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    Flying apparatus and method for removing harmful gases from the atmosphere
    51.
    发明申请
    Flying apparatus and method for removing harmful gases from the atmosphere 有权
    用于从大气中去除有害气体的飞行装置和方法

    公开(公告)号：US20090238741A1

    公开(公告)日：2009-09-24

    申请号：US12380729

    申请日：2009-03-02

    Applicant: Detlev Konigorski

    Inventor： Detlev Konigorski

    IPC: B01D53/34 ,  B01D53/22 ,  B01D61/00 ,  B01D50/00 ,  B01D53/02 ,  B01J19/08 ,  B01J19/12 ,  B01D53/86

    CPC classification number: B64B1/20 ,  B01D53/002 ,  B01D2257/2025 ,  B01D2257/2064 ,  B01D2259/4558 ,  B64B2201/00 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/125 ,  Y10S244/90

    Abstract: An apparatus for removing harmful gas components out of the earth's atmosphere is a free-flying autonomous lightweight aircraft with an onboard gas processing system including gas separation or extraction devices, and inlets and outlets connected to the devices. Solar cells and/or thermoelectric generators provided on the craft produce electrical energy to operate the individual devices. The system may include a cryogenic closed-loop circulation system that participates in liquefying the extracted gas components. The apparatus is preferably a lighter-than-air craft like a dirigible. A method of extracting harmful gas components from the atmosphere involves flying the apparatus at a prescribed altitude level and operating the gas processing system to remove the harmful gas component from the atmosphere, then returning the apparatus to earth to offload the liquefied stored harmful gas component.

    Abstract translation: 用于将有害气体成分从地球大气中除去的装置是一种自由飞行的自主轻型飞机，其具有包括气体分离或提取装置在内的气体处理系统以及连接到装置的入口和出口。 设置在飞行器上的太阳能电池和/或热电发电机产生电能以操作各个装置。 该系统可以包括参与液化提取的气体组分的低温闭环循环系统。 该装置优选地是比较轻便的轻型飞行器。 从大气中提取有害气体成分的方法包括使设备以规定的高度水平飞行，并操作气体处理系统以从大气中除去有害气体成分，然后使设备返回到地面以卸载液化的存储的有害气体成分。

    Airship system
    52.
    发明申请
    Airship system 失效
    飞艇系统

    公开(公告)号：US20030025034A1

    公开(公告)日：2003-02-06

    申请号：US10189796

    申请日：2002-07-03

    Inventor： Yutaka Akahori

    IPC: B64B001/02 ,  B64B001/06

    CPC classification number: G08G5/0052 ,  B64B1/06 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/048 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/167 ,  B64F1/18 ,  G01S5/20 ,  G01S5/22 ,  G05D1/0202 ,  G08G5/00 ,  G08G5/0013

    Abstract: An airship system according to the invention has an airship (110), a base station (120), and at least three measurement points. The airship (110) emits ultrasonic waves upon receiving an instruction from the base station (120). Measurement point units (S1-S3) receive the ultrasonic waves, and thereby measure distances from the airship (110) to the respective measurement points. An MPU that is incorporated in the base station (120) calculates a position of the airship (110). The base station (120) controls a route of the airship (110) based on the calculated position by sending a flight instruction to the airship (110). In this manner, an airship system can be provided that makes it unnecessary for an operator to pilot the airship and that can reduce the load weight and the power consumption of the airship.

    Abstract translation: 根据本发明的飞艇系统具有飞艇（110），基站（120）和至少三个测量点。 飞艇（110）在接收到来自基站（120）的指令时发射超声波。 测量点单元（S1-S3）接收超声波，从而测量从飞艇（110）到相应测量点的距离。 并入基站（120）的MPU计算飞艇（110）的位置。 基站（120）通过向飞艇（110）发送飞行指令，基于计算出的位置来控制飞艇（110）的路线。 以这种方式，可以提供一种飞艇系统，使得飞行员不需要飞行飞艇，并且可以减少飞艇的负载重量和功率消耗。

    AUTONOMOUS LOW-ALTITUDE UAV DETECTION SYSTEM
    54.
    发明公开
    AUTONOMOUS LOW-ALTITUDE UAV DETECTION SYSTEM 审中-公开

    公开(公告)号：US20230222809A1

    公开(公告)日：2023-07-13

    申请号：US17591757

    申请日：2022-02-03

    Applicant: Mazen A. Al-Sinan

    Inventor： Mazen A. Al-Sinan

    IPC: G06V20/58 ,  G06V10/74 ,  B64C39/02 ,  B64D47/08

    CPC classification number: G06V20/58 ,  B64C39/024 ,  B64D47/08 ,  G06V10/761 ,  B64B2201/00 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/127 ,  B64D2211/00

    Abstract: An autonomous unmanned aerial vehicle detecting system for monitoring a geographic area includes an unmanned blimp adapted to hover in air, at least one camera mounted on the blimp to scan at least a portion of the geographic area, a location sensor to determine a location of the blimp, and a controller arranged in communication with blimp, the at least one camera, and the location sensor. The controller is configured to position the blimp at a desired location in the air based on inputs received from the location sensor, and monitor the geographic area based on the images received from at least one camera. The controller is also configured to detect a presence of an unmanned aerial vehicle within the geographic area based on the received images, and determine whether the detected unmanned aerial vehicle is an unauthorized unmanned aerial vehicle based on the received images.

    Unmanned aerial vehicle (UAV) deployment of passive control stabilizers
    55.
    发明授权
    Unmanned aerial vehicle (UAV) deployment of passive control stabilizers 有权

    公开(公告)号：US09938001B1

    公开(公告)日：2018-04-10

    申请号：US14868156

    申请日：2015-09-28

    Applicant: Amazon Technologies, Inc.

    Inventor： Gershon Parent ,  Paul Viola

    IPC: B64C39/02 ,  B64C13/16

    CPC classification number: B64C39/024 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/14 ,  B64C2201/141

    Abstract: A passive control system can be implemented that converts an active control system on a multi-rotor unmanned aerial vehicle (UAV) to a passive control system. In the event that a system health of an active control system on the UAV is compromised, or in other instances, a passive control mechanism can be deployed to restore at least some in-flight stability. In various examples, the passive control system can monitor UAV attitude, velocity, and position to determine an active control system health. In other examples, the passive control system may receive an indication from the active control system itself. In some examples, the passive control mechanisms may include increasing an offset of a center of thrust and the center of gravity of the UAV. In other examples, the passive control mechanisms may include deploying control surfaces that induce a drag force that impedes translational and rotational movement.

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