applicant: SILICIS TECHNOLOGIES INC ,  STIGLER MICHAEL J ,  SETAR NICHOLAS JAMES

Inventor： STIGLER MICHAEL J ,  SETAR NICHOLAS JAMES

IPC: B64B1/00

CPC classification number: B64B1/12 ,  B64B1/005 ,  B64B1/10 ,  B64B1/14 ,  B64B1/18 ,  B64B1/22 ,  B64B1/24 ,  B64B1/36 ,  B64B1/60 ,  B64B1/62 ,  B64B1/64 ,  B64B1/66 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/141 ,  G05D1/0027 ,  G05D1/101 ,  G08G5/0069 ,  G09F21/04 ,  G09F21/06

Abstract: An intelligence, surveillance, and reconnaissance system is disclosed including a ground station and one or more aerial vehicles. The aerial vehicles are autonomous systems capable of communicating intelligence data to the ground station and be used as part of a missile delivery package. A plurality of aerial vehicles can be configured to cast a wide net of reconnaissance over a large area on the ground including smaller overlapping reconnaissance areas provided by each of the plurality of the aerial vehicles.

Abstract translation: 一个情报，监视和侦察系统被披露，包括一个地面站和一个或多个飞行器。 飞行器是能够将情报数据传送到地面站并作为导弹交付包的一部分的自治系统。 多个飞行器可以被配置为在地面上的大面积上投射广泛的侦察网络，包括由多个飞行器中的每一个提供的较小的重叠侦察区域。

公开(公告)号：WO2004087499A3

公开(公告)日：2005-01-20

申请号：PCT/GB2004001488

申请日：2004-04-05

Applicant: LUFFMAN CHARLES RAYMOND

Inventor： LUFFMAN CHARLES RAYMOND

IPC: B64B1/26 ,  B64B1/36 ,  B64B1/66 ,  B64F1/14

CPC classification number: B64B1/26 ,  B64B1/36 ,  B64B1/66 ,  B64F1/14

Abstract: An airship (10) comprising an envelope and a ballonet (32) positioned within the envelope (30). Drive means is provided for supplying lateral thrust for the airship, to improve lateral control of the airship. The drive means has a dual function as it has an air supply system with an air inlet provided at the bow of the envelope of the airship for supplying air to the balonet (32) to aid pressurisation. A mooring system and detachable gondola (14) is also disclosed.

Abstract translation: 飞艇（10）包括一个位于封套（30）内的信封和一个气球（32）。 提供用于为飞艇提供侧向推力的驱动装置，以改善飞艇的横向控制。 驱动装置具有双重功能，因为其具有空气供应系统，其具有设置在飞艇的信封的弓部处的空气入口，用于将空气供给到支架（32）以辅助加压。 还公开了系泊系统和可拆卸式小型车（14）。

公开(公告)号：WO00047468A1

公开(公告)日：2000-08-17

申请号：PCT/GB2000/000380

申请日：2000-02-08

IPC: B64B1/36 ,  B64B1/24

CPC classification number: B64B1/36

Abstract: Airship bow thruster apparatus (7) comprising means (9) for generating a large mass flow of air or exhaust gases and movable deflection means (17-20) at the bow of an airship positionable in the flow path of the air or exhaust gases. The position of the deflection means (17-20) is controlled by control means for controlling the direction that the air or exhaust gases is or are ejected at the bow of the airship. The invention also relates to an airship provided with such bow thruster apparatus.

Abstract translation: 飞艇舷侧推进器装置（7）包括用于在空气或废气的流动路径中的飞艇的弓形处产生大量空气或废气质量流的装置（9）和可移动的偏转装置（17-20）。 偏转装置（17-20）的位置由控制装置控制，用于控制空气或废气在飞艇的弓上被喷射或被喷射的方向。 本发明还涉及一种具有这种船首推进器装置的飞艇。

公开(公告)号：WO00032469A1

公开(公告)日：2000-06-08

申请号：PCT/HU1999/000091

申请日：1999-11-29

IPC: B64B1/06 ,  B64B1/36 ,  B64C27/20

CPC classification number: B64B1/06 ,  B64B1/36 ,  B64C27/20

Abstract: The invention relates to a flying apparatus for the purpose of lifting and carrying extremely large loads by air. The necessary lifting power is produced by the rotary wings situated in the centre of mass. The lifting force of the gas cells placed around the rotary wing and filled with helium keeps in balance with the self-weight of the flying apparatus. The transported load is carried by a gripping device or container placed underneath the centre of mass. The load is lifted by the necessary lifting force generated on the rotary wings. The rotary wings (1), connected to the circular girder (5) with the drive framework (3) and the tangent spoke or girder (4), form a flying unit with the gas cells (13) placed between the profile frame girders (8) departing from the circular girder (5) radially. The permanent moment of stability is ensured by a fluid gyroscope (7).

Abstract translation: 本发明涉及一种用于通过空气提升和承载极大载荷的飞行装置。 必要的提升力由位于质心中心的旋转翼产生。 设置在旋转翼周围并充满氦气的气室的提升力与飞行装置的自重保持平衡。 运输的负载由放置在质心下方的夹紧装置或容器承载。 通过旋转翼上产生的必要的提升力来提升载荷。 连接到具有驱动框架（3）的圆形梁（5）和切线辐条或梁（4）的旋转翼（1）形成飞行单元，其中气室（13）放置在轮廓框架梁 8）径向离开圆形梁（5）。 通过流体陀螺仪（7）确保永久的稳定时刻。