中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

319 records (took 0.042 seconds)

    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM
    162.
    发明申请
    IMAGE AND/OR RADIO SIGNALS CAPTURING PLATFORM 审中-公开
    图像和/或无线电信号捕获平台

    公开(公告)号：WO2016009402A2

    公开(公告)日：2016-01-21

    申请号：PCT/IB2015055429

    申请日：2015-07-17

    Applicant: ALTEC S P A

    Inventor： MUSSO IVANO

    IPC: G01C11/02

    CPC classification number: G01W1/08 ,  B63B35/00 ,  B64C2201/022 ,  B64C2201/125 ,  B64C2201/127 ,  B64D1/12 ,  B64D47/08 ,  G01C11/02 ,  G01S13/953 ,  G01S13/956 ,  G03B15/006 ,  G03B17/08 ,  G03B17/561 ,  H04N5/2252 ,  H04N5/23238 ,  H04N7/18

    Abstract: Platform (100; 200, 200', 200") configured to acquire images and/or radio signals and to be carried by lightweight aviation aircrafts, characterised in that it comprises housing means (1, 3; 22, 201, 202, 203, 31) that houses one or more acquisition sensors selected from the group comprising or consisting of cameras (5; 51; 32) configured to acquire still and/or moving images and radio signal receivers (62; 34) configured to acquire radio signals, said housing means (1, 3; 22, 201, 202, 203, 31) being configured to be coupled to a light aviation aircraft (540), said one or more acquisition sensors (5; 51; 32; 62; 34) being connected to processing means (6; 23) configured to receive sensing data from a position and motion sensing unit (10; 230) coupled to said one or more acquisition sensors (5; 51; 32; 62; 34), said processing means (6; 23) being configured to control and/or program, on the basis of the received sensing data, each acquisition sensor (5; 51; 32; 62; 34) so as to enable the same to acquire images and/or radio signals when such acquisition sensor (5; 51; 32; 62; 34) is in a determined position and is subject to oscillations having a velocity that is not larger in absolute value than a maximum oscillation velocity value, whereby a rate of variation of an actual aiming of such acquisition sensor (5; 51; 32; 62; 34) is not larger in absolute value than a respective maximum value of rate of variation of offset with respect to an ideal aiming at a target, so as to ensure focusing of such acquisition sensor (5; 51; 32; 62; 34) on an aimed area.

    Abstract translation: 平台（100; 200,200'，200“）被配置为获取图像和/或无线电信号并且由轻型航空飞机携带，其特征在于，其包括壳体装置（1,3; 22,201,202,203， 31），其包含从包括被配置为获取静止和/或运动图像的摄像机（5; 51; 32）或由被配置为获取无线电信号的无线电信号接收器（62; 34）组成的组中的一个或多个采集传感器， 所述一个或多个采集传感器（5; 51; 32; 62; 34）被连接到一个或多个采集传感器（5; 51; 32; 62; 34），所述壳体装置（1,3; 22,201,202,203,31） 被配置为从耦合到所述一个或多个采集传感器（5; 51; 32; 62; 34）的位置和运动感测单元（10; 230）接收感测数据的处理装置（6; 23），所述处理装置 ; 23）被配置为基于所接收的感测数据来控制和/或编程每个采集传感器（5; 51; 32; 62; 34），以便能够 当采集传感器（5; 51; 32; 62; 34）处于确定位置并且经受具有绝对值不大于最大振动速度值的速度的振荡，由此获取传感器（5; 51; 32; 62）的实际瞄准的变化率 ; 34）绝对值不比相对于目标的理想目标的偏移的变化率的相应最大值大，以便确保这种采集传感器（5; 51; 32; 62; 34）的聚焦， 在目标区域。

    A MULTI-ROTOR AIRCRAFT
    163.
    发明申请
    A MULTI-ROTOR AIRCRAFT 审中-公开
    多转机飞机

    公开(公告)号：WO2014207732A1

    公开(公告)日：2014-12-31

    申请号：PCT/IB2014/062731

    申请日：2014-06-30

    Applicant: BELLEZZA QUATER, Paolo

    Inventor： BELLEZZA QUATER, Paolo

    IPC: B64C27/20 ,  B64B1/34 ,  B64C3/30 ,  B64C39/02 ,  B64B1/30

    CPC classification number: B64C39/024 ,  B64B1/34 ,  B64C3/30 ,  B64C27/20 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/105 ,  B64C2201/165

    Abstract: Described herein is a multi-rotor aircraft (10; 200) including: - a load-bearing structure (10A; 200A); and - a plurality of propulsion assemblies (M1, M2, M3, M4, M5, M6; M1', M2', M3', M4') each including a rotor (R1, R2, R3, R4, R5, R6; R1', R2', R3', R4'), which can be driven in rotation about a respective axis of rotation (X1, X2, X3, X4, X5, X6; X1', X2', X3', X4'), these propulsion assemblies being coupled to and supported by the load-bearing structure (10A; 200A), wherein the load-bearing structure (10A; 200A) is inflatable (C11, C12, C13, C14, C15, C16; C200).

    Abstract translation: 这里描述的是多转子飞机（10; 200），包括： - 承重结构（10A; 200A）; 每个包括转子（R1，R2，R3，R4，R5，R6; R1）的多个推进组件（M1，M2，M3，M4，M5，M6; M1'，M2'，M3'，M4' （X1，X2，X3，X4，X5，X6; X1'，X2'，X3'，X4'）相对旋转驱动， 这些推进组件联接到承载结构（10A; 200A）并由其承载，其中承载结构（10A; 200A）是可膨胀的（C11，C12，C13，C14，C15，C16; C200）。

    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS
    164.
    发明申请
    SYSTEMS AND METHODS FOR LONG ENDURANCE AIRSHIP OPERATIONS 审中-公开
    长期航空运行的系统和方法

    公开(公告)号：WO2014088680A2

    公开(公告)日：2014-06-12

    申请号：PCT/US2013/060978

    申请日：2013-09-20

    Applicant: HEPPE, Stephen

    Inventor： HEPPE, Stephen

    IPC: B64B1/06

    CPC classification number: B64C37/02 ,  B64B1/06 ,  B64C2201/022 ,  B64C2201/063

    Abstract: In one example, a long endurance airship system includes a payload airship and a first logistics airship mechanically joined to the payload airship to form a first combined airship, the payload airship and the logistics airship having design capabilities differing by at least a factor of two with regard to at least one of: power generation capability, propulsion capability, endurance capability, and lift capability, in which the first combined airship is free flying, lighter-than-air, and configured to maintain aloft for greater than 30 days without physical connection to the ground. Illustrative methods for long endurance airship operations are also provided.

    Abstract translation: 在一个例子中，长期耐力飞艇系统包括有效载运飞艇和与有效载客飞艇机械连接以形成第一组合飞艇的第一物流飞艇，有效载客飞艇和具有至少两倍的设计能力的物流飞艇， 至少有以下至少一个：发电能力，推进能力，耐力能力和升力能力，其中第一组合飞艇是自由飞行的，比空中轻，并且被配置为在没有物理连接的情况下保持高达30天以上 到地面。 还提供了长期耐力飞艇作业的说明性方法。

    NEW KIND OF AIRSHIPS OF THE FUTURE
    167.
    发明申请
    NEW KIND OF AIRSHIPS OF THE FUTURE 审中-公开
    未来的飞艇类新

    公开(公告)号：WO2012135876A3

    公开(公告)日：2013-03-28

    申请号：PCT/AT2012000075

    申请日：2012-03-22

    Applicant: KITA FIROOZ

    Inventor： KITA FIROOZ

    IPC: B64B1/20 ,  B64B1/22 ,  B64B1/34 ,  B64B1/68

    CPC classification number: B64B1/32 ,  B64B1/20 ,  B64B1/22 ,  B64B1/34 ,  B64B1/68 ,  B64B2201/00 ,  B64C2201/022

    Abstract: An airship with a wide and flat, aircraft-like, not cigar-like, form, comprising a centrally arranged long fuselage and two wings, arranged on both sides of said fuselage, wherein a number of chambers or gas tanks that are delimited or separated from one another are provided, at least one, preferably more than one, in each of the two wings, and at least one means of propulsion, preferably a propeller, is provided in the front region and a means of propulsion is provided in the rear region of the airship, specifically on the upper side of the airship, wherein apertures or clearances, into or through which the means of propulsion can be pivoted or swung are formed in the airship or in the wings of the airship.

    Abstract translation: 飞艇具有设置在中心的长舱和两个布置在两侧，以这个舱翼型的宽和平坦的，平面状的，非雪茄的形状，所述设置多个间隔限制或分离的腔室或气体罐，至少一个，优选多个，在各 两翼的，并且，至少一个驱动装置，优选地为螺旋桨，在前部区域，以及一个驱动器在飞艇即的后部，设置在飞艇的顶部，装置，其中通孔的空气容器中或在飞艇的翼片或 形成于或通过驱动装置可枢转或hineinklappbar凹部。

    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM
    168.
    发明申请
    SYSTEM FOR PROVIDING A RAPIDLY ELEVATED AEROSTAT PLATFORM 审中-公开
    提供快速高空作战平台的系统

    公开(公告)号：WO2012099699A1

    公开(公告)日：2012-07-26

    申请号：PCT/US2011/068207

    申请日：2011-12-30

    Applicant: INFORMATION SYSTEMS LABORATORIES, INC.

    Inventor： VAN STAAGEN, Peter, K. ,  MCDANIEL, William, Douglas ,  BOSCHMA, James, H., Jr.

    IPC: B64F3/00

    CPC classification number: B64B1/50 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/201 ,  B64C2201/208 ,  B64F1/14

    Abstract: A system and method for deploying a payload with an aerostat uses a mobile transporter for moving the system to a deployment site. Structurally, the system includes a base unit with a rotation head mounted thereon. An envelope container for holding a deflated aerostat is mounted on the rotation head and a rotation of the container on the rotation head positions the aerostat for optimal compliance with the existing wind condition. Also included in the system is an inflator that is mounted on the base unit to inflate the aerostat with a Helium gas. And, the system includes a tether control unit for maintaining a connection with the aerostat during its deployment, in-flight use, and recovery. Preferably, a deployment computer is used for a coordinated control of the rotation head, inflator and tether.

    Abstract translation: 用空气净化器部署有效载荷的系统和方法使用移动运输装置将系统移动到部署现场。 在结构上，该系统包括其上安装有旋转头的基座单元。 用于保持放气空气净化器的信封容器安装在旋转头上，并且旋转头上的容器的旋转定位了空气调节器，以最佳地符合现有的风况。 还包括在系统中的是充气机，其安装在基座单元上，以用氦气对空气净化器进行充气。 而且，该系统包括一个系绳控制单元，用于在其部署，飞行中使用和恢复期间维持与浮空器的连接。 优选地，部署计算机用于旋转头，充气机和系绳的协调控制。

    자력탐사용 휴대용 무인비행선 및 이를 이용한 자력탐사 시스템
    169.
    发明申请
    자력탐사용 휴대용 무인비행선 및 이를 이용한 자력탐사 시스템 审中-公开
    用于磁力检测的便携式不间断航空和使用其的磁力测量系统

    公开(公告)号：WO2011052822A1

    公开(公告)日：2011-05-05

    申请号：PCT/KR2009/006300

    申请日：2009-10-29

    Applicant: 한국지질자원연구원 ,  조성준 ,  박종서 ,  박계순

    Inventor： 조성준 ,  박종서 ,  박계순

    IPC: B64B1/06 ,  B64C13/16 ,  B64D47/00 ,  B25J5/00

    CPC classification number: G01R33/0385 ,  B64B1/06 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/127 ,  B82Y25/00 ,  G01R33/038

    Abstract: 본 발명은 자력탐사용 휴대용 무인비행선 및 이를 이용한 자력탐사 시스템에 관한 것으로, 기체의 부력을 이용하며 자체 동력으로 추진하는 비행선 본체; 상기 비행선 본체를 자동으로 운항시키기 위한 자동운항장치; 상기 비행선 본체에 설치되며 지표나 지층의 자력을 측정하기 위한 자력측정장치; 상기 자력측정장치를 통해 획득된 자기데이터를 외부로 송신하기 위한 무선통신장치; 및 상기 자동운항장치 및 상기 자력측정장치의 작동을 제어하기 위한 제어모듈; 을 포함한다. 이에 따라, 무인비행선의 전체적인 운항시간을 늘릴 수 있으며, 무인비행선에 적재되는 페이로드(payload)의 하중을 늘릴 수 있는 기술이 개시된다.

    Abstract translation: 本发明涉及一种用于磁力测量的便携式无人飞艇和采用该方法的磁力测量系统，包括：使用气体浮力在其自身动力下推进的主飞艇身体; 用于自动飞行主飞艇身体的自动飞行装置; 磁力测量装置，设在主飞艇身上，用于测量地球表面或地质层的磁力; 用于将经由磁力测量装置获取的磁数据发送到外部的无线通信装置; 以及用于控制自动飞行装置和磁力测量装置的操作的控制模块。 因此，公开了能够增加无人飞艇的总飞行时间并且可以增加载入无人飞艇上的载荷的重量的技术。

Patent Agency Ranking