中科微点-全球专利检索

  1. Login
  2. Sign Up

Search Results

188 records (took 0.031 seconds)

    A MULTI-ROTOR AIRCRAFT
    75.
    发明公开
    A MULTI-ROTOR AIRCRAFT 有权
    FLUGZEUG MIT MEHREREN ROTOREN

    公开(公告)号：EP3013686A1

    公开(公告)日：2016-05-04

    申请号：EP14752660.2

    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）。

    Apparatus and method for launching an unmanned aerial vehicle
    77.
    发明公开
    Apparatus and method for launching an unmanned aerial vehicle 审中-公开
    Vorrichtung und Verfahren zum Starten eines unbemannten Luftfahrzeugs

    公开(公告)号：EP2845800A1

    公开(公告)日：2015-03-11

    申请号：EP13275198.3

    申请日：2013-09-04

    Applicant: BAE Systems PLC

    Inventor： The designation of the inventor has not yet been filed

    IPC: B64C39/02 ,  B63B35/00

    CPC classification number: B64C39/024 ,  B63G8/28 ,  B64C2201/022 ,  B64C2201/082 ,  B64C2201/101

    Abstract: Disclosed is apparatus (10, 10') for launching an unmanned aerial vehicle (20), for example from a vehicle (250) submerged beneath the surface (260) of a body of water (270). The apparatus (10, 10') comprises: an envelope (30) configured to receive and, at least to some extent, retain therewithin a lighter than air, gaseous substance; and coupling means operable to switch between a first state in which the coupling means couples the envelope (30) to the unmanned aerial vehicle (20) and a second state in which the unmanned aerial vehicle (20) is free to move away from the envelope (30). The apparatus (10, 10') is an unmanned apparatus.

    Abstract translation: 公开了用于发射无人驾驶飞行器（20）的装置（10,10'），例如从淹没在水体（270）的表面（260）下面的车辆（250）发射。 所述设备（10,10'）包括：封套（30），其配置成接收并至少在某种程度上在其中比空气中的气体物质更轻; 以及联接装置，其可操作以在所述联接装置将所述封套（30）耦合到所述无人驾驶飞行器（20）的第一状态和所述无人驾驶飞行器（20）能够自由地远离所述信封的第二状态 （30）。 装置（10,10'）是无人装置。

    AIRSHIP AND METHOD OF OPERATION
    78.
    发明公开
    AIRSHIP AND METHOD OF OPERATION 有权
    飞艇工作程序

    公开(公告)号：EP1519873A1

    公开(公告)日：2005-04-06

    申请号：EP03737791.8

    申请日：2003-06-25

    Applicant: 21st Century Airships Inc.

    Inventor： COLTING, Hokan

    IPC: B64B1/00

    CPC classification number: B64B1/34 ,  B64B1/02 ,  B64B1/32 ,  B64C21/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  Y02T50/166

    Abstract: An airship (20) has a generally spherical shape and has an internal envelope (24) for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system (36, 38) that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7 % full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module (180) that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors (44, 46) of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit (52) that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.

    KR102233490B1 - System having 3dimensions target for ball sports
    79.
    发明专利
    KR102233490B1 - System having 3dimensions target for ball sports 有权

    公开(公告)号：KR102233490B1

    公开(公告)日：2021-03-29

    申请号：KR1020190015778A

    申请日：2019-02-11

    Applicant: 차영천

    Inventor： 차영천

    IPC: A63B71/04 ,  A63B71/06 ,  B64C39/02 ,  B64D45/00

    CPC classification number: A63B63/06 ,  A63B69/36 ,  A63B71/04 ,  A63B71/06 ,  A63B71/0605 ,  A63B71/0622 ,  A63B71/0669 ,  B64C39/024 ,  B64D45/00 ,  A63B2102/32 ,  A63B2220/12 ,  A63B2220/17 ,  A63B2220/807 ,  A63B2225/74 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/143

    Abstract: 본 발명은 구기스포츠를 위한 3차원 타겟 시스템에 관한 것으로서, 더욱 상세하게는 드론이나 구체를 이용하여 공중에 떠 있는 타겟을 맞추는 구기스포츠를 위한 3차원 타겟 시스템에 관한 것이다.
    본 발명의 구기스포츠를 이용한 3차원 타격시스템은 타격대상이 이미지가 아닌 실제로 배치되므로 타격감이나 타격체가 타겟에 타격되는 것을 직접 경험하므로 게임의 재미를 높일 수 있는 이점이 있다.
    또한, 본 발명의 구기스포츠를 이용한 3차원 타격시스템은 타격대상이 다양한 위치로 이동 및 위치 복원될 수 있도록 공중에서 비행조종가능한 드론이 적용되므로 사용자가 새로운 형태의 경기를 경험할 수 있으며, 드론의 활용도를 높일 수 있는 이점이 있다.
    그리고, 본 발명의 구기스포츠를 이용한 3차원 타격시스템은 다수의 레이저포인터에 의해 형성된 3D 지도를 통해 다수의 타겟의 위치를 정확하게 파악할 수 있어 다수의 타겟의 정밀한 이동제어가 가능하므로 다수의 타겟의 군집 비행제어효율을 높일 수 있으며, 나아가서는 경기 진행 효율을 향상시킬 수 있는 이점이 있다.

Patent Agency Ranking